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Full-text: July 28 1988. Latest: 1 , 2 , 3
As partially declassified in 1993
Iran Air Flight 655 (July 3 1988, 290 victims)
{4.9mb.pdf:image} SuDoc: D 1.2/2:IR 1
93-FOI-0184
____________________________________
____________________________________
#172
Winner of the Doublespeak Award for 1988
“omission, distortion, contradiction, and misdirection”
“Doublespeak and Iran Air Flight 655” {25kb.pdf, source} (Public Language Award Committee, NCTE: National Council of Teachers of English), and see, D.G. Kehl (Professor of English, Arizona State University), “Doublespeak: Its Meaning and Its Menace” {22kb.pdf, source} (“The Best of the 1988 Quarterly Review of Doublespeak”). –CJHjr
Hormuz, Space Shuttle photo
Admiralty Chart 2888, widths:
620px,
780px,
1000px,
1263px,
1580px
Acronyms –CJHjr
1320
28 Jul 88
SECRET NOFORN
| From: | Rear Admiral William M. Fogarty, USN |
| To: | Commander in Chief, U.S. Central Command |
| Subj: | Formal Investigation into the Circumstances Surrounding the Downing of a Commercial Airliner by the USS Vincennes (CG 49) on 3 July 1988 (U) |
| Ref: | (a) JAG Manual |
Redactions: 1993 v. 1988
Five years later, in 1993, the DoD quietly restored this text in a declassification review.
This webpage is the 1993 text.
Much of the content of the 1988 omissions was slowly revealed, here and there, in the interim.
But, important text they continue to conceal from the public. Especially, most of the prima facie unlawful Rules of Engagement.
So too, the exhibits and enclosures they also conceal from the public. References to these documents (in parentheses) terminate many paragraphs in the report, mostly in part III (“Findings of Fact”). The DoD concealed all these document references, from the retyped 1988 report they released to the public. The number of these, their secret redactions, is so immense, I don’t underline them here, to avoid clutter.
Charles Judson Harwood Jr.
1. (U) As directed by Commander in Chief, U.S. Central Command, and in accordance with reference (a), a formal investigation was convened on 3 July 1988. The original record of hearings and additional documents are forwarded as enclosures (1) through (24).
2. (U) The Investigating Officer, after inquiring in to {sic: into} all facts and circumstances connected with the incident which occasioned the investigation, and having considered the evidence, submits the following preliminary statement, executive summary, findings of fact, opinions and recommendations: {p.3-1993}
1. (U) By order of General George B. Crist, USMC, Commander in Chief, U.S. Central Command, dated 3 July 1988, Rear Admiral William M. Fogarty, USN, Director, Policy and Plans (J-5), U.S. Central Command, was appointed to conduct a formal investigation into the circumstances surrounding the downing of a commercial airliner by the USS Vincennes on 3 July 1988.
2. (U) The formal investigation was conducted at the Administrative Support Unit, Bahrain, with preliminary interviews and information gathering conducted by the investigating team on board USS Vincennes (CG 49), USS Elmer Montgomery (FF 1082), USS Sides (FFG 14), and USS Coronado (AGF 11), flagship for Commander, Joint Task Force Middle East (CJTFME).
3. (U) Rear Admiral Fogarty, and an investigating team composed of five officers, arrived in Bahrain on the evening of 5 July 1988. ¶
Preliminary interviews began on board participating units on 6 July 1988. ¶
Two additional investigating team members arrived 9/10 July 1988, one by way of Commander, Seventh Fleet, where he gathered information on the USS Vincennes pre-deployment training. ¶
The members of the investigation team are as follows:
Rear Adm. W.M. Fogarty, USN
Capt. A. Creely, USN
Capt. D. Albrecht, JAEC, USN
Capt. D. Knappe, USN
Capt. J. Keiley, USN
Capt. R. Horne, USN
Lt. Cdr. T. Bush, USN and
Lt. Cdr. C. Yuhas, JAGC, USN
Technical advisers:
Cdr. M. Cassidy (PMS 400) and
Cdr. W. Kyle (PMS 400).
Senate Hearing, p.22 (Sept. 8 1988)
CJTFME, (b)(6), (b)(7)(C) {RADM A. A. Less, USN}; ¶
USS Vincennes Commanding Officer, Capt W. Rogers, USN; ¶
USS Vincennes Force Anti-Air Warfare Coordinator (FAAWC), (b)(6), (b)(7)(C) {Lieutenant Commander Scott Lustig}; and ¶
USS Vincennes Tactical Action Officer (TAO), (b)(6), (b)(7)(C) {Lieutenant Commander Victor Guillory}, ¶
were designated as parties to the investigation. ¶
Formal hearings began on 13 July 1988 and closed on the afternoon of 19 July 1988. {p.2-1988}
4. (U) The investigation inquired into all the events which occurred prior to, during, and immediately following the engagement of Track Number (TN) 4131, later identified as Iran Air Flight 655. This designation of TN 4131 is used interchangeably with Iran Air Flight 655 throughout the investigation. There were specific, technically complex issues that required the Investigating Officer to call upon the professional expertise of the Commander, Naval Surface Weapons Center (NSWC), Dahlgren, and NAVSEA (PMS-400) personnel. The USS Vincennes data recording tapes were hand delivered under chain-of-custody immediately following the incident to NSWC Dahlgren. After initial data reduction in the United States, technical representatives from NWSC Dahlgren, led by (b)(6), (b)(7)(C) , {Head,} AEGIS Program Office, and NAVSEA (PMS-400) representatives came to Bahrain and provided further analysis on the following matters:
a. AEGIS Weapon System Mark 7 performance and operation;
b. Performance and operation of the AN/SPY-1A radar;
c. Operation and message content in Link 11; {p.4-1993}
d. UPX-29 IFF operations;
e. Reconstruction of Command and Decision (C&D) console operator actions;
f. Comparison of tape data analysis with statements by operators;
g. C&D doctrine enabled and entered;
h. Internal voice configuration and capability; and,
i. Environmental effects on system performance.
5. (U) As the investigation progressed, the statements and testimony of the witnesses were integrated into the timeline extracted from the data reduction, to form a chronology of the engagement. That chronology is attached as I.O. Exhibit (104) to the hearing. Timelines became essential elements of the investigation, particularly as regards the short time period (minutes and seconds) in which the Commanding Officer was required to make his decision to fire. This time period is referred to as the “critical time period” throughout the report.
“Secret” shall be applied to information, the unauthorized disclosure of which reasonably could be expected to cause serious damage to the national security that the original classification authority is able to identify or describe.
Executive Order 13292 (March 25 2003) (Wiki).
6. (S U) Because of a divergence between the recorded data on the USS Vincennes’s tapes and the recollection of the witnesses concerning what they saw and when they reported what they saw, a USN Medical Corps Team consisting of a psychiatrist and a physiologist were requested by the Senior Investigating Officer to come to Bahrain. They arrived in Bahrain after the formal hearing closed. They were requested to determine whether the dynamics of the situation which confronted the crew of the USS Vincennes impacted on their ability to perceive and relay the data which was available to them. Their analysis is provided at Enclosure (18).
7. (U) Certain items relevant to the investigation were not available to the Senior Investigating Officer. These items were primarily those which Iran could best provide (black box, recovery of wreckage, manifest, list of deceased, etc.). Requests for assistance through diplomatic channels were submitted via Commander in Chief, U.S. Central Command, to obtain {p.3-1988} this information for inclusion in the report of investigation as appropriate. (Encl 12).
8. (U) Enclosures (2) through (24) contain information relevant to the investigation, but were obtained or prepared after the adjournment of the investigation hearing.
9. (U) Certain intelligence statements were prepared utilizing documents or sources classified higher than SECRET/NOFORN Dissemination. References to those documents are contained in I.O. Exhibit (232). ¶
10. (U) All times listed in the findings of fact and opinions are {p.5-1993} “Z” time.
Query: “Z” time?
Zulu is Greenwich Mean Time, now termed UTC: Universal Coordinated Time.
Concealed behind this Z-time convention, is this material fact, DoD officials concealed, from this their report:
The warship clock was set 30 minutes different from Bandar Abbas Time:
Senate Hearing, p.26 (Sept. 8 1988)
Doubtless, the warship clock was set to Bahrain Time, the headquarters of the U.S. Navy Fifth Fleet in the Gulf for 40 years. The same as Dubai Time, IR655’s destination: UTC/GMT + 4 hours.
Bandar Abbas Time was 30 minutes earlier: UTC/GMT + 3-1/2 hours.
And what does this mean?
This means, that when Iran Air Flight 655 took off, at 10:17 a.m. Bandar Abbas Time, the warship clock showed 30 minutes later, 10:47 a.m., about an hour after the flight’s Scheduled Time of Departure, as shown on the warship’s airline schedule, either 9:50 a.m. or 9:59 a.m., depending on whether the typographical error in the DoD Report was a faithful copy of the warship’s airline schedule.
In addition to this 30 minutes, senior U.S. military officers also asserted that take-off time (when the wheels leave the ground) was the same as the Scheduled Time of Departure shown on the airline schedule (when the aircraft door closes at the gate). This assertion neglects to allow for the push-back delay at the gate (eg: starting the engines), the taxi-out time to the runway, and the take-off roll. This routine, predictable, time on the ground was 12 minutes, for IR655.
The negligent failure by senior U.S. military officers to inform their warship crews about both of these times issues is one of the many prima facie proximate causes of the ambush.
Hence, their decision to omit, from their misleading report, the warship clock setting, and their decision to misrepresent what take-off time means, in their report and in their sworn testimony to Congress, are prima facie criminal lies.
In combination, these two negligent failings, by senior U.S. military officers, to explain these time issues, recklessly incited their warship crews to wrongly believe, that an airliner — which their duty required them to stand watch for — taking off 15 minutes late from Bandar Abbas was taking off an hour late, instead.
An excellent criminal motive for senior U.S. military officers to unite, in a prima facie criminal conspiracy, to conceal their reckless negligence from their deceitful report.
And, to lie to Congress about the reason the Vincennes crew member, responsible for that duty, did not understand his airline schedule when he looked at it:
Senate Hearing, p.10 (Sept. 8 1988).
Ditto, Admiral Robert J. Kelly, House Hearing, p.89 (Sept. 9 1988). –CJHjr
11. (S U) During the investigation, the importance of the information being presented by way of the USS Vincennes Large Screen Displays (LSD) became apparent. Therefore, an explanation of that system’s capabilities and limitations is provided here for the benefit of the reviewer.
The AEGIS Large Screen Display (LSD) is a part of the AEGIS Display System (ADS) and is a primary visual information source for the CO, TAO and Force Warfare Commanders. It consists of four 42″ x 42″ flat, vertically mounted, 2-dimensional displays which display the tactical picture contained in the C&D computers. This information is displayed as Navy Tactical Display System (NTDS) symbology with appropriate velocity leaders. The range scales can be varied from 8 to 2048 nautical miles. Geographic outline maps as well as operator selectable line segments, points, circles and ellipses can also be displayed. These latter items can be used to construct operational areas, geographic features, range rings, air lanes, etc. The display operator can also attach a 24 character alpha-numeric label (or “tag”) to any track or point. Therefore the track classification, ID, position relative to other tracks, range, bearing, course and speed as well as position relative to geographic features or airlanes, etc., can be displayed. However, it is important to note, that altitude cannot be displayed on the LSD in real-time.
12. (S U) TN 4133, which lifted off from Bandar Abbas shortly after TN 4131, is used as the identifier for an Iranian C-130.
13. (U) A glossary of abbreviations used throughout the report has been compiled and is attached at the end of the transcript of the proceedings.
14. (S U) The Report of Investigation is formatted to give the reviewer a general overview of the events surrounding the incident in the Executive Summary. The Findings of Fact are arranged with background on the intelligence and operational picture in the Persian Gulf to provide the reviewer with essentially the same data which was available to CJTFME and the {p.4-1988} USS Vincennes on 3 July 1988. Environmental factors, commercial air information, data on Iran Air Flight 655, and relevant portions of the Peacetime Rules of Engagement (ROE) are then treated as discrete blocks of information before addressing the USS Vincennes training and readiness, watch organization, overall combat system status, communications, and combat systems doctrine. With the foundation thus laid, the actual events of 3 July 1988 which led to the downing of TN 4131 are examined beginning with the surface engagement which formed an integral part of the decision process of the Commanding Officer, USS Vincennes. The USS Vincennes data recordings have enabled the investigation to break the critical time period, which comprised {p.6-1993} the air engagement, into a minutes and seconds sequence of specific actions as they occurred along a timeline. Finally, post-incident search and rescue efforts, and after action reports are addressed. Opinions and Recommendations conclude this report. {p.7-1993}
A. Introduction.
1. (U) On 3 July 1988, the USS Vincennes (CG 49), operating in the Southern Persian Gulf as a unit assigned to Commander, Joint Task Force Middle East, downed a civilian airliner, Iran Air Flight 655 on a routine scheduled flight from Bandar Abbas to Dubai, with two SM-2 missiles.
“Confidential” shall be applied to information, the unauthorized disclosure of which reasonably could be expected to cause damage to the national security that the original classification authority is able to identify or describe.
Executive Order 13292 (March 25 2003) (Wiki).
2. (C U) The material condition, combat systems, training and personnel readiness of the ship were satisfactory.
3. (U) The following narrative summarizes the events leading up to and including the downing of Iran Air Flight 655. It is in the form of a chronology because the situation leading up to, just prior to, and during the few critical minutes from Iran Air Flight 655 take-off to downing are considered important to a full understanding of the incident. All times in the report are “Z” time.
B. Pre–3 July Scenario.
1. (SNF U) In the three day period prior to the incident, there was heightened air and naval activity in the Persian Gulf. Iraq conducted air strikes against Iranian oil facilities and shipping 30 June through 2 July 1988. Iranian response was to step up ship attacks. Additionally, Iran deployed two, possibly three, F-14’s from Bushehr to Bandar Abbas. U.S. Forces in the Persian Gulf were alerted to the probability of significant Iranian military activity resulting from Iranian retaliation for recent Iraqi military successes. That period covered the fourth of July holiday weekend.
2. (SNF U) During the afternoon and evening hours of 2 July 1988 {p.5-1988} and continuing into the morning of 3 July 1988, Iranian Revolutionary Guard (IRGC) armed small boats (Boghammers, and Boston Whalers) positioned themselves at the western approach to the Strait of Hormuz (SOH). From this position, they were challenging merchant vessels, which has been a precursor to merchant ship attacks. On 2 July 1988, USS Elmer Montgomery was located sufficiently close to a ship attack in progress as to respond to a request for distress assistance and to fire warning shots to ward off IRGC small boats attacking a merchant vessel.
C. 3 July Surface Engagement
1. (S U) On the morning of 3 July 1988, USS Elmer Montgomery was on patrol in the northern portion of Strait of Hormuz Western Patrol Area (SOHWPA). ¶
At approximately 0330Z, USS Montgomery observed seven small Iranian gunboats approaching a Pakistani merchant vessel. The small boats were reported by USS Montgomery {p.8-1993} to have manned machine gun mounts and rocket launchers. Shortly thereafter, USS Montgomery observed a total of 13 Iranian gun boats breaking up into three groups. Each group contained 3 to 4 gun boats with one group of four gun boats taking position off USS Montgomery’s port quarter. ¶
Ted Koppel (Nightline Anchor and Managing Editor), “The USS Vincennes: Public War, Secret War” (ABC News, Nightline, July 1 1992) (TV documentary).
At 0411Z, USS Montgomery heard the gun boats over bridge to bridge challenging merchant ships in the area. USS Montgomery then heard 5 to 7 explosions coming from the north. ¶
At 0412Z, “Golf Sierra” (COMDESRON 25) directed USS Vincennes to proceed north to the vicinity of USS Montgomery and investigate USS Montgomery’s report of small boats preparing to attack a merchant ship. USS Vincennes’s helo (Ocean Lord 25/LAMPS MK-III helo) on routine morning patrol, was vectored north to observe the Iranian small boat activity. USS Vincennes was also monitoring a routine maritime patrol of an Iranian P-3 operating to the west. ¶
At approximately 0615Z, the USS Vincennes’s helicopter was fired upon by one of the small boats. USS Vincennes then took tactical command of USS Montgomery and both ships proceeded to close the position of the helicopter and the small boats at high speed. As USS Vincennes and USS Montgomery approached the position of the small boats, two of them were observed to turn towards USS Vincennes and USS Montgomery. The closing action was interpreted as a demonstration of hostile intent. USS Vincennes then requested and was given permission by CJTFME to engage the small boats with gunfire. ¶
At approximately 0643Z, USS Vincennes opened fire and was actively involved in the surface engagement from the time Iranian Air Flight 655 took off from Bandar Abbas through the downing of Iran Air Flight 655.
2. (S U) During the course of the gun engagement of the Iranian small boats, the USS Vincennes, at approximately 0654Z, had maneuvered into a position 1 mile west of the centerline of civilian airway Amber 59. The USS Sides, transiting from east to west through the SOH, was approximately 18 miles to the east and became involved in the evolving tactical situation. {p.6-1988}
D. Bandar Abbas/Iran Air Flight 655/Air Engagement
1. (SNF U) On 3 July 1988, at approximately 0647Z, an Iran Air Airbus 300, Iran Air Flight 655, took off from the Bandar Abbas joint military/civilian airport destined for Dubai airport. The flight was a routine scheduled, international flight via commercial airway Amber 59.
3. (SNF U) An Iranian military C-130 took off approximately 7 minutes after Iran Air Flight 655, and a number of Iranian F-4’s {p.9-1993} were observed to be operating in the area of Bandar Abbas approximately 30 minutes after the incident.
Query: “7 minutes”?
Let’s see now.
IR655 took off at 0647.
So the C-130 took off at 0654.
Right? –CJHjr
ICAO Report, p. A-8.
4. (SNF U) Iran Air Flight 655 took off on runway 21 (heading 210 degrees true), was directed by the Bandar Abbas Tower to squawk IFF mode III code 6760, and began a normal climb out to assigned altitude of 14,000 feet for the flight, which lasted a total of 7 minutes before the plane was hit by the missiles from USS Vincennes. The pilot remained within the Amber 59 air corridor (20 miles wide, 10 miles each side of centerline), made a routine position report to Bandar Abbas departure control at approximately 0654Z, and was ascending through 12,000 feet at a speed of approximately 380 kts at the time of making his report.
Senate Hearing, p.25 (Sept. 8 1988).
______________________
The intelligence sources, Mr. Fogarty here alludes to, were, presumably:
• Naval/NSA signals intelligence officers onboard the Vincennes itself with the Naval Security Group Command (NSGC) in charge of the Ship’s Signals Exploitation Space (SSES), recording all Iranian radio broadcasts.
• The NSA/DIA on-shore listening/radar station in Oman, on the Musandam Peninsula {photo: 257kb.html, map: 79 kb gif} (with antennas likely at 2,000 feet or better elevation {67 kb gif}, with line-of-sight to the broadcast antenna at Bandar Abbas airport, no more than 45 n.miles north), recording all Iranian radio broadcasts.
• The Hawkeye crew aloft nearby at the time, above the Northern Gulf of Oman, recording all Iranian radio broadcasts.
• The AWACS crew aloft at the time, above the Northern Persian Gulf, recording all Iranian radio broadcasts.
• Possibly, British Intelligence (on its warships, or its likely GCHQ feed from the same listening station at Musandam), recording all Iranian radio broadcasts.
• And, finally, the NSA Head Office at Fort Meade Maryland, and the Defense Intelligence Agency at the Pentagon in Virginia, each recording in real time, via satellite relay from their listening station at Musandam, if that’s they wanted to do, all Iranian radio broadcasts.
Plainly, Mr. Fogarty had in his possession multiple tape recordings and transcripts of the broadcast conversations between Air Traffic Control and the IR655 pilot. And, between the IR655 pilot and his airport office.
And surely these were tone time-stamped, automatically in the recording (like Air Traffic Control tapes are), at the uniform U.S. Military time, synchronized to a zillionth of a second, worldwide, by the U.S. Military’s atomic clocks.
These time-stamped recordings are among the most material facts in this investigation. As we shall soon see. And, not being a nincompoop, William M. Fogarty knew that too.
And yet, Mr. Fogarty concealed these material tapes and transcripts from his report.
Concealed them from the classified exhibits to his report.
And concealed them from the classified enclosures to his report.
Why did Mr. Fogarty decide to omit this material information? And thereby commit a prima facie crime (lying by material omission).
He must have had a good reason.
Could this be the reason?:
Robert J. Kelly (Rear Admiral, Vice Director for Operations, Joint Chiefs of Staff, U.S. Department of Defense), House Hearings, p.184 (Sept. 9 1988)
Senate Hearing (written questions/answers) p.55-56 (Sept. 8 1988)
______________________
And, there are two other good reasons:
• See below, for a warning broadcast by the Vincennes IAD radio-talker, while the IR655 pilot was busy talking to Air Traffic Control — a carefully concealed material fact and prima facie crime.
• And see here, for carefully concealed evidence that the Vincennes and Montgomery IAD radio talkers were broadcasting and talking at the same time, simultaneously, a jumble of nothing any human being could understand — a carefully concealed material fact and prima facie crime.
______________________
These carefully concealed recordings bear directly on the State Responsibility of the United States of America to the Islamic Republic of Iran.
Accordingly, to conceal this material evidence constitutes all those participating in the prima facie criminal conspiracy to lie (a “felony”), in this official report, and in testimony to Congress, equally complicit in the foreseeable consequences of their felony conspiracy, namely:
The felony-murder, or manslaughter, of the mostly American victims of Pan Am 103, bombed a few months later (December 21 1988, 270 victims), a promised, foreseeable, apparent, international countermeasure to the first criminal enterprise, the conspiracy of criminal liars, who decided to lie, and falsely deny responsibility, on behalf of the United States, thereby threatening more of the same in the future, and so legalizing an eye for an eye (a species of self-defense). –CJHjr
5. (S U) At approximately 0654Z, the missiles fired from USS Vincennes impacted the aircraft at an altitude of 13,500 feet, approximately 8 miles from USS Vincennes, with Iran Air Flight 655 still in its assigned air corridor. Debris from the aircraft and a significant number of bodies were found 6.5 miles east of Hengham Island at 26-37.75′N/56-01′E. While no passenger manifest nor list of deceased has been released by Iran, various sources have established that some 290 persons from six nations, were on board Iran Air Flight 655.
