REVIEW OF STATUS ON TACKLE AIRCRAFT LOSS 21 JUNE 1966

Document Type: 
Collection: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP68B00724R000100070005-9
Release Decision: 
RIPPUB
Original Classification: 
T
Document Page Count: 
5
Document Creation Date: 
December 12, 2016
Document Release Date: 
July 16, 2002
Sequence Number: 
5
Case Number: 
Publication Date: 
June 23, 1966
Content Type: 
BRIEF
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PDF icon CIA-RDP68B00724R000100070005-9.pdf193.42 KB
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Approved For Release 0 Copy 23 June 1966 25X6 25X6 25X1A 25X1A 25X1A 25X1A 25X1 A BRIEFING MEMORANDUM FOR THE DD/S&T SUBJECT: Review of Status on TACKLE Aircraft Loss 21 June 1966 1. TACKLE U-2 number 384 departed 21/02002 on a routine training mission. Primary purpose of the flight was a long range (5. 5 hour) high altitude training mission to validate fuel consumption data. Prior to this flight he had logged a total of 3, 208 hours flying time, of which 230 hours were in the U-2. He had completed six operational over- flight missions in the U-2. A full complement of systems, including new lightweight B and tracker cameras, was aboard. 2. Pilot of the aircraft was gave the first indication of trouble. The firstlI chirp revealed DC and AC generators out, RPM below 75 per cent and autopilot disengaged. The last =chirp occurred sixteen seconds after report of initial failure and indicated cockpit pressurization above 35, 000 feet. A pressure sensitive switch should have disabled the SSB transmitter and terminated =transmissions at that time. 4. Any of the four failures noted above would have triggered" however, all appeared on the first chirp, indicating they occurred simultaneously or in very rapid sequence. Since the DC generator should function until RPM approaches 35 per cent, it appears that engine rundown may have been rapid. This could occur with engine seizure or disinte- gration. Teardown and inspection of the engine by the Board of Investi- gation should assist in determining the exact cause of failure. 5. At 0642Z Okinawa lost radar contact with the aircraft at a point approximately 165 NM from Naha Air Base (see attached map) and apparently did not thereafter regain contact. Although the aircraft IFF ceased to operate after 0638Z, thus reducing the capability of the radars Ezck dad iron aubsallc do+vn.^rclin~ and Approved For Release 20 218/ LDP68B00724R000100070005-9 25X1A Apprcl"d?For Release 2002/08/06 : CIA-RDP&&B 724R000100070005-9 25X1A -2604-66 Page Two 25X1A 25X1A 25X1A 25X1A to paint the aircraft, no logical explanation has yet been provided as to why the radars were unable to skin-paint the aircraft during the approxi- mately twenty minutes the aircraft was approaching Naha. It appears that the pilot attempted a power off landing on Okinawa and that he had full control of the aircraft until he ejected. 6. Eye witnesses state that the aircraft approached the point of impact (Keraina Island) franY tie wcst and that it vv,-,.s "v_:-:?y cjuic:" (aircraft was without power). At appro.xln atei;y 3 O feet altitude the pilot was observed to eject through the canopy of the aircraft. His chute partially deployed and then wrapped around his body. He impacted the water in this condition. Local fisherman recovered the body and a USAF helicopter removed it to Naha.AB, Okinawa. 8. After the pilot ejected, the aircraft spir:alled slightly to the right, struck the water and broke up very near the shoreline of Kerama Island. Recovery of the wreckage is being accomplished by a US Army tug under control of the 313th Air Division, Okinawa. Wreckage will be moved from Naha Navy Pier to the secure end of Naha AB and then n transported to this weekend` via USAF C-124, probably not 25X1A 9. An Accident Investigation Board has been convened and is scheduled to arrive on June 25. We expect that approxi- mately two weeks will be required to complete the investigation. U-2 aircraft at 0 have been grounded until the investigation has been completed and corrective actions, if any, accomplished. Based on past experience, it can be assumed that will require at least two addi- 25X1A tional weeks for refresher training and restoration of pilot confidence in the aircraft prior to resumption of operational activities (approximately 1 August 1966). 10. Loss of Article 384 reduces the Agency/SAC inventory to sixteen U-2 aircraft. SAC now has ten aircraft, two of which are at Lockheed undergoing convc sion to the J-75 configuration, and not avail- able for operational activities. CIA now has six U-2 aircraft of which five are operationally ready. Their locations and status are listed as follows: HANDLE VIA Approved For Release ~WOJW~,%' 4-RDP68B00724R0~Qd 7~gQ -?ySTEM 25X1A 25X1A Approved For Release 2002/08/06 : CIA-RDP68BB00724R000100070005-9 Page Three Edwards AFB Edwards AFB Edwards AFB Lockheed Operationally Ready Operationally Ready Operationally Ready Out of Commission 348 349 381 359 25X1 C 25X1A 25X1A Article 359 is being modified, to accept Systems 20 and 22 and will be used for the operational testing of those systems, now scheduled for late July 1966. 11. I I are operationally ready in the TACKLE U-2 aircraft with a total of ten missions left in their combat tour. Two other pilots have completed their U-2 training at and are scheduled to begin training in the J-75 configured U-2 on 5 July 1966. In order to speed up their type conversion, we are considering completing their training at Edwards AFB in our unit there. It is antici- pated that they will be operationally ready between 15 August and 1 September 1966. Attachment: Map Addendum Approved For Release 2002/08/06 : CIA-RDP68B00724R000100070005-9 25X1 A Approv P06r Release 2002/08/06: CIA-RDP6$W0"124 00100 00456 ? Page Four DD/OSA/JACunningham. Jr:dbt (5684 - 23 June 1966) Distribution: #1 - DD/S&T #2 - DD/S&T #3 - D/R/GIA #4 - C/ FE Div #5 - DD/OSA #6 - DD / OSA #7 -' RB/OSA #8- D/FA/OSA #9 - SAL/OSA #10-ID/OSA #11-IDEA/OSA CONTROL SYSTEM Approved Fo;L.Reaease 2002108/06: CIA-RDP68B00724R000100070005-9 Approved For Release 2002/08/06 : CIA-RDP68B00724R000100070005-9 Next 2 Page(s) In Document Exempt Approved For Release 2002/08/06 : CIA-RDP68B00724R000100070005-9