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Aeronautical Design Standard, United States Army Aviation and Missile Command - Radar System Airworthiness Qualification and Verification Requirements

This document establishes the verification methods and
qualification requirements for radar systems installed on U.S. Army
aircraft. A combination of analyses, component testing, ground testing,
and flight testing, will verify the design, installations and
performance of the radar subsystem prior to the formal Airworthiness
Qualification Release.

The documents listed in this section are specified in
sections 3, 4, and 5 of this standard. This section does not include
documents cited in other sections of this standard or recommended for
information or as examples. While every effort has been made to ensure
the completeness of this list, document users are cautioned that they
must meet all specified requirements documents cited in sections 3, 4,
or 5 of this standard, whether or not they are listed.

Specifications, standards, and handbooks. The following
specifications, standards, and handbooks form a part of this document to
the extent specified herein. Unless otherwise specified, the issues of
these documents are those listed in the issue of the Department of
Defense Index of Specifications and Standards (DoDISS) and supplement
thereto, cited in the solicitation.

System Safety. All component tests and subsystem tests shall be
planned and conducted in accordance with MIL—STD—882. Hazard analyses
and safety statements shall be an integral and essential factor in the
preparation, planning, and conduct of all such tests. Tests shall
provide for the assessment of test item hazards associated with further
development and testing. System safety reviews shall be an integral part
of program design review.

Human Factors Engineering (HFE). Surveys, ground, and flight tests
cited herein shall be used to demonstrate the incorporation of HFE
design requirements and criteria in accordance with MIL—STD—l472 and the
Airworthiness Qualification Standard (AQS). Radar display symbology
shall be demonstrated to be in accordance with MIL—STD—2525.

Reliability, Availability, And Maintainability (RAM)
Substantiations and Verifications. For new or modified components, a
combination of substantiation, verification, and demonstration
requirements are applicable to the RAM requirements. Reliability
requirements shall be evaluated against the test program results.
Maintainability characteristics will be evaluated during Government
tests. MIL—HDBK—781 shall be used for guidance.