6. Vincennes—Critical Decision Window
(a) (S U) At approximately 0647Z — Iran Air Flight 655 was detected by the USS Vincennes’s AN/SPY-1A radar bearing 025 degrees, 47NM, at 900 feet and seconds later was assigned TN 4131. At approximately 0648Z, USS Sides detected Iran Air Flight 655, bearing approximately 355 degrees, range approximately 32 miles at 1500 feet altitude. The aircraft continued to close USS Vincennes with a constant bearing, decreasing range. At approximately 0649Z, USS Vincennes issued warnings on Military Air Distress (MAD) (243.0 mHz) and at 0650Z began warnings on International Air Distress (IAD) (121.5 mHz) to TN 4131 located 025 degrees, 40NM from USS Vincennes.
Query: “900 feet”? “1500 feet”?
Are these the same altitude?
They indeed could be.
The explanation, for why these two altitudes could be the same, senior U.S. military officers concealed from their report.
This explanation would reveal some things they were very eager to conceal, namely, that the Vincennes was several miles inside Iranian territorial waters (to be explained).
A fine piece of obfuscation. One of the many elements in this report, and concealed from it, contributing to the richly deserved recognition DoD officials later received: The annual Doublespeak Award for 1988.
We’ve had the warship clock.
Here, now, is another missing piece of this doublespeak jigsaw puzzle:
The 900-feet altitude value, perceived by the Vincennes, was the altitude broadcast by the aircraft’s transponder (mode-C).
An SSR/IFF transponder broadcasts “pressure altitude” (rounded to an even 100 feet), not actual altitude. This is the altitude value used to denominate Air Traffic Control “Flight Levels”. And, because all transponders broadcast this altitude value, Air Traffic Controllers can know with certainty the vertical separation between aircraft aloft.
To accomplish this certainty, the altimeter connected to the transponder, supplies to the transponder an altitude value based on the “standard” barometric pressure of 1013.25 millibars (hPa: hecto-Pascals) (29.92 inches of mercury) (QNE). And this, the pilot cannot alter.
This “standard pressure” was 15 millibars higher than the actual airport air pressure when Iran Air Flight 655 took-off, namely: 998 millibars (hPa) (29.47 inches of mercury) (QNH: adjusted down to mean sea level pressure, by ISA standard formula).
Thus, when the aircraft was sitting on the runway, its transponder (if interrogated) would broadcast an altitude of roughly 400 feet below sea level (about 28 feet per millibar).
This amounts to about 550 feet lower than what the warship radar perceived to be the aircraft’s actual altitude.
See ¶¶ (aa)-(bb), p.56/39, and add 50 feet to the transponder’s altitude broadcast, to reflect the aircraft’s climbing rate of 25 feet per second (1500 feet/minute) during the 2 seconds prior to the warship’s radar altitude value. But see ¶ (g), p.40/28, asserting a 3 second difference, indicating a 525 foot difference instead.
The 150 foot difference (from a runway broadcast) was due to: The 22-foot runway elevation. The height of the warship radar antenna above the sea. The transponder rounding up or down by as much as 50 feet, to an even 100 feet. The DoD report-writers possibly rounding the precise radar altitude value. A slightly different precise air pressure. The state of the tide (on which the warship radar floats up and down, from “mean sea level”): Low tide at 0615. An airport surface air temperature (35°C ) 20°C higher than the ISA standard atmosphere model (15°C), to which altimeters are calibrated. An air temperature at 10,000 feet (18°C) 22.6°C higher than the ISA model, and 2.3°C higher than specified by the ISA “lapse rate” (1.98°C per 1000 feet) from the actual airport temperature. And such. (Meteorological data: ICAO Report, ¶ 1.7, pp.4-5).
The transponder does not broadcast continuously, only in response to an interrogation pulse-train. When interrogated, it broadcasts a pulse-train, encoding either it’s 4-digit identification code number (mode A) or its pressure altitude (mode C) rounded to an even 100 feet. Depending on which pulse-train it received from the interrogator. (The interrogator broadcasts both queries, one after the other).
A transponder broadcasts its reply (on 1090 mHz), 2-microseconds after it receives the last of an interrogation pulse-train (on 1030 mHz). It can reply to 2000 interrogations per second.
The report asserts, that the Vincennes SPY-1 radar interrogated automatically “at one minute intervals”.
Is this a mistake? Perhaps referring to interrogations to an empty sky? Which is not what this report is about. Concealing more frequent automatic interrogations? Once the computer detects a moving target?
I would expect once per second, or thereabouts. An aircraft can cover a lot of altitude in one minute. And though the radar is pulsing fast to watch it, why not pulse the transponder too?
If this assertion be true, and not a mistake, then this detail might have affected events on the day. Because of the sudden jump in altitude displayed to the warship crew, before the radar altitude starts to work (at 6000 feet, in this case). And, thereafter, the jumping disparity between the two altitude values (over a one minute lag). And especially so when, as here, the two altitude values are already more than 500 feet apart to start with.
This sudden jump, in transponder altitude, might be confusing, and suspicious, in a suspicious mind, in a stressed mind. This AirBus was climbing 1500 feet per minute. As it approached.
However, the separate Vincennes rotating air search radar antenna (AN/SPS-49(V)) also interrogates target transponders, as it sweeps, selectable, at either 6 or 12 sweeps per minute (every 10 or 5 seconds). Like an Air Traffic Control radar does. The report does not state whether its radar returns, and transponder responses, are integrated by the SPY-1 computer, automatically updating its database, for all its CRO computer displays. If not, they are anyway certainly shown on the computer console of that rotating radar’s operator (49 ADT).
But I imagine they do update the database, every 5 or 10 seconds. In which event, there is no sudden jump in transponder altitude, and this detail has no bearing on the events of the day.
We’re also supposed to believe this: All warship crew members, in the CIC, having responsibility for aerial threats, can position their computer mouse cursor (“range gate”), on a radar target, displayed on their computer consoles. And thereby manually interrogate a target’s transponder. As often as they wish. And many of them did this, many times, during the flight. Sometimes referred to as a “challenge” (p.48/32, ¶¶ 0650(f); p.49/33, 0651(i)) or an “interrogation” (¶ 7, p.65/47; Crowe endorsement, ¶¶ 5(b)).
This is apparently possible with the UPX-29 transponder-interrogator system:
“The AN/UPX-29 can be controlled from up to 22 manually operated display positions, one semi-automatic operating position, and one shipboard computer controlled interface. These positions can function simultaneously, and AIMS functions are available at each position independent of the functions selected at other positions.”
because its OE-120/UPX antenna is separate from the interrogator antennas connected to the warship’s two radars (phased array and rotating, though the phased array radar may share this interrogator antenna):
“The AIMS antenna consists of 64 radiating elements arrayed in a circle around the ship’s mast. Unlike conventional IFF systems which employ mechanically rotated antennas, the AIMS antenna elements remain stationary while the beam is steered electronically to scan a full 360 degrees around the ship. The beam can also be positioned selectively in any direction within microseconds and has a continuous scan rate of up to 90 revolutions per minute.”
According to this DoD report, the transponder response appears on a separate display from the normal CRO computer screen (which also displays transponder responses, from interrogations by the two radars.) We’ll hear more about this later, in connection with a certain C-130, ducting, and an F-14.
______________________
The Sides was 15 n.miles closer to the airport than the Vincennes. But not in the middle of the airway (as the Vincennes was), due to the geography of the area.
The Sides was, however, likely in Iran’s territorial waters (as the Vincennes was too). I haven’t yet tried to determine the precise territorial boundary at the bend in the Strait of Hormuz, but it looks like the shipping lane boundary is also the territorial boundary. This, because the strait is too narrow to enable ships to be 12 n.miles from all surrounding land. And so, a shipping lane has been agreed by the neighboring countries, to enable the “innocent passage” international law requires.
The Sides was not inside that shipping lane, as I plot its position, but, instead, a mile or two towards the airport from the shipping lane boundary.
This may indicate that the report writers decided to conceal the Sides precise location. And to obfuscate which altitude value they reported. (The lower the altitude, the closer to the airport). And why they use their favorite word, “approximately” (“approximately 355 degrees,” “approximately 32 miles”).
They omitted it too from their classified secret exhibits. They list the position log of the Vincennes, and the Montgomery, but not the Sides. (Position Log: The continuous time-stamped position of the ship, from the inertial navigation system).
Did they have a good reason? To purposely conceal position information on the Sides? Or is this merely their unintentional oversight? Or did they honestly consider that information was not material to their task?
It’s almost like the Sides was standing picket, on the airport, while the Vincennes set out to attack and destroy Iran’s coast guard boats. Part of Operation Praying Mantis.
Being much closer to the airport than the Vincennes, the Sides 1500-foot altitude value, reported by the DoD report-writers, could be the aircraft’s radar altitude, not its mode-C transponder broadcast.
The aircraft was well above the Sides’s horizon, at its 32 n.mile range, and well in view by the Sides radars.
Indeed, at 1500 feet radar altitude, the aircraft would have line-of-sight to the Sides at 45 n.miles. And so, at the airport’s apparent actual range (32-33 n.miles), the Sides could theoretically detect the aircraft at 350 feet transponder pressure altitude (900 feet radar altitude):— Long before it reached 1500 feet transponder pressure altitude (2050 feet radar altitude).
And all this without enhanced detection range, from the ducting they claimed existed on the day.
The Sides AN/SPS-49(V) rotating air search radar is a two dimension radar (2D: range, bearing). It cannot determine the height of a target. (The Vincennes SPY-1A phased array radar can).
Therefore, the Sides could determine the target’s altitude in only two ways: From the target’s transponder broadcast and by locking-on with its fire-control radar, which is a three dimenson radar (3D: range, bearing, altitude) and does determine altitude.
And that’s exactly what the Sides commander did, within a minute or so after take-off.
Hence, the 1500 feet, the DoD report-writers asserted, could be the Sides fire-control radar altitude value, not the aircraft’s transponder broadcast.
And, query, does the Sides fire-control radar have a tape recorder attached? And is there a written log in real-time showing these values (time, range, bearing, altitude)? Is switching on a targeting radar, merely to determine altitude, or to warn a pilot, a big enough deal that the Navy requires a written or tape-recorded record of the event? And a justification for it? Or is it routine, and not logged?
The report asserts, that the Vincennes computer system switched, from the aircraft’s transponder mode-C altitude broadcasts, to the warship’s own SPY-1 phased array radar altitude value, at a range of 34 n.miles, when the aircraft was at about 6000 feet radar altitude, and broadcasting about 5400 feet pressure altitude. This fact they concealed from the public report. One of their many obfuscations.
The Vincennes’s initial altitude value of 900 feet pressure altitude (the transponder broadcast) was detected at 0647:37Z. The DoD report writers concealed from their public report both the time and the altitude. And they concealed the time from their classified report. They disclosed the altitude later, in Congressional hearings. (Senate Hearing, p.10 (Sept. 8 1988); House Hearings, p.88 (Sept. 9 1988)). And the secret ICAO Report later disclosed the exact time (ICAO Report, p. A-3 (Nov. 7 1988)). “At approximately 0647Z,” as the DoD report-writers generalized the time in their report (both classified and public) and in their Congressional testimony.
The Sides, 15 n.miles closer to the airport, was able to detect the aircraft before the Vincennes did. Allowing for a few seconds difference between the two observations, the Sides’s value of 1500 feet, “at approximately 0648Z,” could be identical, if it was a radar altitude value.
But, this cannot be the case.
Unless the report writers misposition on the timeline when the Sides first locked on.
The DoD report writers willfully misposition other events and recollections on the timeline, detailed elsewhere herein, in order to portray a false reality. Did they also do that here?
The report writers positioned directly together on the timeline both the Sides lock-on and the Sides “weapons on target” message to the Vincennes (concealed from the 1988 public report). The lock-on and the message are separated in the DoD report only by supposed recollections of the event.
If the “message” they refer to were a verbal radio conversation, then this is unlikely the case. Because the Sides officer first had to lock-on, and wait, before he could evaluate the pilot’s response, if any.
Did the report writers conceal, that the lock-on was that many seconds sooner than the “message,” that the Sides 1500 feet altitude observation was a radar altitude value, not a transponder value?
The Sides did not report altitude to the Vincennes (at least, the DoD report writers don’t say so). Altitude isn’t what the Sides officer was mainly interested in. And that’s not why he locked-on.
He locked-on because that’s what his Rules of Engagement required him to do. To warn the pilot. To attempt to learn if the aircraft was military or civilian.
And so, that purpose required him to wait some seconds to see if the pilot would react, to the cockpit alarm, from his cockpit radar homing and warning receiver (RHAW), which airliners don’t have.
If the DoD report writers buried the Sides earlier radar altitude observation, in this lock-on “message,” then the Sides was yet another mile or two closer still to the airport, and that much deeper still into Iran’s territorial waters, than if the 1500 feet was a transponder value.
An excellent motive. To obfuscate this altitude observation. And to conceal the position of the Sides.
The DoD report writers had two tape recordings of the conversations between the Sides and the Vincennes, and so had no difficulty in knowing precisely who said what, to whom, and when. Any delay, however, between the initial lock-on, and the “message” to the Vincennes would not appear on those tapes. While the Sides officer was evaluating the target’s reaction to being locked-on.
And did the Sides “weapons on target” message to the Vincennes (omitted from the report) specify a radar altitude?
If the 1500 feet was a transponder value, then the two reported observations are that many seconds apart that the aircraft climbed in the meantime.
And this I believe to be the fact of this particular altitude report.
The Sides certainly observed the aircraft much sooner. And I suppose the DoD report writers simply concealed that fact. Though, it may be, that nobody on the Sides was asked about, or mentioned, a lower altitude observation.
The “message” the DoD report writers refer to (which they concealed from the 1988 version of their report) was not a verbal conversation on the radio. It was computer-talk: An automatic, computer-generated, Link-11, computer message. This fact the DoD report writers concealed, from both the public and the classified versions of their report, presumably to conceal three separate items of negligence discussed below.
______________________
To determine the position of the Sides (which the report writers omit from their report), you have to know, where was the aircraft at 1500 feet altitude? Be that actual or transponder.
How far from the end of the runway?
And to know that, you have to know the weight of the aircraft, and its flight profile, on takeoff.
IR655 may have been at 1500 feet actual altitude directly over the coastline, which lies about 1.5 n.miles off the end of the runway, doing about 150 knots. And, conceivably, he may have been higher. (Admiralty Chart 2888, widths: 620px, 780px, 1000px, 1263px, 1580px).
This, based on its take-off weight of 288,026 pounds (130,921 kg). (ICAO Report, pp. A-4, D-10). And, based on the manual for an AirBus A300B4. (IR655 was a B2, and maybe I can eventually find a B2 manual). And, based on two flight profile sheets from AirBus, in the ICAO Report (pp. D-21, D-22). And, assuming he took off about half way down the runway (2.0 n.miles long).
According to this information, at a take-off weight (TOW) of 290,000 pounds, IR655 rotated (V1), on its take-off roll, at 137 knots, took-off (V2) and climbed under full power at about 150 knots (V2+10 knots), at a pitch of 15-18 degrees nose-up. At 800 feet AGL (above ground level), the pilot reduced thrust to his “climb” power setting, and compensated, by reducing pitch to 10 degrees nose-up, thereby maintaining his speed at about 150 knots, and reducing his rate of climb (but maybe not, as he had also retracted his landing gear by then, and eliminated that drag). By 2000 feet, he may have retracted his flaps (V3: 153 knots), thereby beginning his acceleration. Following slat retraction (V4: 192 knots), he was due to reduce pitch again, to 7.5 degrees nose up, continuing to accelerate to his “final take off” speed (Vfto: 222 knots).
If he took off half way down the runway, then the coastline was 2.5 n.miles away.
Could he get to 1500 feet, in two and a half miles? Or 2000 feet?
At 150 knots? (IAS: Indicated Air Speed, not ground speed).
I guess I need an AirBus pilot with a stop watch, or an Air Traffic Controller, to tell me. But I haven’t given up searching for the answer to this. And I’m even thinking about getting out my graph paper, and see if I can plot this profile. And vector his speed (part up), and determine his altitude, from pitch (assuming little additional lift).
If the aircraft was directly over the coastline, at 1500 feet — be that actual (radar) altitude, or be that transponder altitude (about 2050 feet actual) — then the position of the Sides, at that moment, was about 56-24 E, 26-39.5 N. To the right of the “Z” in “HORMUZ,” on the chart, above the bend in the Strait. (Admiralty Chart 2888, widths: 620px, 780px, 1000px, 1263px, 1580px). This, based on the observation the report writers attribute to the Sides: “bearing approximately 355 degrees, range approximately 32 miles at 1500 feet altitude”. (I’ll plot it exact, later).
______________________
Transponder details: “Aircraft information — Equipment,” ICAO Report, ¶ 1.6(c), p.4 (two Collins 621A-6 transponders, Serial Numbers: 3800, 2881). Specification sheet: Rockwell International, Series 500, Collins ATC Transponder, 621A-6A (specification standard ARINC 572), Rockwell document number 074-3874-000, 7M-SP-3-85 (March 1985). What is a Transponder? (Rockwell International, Collins Air Transport Division, Avionics Group, Cedar Rapids Iowa 52498, Instruction Guide, Rockwell document number 523-0773764-10111R, 10-1-88, 8+56 pages, October 1 1988). (A current model Collins transponder: TPR-901). Basic Flight Instruments, Chapter 4 of Instrument Flying Handbook (U.S. Federal Aviation Administration, Advisory Circular 61-27C, Jan. 1 1980).
–CJHjr
(b) (S U) At approximately 0650Z — Several USS Vincennes CIC personnel heard, on internal Combat Information Center (CIC) voice circuits, a report of F-14 activity ¶
Senate Hearing, written statement, p.54 (Sept. 8 1988)
______________________
Note: I suppose the SSES to be under the command of a National Security Agency (NSA) Naval Officer, with the Naval Security Group Command (NSGC), conducting electronic surveillance. –CJHjr
A momentary {p.7-1988} mode II-1100 IFF indication was detected which was correlated with an Iranian F-14. This was reported throughout CIC over internal CIC voice circuits. Continuous MAD and IAD warnings were ordered at 30NM (5 total warnings on MAD and 4 total warnings on IAD). USS Vincennes continued the surface engagement and experienced a foul bore in Mount 51. In order to unmask the after gun mount, full rudder (at 30 knots) was applied. This added to the increasing tension in CIC. {p.10-1993}
(c) (S U) At approximately 0651Z — As TN 4131 closed to 28NM, USS Vincennes informed CJTFME via the Middle East Force execution net that she had a closing Iranian F-14 which she intended to engage at 20NM unless it turned away. USS Vincennes requested concurrence. CJTFME concurred but told USS Vincennes to warn the aircraft before firing. Warnings continued, but no response from TN 4131 was received, nor did it turn away.
(d) (S U) At approximately 0652Z — Warnings continued over both IAD and MAD. Still no response. Although TN 4131 reached the 20NM point, the CO decided not to engage. The order was given to illuminate the contact with fire-control radar. There were no ESM indications. TN 4131 was ascending through 10,000 feet.
(e) (S U) At approximately 0653Z — At 15-16NM, the last warning over IAD was given by USS Sides to the aircraft bearing 204 degrees to USS Vincennes, range 15.5 miles. During the last 30 seconds of this minute, the CO made his decision to engage TN 4131.
(f) (S U) At approximately 0654:05 — The CO turned the firing key. At approximately 0654:22, two SM-2 Blk II missiles {copy} left the rails. Twenty one seconds later, they intercepted Iran Air Flight 655 at a range of 8NM from USS Vincennes at an altitude of 13,500 feet.
E. Post Incident Investigation
1. (S U) The focus of this investigation was on the key factors that figured in the determination of what information was available to the Commanding Officer upon which to base his decision to engage TN 4131, the validity of that data, and what other factors entered into his decision making process. Essential to this determination was a detailed examination of the USS Vincennes’s data reduction tapes, which portray second-by-second the position, kinematics, IFF information and Link eleven (11) message flow of all contacts held by the USS Vincennes’s AEGIS Weapon System. Immediately following the incident, USS Vincennes’s AEGIS data recording tapes were transported to the Naval Surface Warfare Center, Dahlgren, Virginia for data extraction and evaluation. The data extracted depicted the Iran Air Flight 655 flight profile from first detection to missile intercept. Further, the data allowed reconstruction of all “button actions” by Command and Decision (C&D) console operators in CIC and the information available to them on their console read-outs. Crucial to the investigation became close examination of the approximately 3 minute 45 second period just prior to the Commanding Officer’s {p.8-1988} final decision to fire. During this period, verbal reports were being made by one of the console operators over internal circuits of decreasing range and altitude. Additionally, the fact that the range of TN 4131 was rapidly {p.11-1993} approaching the final weapons release point for the incoming aircraft factors into the decision to fire. Also crucial to the investigation was the explanation (where possible) of the divergence between the data available in the AEGIS system derived from the data reduction tapes and the reports received by the CO and “GW” (the CO’s principal air war advisor), especially the reports of “F-14”, “Mode II code 1100 IFF”, and “decreasing altitude”.
2. (S U) The data from USS Vincennes’s tapes, information from USS Sides and reliable intelligence information, corroborate the fact that TN 4131 was on a normal commercial air flight plan profile, in the assigned airway, squawking Mode III 6760, on a continuous ascent in altitude from take-off at Bandar Abbas to shoot down. {p.12-1993}
A. Setting The Stage
1. Intelligence Background.
a. The Gulf War
(1) (U) The war between Iran and Iraq is the latest iteration of a conflict dating back a thousand years. (IO Exhibit 14, FICPAC Gulf Threat Orientation).
(2) (U) Although Iraq used its superior Air Force to target Iranian oil installations around the head of the Gulf and Kharg Island early in the war, the purchase of EXOCET missiles from France in 1983 provided Iraq with a credible ship attack capability. Anti-shipping strikes commenced in 1984. (IO Exhibit 14, FICPAC Gulf Threat Orientation).
(3) (U) Iraq’s intent on conducting anti-shipping attacks was to put economic pressure on Iran by seeking to limit Iran’s oil revenue and to bring an end to the larger ground war. Iran responded in kind by striking tankers in 1984 to prevent war supplies from reaching Iraq. (IO Exhibit 14, FICPAC Gulf Threat Orientation).
(4) (U) Since the start of the Gulf War, as a subset of the larger Iran/Iraq War, there has been a history of violence in the Persian Gulf. ( (b)(6), (b)(7)(C) , p.6).
