Downloaded from https://www.everyspec.com ADS-65A-HDBK Compliance: Submission of Drawings, schematics, optical prescriptions and performance data describing all items of the entire sensor systems/subsystems. The data should identify by Governmental nomenclature each item of the system/subsystem and should include the functional relationship and purpose of the items. The interconnections to systems, such as structural mounting surface, electrical, and optical requirements should be provided. Structural attachment details of the sensor turret system to the aircraft should also be shown. The structural attachment details should be provided and all loaded joints clearly shown.
Mounting details depicting the attachment of the system/subsystem to brackets, pallets, or description/analysis/diagrams should be provided to indicate the performance requirements for safety are met. Electrical schematics and wire diagrams internal to the system/subsystem and wire/diagrams/cable connections should be provided. Electrical schematics/cable connectors, and wire run diagrams should be provided using MIL-STD-7080 as a guide. An airframe prevention and control procedure containing the following data will be prepared. a.
Materials/finishes to be used during the installation procedure, including but not limited to the mounting hardware, will be compatible with the adjacent airframe structure from a corrosion point of view using MIL-STD-7179 as a guide. b. Description of how system corrosion requirements are translated into sub-tier requirements, considering criticality of particular hardware (as determined by the Failure Modes and Effects Criticality Analysis), severity of local environment, and difficulty of maintenance. c. Bonding materials, procedures and/or modifications for verification of airframe electrical bonding requirements. Installation instructions should be provided for production.
This includes wiring, pinouts, grounding, bonding, and shielding, mounting hardware, connectors, etc. The contractor should provide a document showing what, if any, failures of the environmental and Electromagnetic Interference (EMI) tests would need to be considered by future integrators. The contractor should provide test points on the sensor system to check for bonding of the sensor to the aircraft for maintenance purposes. Reference: MIL-STD-7080, MIL-STD-7179 4.8.2 Equipment Furnished by Contractor Verify Design, Performance, and Operation of Contractor Furnished Test Equipment Standard: Contractor-furnished-test-equipment ( CFTE ) sensor design/analysis/test Compliance:
Contractor-furnished-equipment ( CFTE ) operation and performance characteristics should be submitted when such equipment is furnished as CFTE, or if modification of the Government Property ( GP ) is made. 11