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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AFGS�87219B

Environment	Requirement	Performance
Temperature/Altitude
Humidity Fungus
Vibration
Dust
Salt Fog
Sand and Dust
Rain
Acoustic Noise
Explosive Atmosphere
Shock
Gunfire
Temperature, Humidity, Vibration, Altitude
Acceleration
Vibro-Acoustic, Temperature
Nuclear Exposure

3.3 Electromagnetic interference.

The electromagnetic interference requirements for the EPS shall be as follows: ------------·

3.4 Integrity.

The integrity program requirements shall be in accordance with MIL-STD-1796 for electronics and MIL-STD-1798 for mechanical equipment and subsystems·

3.5 Maintainability.

The EPS maintainability requirements shall be as follows: ------------·

3.6 System safety.

The system safety requirements for the EPS shall be as follows: ------------·

3.7 Interface requirements.

The EPS and its components shall interface with the other aircraft subsystems as necessary to provide the performance specified herein· In addition, the following detailed interface characteristics are required: ------------·