(5) (SNF U) The Gulf War intensified in 1987 when Iraq used its Air Force to conduct an aggressive campaign against Iranian oil facilities and shipping. The campaign was centered in the Central Persian Gulf (CPG) and intensified in May 1987, apparently reflecting an Iraqi decision to take greater risks to successfully strike Iranian shuttle tankers. These expanded operations culminated in the 17 May 1987 erroneous attack on USS Stark. (IO Exhibit 14, FICPAC Gulf Threat Orientation). {p.9-1988}
(6) (U) The United States commenced escorting Kuwaiti reflagged tankers in 1987. ( (b)(6), (b)(7)(C) , p.6-7)
(8) (SNF U) In addition to its strikes against neutral shipping by aircraft, Iran conducted ship attacks with surface ships and small boats. Additionally, Iran also placed six moored mine fields across the Persian Gulf and in the Gulf of Oman in an {p.13-1993} effort to sink US warships and stop convoy operations. These mine fields resulted in severe damage to both Bridgeton in July 1987 and USS Samuel B. Roberts in April 1988. (IO Exhibit 14, Intelligence Background Briefing).
(9) (SNF U) Attacks against shipping in the latter part of 1987 and the first part of 1988 marked the most intensive anti-shipping operations by Iran during the war. The predominant Iranian attack platforms during this period were small boats employing 107mm rocket launchers, rocket propelled grenades, and small arms. Because of the use of various conventional and unconventional tactics, Iranian intentions in the Gulf were suspect at all times. (IO Exhibit 14, FOSIF WESTPAC 060847Z May 88).
(10) (SNF U) Anti-shipping warfare profiles show that Iran conducted 88 ship attacks in 1987. 72% of these occurred in the shipping routes between Abu Musa Island and the UAE. From November 1987 to April 1988, all ship attacks were conducted in the southern Persian Gulf (SPG). During 1987, 50% of the attacks were conducted at night. (IO Exhibit 14, FOSIF WESTPAC 060847Z May 88)
(11) (SNF U) Iran also fired 10 silkworm missiles at Kuwait, damaging 1 U.S. flag vessel (Sea Isle City) and another merchant tanker. In October 1987 the United States responded by an attack on the Iranian owned Rostam Oil platform. (IO Exhibit 14, Intelligence Background Brief)
(12) (SNF U) Seven additional silkworm sites were constructed in the Strait of Hormuz area which threatened seaborne traffic through that choke point. (IO Exhibit 14, Intelligence Background Brief)
b. (SNF U) Iranian Air Reaction to the U.S. retaliation April 1988 (Operation Praying Mantis)
(1) (SNF U) In retaliation for the mining of USS Samuel B. Roberts, the United States attacked the Iranian Sirri and Sasson offshore oil production facilities in the SPG on 18 April 1988. ¶
In response to the U.S. operation, Iranian aircraft and warships deployed from Bandar Abbas to join Iranian Revolutionary Guard Corps (IRGC) small boats from Abu Musa Island and Qeshm Island in attacks on U.S. owned or associated oil rigs, platforms and jack-up rigs. ¶
During the engagement with U.S. forces, 2 Iranian frigates and 1 missile patrol boat were sunk or severely damaged. ¶
Eleven F-4s scrambled during the day from Bandar Abbas. USS Wainwright launched missiles at one of the aircraft, damaging it when the aircraft failed to respond to repeated warnings and continued {p.10-1988} to close the ship. (IO Exhibit 14, Intelligence Background Briefing). {p.14-1993}
(2) (SNF U) The preponderance of the action between U.S. and Iranian forces on 18 April 1988 during Operation Praying Mantis occurred in the same area where the 3 July 1988 incident with USS Vincennes took place. (IO Exhibit 14, Intelligence Background Briefing).
Iran v. United States (“Oil Platforms”) (U.N. I.C.J.: International Court of Justice, The Hague, Judgment on the Merits, November 6 2003) {29.1mb.pdf, source}.
c. Iranian Aircraft Attacks on Shipping
(1) (SNF U) The Iranian Air Force and Iranian warships have conducted a total of 187 attacks on shipping since the campaign began in March 1984, most of those attacks occurred prior to August 1986. Fighter aircraft conducted a majority of these attacks using iron bombs and Maverick missiles. In comparison to the attacks conducted by the IRGC small boats, the air attacks were among the most damaging. (IO Exhibit 14, Intelligence Background Briefing).
(2) (SNF U) Following August 1986, Iranian fighter aircraft were rarely used in the ship attacks in an apparent attempt to conserve platforms. (IO Exhibit 14, FOSIF WESTPAC 060847Z May 88).
(3) ( ) (b)(1) (IO Exhibit 14, Intelligence Background Briefing).
(4) (S U) The Iranians have an inventory of over 1000 Maverick missiles. Each missile can be launched from ranges of .5 to 13 NM and television guided. The launching aircraft must be able to keep visual track of the target but does not have to illuminate the target with radar. (IO Exhibit 14, Possible Iranian F-14 Weapons).
(5) ( ) Although there has been no record of F-14s being used for iron bomb attacks, the aircraft is capable of being modified to be used in that role. To use iron bombs, the F-14 would have to close to within (b)(1) {2 NM} of the target. That information was included in the intelligence information provided to USS Vincennes on inchop. (IO Exhibit 14, Intelligence Background Briefing).
(6) (SNF U) The most recent, confirmed Iranian Air Force anti-shipping attack was on 2 February 1988 when 2 Iranian F-4s launched two Maverick Missiles at the Liberian Tanker, Petrobulk Pilot, at 30NM SSW of the point where USS Vincennes launched its missiles on 3 July. (IO Exhibit 14, Intelligence Background Briefing).
d. Iranian Air Force Operations 3 June–3 July 1988
(1) (SNF U) Iranian Air Force operating patterns changed significantly, particularly at Bandar Abbas, in the month prior to 3 July 1988. ¶
(2) (S U) Iranian F-14’s have been observed to fly at airspeeds of between 250 KTS while climbing to patrol station and 350 – 400 KTS while on patrol. During air to air intercepts the F-14’s have achieved speeds of 500 – 550 KTS. ( (b)(6), (b)(7)(C) , p.367). {p.11-1988}
(3) (SNF U) At least one, possibly 2 or 3 Iranian F-14s were transferred to Bandar Abbas from their home field at Bushehr on 25 June 1988. (IO Exhibit 14, Intelligence Background Briefing).
(4) (SNF U) The addition of the F-14s to the air order of battle at Bandar Abbas was perceived by CJTFME as a significant upgrade in Iranian air capability at Bandar Abbas. (IO Exhibit 14, Intelligence Background Briefing).
(5) (SNF U) USS Vincennes was advised by CJTFME on 18 June 1988 of the changing patterns of F-4s operating from Bandar Abbas:
“All units are cautioned to be on the alert for more aggressive behavior. ¶
(IO Exhibit 14, CJTFME 181225Z Jun 88).
(7) (SNF U) USS Vincennes was advised on 26 June 1988 of the unprecedented deployment of Iranian F-14’s to Bandar Abbas:
“The F-14 deployment represents an increased threat to allied aircraft operating in SOH, SPG, and GOO.”
(IO Exhibit 14, CJTFME//J2//260900Z Jun 88).
e. The Iranian Posture 25 June–2 July {p.16-1993}
(1) (SNF U) In the week preceding the USS Vincennes incident the Iraqi Air Force stepped up its attacks on Iranian oil facilities and shuttle convoys in the Northern Persian Gulf (NPG). Iranian reaction to these successful Iraqi attacks was anticipated by CJTFME and they warned the Middle East Force, including USS Vincennes, on 2 July 1988. (IO Exhibit 14, Intelligence Background Briefing).
(2) (SNF U) USS Vincennes was apprised of the general Iranian situation on 30 June and 1 July, specifically that because Iraq had extended its successes in the ground war to the NPG with a renewed air campaign against Iranian shipping and oil facilities, Iranian reaction should be expected.
“...in the meantime, anticipate IRGC ship attacks in retaliation for Iraqi Air Force attacks on Iranian shuttle tankers.”
(IO Exhibit 14, CJTFME//J2//0212900Z July 1988).
(4) (SNF U) The F-14 flights from Bandar Abbas during this period were:
25 June — patrol (0500-0600Z)
26 June — patrol (1300-1400Z)
27 June — patrol (0500-0700Z)
28 June — patrol (1300-1400Z)
29 June — patrol (0700-0900Z)
30 June — patrol (0500-0600Z)
1 July — patrol (0700-0900Z) {p.12-1988}
2 July — patrol (0700-0900Z)
(IO Exhibit 14, Iranian Air Force Activity from Bandar Abbas).
f. Activity on 2 July, 1988 — The Maersk Attack
(1) (SNF U) At 021600Z the Danish ship, Karma Maersk {sic: Karama Maersk}, outbound from Saudi Arabia, was repeatedly, though unsuccessfully, attacked by IRGC small boats staging out of Abu Musa Island at a point 20NM SW of that island. (IO Exhibit 14, Intelligence Background Brief). {p.17-1993}
(2) (SNF U) The Karama Maersk issued a “Mayday” requesting assistance and USS Elmer Montgomery responded and observed several IRGC small boats fire 3 rockets at the Danish merchant at 1630Z. The IRGC boats included at least 1 Boghammer and 2 machine gun equipped Boston whalers. (IO Exhibit 14, USS Montgomery 022230Z Jul 88, Intelligence Background Brief).
(3) (SNF U) The USS Montgomery fired a warning shot at the small boats at about 1730Z and the boats retired to the NW. (IO Exhibit 14, CJTFME//J2//040030Z Jul 88).
2. Operational Background.
a. (U) The Administrative and Operational Organization Charts for the JTFME are contained in this report as IO Exhibit 141.
b. (U) (b)(6), (b)(7)(C) {RADM Anthony A. Less}, USN, was CJTFME and designated “GB” (the radio call sign for the Officer in Tactical Command) on 3 July 1988. He and his staff were embarked in USS Coronado (AFG 11). (IO Exhibits 61, 134, 141).
c. (U) Commander Destroyer Squadron 25, was embarked in the USS John Hancock (DD 981) and was designated “GS” (the radio call sign for the Surface Warfare Commander) by CJTFME. (IO Exhibits 61, 141).
d. (U) The Commanding Officer USS Vincennes (CG 49) was designated “GW” (the radio call sign for the Anti-Air Warfare Commander) by CJTFME. (IO Exhibits 61, 141).
h. (S U) Key CJTFME personnel in flag plot during the engagement of the small boats and track 4131 were:
(1) (b)(6), (b)(7)(C) {RADM Less} — CJTFME {p.18-1993}
(2) (b)(6), (b)(7)(C) — Deputy CJTFME
(3) (b)(6), (b)(7)(C) — Chief of Staff, CJTFME
(4) (b)(6), (b)(7)(C) — Assistant Operations Officer, CJTFME {p.13-1988}
(5) (b)(6), (b)(7)(C) — Intelligence Officer, CJTFME
(IO Exhibits 128, 140, (b)(6), (b)(7)(C) p.443).
i. (U) COMAIR Schedules and routes were not plotted in Flag Plot but were available in the Operations Office. (IO Exhibit 116).
3. Rules of Engagement.
a. General
(1) (U) The USS Vincennes had on board a current copy of the effective ROE for the Persian Gulf. ( (b)(6), (b)(7)(C) p.422).
(2) (S U) The primary responsibility of the Commanding Officer under the ROE is the defense of his ship from attack or the threat of imminent attack. (Exhibit 131, USCINCCENT 232220Z May 88.) {[Remainder of ROE deleted.]}
4. Environmental Data.
a. (U) At 030400Z Jul 88, the following environmental data existed:
(1) Wind Speed/Direction: 10Kts/340 degrees T
(2) Sea Temp: 30 degrees C
(3) Air temp: 28.3 degrees C
(4) Relative Humidity: 62%
(5) Evaporation Duct Height: 78.5 ft
(6) Surface Pressure: 998.0 MB
(7) Visibility estimate was 8-10 miles
(8) Ceiling: approximately 200 ft/scattered
(I.O. Exhibit 177).
b. (U) Predicated on the environmental data provided from USS Vincennes on 3 July 1988, which is summarized in I.O. Exhibit 177, Joint Electronic Warfare Center (JEWC) San Antonio, Texas, concluded the following as regards ducting:
(1) (C U) Atmospheric conditions suggest USS Vincennes was operating with a strong surface based duct (extending up to approximately 485 ft) and also within an evaporation duct extending up to approximately 78 ft. (IO Exhibit 179).
(2) (S U) AN/SPY-1 (AEGIS radar), AN/AWG-9 (F-14 radar) and AN/UPX-29 (IFF) emitters show strong coupling with these ducts greatly enhancing detection ranges. (IO Exhibits 179). {p.14-1988}
(3) (S U) The data provided by NSWC Dahlgren also validates that, in fact, SPY radar was ducting, resulting in greatly enhanced detection ranges. (IO Exhibits 86, 87, 88, and 184)
5. Commercial Air
a. General {p.23-1993}
(1) (U) Bandar Abbas International is a joint military/commercial airfield. (IO Exhibit 90, (b)(6), (b)(7)(C) p.418).
(2) (U) A total of 18 commercial air routes cross the Persian Gulf area covering at least 50% of the navigable waters. (IO Exhibit 90, (b)(6), (b)(7)(C) p.407).
(3) (U) A total of 12 commercial air routes cross the southern Persian Gulf/Strait of Hormuz area alone. Specifically, 7 into or out of Dubai/Sharjah Terminal Control Area and 5 into or out of Abu Dhabi Terminal Control Area. (IO Exhibit 90).
(4) (S U) Commerical air flights that do not approach Iran during any part of the flight or come from non-belligerent air space and are at the high altitudes normally flown by air carriers are relatively easy to identify. (Enclosure (21)).
(5) (U) The width of the airway assigned to Iranian Air Flt 655 (A-59) was: 20NM (10NM either side of centerline) from Bandar Abbas to reporting position DARAX and 10NM (5NM either side of center line to Sharjah. Airway A-59 runs from an altitude of 4500 feet to infinity. The total length of the air route is 123NM. (IO Exhibit 249).
(6) (U) At least one thousand seven hundred and seventy-five commercial air flights passed through Oman Center for the week ending 13 July 1988. ( (b)(6), (b)(7)(C) p.410).
(7) (S U) The only message traffic available to CJTFME on civilian airline schedules was the “FICPAC” message of 25 June 1988. That message was readdressed to all CJTFME units on 28 June 1988. (IO Exhibit 124, (b)(6), (b)(7)(C) pgs. 394, 408).
(8) (U) The CJTFME’s inchop brief discusses commercial air traffic in general but does not focus on any specific air routes or COMAIR schedules. (IO Exhibit 8 and (b)(6), (b)(7)(C) p.392).
(9) (S U) CJTFME’s inchop brief discusses the use of MAD (Military Air Distress) and comments that, “Iranians won’t answer nor will commercial aircraft”. Moreover ships are told to use IAD (International Air Distress) to contact commercial aircraft and “unless you are up a regional ATC frequency, use IAD to try to contact ATC”. (IO Exhibit 8, MEF Brief p.4).
(10) (U) The inchop brief alludes to the “very complex but ordered” commercial air picture. It cautions all units to be concerned with those air contacts which deviate from the normal pattern. (IO Exhibit 9, MEF Brief p.3). {p.24-1993} {p.15-1988}
(11) (U) The first time that CJTFME promulgated commercial airline flight information to the ships in the Persian Gulf area was on 28 June 1988. This message showed IR 655 scheduled to depart Bandar Abbas at 0950L (0620Z) on Tuesday and Sunday of each week. (IO Exhibit 124, (b)(6), (b)(7)(C) p. 409).
(12) (S U) The first documentation of conflict between civilian COMAIR and a CJTFME unit was on 8 June 1988 when the USS Halyburton issued nearly continuous challenges to an aircraft landing at Dubai International. British Airway FLT 147 acknowledged the challenge, made the turn as directed by the USS Halyburton and immediately came into a “near miss” situation with another civilian aircraft. A formal protest was filed by ATC Dubai and an American Embassy letter of apology resulted. (IO Exhibit 119, p.274).
(13) (S U) The only commercial/military IFF information available to any JTFME unit were pass-down items from other Middle East Force ships. (IO Exhibits 120, 121, 122, (b)(6), (b)(7)(C) p.182, (b)(6), (b)(7)(C) p.197).
(14) (S U) U.S. ships deployed to Persian Gulf area are limited to a single VHF radio which is tuned to International Air Distress (IAD) frequency 121.5 mHz. ¶
(15) (U) During USS Vincennes inchop brief, conducted on 22 May, (b)(6), (b)(7)(C) (CJTFME/Air Ops) and (b)(6), (b)(7)(C) (CJTFME/Asst Air Ops) briefed the Helo Det on helo ops but did not specifically discuss commercial air routes or schedules. (IO Exhibit 8 p.176, (b)(6), (b)(7)(C) p.392).
(16) (U) On Sunday, 3 July 1988, there were 10 civilian flights scheduled from Bandar Abbas. They were:
| Flight No. | To | Depart Time | Aircraft Type |
| IR 655 | Dubai | 0959L | AirBus 300 |
| IR 236 | Bandarlengeh | 1240L | 737 |
| IR 236 | Shiraz | 1240L | 737 |
| IR 236 | Tehran | 1240L | 737 |
| IR 452 | Tehran | 1340L | AirBus 300 |
| IR 394 | Isfahan | 1400L | 737 |
| IR 394 | Tehran | 1400L | 737 |
| IR 134 | Shiraz | 2050L | 737 |
| IR 134 | Tehran | 2050L | 737 |
| IR 458 | Tehran | 2245L | AirBus 300 |
There is no information to the contrary that the remaining flights did not launch. (IO Exhibit 162, 232).
Query: “10” flights?
These are 6 flights. Not 10. All are domestic flights, internal to Iran, except for IR 655. Which is the only flight scheduled to depart that morning. And the only departing flight scheduled to cross the Gulf that day.
Query: “0959L”?
The scheduled time of departure for IR 655 — wrongly listed here at 0959 local time — was 0950L, 9 minutes earlier. Fogarty corrected this mistake in a written statement to the Senate. He said it was a typographical error. (Senate Hearing, p.26 (Sept. 8 1988)).
But he did not say who made this error. Was this a typo by the DoD Report-writers? Or, instead, did they accurately copy a typo present on the warship’s flight schedule. If it was an accurate copy, then the take-off delay of IR 655 was reduced, by the typo, from 15 minutes (actual) to 6 minutes (perceived).
Query: “IR 452”? “No information to the contrary”?
IR 452 would have been the IR 655 AirBus and crew, on their return from Dubai, stopping over at Bandar Abbas on their way back to Tehran, to complete their round trip flight for the day. It “did not launch”. ICAO Report, p.1, ¶ 1.1.1.
–CJHjr
(17) (U) As a result of the attack of the USS Stark, the JCS issued an up-dated Notice to Airman (NOTAM) for the {p.25-1993} Persian Gulf, Strait of Hormuz, Gulf of Oman and North Arabian Sea dated 8 September 1987, which notified all Persian Gulf countries of additional defense precautions which U.S. warships would be exercising. It highlighted the requirement for aircraft operating in the area to maintain a listening watch on 121.5 mHz VHF or {p.16-1988} 234.0 mHz UHF {sic: 243.0 mHz}. Both Department of State and ICAO report that this NOTAM was transmitted through channels to the Government of Iran. (IO Exhibit 52 {and 135}).
Query: “Up-dated”?
This was not an “up-dated” NOTAM.
It was merely a supplemental NOTAM.
Which left in place this NOTAM, which senior U.S. military officers concealed from their report:
NOTAM, 112119 KFDC.
Iran Air Flight 655 was never “less than 2000-feet” “within 5 n.miles” of any U.S. warship. IR655 was about 15 n.miles inside Iranian territory (along its route), at 12,500 feet and climbing, and 12 n.miles away, when Vincennes Commander William Rogers turned his firing key.
Could that be why senior U.S. military officers omitted this NOTAM from their report? A material omitted fact.
And, why did they omit to quote, in their report, the one NOTAM they did refer to, but carefully concealed, amongst their classified exhibits? (IO Exhibit 52 and 135).
Could this be the reason?:
NOTAM FAA FDC 052/87.
IR655 pilots were never once “requested to identify themselves and state their intentions”. As this NOTAM required U.S. radio-talkers to do.
And, this NOTAM assured pilots that they were entitled overfly U.S. warships. A promise to pilots, that U.S. military officers would not deem it hostile intent, if a pilot, high and climbing, approached a U.S. warship in an airway.
Little wonder, senior U.S. military officers, united in a prima facie criminal conspiracy, decided to file an official U.S. report full of misleading prima facie criminal lies of omission. And, to deliver these prima facie criminal lies to Congress.
Here’s what these senior U.S. military officers concealed: The full text of both U.S. NOTAMs, exactly as they appear on the page, in every weekly edition, prior to the ambush, of the U.S. International Notices to Airmen:
Iran – Persian Gulf
In response to the recent attack on the USS Stark and the continuing terrorist threat in the region, U.S. naval vessels operating within the Persian Gulf, Strait of Hormuz, Gulf of Oman, and the Arabian Sea, north of 20 degrees north, are taking additional defensive precautions. Aircraft (fixed wing and helicopters) operating in these areas should maintain a listening watch on 121.5 mHz VHF or 243.0 mHz UHF. ¶
Unidentified aircraft, whose intentions are unclear or who are approaching U.S. naval vessels, will be contacted on these frequencies and requested to identify themselves and state their intentions as soon as they are detected. ¶
In order to avoid inadvertent confrontation, aircraft (fixed wing and helicopters) including military aircraft may be requested to remain well clear of U.S. vessels. ¶
Failure to respond to requests for identification and intentions, or to warnings, and operating in a threatening manner could place the aircraft (fixed wing and helicopters) at risk by U.S. defensive measures. Illumination of a U.S. naval vessel with a weapons fire-control radar will be viewed with suspicion and could result in immediate U.S. defensive reaction. ¶
This notice is published solely to advise that measures in self-defense are being exercised by U.S. naval forces in this region. The measures will be implemented in a manner which does not unduly interfere with the freedom of navigation and overflight. (FAA FDC 052/87)
U.S. Naval Forces in the Persian Gulf, Strait of Hormuz, Gulf of Oman, and Arabian Sea (North of 20 Degrees North) are taking additional defensive precautions against terrorist threats. ¶
Aircraft at altitudes less than 2000-feet AGL which are not cleared for approach/departure to or from a regional airport are requested to avoid approaching closer than 5-nm to U.S. naval forces.
