MIL-A-8867C

NAVY - AS - Naval Air Systems Command

AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS

Organization:

Year: 1987

Abstract: This specification contains the requirements which, in combination with other applicable specifications, define the ground tests required for structural evaluation of fixed wing piloted airplanes. The types of testing include, but are not limited to:
a. Design development tests.
b. Pre-production component tests.
c. Static tests-complete airframe.
d. Fatigue tests-complete airframe.
e. Drop tests of structurally complete airframe.
f. Cabin pressure tests.
g. Leakage tests of integral fuel tanks.
h. Structural dynamic tests.
i. Proof tests for flight articles. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Naval Air Engineering Center, Systems Engineering and Standardization Department (Code 53), Lakehurst, NJ 08733-5100, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document, or by letter. Intended Use: The requirements of this specification are intended for use in the structural design and substantiation of airplanes.

URI: https://yse.yabesh.ir/std/handle/yse/85450

Subject: Airplane tests

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NAVY - AS - Naval Air Systems Command

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contributor author	NAVY - AS - Naval Air Systems Command
date accessioned	2017-09-04T16:22:05Z
date available	2017-09-04T16:22:05Z
date copyright	06/10/1987
date issued	1987
identifier other	TPCJDAAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/85450
description abstract	This specification contains the requirements which, in combination with other applicable specifications, define the ground tests required for structural evaluation of fixed wing piloted airplanes. The types of testing include, but are not limited to: a. Design development tests. b. Pre-production component tests. c. Static tests-complete airframe. d. Fatigue tests-complete airframe. e. Drop tests of structurally complete airframe. f. Cabin pressure tests. g. Leakage tests of integral fuel tanks. h. Structural dynamic tests. i. Proof tests for flight articles. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Naval Air Engineering Center, Systems Engineering and Standardization Department (Code 53), Lakehurst, NJ 08733-5100, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document, or by letter. Intended Use: The requirements of this specification are intended for use in the structural design and substantiation of airplanes.
language	English
title	MIL-A-8867C	num
title	AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS	en
type	standard
page	50
status	Active
tree	NAVY - AS - Naval Air Systems Command:;1987
contenttype	fulltext
subject keywords	Airplane tests
subject keywords	Arresting tests
subject keywords	Cabin pressure tests
subject keywords	Carrier-based airplanes
subject keywords	Catapult tests
subject keywords	Control system tests
subject keywords	Drop tests
subject keywords	Elevated temperature tests
subject keywords	Engine-mounted tests
subject keywords	Fatigue tests
subject keywords	Fuel tank leakage
subject keywords	Fuselage tests
subject keywords	Ground tests
subject keywords	Landing gear installation tests
subject keywords	Repeated load tests
subject keywords	Static tests
subject keywords	Strength tests
subject keywords	Tail group tests
subject keywords	Test measurements
subject keywords	Trainers
subject keywords	Vibration tests
subject keywords	Wing group tests