KIL-A-88-flA(usAF)
1 July 1971
SUTERS~ING
MIL-A-8871(USAF)
8 October1968
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MILITARYSPECIFICATION
AIRPLANESTRENG’1’RAND
RIGIDITY
FLIGHTMD GROUND OPERATIONSTESTS
1. SCOPE
1.1 This specifIcation covers the flight test requirements for the
structural integrity flight and ground evaluation and demonstration of
piloted airplanes.
2.
JWPLICABLEIWUMENTS
2.1
The following documents, of the issue in effect on date of invitation
for bids or request for proposal, form a part of this specification to the
extent specified herein:
SPECIFICATIONS
●
✚✎✎✎
,,)
Milit@’y
MILA-8860
Airplane Strength and Rigidity - General Specification &
MILA-8861.
Airplsne Strength and Rigidity, Flight Loads
MIL-A-8862 Airplane Strength and Rigidity, Landplane Landing and
Ground Handling Loads
MIL-A-8865
Airplane Strength and Rigidity - Miscellaneous Lnad8
MIGA-8868
Airplane Strength and Rigidity, Data and Reports
PUBLICATION
WADC Technical
Preparation of Strength S~ary and Operating
Report
57-162 RestrictionsReports (AD 118326)
(Cbpies of specifications, standards, drawings, and publications required
by suppliers in connection with specific procurement functions should be
,,
obtained from the procuring activity or as directed by the contracting
i
officer.)
~
,:
2.2 Other publication.
The following document forms a part of this speci-
fication to the extent specified herein.
—
Unless otherwise indicated, the
it., issue in effect on the date of invitation
1
pOSEd shall apply.
for bi& or request for pro-
F$c 1510
Q:
)
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