It is requested that aircraft approaching within 5-nm of U.S. naval forces establish and maintain radio contact with U.S. naval forces on 121.5-mHz VHF or 243.0-mHz UHF. ¶
Aircraft which approach within 5-nm at altitudes less than 2000-feet AGL whose intentions are unclear to U.S. naval forces may be held at risk by U.S. defensive measures. ¶
This is a joint USCINCPAC and USCINCCENT NOTAM affecting operations within their respective area of responsibility. (112119 KFDC)
Source: “Foreign Notices, Iran–Persian Gulf,” International Notices to Airmen, June 30 1988 (U.S. Department of Transportation, Federal Aviation Administration) {SuDoc: TD 4.11:, ISSN: 0364-6742, LCCN: 76648577, OCLC: 02169082, GPOCat, paper, DL, WorldCat}, bold-italics and additional paragraphing added. Photocopy: ICAO Report, p.F-4. NOTAM FAA FDC 052/87 was originally issued Sept. 8 1987. NOTAM 112119 KFDC was originally issued in 1984 (ICAO Report, ¶ 2.2.1, p.10).
Both appeared together in every weekly edition of FAA NOTAMs.
Both were in force on the day of the ambush. –CJHjr
(18) (S U) The current verbal warnings issued by CJTFME units do not clearly identify exactly which aircraft the ship is attempting to contact. (IO Exhibits 275, 306).
(19) (S U) Commercial aircraft normally do not have radar homing and warning (RHAW) equipment. U.S. Navy ships either “locking up” with pulsed fire-control or continuous wave radars expect no reaction from a commerical {sic: commercial} air flight. (Enclosure (21)).
(20) (U) For the period of 2 June 1988 to 2 July 1988, analysis of challenges and warnings conducted by CJTFME resulted in the following statistics:
(a) 150 challenges were issued
(b) only 2 were to COMAIR (1.3%)
(c) 125 were to Iranian military aircraft (83%)
(d) Largest number of challenges issued were by the USS Spruance patrolling the eastern entrance of the SOH.
(IO Exhibit 118).
(21) (S U) No Iranian F-14’s were challenged during the 2-17 June 1988 timeframe but seven were challenged in the 13 June – 2 July 1988 time period. (IO Enclosure (21)).
(22) (U) Commercial air carriers have been observed changing IFF {modes and} codes when crossing the Persian Gulf area. (IO Exhibits 54, 55, (b)(6), (b)(7)(C) p.174, (b)(6), (b)(7)(C) p.194).
(23) (U) Iranian military aircraft have been observed squawking all IFF modes (I, II, and III) and codes and at times follow commercial air routes within the Persian Gulf. (IO Exhibits 54, 55, (b)(6), (b)(7)(C) p.174, (b)(6), (b)(7)(C) p.7).
(24) (U) Iraqi military aircraft have followed the air routes from Iraq during Persian Gulf ship attack profile (SAP) missions and return using the same air routes. (IO Exhibit 15, (b)(6), (b)(7)(C) p.7).
(25) (U) Iran Air Flight 655 a was {sic: was a} regularly scheduled biweekly flight from Bandar Abbas to Sharjah, often referred to as a “HAJ” flight by ships’ crews. (IO Exhibit 162, 54, 55, 73, (b)(6), (b)(7)(C) p.175, (b)(6), (b)(7)(C) p.197). {p.26-1993}
(26) (U) CJTFME and CO USS Vincennes discussed the complexity of the commercial air picture on several occasions prior to 3 July 1988. ( (b)(6), (b)(7)(C) p.856, 861).
(27) (S U) Airbus’ normally climb at 350–370 KTS and cruise at 450–460 KTS. (IO Exhibit 238).
b. Iran Air Flight 655 {p.17-1988}
(1) (U) Iran Air Flight 655 Airbus, A-300B2-202, was delivered by the French Airbus Industrie on 30 April 1982 configured with a standard civilian type Dual Collins 621-A6 IFF. The General Electric engines are identified as GE CF6-50C2. Airbus Industrie has never delivered an Airbus equipped with an IFF radar Mode II. (IO Exhibit 247).
(2) (U) Bandar Abbas International is the only active, joint use (military/civilian) Iranian airport in the southern Persian Gulf area. (IO Exhibit 90, (b)(6), (b)(7)(C) p. 418).
(3) (S U) Iran Air Flight 655 was scheduled to depart Bandar Abbas at 0950(L) or 0620Z but actually took off at 1017(L) or 0647Z. (IO Exhibit 232 & 280).
Query: “But”?
Scheduled Time of Departure (when the aircraft door closes at the departure gate) is shown on a published airline schedule.
Take-off time (when the wheels leave the ground) is not shown on an airline schedule.
These are different events.
Hence, they cannot be contrasted by a “but”.
But, this “but” — purporting to contrast them — foreshadows an intensive campaign of deceit, by senior U.S. military officers, asserting unanimously, that the flight “took off 27 minutes late”.
IR655 took off 15 minutes late, due to an immigration problem of one passenger at the gate, which delayed closing the aircraft door by 15 minutes.
The unanimous deceitful assertion, of 27-minutes, was made by senior U.S. military officers in an official written endorsement of this report. In sworn testimony and written statements to Congress. And in press conferences and other public statements.
Billions of people in the world have never flown on an airliner. And, hence, have never had to apply their minds, to when they have to be at the airport gate to board a flight.
But these senior U.S. military officers are not among them.
It’s impossible to believe, that these senior U.S. military officers actually believed their own assertion: That an airline’s published scheduled time of departure is the same event as its take off time.
Yet, unanimously, that’s exactly what they asserted. As an unassailable fact.
Nevertheless, regardless of what they believed, they were negligent. By failing in their duty to inform their warship crews, of the difference between these two events.
Without this explanation, they incited their warship crews to wrongly believe that an airliner taking off on time (eg: 12 minutes after its scheduled time of departure) was taking off 12 minutes late.
Adding this item of negligence to their apparent negligence in failing to explain the 30-minute warship clock issue, senior U.S. military officers negligently incited their warship crews to wrongly believe, that an airliner taking off 15 minutes late from Bandar Abbas was taking off an hour late.
Senior U.S. military officers united in this prima facie criminal conspiracy, to diminish the perception of their negligence, in failing to properly instruct their warship crews on these time issues.
So that their warship crews could properly stand watch. For the only airliner scheduled to depart Bandar Abbas airport that morning. And the only departing airliner scheduled to cross the Gulf that day.
“Reckless” negligence. Because they could foresee the deadly consequences of their neglect to do their duty.
This negligence, by senior U.S. military officers, to properly instruct their warship crews on these time issues, is a prima facie proximate cause of the ambush.
An excellent criminal motive for senior U.S. military officers to lie about the extent of the take-off delay. And to conceal the warship clock setting, from their deceitful report. –CJHjr
(5) (U) The control tower at Bandar Abbas failed to warn Iran Air Flight 655 that there was an ongoing naval engagement between U.S. Naval Forces and Iranian Revolutionary Guard naval forces (IRGN). (IO Exhibits 280, 232).
(6) (S U) Iran Air Flight 655, on direction of the control tower at Bandar Abbas International, turned on its IFF Mode III to 6760 on deck prior to launch and the mode was read correctly by the tower as 6760. (IO Exhibit 280).
(7) (S U) Iran Air Flight 655 took off from Bandar Abbas International Airfield on runway 21 at 0647Z. It was cleared to Dubai via A-59 at FL 140 (14,000 FT) with an assigned IFF Mode III squawk of 6760. The pilot reported passing MOBET (position report) at 0654Z and vacating FL 120 (12,000 feet). (IO Exhibits 232, 235, 236, 280).
(8) (S U) Iran Air Flight 655 squawked Mode III 6760 from take off to missile intercept. (IO Exhibits 91, 280).
(9) (S U) IR 655 was 3.35NM west of the centerline of air route A-59 at missile intercept, time 0654:43, passing {p.27-1993} 13,500 climbing to an assigned altitude of FL 140 (14,000 FT), on course of 209.5T, at 383 KTS. (IO Exhibits 91 and 102).
(10) (U) Air Traffic Control Center at Abu Dhabi neither gained radar video nor established communications with Iran Air Flight 655. (IO Exhibits 306, 275).
6. USS Vincennes
a. Training and Readiness.
(1) (U) USS Vincennes deployed 25 April 1988, on short notice, to the Persian Gulf/Middle East Force. (IO Exhibit 166: Encl 1 and 4). {p.18-1988}
(2) (U) USS Vincennes was directed on 20 April 1988 to detach from FLEETEX 88-2 for immediate return to homeport and a 21 April 1988 deployment to the Persian Gulf/Middle East Force. USS Vincennes transit was to be directly from San Diego to Subic Bay and onward to Middle East Force with an arrival in the Persian Gulf of 16 May 1988. (IO Exhibit 166: Encl 2).
(3) (CU) Upon notice of deployment on 20 April 1988, USS Vincennes was in the highest state of training and readiness: C1 in Personnel, Supply, Equipment and Training; M1 in AAW, AMW, ASW, ASUW, C3, EW, and training areas. (IO Exhibit 166: Encl 2A; Definitions of readiness and training ratings included in IO Exhibit 166: Encl 2B).
(4) (CU) Prior to deployment on 25 April 1988, USS Vincennes participated in interim refresher training (26 Oct – 6 Nov 1987), FLEETEX 88-1/COMPUTEX 88-3 (1-12 FEB 88) and a portion of FLEETEX 88-2 (8-19 APR 88). On completion of interim refresher training, USS Vincennes was found to be fully capable of performing duties as AAWC or LAAWC in Battle Group operations. (IO Exhibit 166: Encl 2b, 3a, 4, 2c).
(5) (CU) During FLEETEX 88-1, USS Vincennes participated in a Middle East Force Exercise (MEFEX) 5-8 FEB 88. This exercise simulated an “Earnest Will” {1069kb.pdf} escort mission, and provided: anti-silkworm training, terrorist aircraft training, terrorist small boat defense, and anti-swimmer defense. (IO Exhibit 166: Encl 2a, 3, 4, 2c).
(6) (CU) USS Vincennes did not complete FLEETEX 88-2 due to her early deployment; however, USS Vincennes participated in the following training evolutions during FLEETEX 88-2: extensive war-at-sea strike exercises (WASEX); Silkworm missile attacks; training in ROE; and fast patrol boat attack simulations. (IO Exhibit 166: Encl 2a, 3, 4, 2c). {p.28-1993}
(7) (CU) A normal MEF augmenter pre-deployment schedule would have included in addition to the exercises listed in Finding of Facts A.6.a. (4) and (5), two Middle East Force Exercises (MEFEXs) at PMTC, PT Mugu, California, and PMRF Barking Sands, Hawaii. USS Vincennes did not conduct these exercises because of her early deployment and accelerated transit to Subic Bay, RP. (IO Exhibit 166, Encl 4).
(8) (CU) USS Vincennes was provided AEGIS Training Center Briefs on lessons learned on the operation of SPY-1A radar in the Strait of Hormuz/Persian Gulf by AEGIS Training Center, Dahlgren, VA, while inport Subic Bay, RP, on 11 May 1988. (IO Exhibit 166: Encl 8, 9, and 9a).
(9) (CU) During a four day period (9-12 May), USS Vincennes conducted the following Middle East Force training in the Subic Bay operating areas: two missile firings (both successful), one war-at-sea strike exercise (against 17 aircraft), CIWS tracking/firing, Silkworm profiles, air intercept controlling, anti-fast patrol boat exercises (night and day), surface gunnery, and surface to air gunnery. (IO Exhibit 166: Encl 17, 18, 19, 20, and 20a).
(10) (CU) The WASEX conducted on 9 May 1988 included 17 attacking aircraft: 10 USAF (4 Wild Weasel and 6 Pave Tack) and 7 USMC (4 A-6 and 3 F/A-18). A post exercise critique was conducted on 10 {p.19-1988} May with USAF, USMC, and USS Vincennes personnel present. USS Vincennes Large Screen Display (LSD) information was used to reconstruct the events of the exercise. This reconstruction revealed USS Vincennes had to discriminate threat aircraft from numerous other air contacts in the area including USAF AIR-AIR missile participants and normal air traffic in the vicinity of Clark AFB and Crow Valley, RP. ¶
(11) (CU) Prior to arrival Subic Bay, RP, USS Vincennes modified her Battle Organization to conform to the expected “GW” assignment in the Middle East Force. In a meeting with the CO, XO, CSO and OPSO in attendance, the CO decided that CSO and OPS officer would stand watch as “GW”, operating from the embarked commander’s console (LSD #2). ¶
(13) (CU) USS Vincennes reported this Battle Organization modification was implemented during the transit from San Diego to Subic Bay, RP, and exercised during MEF training periods in Subic Bay, RP operating areas (9-12 May 1988) and during the JTFME CVBG familiarization training (21-24 May 88). (Rogers p.834, (b)(6), (b)(7)(C) p.809, (b)(6), (b)(7)(C) p.788).
(14) (CU) Three Rules of Engagement Exercises (ROEX) were conducted by USS Vincennes during the period 6-20 May 88. These exercises tested USS Vincennes’s interpretation and correct response to current ROE for the Persian Gulf/Middle East Force. (IO Exhibit 166: Encls 21, 22, 23, 24, 25, and 26).
(15) (CU) USS Vincennes chopped to CJTFME on 20 May 1988 and was C1 in areas of Personnel, Supply, Equipment and Training as well as being M1 in AAW, AMW, ASUW, ASW, CCC, ELW and MOB. (IO Exhibit 166: Encl 27).
(16) (CU) USS Vincennes CO, TAO and GW stated in their testimony that USS Vincennes was well prepared for their assignment to the Middle East Force by virtue of their AW (in workup exercises), “GW” experience, and in depth MEF augmenter training. (Rogers p. 835, (b)(6), (b)(7)(C) p.824, (b)(6), (b)(7)(C) p.804).
(17) (CU) USS Vincennes conducted Battle Group familiarization training with the CVBG assigned to JTFME in the Gulf of Oman (21-24 May 88) prior to entering the Persian Gulf. Exercises conducted provided training in: WASEX, Silkworm profiles, SUCAP coordination and A/C training. (IO Exhibit 166: Encl 28).
(18) (CU) Summary of USS Vincennes operations since arriving in the Middle East Force: {p.20-1988}
| {27} 25 - 27 May 88 | Task Group Exercise |
| 29 May 88 | Sitrah anchorage inchop briefings |
| 30 May 88 | Sitrah anchorage AWACS/LINK interoperability |
| 01 - 08 Jun 88 | SOHWPA patrol {p.30-1993} |
| 10 - 11 Jun 88 | Sitrah anchorage for upkeep |
| 12 - 16 Jun 88 | SOHWPA patrol, conducting AAW and ASUW surveillance |
| 17 Jun 88 | RPS patrol, conducting AAW surveillance |
| 18 Jun 88 | Sitrah anchorage for upkeep |
| 19 - 20 Jun 88 | RPS patrol, conducting AAW surveillance |
| 21 - 29 Jun 88 | CPG/Escort, AAW surveillance and escort operations |
| 30 Jun 88 | OPS outside Straits |
| 01 Jul 88 | CPG (E)/SOHWPA/SOH/FUJAIRAH |
| 02 Jul 88 | FUJAIRAH/SOH/SOHWPA, AAW and ASUW surveillance |
| 03 Jul 88 | CPG (E)/SOHWPA, AAW and ASUW surveillance |
(IO Exhibit 159).
(19) (U) USS Vincennes had not experienced combat prior to 3 July 1988. (IO Exhibit 159, (b)(6), (b)(7)(C) p.816).
b. Watch Organization
(1) (U) USS Vincennes’ Battle Doctrine (VincennesINST C3510.1) was signed by Capt G.N. Gee, USN, the Commanding Officer USS Vincennes just prior to Capt Rogers, on 1 May 85. This document has subsequently been used as a baseline for Pacific Fleet AEGIS cruisers. (IO Exhibit 160, and (b)(6), (b)(7)(C) p.809).
(2) (CU) CO USS Vincennes Standing, Steaming and Battle Orders were signed on 9 Jan 1988 by Capt Rogers as a modification and sub-doctrine to USS Vincennes Battle Doctrine. ¶
(3) (U) USS Vincennes’ watch organization during pre-deployment training was in accordance with CO’s Battle Doctrine and Standing Orders. (IO Exhibit 160, { (b)(6), (b)(7)(C) } 809). {p.31-1993} {p.21-1988}
(4) (U) The CO modified basic Battle Doctrine for PG Ops by placing the SITREP officer at OSDA #1 and International Air Distress (IAD) operator at LSD #1. He also placed the data recorder (CICO) directly behind LSD #2 and #3 to maintain a timeline of events. The CICO was in view of all large screens and could see “GW’s” CRO. ( (b)(6), (b)(7)(C) p.570).
(5) (U) On 3 Jul 88, USS Vincennes’ primary AAW watch organization was as follows:
| CO | Capt Rogers |
| XO | (b)(6), (b)(7)(C) (on the bridge) |
| TAO | (b)(6), (b)(7)(C) |
| OSDA | (b)(6), (b)(7)(C) |
| GW/FAAWC | (b)(6), (b)(7)(C) (At EC console at ADS) |
| CIC Officer | (b)(6), (b)(7)(C) (No console) (worktable behind “GW”) |
| IAD Talker | (b)(6), (b)(7)(C) (STAO console at ADS) |
| CSC | (b)(6), (b)(7)(C) |
| TIC | (b)(6), (b)(7)(C) (DSA/AAW ASUW C&R Net) |
| IDS | (b)(6), (b)(7)(C) |
| SLQ-32 | (b)(6), (b)(7)(C) |
| EWS | (b)(6), (b)(7)(C) |
| MSS | (b)(6), (b)(7)(C) |
| ARC | (b)(6), (b)(7)(C) (MAD Talker) |
| AAWC | (b)(6), (b)(7)(C) |
| ACS | (b)(6), (b)(7)(C) |
(IO Exhibit 174).
(6) (U) USS Vincennes’ enlisted general quarters CIC watchstanders for 3 Jul 1988 were PQS qualified for watches held that day (IO Exhibit 167, 170).
(7) (U) The Commanding Officer USS Vincennes certified all officer watchstanders as qualified; however (b)(6), (b)(7)(C) {Lieutenant Clay Zocher} had not completed PQS for AAWC (his 3 July 1988 GQ station). (IO Exhibits 151, 152, (b)(6), (b)(7)(C) p.722).
Personnel Qualification Standards (PQS). –CJHjr
(8) (S U) The Commanding Officer USS Vincennes stated his confidence level before and subsequent to the incident in (b)(6), (b)(7)(C) and (b)(6), (b)(7)(C) was the highest it could be. He also stated he had great faith in his “GW” organization and his CIC team’s experience. (Rogers p. 834-840).
c. Overall Combat System Status
(1) (U) USS Vincennes’ Preventive Maintenance System (PMS), which covers the AEGIS combat system, was recorded {p.32-1993} properly and showed no significant discrepancies. (IO Exhibit 147).
(2) (U) The AEGIS combat system was working exceptionally well on 3 July. No anomalies were noted in data analysis or from operator statements. (Enclosure 15). {p.22-1988}
(3) (U) Semi-annual check for the OE120 IFF Phased Array Antenna was last completed in February 1988 with its next scheduled check to be completed on 12 July 1988. (IO Exhibit 145, (b)(6), (b)(7)(C) p.350).
(4) (U) Upon the completion of the OE120 July Semi-Annual PMS check of the OE120 IFF antenna, the following discrepancies were noted: Phase Shifter #13 had no power out; #12 was 1.0 db below PMS Spec; one Phase Shifter was within spec. The OE 120 has a total of 16 phase shifters ( (b)(6), (b)(7)(C) p.350).
(6) (U) The CASREP summary for USS Vincennes shows no significant degradations of AEGIS Combat System as of the 8 o’clock reports for 2 July 1988, with the exception of CIWS (close in weapons system) Mount 22. (IO Exhibit 139). The data from NWSC Dahlgren substantiates the excellent performance of the system. (IO Exhibit 91; enclosure 15).
(7) (U) The SPY-1A signal processor alignment was completed during the last week of April 1988 and the first week of May 1988. Operational Performance Tests (OPTS) were run weekly with no significant degradation. The system had been operational almost non-stop since arrival in Gulf. Its performance was exceptional. (IO Exhibit 147, 148, 142, 153).
(8) (U) One of the consoles in CIC (AIC) was down. ( (b)(6), (b)(7)(C) p.707).
(9) (U) At the time of the incident, Mount 22 (CIWS) was down and Mount 21 was in “AAW AUTO” mode with “hold fire” on. (IO Exhibit 91).
d. Communications
Senate Hearing, p.30 (Sept. 8 1988)
(2) (U) USS Vincennes’s primary radio telephone talker for MEF Execution was the FAAWC “GW”. He was directly responsible for relaying both the surface and air tactical picture, as seen on USS Vincennes, along with the force air picture, as seen on USS Sides and USS Elmer Montgomery, to “GB”. ( (b)(6), (b)(7)(C) , p.809, (b)(6), (b)(7)(C) , p.788).
(3) (U) USS Vincennes internal net 15 is designated for warfare coordinators, only, i.e. CO, TAO, OOD, SSWC, CSC, TIC, SSES. (IO Exhibit 160).
(4) (U) On 3 July 1988, the following CIC operators were using net 15 or 16 in addition to warfare coordinators: FWC, IDS, EWS, RSC, SITREP Officer at ECDA, EWS, EWCO and various other stations that had “punched” into the net. (IO Exhibit 160, pp.1-5; (b)(6), (b)(7)(C) , p.528).
(5) (U) Internal communications had to be shifted between net 15 and 16 due to degradation of the CKT during the 3 July 1988 events. ( (b)(6), (b)(7)(C) p.528). {p.23-1988}
(6) (U) Internal net 15/16 was heavily used and difficult to get information across. ( (b)(6), (b)(7)(C) , p.684).
(7) (U) Internal communications procedures, i.e. specific call ups in accordance with standard procedures, were known by operators but not always used. ( (b)(6), (b)(7)(C) , p.567).
e. Combat Systems Doctrine
B. Events Leading up to the Air Engagement
1. Ancillary Air Data
a. (U) At 0330Z 3 July 1988 the disposition of the non-participant ships, both U.S. and Allied, was as follows:
(1) (U) USS John Hancock was at SITRAH anchorage in Manama, Bahrain.
(2) (U) Halsey was in the Northern Persian Gulf, RPS.
(3) (U) USS O'Brien was off Kuwait waiting to begin the outbound transit of Sea Isle City and M/V Patriot.
(4) (U) USS Fahrion was inport Ras al Khaimah for a routine port visit.
