AFGS-87219 Electrical Power Systems, AircraftThis specification establishes the performance requirements and verifications for electric power subsystems EPS for aerospace vehicles, including aircraft, helicopters, and missiles.

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A.4.2.9.S    Other.

AFGS�87219B APPENDIX A

The compliance of other components with the requirements of 3.2.9.5 shall be verified by

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VERIFICATION RATIONALE (A.4.2.9.S)

System analyses, component qualification tests and integrated EPS tests have proven to be required on other major components and should be considered for verification of other major components.

VERIFICATION GUIDANCE (A.4.2.9.S)

a.   Analyses appropriate to the major component installation include electrical load analyses, failure mode and effect analyses, hazard analyses and reliability analyses.

b.   Each major component should be tested to its specification requirements.

c.    The major component should be tested in an integrated EPS mockup and after installation in the vehicle.

VERIFICATION LESSONS LEARNED (A.4.2.9.S)

All unique components must be qualified to their individual performance specifications to assure compatibility on the aircraft.

A.3.2.10  Environmental conditions.

The EPS and its components shall be capable of withstanding and operating under the following environmental conditions to which they are subjected during all phases of aircraft operation:

------------.  Performance shall be as follows: ------------.

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