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Aeronautical Design Standard, United States Army Aviation and Missile Command - Data and Test Requirements for Airworthiness Release for Helicopter Sensor Data and Testing Requirements in Development Stage

Sensor package description and installation. Drawings, schematics, and performance data shall
describe all items of the entire sensor systems/subsystems. The data shall identify by Governmental
nomenclature, each item of the system/ subsystem and shall include the functional relationship and purpose
of the items. The interconnections to systems, such as structural mounting surface, electrical, and optical
requirements shall be provided. Structural attachment details of the sensor turret system (Pilotage and
Target Acquisition] Designator) to the aircraft shall be shown. The structural attachment details shall be
provided and all loaded joints clearly shown. Mounting details depicting the system/subsystem to brackets
or pallets or rack attachments to the aircraft shall be provided. Electro-optical and optical
description/analysis/diagrams shall be provided to indicate the performance requirements for safety are met
( Pilotage/Laser subsystem). Electrical schematics and wire diagrams internal to the system/ subsystem and
wire diagrams/cable connections shall be provided. Electrical schematics/cable connectors, and wire run
diagrams shall be provided using SAE-AS-50881and MIL-STD-7080 as guides.
ADS-62-SP

Location of sensor package. Equipment installations and arrangement drawings showing the location
of all major items of the sensor equipment for which provisions has been made and any exterior equipment
shall be provided.

Equipment furnished to contractor. Contractor-furnished-equipment (CFE) sensor design/analysis/test
design data, shall be required when such equipment is furnished as CFE Sensor equipment
systems/ subsystems, or if modification of the Govemment-Furnished Equipment (GFE) is made.

Pilotage night Vision systems. Pilotage night Vision systems such as Forward Looking Infra-red
(FLIR) coupled to a helmet mounted display or helmet mounted night Vision goggle with a pointing Fire
Control System in the aircraft shall be designed and evaluated by analysis. The analysis shall provide
sufficient field of view and resolution to allow safe flying of the aircraft in marginal light conditions and
marginal weather and at nap of the earth (NOE) or above altitudes.