(5) (U) USS Coronado was pier side, Mina Sulman at Manama, Bahrain with CJTFME embarked.
(6) (U) HMS Manchester was 150 NM from the incident, outside the SOH. HMS Beaver and the Italian warship Espero were in the Southern SOH, approximately 75 NM from the incident.
(7) (CU) CJTFME requested all three Allied ships to provide any information relative to TN 4131 and whether they had heard the warnings on IAD. HMS Beaver responded by delivering its recordings and transcripts of the USS Vincennes IAD warnings to the Senior Investigating Officer. HMS Manchester indicated that it did not hear the warnings over IAD. Information received from the Italian Naval Headquarters indicated that the Espero did not hear the IAD warnings.
Query: “Beaver ... Espero ... 75 n.miles”?
Why did the Beaver record IAD broadcasts, but not the Espero? When they were both together?
And how did the Beaver receive a line-of-sight VHF broadcast (121.5 mHz), over the horizon, from a surface vessel, 75 n.miles away?
The answer to these questions senior U.S. military officers concealed, from the public, when they released their report, in 1988.
But in 1993, a possible answer became apparent:
DoD Report, ¶ (3)(f), p.44 (below).
And so, the Beaver crew might not have received this broadcast via VHF. They might have copied it via UHF relay from Hawkeye, or off the satellite (UHF SATCOM), if the Vincennes sent that IAD communication net to the fleet.
This, because, if the Beaver logged on to Link-11, then they also likely acquired the fleet voice communications, at the same time.
Link-11 was developed for data communications of radar track data, e.g., from warships on radar picket duty.
Initially, Link-11 was broadcast by a HF radio (High Frequency: 2-30 MHz), which normally carries over the horizon, because its long wave-length normally reflects back to earth, bouncing off the earth’s ionosphere. Those who remember long distance AM radio (50,000 watts) will remember its vagaries: sometimes a good powerful signal, and sometimes not, with reception dead-spots, depending on your location in the hop, skip, and jump pattern of the signal bounce, varying with location and time of day (ionosphere altitude and density), and interference, from sun spot activity, distant broadcasts on the same frequency, lightning, rain, wind turbulence (?), and such. Also, such broadcasts require high power (electricity demand) and, for that reason, might also pose a radio frequency radiation hazard to the sailors.
In theory, Link-11 data can also be broadcast by low-powered UHF radio (Ultra High Frequency: 225-400 MHz), line-of-sight to nearby warships, via NTDS (Naval Tactical Data System), and for relay by Hawkeye, via ATDS (Airborne Tactical Data System). UHF normally does not carry over the horizon, because its short wave length normally penetrates the ionosphere and escapes into space.
But, apparently, Link-11 data can also be transmitted via satellite (why not), and this may be what the Vincennes did, according to the ICAO Report (¶ 1.16.1.3, p.8), via its “link 11 OE-82 satellite communications antenna”.
Satellite Link-11 would enable the Pentagon to follow the action in real-time, near Washington D.C. And, enables the Pentagon to tape-record the action, including the position of its warships and all of the radar tracks.
May be, the Link-11 data is broadcast (as designed) by HF radio, and also by satellite, or relayed to the satellite by the NSA/GCHQ listening station on the Musandam Peninsula, or by fleet HQ at Bahrain, so the Pentagon can have it in real time, and so too submarines, aircraft and ships with poor HF reception.
The position of the warship derives automatically from SINS (Ship Inertial Navigation System), a continuous, time-stamped, report of the warship’s exact geographical coordinates, to 5 decimal places (10 yards or so, I suppose, I’ll compute it eventually).
The listening station on the Musandam Peninsula might also be a UHF relay station, receiving UHF broadcasts from warships and aircraft (eg: the AWACS over the Northern Gulf) and rebroadcasting, from its various microwave-linked antennas sited, at high elevations (up to 6800 feet). And, were it necessary (it’s not), thousands of feet higher still, from a tethered helium balloon. The elevations on the linked admiralty chart are in meters. The highest point on the linked image is 1845 meters = 5996 feet. Two n.miles southwest, not shown on that image, the highest point is 2086 meters = 6779 feet (Jabal al Harim, 56-13-54 E, 25-58-38 N, 56.23167 E, 25.97722 N). (Admiralty Chart 2888, widths: 620px, 780px, 1000px, 1263px, 1580px).
Why did senior U.S. military officers decide to conceal what the Beaver did, their business with Link-11?
Could this be the reason?:
There’s no trustworthy proof the IAD broadcasts were ever, in fact, broadcast. (ICAO Report, pp. 15-16, quoted below).
Merely an assertion, this solitary assertion, that the Beaver received it.
And now we learn, the Beaver may not have received it.
The ‘broadcast’ could be recorded, by the warship’s tape recorder, and communicated to its Link-11 transmitter, or its UHF radio transmitter, or its UHF satellite transmitter, via the warship’s internal communication net, its Integrated Communication System.
Without ever being broadcast on VHF.
Without the IAD radio-talker being connected to a VHF transceiver, or that transceiver being connected to an antenna.
Is that what happened?
Emirates Area Control Center had a complete tape recording of the Vincennes warnings on the military frequency (243.0 mHz).
But not the IAD broadcasts.
The Dubai Approach Control IAD tape was blank, recording no broadcasts.
The Bandar Abbas Tower tape contained only part of an IAD broadcast, after the ambush, at 0656:43, to the C-130. Which the report writers omitted from their report. Presumably because it disproves their ducting tale, to do with an F-14 (yet to be explained, below).
This could mean the Vincennes radio crew meanwhile realized the IAD radio-talker was not connected to a VHF transceiver, or that transceiver was not connected to a VHF antenna, and connected him. Perhaps they had the surface warfare radio-talker connected to that transceiver/antenna, because that same frequency is also the emergency frequency for surface vessels. They surely have many antennas. But they have to be connected. And they don’t want two people broadcasting at the same time on the same frequency. So there may be an either/or switch, in the radio room, for that VHF transceiver/antenna. Though, perhaps that’s handled automatically, in the warship’s communication circuitry.
Or, maybe the IAD radio-talker pushed the wrong buttons, on his handset, on the warship’s Integrated Communication System. And thought he was broadcasting, and wasn’t. And someone straightened him out. Judging from where he was sitting, at the Captain’s table, he was not a regular part of the warship crew. A visiting officer, perhaps. He did not obey his talking script (assuming anybody give it to him). Another marker, that he was not trained, and not suited, for the task he misperformed. (Text of talking script to come).
This lack of proof does not mean, with certainty, the broadcasts were not made. There could be some explanation, for example, why the Sides, and the Montgomery, and Hawkeye, and AWACS, and the Musandam NSA/DIA/GCHQ listening station, did not record or report these broadcasts (if any). Ditto the many other ships and boats in that crowded sea. Including the Oman Coast Guard.
But it does mean, that the senior U.S. military officers, who decided what to conceal from the public, were concerned enough about it, that they decided to deceive, and mislead, the public, and Congress, by reporting this Beaver assertion, but concealing, as ‘Secret,’ the possible explanation.
It proves they were willing to lie, to make their case.
If, that is, the Beaver did not copy the IAD ‘broadcast’ on the VHF frequency it was (allegedly) broadcast on.
The asserted Beaver reception is probably fictitious, a malicious, fabricated, lie — the transcript of the asserted recording was later proven to be a lie, by the ICAO report, the British military or MoD or Foreign Office lying to help the Americans.
But there’s another reason the DoD report writers may have cited the Beaver, as the only “proof” of the Vincennes VHF “broadcasts”:
It’s very likely their very many tape recordings of actual VHF broadcasts (as opposed to the Vincennes IAD net, ie: prior to broadcast) revealed a devastating fact:
That each time the Vincennes IAD talker broadcast a “warning,” the Sides IAD talker was also broadcasting a “warning.”
A mish-mash jumble of people talking at the same time, on the same frequency, which no human being could possibly understand.
The evidence of this apparent fact is explained here.
Such simultaneous broadcasts might explain why no other land station received the supposed broadcasts: Their squelch circuits were likely adjusted to mute an over-modulated signal, which this would be, double the usual transmitter power.
If this be the case — simultaneous broadcasts — then this is a prima facie criminal lie by a large prima facie criminal conspiracy of U.S. official criminal liars.
A criminal conspiracy some Members of Congress were likely members of.
As principals.
Each of whom could foresee the deadly consequences of their crimes, namely:
Their felony-murder, or manslaughter, of the mostly American victims of Pan Am 103. A prima facie lawful bombing, a few months later (December 21 1988, 270 victims), if it was conducted by law enforcement officers, acting for Iran, to conduct an international countermeasure (a species of self-defense) to the U.S. refusal to either admit wrongdoing or submit to proper litigation. As Iran publicly promised it would do, if that’s the course U.S. officials decided they preferred.
Finally, there’s always the possibility that the Beaver did not copy these broadcasts. U.K. military officers have lied under oath in their own courtrooms. And so, it’s a very minor matter, for them to step up the plate with a little deceit, to aid and abet an official U.S. Government criminal conspiracy.
Part of a “special relationship.”
A payback, for example, by Margaret Thatcher to Ronald Reagan, for the new generation Sidewinder missiles Reagan gave her for the Falklands war (1982), which enabled her pilots to attack an approaching Argentine aircraft, nose-on, not merely from behind, as before. –CJHjr
2.10.2 Military air distress frequency 243 MHz. A recording of communications on 243 MHz on 3 July 1988 was available from the Emirates ACC (Abu Dhabi). A transcript and recording was also available from USS Vincennes. ... Except for the Italian warship Espero, no other stations reported having heard or recorded communications on 243 MHz at the time of flight IR655.
2.10.3 As civil aircraft did not carry radio equipment capable of being tuned to 243 MHz, these transmissions had no relevance as challenges to a civil aircraft. ...
2.10.5 International air distress frequency 121.5-MHz. A transcript and recording of messages broadcast on the international air distress frequency 121.5 MHz was available from the British warship HMS Beaver and from USS Vincennes.
2.10.6 Personnel at Dubai approach control had listened to their recording of 121.5 MHz for the period 0645 to 0715 hours on 3 July 1988, and reported that there were no messages recorded. The tape was not available. An operator of an oil company radio station located 40 NM south of Dubai reported having heard challenges on 121.5 MHz at about the time of flight IR655 and having recorded the last two or three messages. Requests to verify this report on site by interviewing the operator were denied. No other stations reported having heard or recorded transmissions on 121.5 MHz at that time.
2.10.7 The recording of frequency 121.5 MHz at Bandar Abbas ATC did not contain any communications from 0640 until 0656:43 hours when the latter part of a challenge was recorded. This recording corresponded to a challenge broadcast by USS Vincennes to another unidentified contact (military C-130) approximately two minutes after the destruction of flight IR655.
ICAO Report, pp. 15-16.
b. (U) At 0610Z the three principal U.S. Navy warships involved in Iran Air Flight 655 incident were:
(1) (U) USS Vincennes (CG 49), located at 26-26 N 056-02E.
(2) (U) USS Elmer Montgomery (FF 1082), located approximately 5 NM from USS Vincennes. {p.24-1988}
Query: “Located”?
My, my.
Now what would that bearing be?
Is that an unintentional oversight?
Omitting that material bearing? –CJHjr
(IO Exhibits 17, 102). {p.36-1993}
c. (U) The USS Forrestal was on routine patrol in the Northern GOO area. (IO Exhibit 250).
d. (S U) The USS Forrestal called away and launched the ALERT-7 F-14 and E-2C at 0647Z. (IO Exhibit 250).
i. ( ) (b)(1) .
(IO Exhibit 234).
2. Surface Engagement
a. (S U) At approximately 0330Z, 3 July, USS Montgomery observed seven small Iranian gunboats approaching a Pakistani merchant vessel. USS Montgomery reported over MEFEX net at 0333Z that the small boats had manned machine gun mounts and rocket launchers. (IO Exhibit 130, (b)(6), (b)(7)(C) p.44).
b. (S U) Shortly thereafter USS Montgomery observed a total of 13 Iranian gunboats breaking into three groups. Each group contained 3 to 4 gunboats with one group of four gunboats taking position off USS Montgomery’s port quarter. (IO Exhibit 130 and (b)(6), (b)(7)(C) p.44).
d. (U) At 0411Z USS Montgomery heard, over bridge to bridge, the gunboats questioning merchants in the area, and at {p.37-1993} approximately the same time heard 5 to 7 explosions coming from the north. (IO Exhibit 172, (b)(6), (b)(7)(C) p.44).
e. (S U) No merchant vessels requested assistance and by direction of “GS”, at approximately 0411Z, USS Montgomery proceeded to the southern section of SOHWPA. ( (b)(6), (b)(7)(C) , p.44).
f. (S U) At 0412Z, “GS” directed USS Vincennes to proceed north to the vicinity of USS Montgomery and to investigate USS Montgomery’s report of small boats preparing to attack a merchant. USS Vincennes’s helo Ocean Lord 25 (LAMPS MK-III) on routine morning patrol was vectored to the north to monitor the Iranian small boat activity in preparation for USS Sides transit. (IO Exhibits 130, 172).
h. (S U) At 0615Z Ocean Lord 25 reported being fired on by one group of small boats (TN 4667). (IO Exhibits 149, 172, 212).
i. (U) (b)(6), (b)(7)(C) and (b)(6), (b)(7)(C) , Ocean Lord 25 crew, observed several small flashes and puffs of smoke approximately 100 yards from the helo. (IO Exhibits 149, 212).
j. (U) At the time of firing, Ocean Lord 25 was 8-10 miles to the north of USS Montgomery. ( (b)(6), (b)(7)(C) p.45).
k. (U) Bridge personnel on USS Montgomery reported hearing five detonations to the north just prior to USS Vincennes’s report of the firing on Ocean Lord 25 over MEFEX net. ( (b)(6), (b)(7)(C) p.45).
Query: “8-10 miles to the north”?
Let’s see now.
North. That’s towards Iran.
But whoops.
We don’t know where the Montgomery was.
So how can we know where the helicopter was?
Is that an unintentional oversight?
Omitting that material information?
Or is this an intentional, prima facie criminal lie (by material omission)?
And is this the reason for that lie?:
The Vincennes was at 26 26 N, 056 02 E. (Admiralty Chart 2888, widths: 620px, 780px, 1000px, 1263px, 1580px).
The Montgomery, at this same time (0610), was “approximately 5 NM to the north-west” of the Vincennes (the missing bearing, omitted by the DoD report writers).
This, according to the secret ICAO Report (p. A-1). Later confirmed by the U.S. Government in its court papers, filed in the U.N. International Court of Justice (quoted below).
That puts the Montgomery in international waters, 1/2 mile outside Iran’s territorial waters, 12.5 n.miles offshore Iran (Hangam Island), at 26 29 31 N, 55 58 01 E (26.492 N, 55.967 E).
That puts the helicopter 2.5 to 4.2 n.miles offshore Iran (Qeshm Island and Hangam Island). Menacing the small boats, defying Iran’s territorial boundaries. As deep as 9-1/2 n.miles into Iran’s territorial waters.
That’s the Vincennes helicopter we’re talking about, the one that’s 8-10 n.miles north of the Montgomery, 5 minutes after this position report, when the small boats fired their warning shots (0615). The military helicopter, at 26 39 32 N, 55 58 01 E (26.659 N, 55.967 E) (10 n.miles), or 26 37 30 N (26.625 N) (8 n.miles).
U.S. lawyers, in their court papers, defy charts, coordinates, mathematics, and such, and claim:
(Cited below, p.25, footnote 3).
A miracle of fantasy and imagination.
Contradicted by the facts they admit.
And substantiated by no supposed information. Such as the continuous, automatic, time-stamped, inertial navigation, position logs of the Vincennes, and the Montgomery.
Which they carefully conceal.
I guess they decided to lie themselves, or neglect their duty to investigate the truth of their factual assertions, to save exposing this prima facie criminal lie, to Congress, by Ronald Reagan, and the prima facie criminal conspiracy of criminal liars assisting him:
Ronald Reagan (U.S. President), Report on United States Military Action (White House, July 4 1988) (U.S. Congress 100-2, House Document 100-210, July 6 1988) {SuDoc: Y 1.1/7:100-210, Serial Set: 13880, CIS: 88 H380-8, OCLC: 18239512, GPOCat, paper, microfiche, DL, WorldCat}, reprinted, “Letter to the Speaker of the House of Representatives and the President Pro Tempore of the Senate on the Destruction of an Iranian Jetliner by the United States Navy Over the Persian Gulf” (July 4 1988) (“Dear Mr. Speaker (Dear Mr. President)”), 1988-89 PPPUS 920-921 (book 2) {ucsb, rr}, Public Papers of the Presidents of the United States: Ronald Reagan, 1988-89 (book 2) {SuDoc: AE 2.114:988-89/BK.2, ISSN: 0079-7626, LCCN: 58061050, OCLC: 9054188, 1198154, GPOCat, paper, DL, WorldCat}.
_______________
30 minutes later, the Montgomery was itself more than 5.5 n.miles deep into Iran’s territorial waters, 4 n.miles west of the Vincennes. Itself 3 n.miles deep into Iran’s territorial waters. (Positions at 0654).
When they opened fire on Iran’s small boats (0643).
North and northwest of them (several miles deeper still inside Iran’s territorial waters).
The small boats were lawfully entitled to fire warning shots. Against the armed military helicopter.
They are law enforcement officers. A military force.
Entitled to enforce their nation’s territorial boundary.
Against an unlawful, armed, military invasion of their homeland.
And, had they been in international waters (which they weren’t, according to the two reports), they would also be entitled to fire warning shots, in their self defense, against an armed, hostile, military aircraft, menacing them.
From a nation which had attacked and destroyed half their naval force, less than 3 months earlier. An unlawful, offensive, pre-mediated, crushing, military attack.
A warning to keep its distance.
And, of course, they were entitled to return fire against two warships, which initiated an armed attack against them.
Warning shots.
Is that exactly what Rogers hoped for?
And ordered his helicopter crew to provoke?
To create a pretext?
For him to attack the small boats?
30 minutes later?
“Justified”?
If nobody knew the facts?
And if people believed, or couldn’t disprove, the later lies by the U.S. Government?
Such as lies by Ronald Reagan (U.S. President), to Congress (July 4 1988)?
And lies by Richard S. Williamson (Assistant Secretary of State), to the U.N. ICAO (July 13 1988).
And lies by George H.W. Bush (U.S. Vice President), to the U.N. Security Council (July 14 1988)?
And lies by William M. Fogarty (U.S. Central Command), to the Defense Department (July 18 1988), and to Congress (September 8-9 1988)?
And lies by their many assistants? Aiding and abetting? Conspiring?
Prima facie murder and arson?
Prima facie criminal Rules of Engagement?
Excellent motives for a criminal lie.
By a criminal conspiracy.
Of violent criminals.
And criminal liars.
Richly substantiating this asserton:
Usama Bin Laden, March 20 1997, CNN {543kb.pdf}
_______________
There’s no self defense against self defense.
It’s not self defense to launch an offensive attack 30 minutes after your pretext, even if the pretext had been valid.
It’s no self defense to charge into somebody else’s territorial waters, to menace them, to defy their borders, and to initiate an armed attack. On small boats 10-12 n.miles deep inside their own territorial waters.
The DoD Report writers concealed the position of the Montgomery at this time.
And they concealed the position of the Montgomery and Vincennes both, at the time of the ambush.
But both were later disclosed in the secret ICAO Report.
And in court papers, the U.S. filed in the U.N. International Court of Justice, when Iran sued for this ambush. –CJHjr
______________________
All U.S. naval vessels prior to the engagement with Iranian small boats were in international waters. The ICAO investigation determined that at 6:10 a.m. the position of the three U.S. ships was as follows:
USS Vincennes— 26 26 N, 056 02 E.
USS Elmer Montgomery— 5 nautical miles northwest of the USS Vincennes
USS Sides— 18 nautical miles northeast of the USS Vincennes
See ICAO Report, Appendix A, p. A-1. These positions are all outside of Iranian territorial waters.
* * *
[D]uring the 17 minute engagement it became necessary for the USS Vincennes, in defending itself, to maneuver into waters claimed by Iran as territorial waters. ...
At the time the USS Vincennes fired its surface-to-air missiles (6:54 UTC), it was located at 26 30 47 N, 056 00 57 E.
“Preliminary Objections by the United States of America” {7.25mb.pdf, source}, pages 24 n.1, 27, 27 n.1 (March 4 1991), Iran v. United States (“Aerial Incident of 3 July 1988”) (U.N. I.C.J.: International Court of Justice, The Hague, filed, May 17 1989) {70kb.pdf, source, 437kb.pdf, source}, discontinued on settlement, February 22 1996) {115.1kb.pdf, source, 248.7kb.pdf, source}.
_______________
Chart, widths: 620px, 780px, 1000px, 1263px, 1580px}
0610 USS Vincennes in position 26 26 N, 056 02 E.
USS Montgomery approximately 5 NM to the north-west {315°}.
USS Sides approximately 18 NM to the north-east.
0615 USS Vincennes’ helicopter in a position 8 to 10 NM north {0°/360°} of USS Montgomery is fired upon by small boats.
* * *
0654:22 USS Vincennes, first missile launch followed by the second missile. ...
IR655 approximate position 26 40 06 N, 056 02 41 E.
USS Vincennes is at position 26 30 47 N, 056 00 57 E, track 058 degrees, speed 22 kt.
USS Montgomery approximate position 26 31 N, 055 55 12 E, track 132 degrees, speed 17 kt.
* * *
2.11.7 Positions of USS Vincennes and IR655. The position of USS Vincennes at the time of missile launch based on the AEGIS-system data was given as 26 30 47 N, 056 00 57 E and that of flight IR655 as 26 40 06 N, 056 02 41 E.
