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|  MIL-W-81752A(AS)
4.1 - Responsibility for inspection - Unless otherwise specified
in the contract or purchase order, the contractor is responsible for
the performance of all inspection requirements as specified herein.
Except as otherwise specified in the-contract or purchase order, the
contractor may utilize his own facilities or any other facilities
suitable for the performance of the inspection requirements specified
herein, unless disapproved by the government. The government reserves
the right to perform any of the inspections set forth in the
specification where such inspections are deemed necessary to assure
supplies and services conform to prescribed requirements.
4.1.1 Responsibility for compliance. All items must meet all
requirements of sections 3 and 5. The inspection set forth in this
specification shall become a part of the contractor's overall
inspection system or quality program. The absence of any inspection
requirements in the specification shall not relieve the contractor of
the responsibility of assuring that all products or supplies submitted
to the Government for acceptance comply with all requirements of the
Sampling in quality conformance does not authorize
contract.
submission of known defective material, either indicated or actual,
nor does it commit the Government to acceptance of defective material.
4.2 - Classification of tests - The inspection requirements
specified herein are be classified as follows:
First article inspection (See 4.3)
a.
b.
Acceptance Tests (See 4.4)
4.3 - First article inspection - First article tests shall
consist of the quality conformance tests herein and the additional
tests specified in 4.3.1 and subparagraphs thereto.
4.3.1 - Strength testing - Tests shall be conducted to prove that
adequate strength exists in all parts of the windshield system to
meet the minimum strength and rigidity requirements imposed on the
Airplanes designed in accordance with SD-24 shall be tested
airplane.
in accordance with MIL-A-8860 with the windshield installed.
4.3.1.1 - Test loads - The magnitude of the test loads shall
include the factors of safety specified in MIL-A-8860, and as
specified in 3.6.2 herein.
4.3.1.2 - Test setup - The windshield shall be tested as part of a
complete airplane or on a test specimen, consisting of at least the
cockpit portion of the fuselage together with the entire cockpit
enclosure installed in operational condition.
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