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| MIL-T-81783C(AS)
PUBLICATIONS
Hughes Aircraft Company
3282205
Acceptance Test Procedure, Test Station,
Controls-Displays-Doppler Filter
Applicable (see 6.6).
2.2
Availability of documents.
Precedence of documents. When the requirements of the contract, this
2.3
specification, or applicable subsidiary documents are in conflict, the follow-
ing precedence shall apply:
a.
Contract - The contract shall have precedence over any other document.
b. This specification - This specification shall have precedence over all
applicable subsidiary documents (see 6.6).
c. Referenced documents - Any document referenced in this specification
shall have precedence over all applicable documents referenced therein.
3.
REQUIREMENTS
Materials,
parts, and processes.
Applicable (see 6.6).
3.1
3.2
Design and construction.
Applicable except as follows.
Design features.
Applicable except as follows.
3.2.1
3.2.1.1
Method of operation.
Applicable.
Applicable.
Commercial test equipment.
3.2.1.2
Other commercial components.
Applicable.
3.2.1.2.1
Circuit grounds.
Applicable.
3.2.1.3
Applicable.
Interchangeability.
3.2.1.4
Applicable.
Identification of product.
3.2.1.5
Applicable.
3.2.1.6
Human factors.
Test set generated acoustic noise.
Applicable.
3.2.1.7
Not applicable.
Forced-liquid cooling.
3.2.1.8
Space and weight limitations. The weight of the C&D TS shall
3.2.1.9
not exceed 1600 pounds. Maximum dimensions shall be 48 inches by 54 inches
by 75 inches with all drawers and retractable mounting fixtures in the re-
tracted position.
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