ICAO Report, pp. A-1, A-11, 19 (Nov. 7 1988)
l. (U) At 0613Z USS Vincennes sounded General Quarters and proceeded north at high speed in the general direction of where Ocean Lord 25 had been fired upon by the small boats. (IO Exhibits 157, 172).
m. (S U) Before returning to USS Vincennes at high speed, Ocean Lord 25 was able to identify the group of small boats that fired at it and, via the LAMPS MK-III data link, identify the group to USS Vincennes. ( (b)(6), (b)(7)(C) p.798, (b)(6), (b)(7)(C) p.476).
n. (U) At approximately 0618Z, USS Vincennes observed two groups of small boats 7 to 8 miles away. (IO Exhibit 172, (b)(6), (b)(7)(C) p.792).
o. (U) The two groups of small boats then closed to approximately 4 miles off USS Vincennes’s starboard bow. ( (b)(6), (b)(7)(C) p.792). {p.38-1993}
p. (S U) At 0620Z USS Vincennes was directed by “GS” to take tactical control of USS Montgomery. USS Vincennes assumed tactical control and positioned Montgomery 8,000 yards off her port quarter. (IO Exhibits 130, 172).
q. (S U) At 0639Z USS Vincennes requested permission by “GS” and “GB” to engage the small boats (TN 4667) with 5″/54 guns {127mm, range 13 n.miles, 22 kb jpg}. (IO Exhibits 130, 172).
r. (S U) At 0639Z “GB” requested USS Vincennes to verify the small boats were not departing. USS Vincennes reported the boats were closing the USS Vincennes and the USS Montgomery. (IO Exhibits 130, (b)(6), (b)(7)(C) p.794, (b)(6), (b)(7)(C) p.47).
s. (S U) At 0641Z “GS” gave permission to engage the small boats with gunfire. (IO Exhibit 130).
Query: “At 0639Z ... reported the boats were closing”?
House Hearing, p.18 (July 21 1992).
t. (U) At 0643Z USS Vincennes and USS Montgomery opened fire on two closing groups of Iranian small boats, including the group of small boats which had fired on Ocean Lord 25. (IO Exhibits 172, (b)(6), (b)(7)(C) p.48).
u. (U) CO Montgomery reported that two small boats maneuvered erratically and appeared to close USS Montgomery and USS Vincennes. CO USS Montgomery also stated his lookouts reported small arms fire coming from the small boats. ( (b)(6), (b)(7)(C) p.47 and p.50).
v. (U) Crew members topside on USS Vincennes reported small arms fire from the boats, and Repair Locker 2 personnel in USS {p.26-1988} Vincennes reported hearing what might have been small arms rounds impacting the starboard bow area. (IO Exhibits 224, 225, Rogers p.837).
w. (U) CO USS Vincennes stated that the post-action analysis indicated that shrapnel, and/or spent bullets, impacted the starboard bow of the ship and the ablative coating behind the forward missile launcher. (Rogers p.838).
Query: “Shrapnel, and/or spent bullets”?
Hummm ...
Now what might that be?
At 1,000 yards, a NATO 7.62mm round is dropping 8 inches per 10 yards. And that drop accelerates, as its velocity decays.
But let’s imagine it maintains its velocity.
Over the second 1,000 yards it would drop 67 feet.
What does this trajectory bring to mind?
Splash!
Springs to my mind.
Well, how about a .50 caliber machine gun?
The maximum effective range of a U.S. M2 .50 Caliber (12.7mm) Browning Machine Gun is 2,000 meters (2,166 yards). And, you only have a 50% chance, at 1,600 meters, of hitting something the size of a warship.
Its absolute maximum range is 6,800 meters (7,366 yards). With its barrel cocked-up 45-degrees, I suppose. But its tracer rounds burn out at 2,200 meters (2,383 yards). So it can’t be targeted beyond that. And especially, from a small boat, bouncing on the sea, at 45+ knots.
Now let’s see. How far away was the Vincennes?
They don’t say. In their report. But they said this to the Senate. –CJHjr:
Senate Hearing, pp.47-48 (Sept. 8 1988)
_______________
Must have been the Hand of God. –CJHjr
x. (U) At approximately 0646Z, USS Montgomery opened fire with her 5″/54 {127mm, range 13 n.miles, 22 kb jpg} at the two westernmost contacts of the group of four. This is the group USS Vincennes initially engaged. (IO Exhibit 172, (b)(6), (b)(7)(C) p.48).
Query: “The group USS Vincennes initially engaged”?
So this group of small boats, deep inside their own nation’s territorial waters, fleeing for their lives, from the Vincennes, attacking them in “self defense,” then find themselves fleeing into a trap? Set by Rogers? Fleeing into the sights of the Montgomery? Waiting to attack them? 6 miles deep into those same territorial waters. In its “self defense”? –CJHjr
y. (CU) At 0649Z one group of small boats (TN 4456), 027 degrees true from USS Vincennes, was reported inbound and was taken under fire by USS Vincennes’s MT52. (IO Exhibit 172).
z. (S U) At 0650Z USS Vincennes suffered a gun casualty to MT51 resulting in a foul bore (chambered round in the gun that could not be fired). (IO Exhibit 172, (b)(6), (b)(7)(C) p.796). {p.39-1993}
aa. (S U) At 0651Z, “GS”, in a transmission to both USS Vincennes and USS Sides, ordered USS Vincennes to take tactical control of USS Sides. (IO Exhibit 130).
bb. (U) The foul bore in MT51 caused the TAO to maneuver the ship radically, using 30 degrees rudder at 30 KTS ship’s speed, in order to keep MT52 pointed at the most threatening of the surface contacts. (IO Exhibit 157, (b)(6), (b)(7)(C) p.796).
cc. (S U) The high speed, large rudder angle turn caused books, publications, and loose equipment to fall from desks and consoles in CIC. (IO Exhibit 157, (b)(6), (b)(7)(C) p.796).
dd. (S U) At 0703Z USS Vincennes ceased firing on the small boats. A total of 72 rounds of 5″/54 ammunition was expended (HE CVT-51 RDS, VT-FRAG-16 RDS, WHITE PHOS-3 RDS, VT-NONFRAG-2 RDS). (IO Exhibit 172).
ee. (S U) At 0706Z USS Montgomery reported confirmed kill on TN 4456. USS Montgomery expended a total of 47 RDS of 5″/54 ammunition. (IO Exhibits 172).
gg. (U) Captain Rogers considered applicable ROE before requesting permission to engage the small boats. Those criteria included:
(1) (S U) The small boats had already committed a hostile act against his unit by firing on Ocean Lord 25. (Rogers p. 837)
(2) (S U) He had positive identification of the small boats as those that had committed the hostile act against Ocean Lord 25. (Rogers p. 837)
(3) (S U) He was initially prepared to disengage from the {p.27-1988} small boats when they appeared to present no further threat to his units. (Rogers pp. 836-837)
(4) (S U) His decision to disengage was changed only when the small boats began to close his units. (Rogers p. 837)
(5) (S U) The small boats have greater speed and maneuverability than the USS Vincennes. (Rogers p. 842)
Query: “Greater speed”?
Probably not.
By convention, the speed of the Vincennes, and other U.S. Navy warships, is stated to be “more than 30 knots”.
But this convention is adopted precisely to conceal their true speed, which is a secret.
The Vincennes is powered by 4 jet engines (General Electric gas turbines), the same ones used to power airliners, on two drive shafts (8,000 SHP: shaft horsepower), with two (presumably) computer-designed low drag propellers (anti-cavitating). And it has a narrow hull design (ie: low drag).
In an inteview at the time, Anders Boghammer, an expert in ship design, was adamant the Vincennes was likely faster than his Boghammer small boats, the ones Iran then had, or at least as fast.
When they were loaded down with weapons, fuel, ammunition, and people.
And with their engines not tuned to their peak performance.
As they were, when he conducted a speed trial on the boats, before he delivered them to Iran.
He told me, in 1988 when I interviewed him, the 50 boats he and his brother Lars supplied to the Iranians (model RL-120-2A) had twin Volvo-Penta 70-D diesel 300 SHP engines (shaft horsepower).
In trials, he said, when new, they achieved 45 knots at 100% engine power with a 60% fuel load (600 liters of the 1,000 maximum) and 4 occupants in still air and deep water. From the photographs he saw at the Swedish Ministry of Defense, he guessed they could do 40 knots, configured with the added weight and drag of rocket-launchers mounted over the forward deck, depending on the weight of the rockets and other ammunition and their fuel load. Fully-fueled with 1,000 liters of diesel, he says their range was about 500 nautical miles. They each had a radar and VHF transceiver and cost about $240,000, in 1988 U.S. dollars.
He was confident the Vincennes could do 45 knots or better, based on its dimensions and specifications (from Jane’s Fighting Ships), and allowing for drag from the super-structure, the generators, and other loads.
He explained that “speed” is specified as the speed in still air, with a normal load, and the engines turning at their maximum recommended sustainable revolutions-per-minute (RPMs), typically 80% of maximum RPMs.
But there are higher speeds.
Engine makers, he said, specify both the recommended and the actual maximum RPMs and state how long the engines can be run, without damage, on “overload” (at various RPMs above the recommended maximum), and for how long at each setting. For example, they might specify 88% of maximum for 1 hour every 12 hours, or maybe 30 minutes every 6 hours, and maybe 96% of maximum for 30 minutes every 12 hours.
And speed is affected by loads. For example: generators, bilge-pumps, and other such equipment can pull up to 5% or more of an engine’s power, he said.
During a high-speed chase, a ship seeking full power can disconnect its generators — and increase its RPMs to reload the engines (compensate for the decreased generator load) — and switch to batteries, causing the lights to flicker, when switching over and back again, when later reconnecting the generator.
A tail-wind decreases load, enabling a higher engine RPM, and higher horsepower, without increasing engine load. The Vincennes had a 10-knot tail-wind, when pursuing the small boats in Iran’s territorial waters, until its sharp right turn, at full-rudder.
______________________
The Vincennes was engaged in offensive warfare when it pursued the fleeing boats into Iranian territorial waters.
This is not an act of self-defense.
Likewise, the Vincennes’s helicopter. Deep inside Iranian waters. Menacing the small boats. This too was an offensive threatening act. And a military invasion of their homeland. Against which the Iranians were entitled to defend themselves, by warning shots.
None of this entitled the Vincennes to offensively attack the small boats 30 minutes later.
Which had the legal right to exist.
And the legal right to enforce the integrity of their nation’s territorial boundaries. By firing warning shots at an armed, military, helicopter invading their homeland. And menacing them. And firing at armed, hostile, military, warships invading their homeland.
And the legal right to return fire at armed, hostile, military, warships invading their homeland and initiating fire upon them.
And the legal right — under the international law of blockade — to stop and search passing ships, for contraband, destined for their opponent in a war (Iraq).
And the legal right to attack those who refuse to stop, and submit to a search.
Interfering with their legal right to stop and search is an act of war.
The U.S. Congress has the exclusive legal authority, under the U.S. Constitution, to authorize offensive war. The President has no vote. And Congress did not authorize war against Iran.
The President and his henchmen, the U.S. Military, are prohibited by the U.S. Constitution to usurp the authority of Congress. And any actions they take purporting to do so are unlawful.
Absent a lawful war, offensive acts of war are prima facie criminal, under the laws of peace. Such as attacking Iran’s small boats. These attacks are prima facie attempted murder and arson if they are unsuccessful. And prima facie murder and arson if they succeed.
If the Vincennes had not been engaging in this unlawful activity, it would never have been in the middle of an airway in the first place.
Commanded by a commander, with a guilty conscience. Who knew — or should have known — he was committing a violent crime. And expecting a counter attack. Or at least on guard for one. And in a mind set to convince himself, that any approaching aircraft was military.
And who knew — or should have known — that any airliner he might ambush in the process, of his prima facie criminal attack on the small boats, would be prima facie murder.
Not least, because any military aircraft which might come to attack him would be legally entitled to do so.
A hoodlum — in the act of attempted arson-murder — can not claim self-defense, for killing a pursuing law enforcement officer.
–CJHjr
(6) (S U) The small boats carry weapons capable of inflicting significant personnel and equipment casualties. (Rogers p.838) {p.40-1993}
(7) (S U) Experience with small boat tactics shows that the greatest threat they present is personnel and equipment casualties when they make high speed massed attacks on their targets, raking the superstructures of ships with gunfire and rockets. (Rogers p.841)
(8) (S U) The small boats did not turn away after the USS Vincennes fired its first round, but continued to close. (Rogers p.837).
hh. (S U) CJTFME considered the following ROE cumulative indicators in granting permission to engage the small boats:
(1) (S U) Positive identification of the boats as those having committed a hostile act against a U.S. ship.
(2) (S U) The small boats were not leaving the area.
(3) (S U) The small boats were closing the USS Vincennes and USS Montgomery. ( (b)(6), (b)(7)(C) p.856, (b)(6), (b)(7)(C) p.425)
ii. (S U) USS Montgomery and USS Vincennes disengaged from the small boats when they ceased presenting a threat to U.S. ships. ( (b)(6), (b)(7)(C) p.51, (b)(6), (b)(7)(C) p.518, Rogers p.839)
C. Air Engagement
1. Data Extraction Background
a. (U) USS Vincennes’s magnetic tapes containing data extracted from her SPY-1A, Command and Decision, and Weapons Control System computers, were transferred by courier from USS Vincennes to Naval Surface Warfare Center, Dahlgren (NSWC) on 5 July 1988. ( (b)(6), (b)(7)(C) , p. 280)
b. (U) NSWC Dahlgren signed a receipt for the tapes on 6 July 1988. ( (b)(6), (b)(7)(C) , p.281)
c. (U) NSWC Dahlgren copied the tapes and performed data reduction on the USS Vincennes’s tapes IAW standard procedures.
d. (U) The results of that data reduction are included as IO Exhibits 81-105. ( (b)(6), (b)(7)(C) , pp.279-371) {p.28-1988}
e. (U) Preliminary data extraction results were provided by CO NAVSWC Dahlgren messages 080516Z Jul 88 and 090708Z Jul 88. The former message stated: “Data received and successfully duplicated with the exception of less than 1% of one non-critical WCS tape. Initial basic analysis runs complete and checked. This report based on excellent SPY-1A data and correlations between SPY-1A, C&D, and WCS.” (IO Exhibit 91). {p.41-1993}
f. (U) (b)(6), (b)(7)(C) ({Head,} AEGIS Program Office, NSWC) stated that the quality of data received was “as good as any data they (his analysts) have ever worked with.” ( (b)(6), (b)(7)(C) , p.284).
g. (U) The data examined by NSWC Dahlgren indicated the following regarding the track of interest (TN 4131):
(1) (S U) Altitude as seen by SPY-1 increased steadily, after leaving low elevation, to a maximum of 13,500 feet at intercept. (IO Exhibit 91).
(2) (S U) Altitude readings received from TN 4131’s Mode III-C IFF transmission increased steadily from take-off at Bandar Abbas to a maximum of 12,900 feet 3 seconds before intercept. (IO Exhibit 91).
(3) (S U) The only IFF Modes received from TN 4131 as a result of interrogations by the system was Mode III-6760. (IO Exhibit 91).
h. (U) AEGIS Display System (ADS) data cannot be extracted. Therefore, console actions at the CO, “GW”, and TAO positions cannot be determined. (IO Exhibit 91).
i. (S U) No data tapes were available from other units, but the Mode III IFF of 6760 and increasing altitude seen in the data tapes from USS Vincennes were corroborated by testimony and statements from USS Sides. (IO Exhibits 65-73).
j. (a) Information obtained from intelligence sources further corroborated that TN 4131 was squawking Mode III-6760. (IO Exhibit 6).
2. Time Line
a. (U) The time line below is a summary of all the events dealing with the air engagement which occurred between 0647Z and 0654Z on 3 July 1988. From detection to intercept this was a time window of 7 minutes and 8 seconds. The time line is a reconstruction based on data extraction from USS Vincennes’s tapes, as well as statements, testimony, and log entries from USS Vincennes, USS Sides, and USS Elmer Montgomery. The events derived from data tape extraction are underlined. The events are in chronological order, but some event times had to be estimated and may not be in precise time sequence.
c. (U) Unless otherwise noted, names and associated console {p.29-1988} positions refer to USS Vincennes’s CIC operator positions. (See Figure 1. Figure 1 is duplication of IO Exhibit 174 and is inserted here for ease of review.) {p.43-1993} {p.29a-1988}
{Figure-1: Plan of Vincennes Combat Information Center: Widths: 640px, 800px, 1024px, 1280px} {p.44-1993}
d. (U) When the term “in close control” or “hooked” is used with a TN it means that the operator referred to has the following displayed on the Character Read Out (CRO) display located on his console: TN, ID, grid coordinates, course, speed, altitude, ID amplifying information, Mode I/II/III IFF received, tracking quality, bearing and range.
(1) 0647Z
(a) (S U) (b)(6), (b)(7)(C) (EWS), (b)(6), (b)(7)(C) (IDS), and (b)(6), (b)(7)(C) (AIC-3 ) had an Iranian P-3 in close control. The P-3 was 62 miles west of Vincennes, heading 085. ¶
(b) (S U) The E-2C (AE-602) launched in an alert status from USS Forrestal (CV 59), and proceeded to its assigned “Earnest Will” {1069kb.pdf} station. (IO Exhibit 250).
(c) (S U) The SPY-1 radar initially reported the track of interest at a range of 47NM, bearing 025, ¶
Initial course was 210. Mode III was 6760. (IO Exhibits 91 & 232).
(d) (S U) The radar operators in USS Vincennes cannot discriminate size of a contact regardless of aspect angle. (IO Exhibit 183) ( (b)(6), (b)(7)(C) , p.544).
(e) (S U) (b)(6), (b)(7)(C) (RSC) determined from the A-scope that TN 4131 was a single track. ( (b)(6), (b)(7)(C) , p.544).
(f) (S U) (b)(6), (b)(7)(C) (49 ADT) first took close control of the southbound track out of Bandar Abbas and made an identification as “Unknown–Assumed Enemy” as it went “feet wet” in accordance ¶
(g) (S U) (b)(6), (b)(7)(C) (Air Detector Tracker and Track Supervisor-Sides) recalled picking up the track on a course of 200, speed 300kts, with a Mode III–6700 block. (IO Exhibit 71). {p.45-1993}
(h) (S U) (b)(6), (b)(7)(C) (IDS) picked up Mode III-6675 as the aircraft departed Bandar Abbas. System data continued to show a Mode III of 6760. (IO Exhibits 91 & 190).
(i) (S U) (b)(6), (b)(7)(C) (AIC-3) also recalled seeing Mode III-6675 on his CRO. (IO Exhibit 196).
(j) (S U) (b)(6), (b)(7)(C) (UBS) saw Mode III-66?? and later saw an unspecified Mode II. ( (b)(6), (b)(7)(C) , p.755).
(l) (S U) (b)(6), (b)(7)(C) (TIC) recalled hearing “possible F-4” launch from Bandar Abbas ¶
(m) (S U) (b)(6), (b)(7)(C) (IAD) believed he heard a report of F-14’s from SSES. (IO Exhibit 189).
(n) (U) (b)(6), (b)(7)(C) (“GW”) believed he heard “F-14” reported from SSES. ( (b)(6), (b)(7)(C) , p.812).
(o) (S U) Track of interest is reported by USS Vincennes over Link 11 as TN 4474. (IO Exhibit 91).
(p) (S U) (b)(6), (b)(7)(C) (CSC), (b)(6), (b)(7)(C) (UBS), (b)(6), (b)(7)(C) (IDS), (b)(6), (b)(7)(C) (TIC), (b)(6), (b)(7)(C) (FC-1), (b)(6), (b)(7)(C) (AAWC), and (b)(6), (b)(7)(C) (EWS) all have track of interest (TN 4474) in close control. (IO Exhibit 91).
(q) (S U) (b)(6), (b)(7)(C) (49 ADT) stated TN 4474 was squawking Modes II and III. ( (b)(6), (b)(7)(C) , p.588).
Query: “49 ADT”? “Mode II”? “0647”?
The 49 ADT — the operator of the warship’s rotating air search radar (AN/SPS-49(V)) — said he saw a mode II:–
“Only one time”.
“At 20 miles”.
At 0652 Zulu.
Five minutes later, from this timeline time.
Here, we’re at 45 n.miles, on the timeline. At 0647 Zulu.
This statement is misplaced on the timeline.
Nobody is making any claims, at this early time, of seeing anything other than reality. That the aircraft was squawking civilian, with its transponder.
Is this an honest mistake, Mr. Fogarty?
Or is this a willful, purposeful, malicious lie?
Preparing us? To excuse Scott Lustig’s F-14 lie?
–CJHjr
(2) 0648Z
(a) (S U) (b)(6), (b)(7)(C) (TIC) recalled noting Mode III in his CRO for TN 4131. ( (b)(6), (b)(7)(C) , p.676).
(b) (U) Commercial air schedules were available in CIC and reviewed by decision-making personnel (CO, TAO, “GW”, TIC, IDS) on a regular basis prior to the engagement. The IDS specifically looked at the schedule at his console when TN 4131 first appeared. (IO Exhibits 190 & 195, Rogers, p.839, (b)(6), (b)(7)(C) , p.621). {p.46-1993}
(c) (S U) (b)(6), (b)(7)(C) (FC-1), (b)(6), (b)(7)(C) (49 ADT), and (b)(6), (b)(7)(C) (AAWC) took a non-squawking P-3 (track 4472) to the west (RNG 64, BRG 266, CSE 085) in close control for several seconds and returned to the track of interest (TN 4474). (IO Exhibit 91).
(d) (S U) (b)(6), (b)(7)(C) (TIC) recalled seeing Mode I and Mode III on the P-3 (TN 4472). ( (b)(6), (b)(7)(C) , p.646).
(e) (S U) The P-3 (TN 4472) was challenged over both MAD and IAD. The P-3 responded that he was on a search mission and that he would stay away from USS Vincennes. The form of the challenge was:
“Iranian P-3 on course 085 speed 270 this is USN warship BRG 085 64 miles, request you state your intentions.”
(IO Exhibit 203).
(f) (S U) The track of interest (TN 4474) was at a range of 44 NM, BRG 025, CSE 202, SPD 232, and at an altitude of 2500 ft. The altitude source to consoles continued to be Mode C IFF from the aircraft which was still ascending. (IO Exhibit 91).
(g) (U) (b)(6), (b)(7)(C) (SSES) took TN 4131 in close control. (IO Exhibit 91). {p.31-1988}
(i) (S U) USS Elmer Montgomery never gained radar contact on TN 4131. ( (b)(6), (b)(7)(C) , p.88), (IO Exhibit 33).
Senate Hearing, pp.48-49 (Sept. 8 1988)
(j) (S U) (b)(6), (b)(7)(C) (TIC) recalled that the track number changed to TN 4131 occurred somewhere beyond 30 NM. ( (b)(6), (b)(7)(C) , p.675).
(k) (S U) (b)(6), (b)(7)(C) (TAO-Sides) observed TN 4131 leaving Bandar Abbas and although it was crossing with respect to USS Sides, he directed his Weapons Control Officer to lock-on with FC-2. The aircraft was heading southwesterly at approximately 400kts at an altitude of about 10,000 ft. (IO Exhibit 59, (b)(6), (b)(7)(C) , pp.247, 248).
