Document Number (FOIA) /ESDN (CREST):
CIA-RDP74B00447R000100010038-0
Body:
Approved For Release 2002/06/18 3ftWP74B00447R000100010038-0
IDEALIST
IDEA 3004
Copy 2
8 March 1966
25X1f
25X1A
SUBJECT:
RECORD
1. I ladvised, by telephone, that indica-
tions are Ya e a rcraft was over stressed causing the
left wing to fall about 12 to 1S inches outboard from the
wing root. This failure was followed by a fairly severe
pitch up which probably caused the engine mounts to fall
and the rest of the aircraft came apart at that time.
2. There are several factors which may have contributed
to the structural failure. The fact that the aircraft was
indicated approximately 210 knots at 35,000 feet in a posi--
tion of a climbing right turn with empty main fuel tanks
and fuel in the auxiliary fuel tanks may have contributed
to the initial failure. With fuel in the auxiliary tanks
and empty main tanks the rigidity of the wing is affected.
Added to this is the unknown force applied by the use of
the right aileron at the aims time. While the critical G
force at the portion of the wing which failed is stated to
be 4.5, it seems unlikely that any qualified pilot would
apply 4.5 0 to this aircraft. It may follow that the con-
ditions noted above have reduced the force required to
cause structural failure to a sufficient degree that the
maneuver resulted structural failure.
3. It is my understanding that as a result of the above
Information, which was passed to Gen. Geary, by phone, by
Mr. Kelly Johnson, the Air Force has released their U_2 air-
craft for flight and are no 1 n interested in a special
inspection to be performed at 25X1A
4. The above information is not official and should
not be used to make decisions regarding the accident.
colonel USAF
Deputy for Field Activities., OSA
Approved For Release 2002/06/18 : CIA-RDP74B00447R000100010038-0
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ID 3004
Pages 2
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Approved For Release 2002/06/18 : CIA-RDP74B00447R000100010038-0