(l) (S U) (b)(6), (b)(7)(C) (WCO-Sides) confirmed receiving the order and recalled that FC-2 acquired the target 50-60 kyds from USS Sides. He thought he noticed an IFF of 6710 but didn’t see an altitude. (IO Exhibit 69, (b)(6), (b)(7)(C) , p.269). {p.47-1993}
(m) (S U) (b)(6), (b)(7)(C) (WCC2-Sides) generally confirmed the range report and recalled an altitude of 3500 ft with speed 480 kts. (IO Exhibit 57).
Query: A “Weapons on Target” message?
Why did senior U.S. military officers decide to conceal this, from the 1988 version of their report?
And why did the DoD report writers decide to conceal what this means? From both the public and the classified versions of their report? The nature of this “message”?
Could this be the reason?:
The truth would expose, highlight, and emphasize the reckless negligence of the Vincennes officers and crew.
It was not until 5 years later, that we learned the Sides sent any “message” to the Vincennes (here, in this partially declassified version of the DoD report). And it was not until 12 years later that we learned the nature of this “message.” And what it means.
It was automatic computer-talk:
______________________
Reuben S. Pitts III (“Head of the Data Analysis Team that supported Admiral Fogarty’s formal investigation”), “Human-Centric Warfare,” in “Anonymous” (Comment and Discussion), Proceedings of the United States Naval Institute, volume 126, Issue 3, March 2000, pages 10 et seq. (U.S. Naval Institute, Annapolis Maryland) {ISSN: 0041-798X, OCLC: 02496995, LCCN: 64054905, WorldCat}.
“Voice recordings”?
The 5 erased tracks?
______________________
This fact, concealed from the DoD report, highlights three items of negligence, each a separate prima facie proximate cause of the ambush:
First, Scott Lustig negligently failed to report the Sides lock-on to Anthony Less at Bahrain (0650-0651 Zulu). When seeking permission to attack the aircraft. A material fact in evaluating whether the target was hostile.
Second, the Vincennes officers and crew negligently failed to evaluate the significance of what was staring each of them in the face, on their computer screens: The aircraft did not react to being locked-on by the Sides. A factor their Rules of Engagement explicitly required them to evaluate. No reaction suggests a civilian aircraft because, with no RHWR receiver, it does not know it has been locked-on:
DoD Report, ¶ 19, p.25 (1988: p.16) (above).
Third, concealing the truth, also conceals why the Vincennes crew did not do their duty. Namely, the Commander of the Vincennes violated his duty, and Naval Regulations, and falsely certified an untrained officer as qualified for a duty he was not qualified for. The Vincennes crew were distracted, for several minutes, by this officer’s inability to lock-on with the Vincennes fire control radar — 30 failures to push the correct buttons (all of them concealed from the 1988 public version of the DoD report).
–CJHjr
(3) 0649Z
(a) (S U) USS Vincennes’s Link 11 was off for 28 seconds. (IO Exhibit 91).
Query: “Link 11 was off for 28 seconds”?
Now why might that be?
Could this be a clue?:
Frank C. Carlucci (U.S. Secretary of Defense), Press Briefing, August 19 1988, p.2.
ICAO Report, ¶ 1.16.1.3, p.8.
The warship’s satellite antenna is not likely mounted on a gimbal. To avoid movement by the wind. It’s surely stabilized by gyroscopes.
It stays pointed at the satellite, automatically, as the warship turns.
But not when it heels over:
Electronics Technician, Volume 07— Antennas and Wave Propagation, Chapter 2: Antennas, Satellite Systems, Antenna Groups OE-82B/WSC-1(V) and OE-82C/WSC-1(V), page 2-16 {968kb.pdf}.
Presumably, at the warship’s 32-degree list, the satellite antenna lost its lock on the satellite, and had to regain the satellite after the list abated. And, perhaps the operator had to log-on again, to the Link-11 net. Though log-on is likely automatic, in the warship’s computer software.
And all that took 28 seconds.
The report asserts this turn occurred at 0651 Zulu. Not at 0649 Zulu, here, when it asserts Link-11 disconnected. The report asserts that the foul bore, the asserted reason for the turn, occurred at 0650 Zulu
This could be faulty logging in the Vincennes deck log, which the report writers cite as authority for the time of the turn. And faulty recollection by the redacted individual they cite as additional authority.
But, the time of this turn is shown precisely on the authoritative, secret, time-stamped, Vincennes position log, automatically recorded from the warship’s inertial navigation system.
Which the report writers could have cited.
And didn’t.
DoD Report, ¶ 2, p.41 (1988: p.28).
Senate Hearing, p.47 (Sept. 8 1988)
Perhaps they wanted to obfuscate why Link-11 disconnected.
Perhaps they wanted to create the false illusion that “This turn took place just at the crucial decision point,” a distraction, near to the decision to launch the missiles (0654:05 Zulu).
Instead of when it likely occurred (0649 Zulu).
Or both. –CJHjr
(b) (S U) (b)(6), (b)(7)(C) (AAWC) ordered TN 4131 to be challenged over the MAD and IAD nets. (IO Exhibit 204).
(c) (S U) A MAD warning was issued by USS Vincennes to TN 4131
{06:49:39–0650:06 Zulu}: “Unidentified Iranian aircraft on course 203, speed 303, altitude 4000, this is U.S. Naval warship, bearing 205, 40 miles from you. You are approaching U.S. Naval warship operating in international waters. Request you state your intentions.”
(IO Exhibit 203) {times, from ICAO Report, p.15 ¶ 2.10.2, pp.B-17, B-24 (Nov. 7 1988). –CJHjr}.
Query: “MAD”?
No airliner is equipped with a UHF transceiver (military frequencies). Hence, no airliner can receive a MAD broadcast. Military Air Distress is a military frequency: 243.0 mHz. –CJHjr
(d) (S U) (b)(6), (b)(7)(C) (49 ADT) later recalled that his speed challenges on the MAD net were much slower (about 100kts) than those given on the IAD net. ( (b)(6), (b)(7)(C) , p.602).
(4) 0650Z
(a) (S U) The following warning was issued to TN 4131 over IAD by USS Vincennes:
{0650:02–0650:22 Zulu}: “Unknown aircraft on course 206, speed 316 position 2702N/05616E you are approaching US Naval warship request you remain clear.”
USS Vincennes’s system data indicated the same parameters. (IO Exhibits 91 & 203). {Time, from ICAO Report, p.16 ¶ 2.10.8, p.B-16 (Nov. 7 1988). –CJHjr}. {p.32-1988}
Richard S. Williamson (Assistant Secretary of State, International Organization Affairs, 1988-1989, a lawyer), statement, ICAO meeting, Montreal Canada, July 13 1988 (ICAO: U.N. International Civil Aviation Organization), printed, “Assistant Secretary Williamson, ICAO Council, Montreal, July 13, 1988,” in “Middle East, Iranian Airbus Tragedy” (Department of State Bulletin, volume 88, number 2138, September 1988, pages 38-43, at 39-42) (“The official monthly record of United States foreign policy”) {3 issues, July.-Sept., 1.61mb.txt, 23.84mb.pdf, source} {SuDoc: S 1.3, LCCN: 39026945, ISSN: 0041-7610, OCLC: 1639364, GPOCat, WorldCat}, reported, Jeff Bradley, “Council Agrees on ICAO Probe, Four Favor Condemnation” (Associated Press, July 14 1988, 12:23 EDT, AP880714-0103), reprinted, in the House Report (yet to be posted).
______________________
Query: “Warning”?
The Vincennes IAD radio-talker did not ask the pilot to identify himself and state his intentions.
As his talking script required him to do.
As the U.S. NOTAM required him to do.
This is not a “warning”:
It contains no threat. Issues no instructions. Requests no reply. And conceals the location of the warship (to “remain clear” of).
It’s a mere “hello” message, informing the pilot (if s/he’s listening) that the warship has radar contact.
This broadcast violated the written orders issued to the IAD radio-talker: His written talking script. Which required him to ask the pilot to identify himself and state his intentions.
This talking-script is a material fact omitted from the DoD Report, and hence a prima facie criminal lie.
This violation, by the IAD radio-talker, of his orders, is a prima facie proximate cause of the ambush.
An excellent criminal motive for senior U.S. military officers to conceal the radio-talker’s talking script from their deceitful report.
Query: “Issued to”?
This was a broadcast (allegedly).
Heard by whomever happened to hear it.
It was not “issued to” anybody.
But, it’s a simple matter to “issue to” a target aircraft, a broadcast.
And that’s by speaking the target’s transponder squawk code, a unique identifier, which the pilot knows. (And, of course, broadcasting on a frequency the pilot is certain to be listening to, his Air Traffic Control frequency).
Only if the radio-talker speaks the aircraft’s transponder squawk-code, can a pilot know for certain who the radio-talker is referring to. (If, of course, s/he happens to be listening to the broadcast frequency).
The recklessly negligent failure of senior U.S. military officers to require their warship radio-talkers to speak the transponder squawk-code, when seeking to broadcast to a target aircraft, is a prima facie proximate cause of the ambush.
An excellent criminal motive for senior U.S. military officers to conceal, from their deceitful report, the text of the recklessly negligent talking script, which they issued to their warship radio-talkers.
–CJHjr
(b) (S U) (b)(6), (b)(7)(C) (IDS) reported seeing a Mode II-1100 and Mode III-6675 on his RCI about 3-4 minutes before engagement when TN 4131 was at 9000 ft and near the SE corner of Qeshm Island. He reported possible F-14 and Mode II-1100 over net 15/16 to “all stations.” USS Vincennes’s system {p.48-1993} data showed only Mode III-6760 at this time. (IO Exhibit 91, (b)(6), (b)(7)(C) , p.626).
Query: “9000 feet”?
Whoops!
We’re at 4000-4500 feet, Mr. Fogarty.
This 9000-foot recollection doesn’t belong at this point. On the timeline. Where you decided to put it.
It belongs down below.
Two minutes later.
At 0652Z.
When IR655 was at 9000 feet.
Just where the IDS recollected it.
After the IDS’s boss — an authority figure — had publicly proclaimed, the target was an F-14.
Talking on the radio to Bahrain.
Are you trying to trick and deceive us, Mr. Fogarty?
Pretending, that the chicken was the egg?
Pretending, that Lustig and Rogers had some reason to suppose the target was an F-14?
Pretending that — when they decided to lie to Less — their lie was merely negligently reckless? Instead of willfully reckless?
Query: A “possible F-14”?
This was a negligent act. To report a “possible” F-14 without also reporting it was only squawking a civilian squawk-code, staring the IDS in the face from his computer console.
His negligent failure (if that’s what he did), to report the civilian squawk-code, was a prima-facie proximate cause of the ambush.
However, the IDS was not a reckless liar. Like Lustig and Rogers were. He did not pretend to know for certain it was an F-14. As they did. That’s what the word “possible” means: Uncertainty. That’s exactly what he was. And exactly what he said. (According to Fogarty).
This would have been a less faulty report, if he had also reported the civilian-only squawk code. Displayed on the computer console of everyone in the CIC to do with aerial threats.
But, the IDS had neglected to note the scheduled departure on his airline schedule, when he looked at it. Or, more likely, his senior officers had recklessly neglected to inform him about the time issues, so that he could understand what he was looking at.
Yet, the IDS was negligent in failing to inquire about these time issues. Because he had a job to do. And he knew, or should have known, that he couldn’t do his job without understanding time issues.
Combining the negligence of himself and his senior officers, the IDS was negligent in failing to stand watch for this airliner.
Which his airline schedule plainly informed him was due to take off 15 minutes before it actually did.
The IDS’s task was greatly encumbered, fatally so, by the reckless negligence of senior U.S. military officers to properly equip his warship with sufficient VHF transceivers, so that he could monitor Air Traffic Control frequencies. And listen to the conversations of the pilot.
A citizen of a country with which the United States was not at war.
And which had never attacked a U.S. warship. –CJHjr
(c) (S U) Not all RCI indications are displayed in an operator’s CRO because RCI data is not always correlated with a track in the system. IFF data in C&D is always correlated with a track number. (AF Exhibit Enclosure 17).
(d) (S U) Multiple CIC personnel recalled hearing F-14 report on internal net 15 or 16, or recall it being said aloud. ( (b)(6), (b)(7)(C) , p.812; (b)(6), (b)(7)(C) , p.677; (b)(6), (b)(7)(C) , p.537; (b)(6), (b)(7)(C) , p.637; (b)(6), (b)(7)(C) , p.560; (b)(6), (b)(7)(C) , p.543; (b)(6), (b)(7)(C) , p.570; (b)(6), (b)(7)(C) p.593; (b)(6), (b)(7)(C) , p.650).
Query: “Recalled hearing F-14 report”? “Said aloud”?
Well that’s hardly surprising.
That crew members would repeat what they heard their boss say aloud.
After Scott Lustig said it aloud.
Talking on the radio to Anthony Less, at Bahrain.
An authority figure.
Making an official report.
To another authority figure.
Looks like another misposition on the timeline.
Pretending this gaggle of witnesses recollected beforehand what, instead, they heard Lustig say out loud.
Preparing us? To excuse Scott Lustig’s F-14 lie? –CJHjr
(e) (S U) (b)(6), (b)(7)(C) (CSC) never saw Mode II, but (b)(6), (b)(7)(C) (AIC) saw Mode II-1100 and Mode III-6675 on his CRO. (b)(6), (b)(7)(C) (AAWC) also saw Mode II-1100. USS Vincennes’s system still held no IFF Mode II and held Mode III-6760 for TN 4131. ( (b)(6), (b)(7)(C) , p.537; (b)(6), (b)(7)(C) , p.706; (b)(6), (b)(7)(C) , p.727) (IO Exhibit 91).
(f) (S U) (b)(6), (b)(7)(C) (TIC) reported rechallenging TN 4131 after Mode II report but only got a Mode III ( (b)(6), (b)(7)(C) , p.678).
(g) (S U) (b)(6), (b)(7)(C) (WCC2-Sides) noted TN 4131 climb to 5000 ft. (IO Exhibit 57, (b)(6), (b)(7)(C) , p.236).
(i) (S U) TN 4131 was at range of 34 NM, BRG 025, ALT 6160, and a SPD 334. (IO Exhibit 91).
(j) (S U) (b)(6), (b)(7)(C) (“GW”) reported an inbound Iranian F-14 to “GB” on MEF Execution net (BRG 025/RNG 32NM). He also reported on the net that he had warned TN 4131 and that the challenge was ignored. (IO Exhibit 203).
Query: “F-14”?
This is a reckless lie.
Scott Lustig (the radio-talker) and William Rogers (the warship commander), seated next to Lustig, both knew for a fact, they had no idea what aircraft was approaching, and that no crew member could possibly know what it was.
Yet, they lied to Less (their commander, at Bahrain) it was an F-14.
Rogers acknowledged, in his testimony, to the DoD investigators, that he didn’t know what it was. And the DoD investigators concealed from their report what he said:
Senate Hearing, p.20 (Sept. 8 1988)
This lie, by Rogers and Lustig to Less, was a prima facie proximate cause of the ambush.
Query: “Warned”?
The IAD broadcast was not a “warning”: It contained no threat. Issued no instructions. Requested no reply. Contrary to what Rogers and Lustig assured Less.
And this, Lustig should have known, because he was seated right next to the IAD radio-talker. Between the IAD and Rogers.
This erroneous assertion by Rogers and Lustig, misinforming Less, that they had issued a “warning,” was a prima facie proximate cause of the ambush.
Query: “Ignored”?
The IAD broadcast did not ask the pilot to identify himself and state his intentions (as his talking script, and a U.S. NOTAM, required him to do). Or, to alter his course. Or, to reply.
Hence, the pilot did not “ignore” the broadcast. Contrary to what Rogers and Lustig assured Less.
And this, Lustig should have known, because he was seated right next to the IAD radio-talker.
This erroneous assertion by Rogers and Lustig, misinforming Less, that the pilot had “ignored” a “warning,” was a prima facie proximate cause of the ambush.
Query: “Inbound”?
Rogers and Lustig concealed from Less, that the warship was in the center of an airway, and inside Iran’s territorial waters.
This location of the warship was an innocent explanation for why an aircraft from Iran might be “inbound” to the warship.
This omission, by Rogers and Lustig, concealing from Less material information, bearing on the threat assessment, and the proper application of the Rules of Engagement, was a prima facie proximate cause of the ambush.
Query: Illumination?
Rogers and Lustig concealed from Less, that the target had been illuminated with a fire-control radar and did not react.
This is diagnostic of a civilian aircraft.
A military aircraft has a “radar homing and warning” receiver (RHAW) which sounds a loud alarm when it receives such radar broadcasts. A military pilot, on such an occasion, will normally jenk course, to placate the radar operator, by thereby demonstrating the pilot does not intend to attack.
Civilian aircraft, including airliners, do not have such equipment and are therefore oblivious, when they are illuminated by a fire-control radar. Hence, they do not react to such illumination.
And IR655 did not react. When illuminated by the USS Sides fire-control radar, 1-minute after take-off. The USS Sides reported this illumination, to the USS Vincennes, over their Link-11.
But the USS Vincennes crew negligently paid no mind to this important information. Which their Rules of Engagement required them to pay mind to.
And, Rogers and Lustig concealed from Less, that they had not complied with their Rules of Engagement, which required them to illuminate the target, with their own fire-control radar. A necessary step in the process of identifying aerial targets.
This omission, by Rogers and Lustig, concealing from Less material information, bearing on the threat assessment, and the proper application of the Rules of Engagement, was a prima facie proximate cause of the ambush.
Query: Altitude?
Rogers and Lustig concealed from Less, the aircraft’s altitude. They informed Less only of its range and bearing. This, even though that altitude was staring each of them in their face — on their computer consoles (CRO), directly in front of each of them.
The high altitude of the target was a non-threatening indicator.
The DoD Report writers also concealed the altitude at the time of this radio message (at range 32 NM). At range 34 NM it was at 6160 feet. At range 29 NM it was at 7000 feet.
Extrapolating, IR655 was at 6500 feet at the time of this message to Less.
This omission, by Rogers and Lustig, concealing from Less material information, bearing on the threat assessment, and the proper application of the Rules of Engagement, was a prima facie proximate cause of the ambush.
Query: Flight profile?
Rogers and Lustig concealed from Less, that the aircraft had an innocent, non-threatening flight profile: Climbing, steeply and steadily, from take-off. At 1500 feet per minute.
This omission, by Rogers and Lustig, concealing from Less material information, bearing on the threat assessment, and the proper application of the Rules of Engagement, was a prima facie proximate cause of the ambush.
Query: Airline schedule?
Rogers and Lustig concealed from Less, that an airliner, scheduled to take off about 15 minutes earlier, had not previously taken off. An innocent explanation for the approaching, high, and climbing, target.
This omission, by Rogers and Lustig, concealing from Less material information, bearing on the threat assessment, and the proper application of the Rules of Engagement, was a prima facie proximate cause of the ambush.
Query: Squawk Code?
Rogers and Lustig concealed from Less, the aircraft’s civilian squawk code. This, even though that squawk code was staring each of them in their face — on their computer consoles (CRO), directly in front of each of them.
A civilian squawk code is a non-threatening indicator.
This omission, by Rogers and Lustig, concealing from Less material information, bearing on the threat assessment, and the proper application of the Rules of Engagement, was a prima facie proximate cause of the ambush.
–CJHjr
(k) (S U) (b)(6), (b)(7)(C) (“GW”) recalled making a MEF Execution net report when TN 4131 was at 32 NM and recalled an earlier altitude of 9800 ft when TN 4131 was between 38-40 NM. ( (b)(6), (b)(7)(C) , pp.813, 814).
(l) (S U) USS Vincennes ordered to take tactical control of USS Sides by “GS”. (IO Exhibit 203).
(n) (S U) (b)(6), (b)(7)(C) (OSDA) tagged TN 4131 as F-14 on the LSD. ( (b)(6), (b)(7)(C) , p.781). {p.49-1993} {p.33-1988}
(5) 0651Z
(a) (S U) “GW” identified TN 4131 as Iranian F-14 (BRG 024/RNG 28) over CMEF Execution net. Indicated intention to engage at 20 NM unless he turned away. Asked “GB” if he concurred. “GB” told USS Vincennes to warn aircraft first before firing. (IO Exhibit 203).
(b) (U) In the limited time available, CJTFME could not verify the information passed by USS Vincennes on TN 4131. ( (b)(6), (b)(7)(C) , p.859; (b)(6), (b)(7)(C) , p.446).
(c) (S U) (b)(6), (b)(7)(C) (TAO-Sides) recalled first being alerted to TN 4131 when USS Vincennes reported an F-14 over CMEF Execution Net. ( (b)(6), (b)(7)(C) , p.247).
(e) (S U) (b)(6), (b)(7)(C) (AAWC) recalled altitude at 8-9 kft at 30 NM and ordered continuous challenge until engagement. (IO Exhibit 204, (b)(6), (b)(7)(C) , p.730).
(f) (S U) The following MAD challenge was issued by USS Vincennes:
{0651:11–0651:33 Zulu}: “Iranian fighter on course 210, speed 353, altitude 7000 ft. you are approaching US Naval warship, operating in international waters. If you maintain current course you are standing into danger and are subject to USN defense measures. Request you change course 270 repeat 270.”
(b)(6), (b)(7)(C) (Sides) recalled hearing this report. USS Vincennes’s system data indicated the same course, speed, and altitude. (IO Exhibit 203 (b)(6), (b)(7)(C) , p.171) {times, from ICAO Report, p.15 ¶ 2.10.2, pp.B-18, B-24 (Nov. 7 1988). –CJHjr}.
(g) (S U) An IAD challenge was issued by USS Vincennes to TN 4131:
{0651:09–0651:43 Zulu}: “Unidentified aircraft on course 207, speed 350, altitude 7000. You are approaching US Naval warship bearing 205, 30 miles from you. Your identity is not known, your intentions are not clear. You are standing into danger and may be subject to USN defensive measures. Request you alter course immediately to 270.”
USS Vincennes’s system data indicated the same. (IO Exhibits 91 & 203). {Time, from ICAO Report, p.16 ¶ 2.10.8, p.B-16 (Nov. 7 1988). –CJHjr}.
Richard S. Williamson (Assistant Secretary of State, International Organization Affairs, 1988-1989, a lawyer), statement, ICAO meeting, Montreal Canada, July 13 1988 (ICAO: U.N. International Civil Aviation Organization) (AP880714-0103).
______________________
Query: “Challenge”?
The Vincennes IAD radio-talker did not ask the pilot to identify himself and state his intentions.
As the U.S. NOTAM required him to do.
This warning — the first of two by the Vincennes IAD radio-talker — was broadcast (0651:09–0651:43) while the IR 655 pilot was busy talking to Tehran Area Control Center (0650:54–0651:30):
| UTC | Talker | Transcript |
| Tehran Area Control Centre (THR ACC) 133.4 MHz | ||
| 0650:54 | IR 655 | ... (unreadable) ... |
| 0650:59 | THR ACC | Station calling Tehran |
| 0651:04 | IR 655 | IranAir 655 from Bandar Abbas to Dubai; out of level 70 {7,550 feet radar actual} for 140; estimating FIR 58, Dubai 0715 |
| 0651:20 | THR ACC | Roger; report maintaining 140 and passing DARAX |
| 0651:26 | IR 655 | Roger |
| 0651:28 | THR ACC | Confirm you are squawking 6760 |
| 0651:30 | IR 655 | Affirmative |
ICAO Report, p.B-16 and p.16 ¶ 2.10.8 (Nov. 7 1988)
______________________
This material fact senior U.S. military officers concealed from their DoD Report, concealed in their press conferences, and concealed in their sworn testimony to Congress. A prima facie criminal lie.
It’s a material fact, because it highlights the reckless negligence of senior U.S. military officers who failed in their duty to order their warship IAD radio-talkers to monitor and broadcast on relevant civilian ATC frequencies, and not on the IAD frequency, which no civilian aircraft is required to monitor, outside the U.S., unless they are over a vast ocean.
This reckless negligence, by senior U.S. military officers, is a prima facie proximate cause of the ambush.
An excellent criminal motive for senior U.S. military officers to unite, in a prima facie criminal conspiracy, to lie in an official U.S. Government report, and to lie to Congress, by concealing, from their deceitful report, the text and time-stamps, of the radio conversations by the IR 655 pilot and the time-stamps of the Vincennes IAD broadcast.
Query: “Unidentified aircraft”?
IR 655 was not an “unidentified aircraft”:
It was well identified, by its transponder (SSR) squawk code staring the Vincennes IAD radio-talker in the face from his computer console (CRO).
The recklessly negligent failure of senior U.S. military officers to require their warship radio-talkers to speak the transponder squawk-code, when seeking to broadcast to a target aircraft, is a prima facie proximate cause of the ambush.
An excellent criminal motive for senior U.S. military officers to unite, in a prima facie criminal conspiracy, to lie in an official U.S. Government report, and to lie to Congress, by concealing, from their deceitful report, the text of the recklessly negligent talking script, which they issued to their warship radio-talkers.
Query: “Your identity is not known”?
The Vincennes IAD radio-talker did not ask the pilot to identify himself and state his intentions. As a U.S. NOTAM required all U.S. radio-talkers to do.
This violation, by the Vincennes IAD radio-talker, of the U.S. NOTAM, is a prima facie proximate cause of the ambush.
An excellent criminal motive for senior U.S. military officers to unite, in a prima facie criminal conspiracy, to lie in an official U.S. Government report, and to lie to Congress, by concealing, from their deceitful report, the text of that U.S. NOTAM. And the text of the radio-talker’s talking script, which they negligently drafted and issued to him.
Query: “To 270”?
These words were not broadcast by the Vincennes radio-talker. They were broadcast by the Sides radio-talker, according to the later ICAO Report, p.16 ¶ 2.10.8 (Nov. 7 1988).
A material omission and a prima facie criminal lie. Because it concealed this:
The recklessly negligent failure of the Vincennes IAD radio-talker to give the pilot instructions — as his talking-script required him to do. This is a prima facie proximate cause of the ambush.
And this: The Sides was apparently broadcasting at the same time as the Vincennes, nullifying the “warning,” because nobody can understand people talking at the same time on a radio.
An excellent criminal motive for senior U.S. military officers to unite, in a prima facie criminal conspiracy, to lie in an official U.S. Government report, and to lie to Congress, that these words were spoken by the Vincennes radio-talker, when — in fact — the Vincennes radio-talker recklessly neglected to speak these words.
And an excellent criminal motive for senior U.S. military officers to unite, in a prima facie criminal conspiracy, to lie in an official U.S. Government report, and to lie to Congress, by concealing from their deceitful report, transcripts of actual VHF broadcasts, an unintelligible jumble. –CJHjr
(h) (S U) USS Vincennes’s systems held TN 4131 at an altitude of 7000 ft at 29 NM. (IO Exhibit 91).
(i) (S U) (b)(6), (b)(7)(C) (Sides) recalled challenging TN 4131 after “GS’s” report and reading an IFF altitude of 7,000 {p.50-1993} ft with a Mode III of 6707. He evaluated it as an Iranian HAJ flight. (IO Exhibit 55, (b)(6), (b)(7)(C) p.196).
(j) (S U) (b)(6), (b)(7)(C) (Sides) recalled the evaluation as a HAJ flight and that he and (b)(6), (b)(7)(C) had reported it to the TAO. (b)(6), (b)(7)(C) (TAO — Sides) does not recall hearing the report of HAJ flight. (IO Exhibits 54 & 59, (b)(6), (b)(7)(C) , p.251; (b)(6), (b)(7)(C) , p.177).
(l) (S U) (b)(6), (b)(7)(C) (OSDA) recalled TN 4131 being at an altitude of 8000 ft at SE corner of Qeshm Island and descending. ( (b)(6), (b)(7)(C) , p.210). {p.34-1988}
(m) (S U) (b)(6), (b)(7)(C) (AIC-3) recalled that on his 3rd look TN 4131 was just east of Qeshm Island at 9000 ft and 30 NM. ( (b)(6), (b)(7)(C) , pp.706 & 712).
(q) (S U) (b)(6), (b)(7)(C) observed TN 4131 slowly rising at around 8-9 kft. He jumped up and said “possible COMAIR” to the CO and (b)(6), (b)(7)(C) (“GW”). The CO acknowledged the report by raising his hand. ( (b)(6), (b)(7)(C) , p.571, Rogers p.849).
(r) (S U) Airway (A-59) was depicted on LSD #2 in front of “GW” as single line and was slightly west of the actual centerline of the 20 mi wide airway. (IO Exhibit 187).
Query: “Holding both tracks”?
How can an aircraft carrier, over the horizon, in the Northern Gulf of Oman, be “holding both tracks” on targets out of reach of its radar?
The report doesn’t give the position of the Forrestal. IR655 being at 9000 feet at this time, the Forrestal would have to be within 110 n.miles, to have line of sight on it, with its own radar.
But Link-11 is the likely answer instead. A radio broadcast encoding radar track data: coordinates, altitude, and such (I suppose), from which the computer can compute course and speed and range and bearing to the various warships on that Link-11 net.
The Vincennes and the Sides each broadcast Link-11 data and, apparently, via “link 11 OE-82 satellite communications antenna”. (ICAO Report ¶ 1.16.1.3, p.8, describing Vincennes equipment).
And that presumably is what the Forrestal received: radar track data, via Link-11, via satellite.
–CJHjr
(6) 0652Z
(a) (S U) A MAD warning was issued to TN 4131:
{0652:00–0652:21 Zulu}: “Iran aircraft fighter on CSE 211, SPD 360, ALT 9000. This is {p.51-1993} USN warship BRG 202 from you. Request you change course immediately to 270. If you maintain current course you are steering into danger and are subject to USN defensive measures.”
USS Vincennes’s system data indicated the same. (IO Exhibits 91 & 203) {times, from ICAO Report, p.15 ¶ 2.10.2, pp.B-18, B-24 (Nov. 7 1988). –CJHjr}.
(b) (S U) (b)(6), (b)(7)(C) (AAWC) recalled seeing TN 4131 with an altitude of approximately 9000 ft and a speed of 360-380 kts. So did the USS Vincennes’s system. (IO Exhibit 91, (b)(6), (b)(7)(C) , p.728).
(c) (S U) (b)(6), (b)(7)(C) (49 ADT) recalled that the highest altitude for TN 4131 was 12,000 ft at 25 NM. The system held TN 4131 at 8,400 ft when it was at 25 NM. (IO Exhibit 91, (b)(6), (b)(7)(C) , p.596).
(d) (S U) HMS Manchester went off Link 11. (b)(6), (b)(7)(C) (FC-1) hooked TN 4474 for 5 secs (RNG 110 NM, BRG 139, ALT 11,900, SPD 448). Forty seconds later TN 4474 was dropped from system. (IO Exhibit 91).
(e) (S U) (b)(6), (b)(7)(C) (CSC) recalled that the last time he looked at altitude, TN 4131 was at 22 NM at 10,300 ft. At 22 NM, USS Vincennes’s system held TN 4131 at 9200 ft. (IO Exhibit 91, (b)(6), (b)(7)(C) , p.531).
(g) (S U) (b)(6), (b)(7)(C) (AAWC) recalled requesting and receiving permission to illuminate at 20 NM. ( (b)(6), (b)(7)(C) , p.730).
(h) (S U) USS Vincennes issued a challenge over IAD to TN 4131:
{0652:33–0653:03 Zulu}: “Unknown aircraft on CSE-210, SPD-360, ALT 10,000. You are approaching USN warship BRG 201, 20 miles from you. You are standing into danger and may be subject to USN defensive measures.”
The TN 4131 range and kinematics agreed with the USS Vincennes’s system values. (IO Exhibits 91 & 203) {times, from ICAO Report, p.16 ¶ 2.10.8, p.B-16 (Nov. 7 1988). –CJHjr}.
Richard S. Williamson (Assistant Secretary of State, International Organization Affairs, 1988-1989, a lawyer), statement, ICAO meeting, Montreal Canada, July 13 1988 (ICAO: U.N. International Civil Aviation Organization) (AP880714-0103).
______________________
Query: “Challenge”?
The Vincennes IAD radio-talker did not ask the pilot to identify himself and state his intentions.
As the U.S. NOTAM required him to do.
The first warning, the Vincennes IAD radio-talker broadcast (allegedly) while the pilot was busy talking on another frequency, to Air Traffic Control.
This is his second and final warning.
He allegedly broadcast it while the pilot was one n.mile offshore Iranian soil, 22-25 n.miles from international waters, at 10,000 feet and climbing.
That deep inside Iranian territory, that close to Iranian soil, that far from where any warship might be, and that high, the pilot might not be monitoring the IAD frequency.
Also, the pilot was not headed for the warship. According to the radio-talker, the pilot’s course (210) was different from his bearing to the warship (201). And this means, the aircraft would pass more than 3 n.miles wide of the warship, at 14,550 feet. Way above the NOTAM’s 2,000 foot safety limit.
Or, he could not recognize himself in the warship broadcast.
Because the USS Sides might have been broadcasting at the same time, on the same frequency — an unintelligible jumble of simultaneous broadcasts no human being could understand.
Senior U.S. military officers concealed four of the five Sides warnings from their report. Presumably, to conceal this very fact. Likewise, this is surely the reason they did not disclose any recording or transcripts of any actual VHF broadcasts. They only disclosed a transcript of portions of the internal Vincennes IAD communication net, before it reached the VHF transmitter. And, it may never have been broadcast anyway. There is no trustworthy proof it was.
Even if the Vincennes did broadcast, and even if the Sides did not “step on” the Vincennes broadcast, the pilot would have a hard time knowing who the radio-talker was talking to. This, because senior U.S. military officers recklessly failed in their duty, to require their warship radio-talker to comply with international Air Traffic Control regulations, and speak the aircraft’s unique squawk-code.
And because senior U.S. military officers recklessly failed in their duty, to require their warship radio-talker to broadcast on the Air Traffic Control frequency. Which the pilot was required to monitor. Using the radio-talker’s main VHF transceiver, or his backup VHF. Which he surely had. And which the deceitful report-writers concealed from their report. Nobody goes anywhere in any warship or aircraft without a backup radio, in case one fails.
The Vincennes radio-talker in this broadcast did not ask the pilot to change course, as his talking script required him to do. And, he did not ask the pilot “to identify themselves and state their intentions,” as the U.S. NOTAM required him to do.
Not much of a “warning,” that a firing key will be turned, in exactly one minute (0654:05), and you’ll be dead, in less than two minutes (0654:43).
Even if he broadcast on the right frequency.
And even if he spoke the squawk-code.
Fishy.
And especially so, as the Vincennes IAD radio-talker did not use the mandatory emergency language (“Mayday, Mayday, Mayday”). Even though he was seated right next to Scott Lustig and heard Lustig announce his intention to attack. A minute and a half earlier.
Very, very, Fishy.
But very understandable, as part of Operation Praying Mantis. An unlawful, offensive, prima facie criminal, war of aggression, to destroy Iran’s military assets.
The prima facie violent criminals in such an unlawful U.S. Military Operation seek a pretext to attack. Like Vincennes Commander William Rogers did, when he unlawfully attacked the small boats.
And if they convince themselves, that an approaching aircraft is military, or recklessly hope so, and are willing to gamble, then they likely too would give a purposely defective “warning,” to trick the pilot into doing nothing, so they can kill him, and later claim they did nothing wrong, because they gave him a “warning”.
Is this why they also did not illuminate him with their fire-control radar? As their Rules of Engagement required them to do? Until they launched their missiles? So the pilot would not have a chance to jenk course? To save himself? By demonstrating no hostile intent?
Sick. (If that’s what they did).
But what they claim is, that their unqualified officer did not know what buttons to push, or that he needed to push any buttons, to authorize a lock-on with a fire control radar.
This, because Rogers violated Navy Regulations, and negligently certified as qualified, an officer whom he knew was not qualified, for want of training, to do the job.
–CJHjr
(i) (S U) USS Vincennes issued a challenge over MAD to TN 4131:
{0652:44–0653:04 Zulu}: “Iranian F-14 this is USN warship bearing 199, 20 miles. Request you change course 270 immediately. If maintain current course you are subject to USN defensive measures.”
USS Vincennes’s system data indicated the same. (IO Exhibits 203, 91) {times, from ICAO Report, p.15 ¶ 2.10.2, pp.B-18, B-25 (Nov. 7 1988). –CJHjr}.
(j) (S U) (b)(6), (b)(7)(C) (TAO observer-USS Sides) recalled TN 4131 rising in altitude and as it reached CPA and continuing to rise to 10 or 11 kft. (IO Exhibit 56, (b)(6), (b)(7)(C) , p.222). {p.52-1993}
(k) (S U) (b)(6), (b)(7)(C) (49 ADT) stated that TN 4131 IFF broke Mode II on his RCI (not on CRO) only one time. That occurred when it was at 20 miles. It then started to decrease in altitude between 25 and 20 miles. He said on net 12 that the contact was decreasing but did not refer to it by TN. IDS and TIC also noticed a decrease according to (b)(6), (b)(7)(C) and they said it aloud on net. USS Vincennes’s system data indicated TN 4131 was still ascending. (IO Exhibit 91, (b)(6), (b)(7)(C) , pp.588, 595).
(l) (S U) (b)(6), (b)(7)(C) (MSS) recalled altitude decreasing at 20 NM. ( (b)(6), (b)(7)(C) , p.749).
(m) (S U) (b)(6), (b)(7)(C) (IAD) did not recall hearing declining altitude reports on net 12. ( (b)(6), (b)(7)(C) , p.614).
(n) (S U) (b)(6), (b)(7)(C) (OPREPP/SITREP writer) recalled hearing descending altitude ( (b)(6), (b)(7)(C) , p.763).
(o) (S U) (b)(6), (b)(7)(C) (AIC-3) recalled an altitude of 9000 ft. at 20 NM. USS Vincennes’s system data indicated the same. (IO Exhibit 91, (b)(6), (b)(7)(C) , pp.706, 712).
(s) (S U) (b)(6), (b)(7)(C) (IAD) recalled seeing altitude 10,500 on TN 4131 ( (b)(6), (b)(7)(C) , p.609). {p.36-1988}
(7) 0653Z
(a) (S U) USS Vincennes reported altitude of TN 4131 at 10,500 ft over Link 11. (IO Exhibit 91).
(c) (S U) (b)(6), (b)(7)(C) (WCC-Sides) Recalled that at the time of engagement, TN 4131 altitude was at 11,000 feet about 15 NM on a course paralleling Sides. (IO Exhibit 70).
(d) (S U) (b)(6), (b)(7)(C) (observer-Sides) confirmed {p.53-1993} growing excitement and yelling in CIC about COMAIR. He looked at WCO’s IFF box and “read 6700 block”, altitude about 11,000 ft. (IO Exhibit 73).
(e) (S U) (b)(6), (b)(7)(C) {David R. Carlson (Captain, U.S. Navy), Commanding Officer of the USS Sides} (CO-Sides) recalled evaluating TN 4131 as a non-threat based on CPA to USS Sides, F-14 ASUW capability, lack of ESM and precedent. He noted an altitude of 11,000 ft and shifted his attention to the P-3 to the west. (IO Exhibit 48) ( (b)(6), (b)(7)(C) , pp.151, 153).
(f) ( ) (b)(1) {ESM intercept:}
(1) (S U) Airbus A300 carries WXR-700C-X NAV/Weather Avoidance Radar
(2) ( ) (b)(1) {AN/SLQ-32 will show WXR-700-X}.
(4) (S U) Neither USS Vincennes, USS Elmer Montgomery, nor USS Sides had a AN/SLQ-32 intercept of the Airbus radar (Enclosure 16).
(g) (S U) USS Elmer Montgomery had no ESM contacts that would have correlated TN 4131 to an F-14. (IO Exhibits 27 & 33, (b)(6), (b)(7)(C) p.89).
(h) (S U) (b)(6), (b)(7)(C) never recalled seeing an altitude above 11,000 ft. ( (b)(6), (b)(7)(C) , p.814).
(i) (S U) TN 4131 was at 16 NM, BRG 018, SPD 371 and ALT 11,230. (IO Exhibit 91).
(j) (S U) (b)(6), (b)(7)(C) (TIC) recalled target altitude of 11,000 ft at 15 NM. He began to update the range every open spot on net 15/16. USS Vincennes’s system data indicated 11,400 feet {the same values} at 0653:31. (IO Exhibit 91, (b)(6), (b)(7)(C) , p.682).
(k) (S U) (b)(6), (b)(7)(C) (GW) heard continuous reports of declining altitude. ( (b)(6), (b)(7)(C) , p.815). {p.37-1988}
(l) (S U) (b)(6), (b)(7)(C) (IAD) recalled being prepared to give the final warning when another ship came up and gave a challenge. (b)(6), (b)(7)(C) also recalled that the aircraft was at 7800 ft at that time and at 450 kts. The USS Vincennes’s system data did not hold this altitude until after missile intercept. (IO Exhibit 91, (b)(6), (b)(7)(C) , p.610).
(m) (S U) IAD challenge issued by (b)(6), (b)(7)(C) (USS Sides) to aircraft BRG 204 to Vincennes, RNG 31kyds, {p.54-1993} squawking Mode III-6700. USS Vincennes’s system data indicated the same. (IO Exhibits 71 & 91, (b)(6), (b)(7)(C) , p.172).
Richard S. Williamson (Assistant Secretary of State, International Organization Affairs, 1988-1989, a lawyer), statement, ICAO meeting, Montreal Canada, July 13 1988 (ICAO: U.N. International Civil Aviation Organization) (AP880714-0103).
______________________
Query: “Challenge”?
The Sides IAD radio-talker did not ask the pilot to identify himself and state his intentions.
As the U.S. NOTAM required him to do.
This is what the Sides radio-talker actually said:
{0653:25–0653:43}: “Unidentified aircraft squawking 6760 mode-3, you are approaching a US Navy war-ship bearing 090, correction 204, at 31,000 yards. You are standing into danger. Request you alter course 270.”
ICAO Report, p.B-16. {Time, from ICAO Report, p.B-16 and p.16 ¶ 2.10.8 (Nov. 7 1988). –CJHjr}
The distance in yards (15.3 n.miles) is U.S. Navy jargon, for surface distance, unknown to pilots. So too, the term “mode-3,” referring to a military transponder, which can broadcast civilian responses in addition to military responses (modes 1, 2, 4).
The Sides radio-talker broadcast this warning as the pilot was approaching MOBET, a mandatory Air Traffic Control reporting waypoint, 12 n.miles inside Iran’s territory.
17 seconds after this broadcast, the pilot commenced his mandatory report, to the Bandar Abbas Approach/Departure Control (0654:00–0654:11).
When he finished, he was obliged to switch frequencies, to the Tehran Area Control Center (relayed to Tehran via a microwave telecoms network, from an antenna at the Bandar Abbas airport), to make his next mandatory report, less than a minute later, when he reached his assigned flight level 140 (14,550 feet, on that day).
More than 12 n.miles deep inside his own territory, just a mile or two offshore, on the verge of broadcasting these two mandatory reports, and changing frequencies, the pilot was not likely monitoring the IAD frequency.
Senior U.S. military officers recklessly failed in their duty, to require their warship radio-talker to broadcast on the Air Traffic Control frequency. The frequency the pilot was required to monitor.
This ‘warning’ too does not contain emergency language (“Mayday, Mayday, Mayday”).
Yet, it was an heroic effort, by the Sides radio-talker, butting into somebody else’s business, doing the best he knew how to do, to warn the pilot.
While the pilot was switching frequencies, two missiles from the warship were enroute, on their 21 second flight.
Precisely one minute after the Sides broadcast, the aircraft, and its 290 souls on board, were shredded, by two explosions, and 10,000 steel ball bearings (0654:43).
–CJHjr
(n) (S U) (b)(6), (b)(7)(C) (AIC-3) recalled an altitude of 7700 feet on his fourth look at TN 4131 when it was at 15 NM. USS Vincennes’s system data at 15 MM showed an altitude of 11,000 ft. (IO Exhibit 91, (b)(6), (b)(7)(C) , pp.706, 712).
(r) (S U) TN 4131 was at 14 NM, ALT 12,000, and still at SPD 382. (IO Exhibit 91).
(8) 0654Z
(a) (S U) USS Vincennes’s system held TN 4131 at RNG 12 NM, SPD 380, ALT 12,370, CSE 211 at the beginning of this minute. (IO Exhibit 91).
(b) (S U) (b)(6), (b)(7)(C) (RSC) reported hearing that the target had dropped in altitude 5-6000 ft at 12 NM. ¶
(d) (S U) USS Vincennes issued a MAD challenge to TN 4131 {06:53:48–0654:10 Zulu} CSE 211, SPD 385. In background noise “Standard missile, hit Standard missile” is heard. USS Vincennes’s system data indicated the same. (IO Exhibits 91 &