Downloaded from https://www.everyspec.com ADS-65A-HDBK within 30 seconds. All exit doors must be closed and all personnel must start in a seated position with a locked harness/restraint and hands on controls. All personnel must exit through the same exit (door) location, and at least two-thirds of all possible exits must be tested. ii. Aircraft not equipped with crashworthy fuel cells must demonstrate emergency egress provisions as stated above, but within 20 seconds. iii. Assisted Egress must be accomplished within 3 minutes from time of arrival on scene. Assisted egress includes immobilizing the crew members and extracting crew members without adding injury or compounding existing injury.
Evacuation times should be demonstrated by actual tests using personnel approximating 95th- percentile troops with full combat equipment for passengers and 95th-percentile aviators with arctic flight gear and body armor for crew members. Reference: MIL-STD-810 4.8.3.7 Mechanical Load Analysis Verify Structural Integrity and Mechanical Load of the Sensor System Standard: Demonstrate the structural integrity of the sensor turret and the supporting structure of the aircraft. Compliance: The mechanical load analysis should demonstrate the structural integrity of the sensor turret and the supporting structure of the aircraft.
The expected loads should not exceed critical limits and should use the guidance of ADS-51-HDBK . Reference: ADS-51-HDBK 4.8.3.8 Weight and Balance Report Verify Weight and Balance Standard: A weight and balance report should show accurate and complete weight and balance calculations of the sensor system. Compliance: Submission of weight and balance report. This report should show accurate and complete weight and balance calculations of the sensor system. Tables should include the weights, moment of inertia, and center of gravity ( cg ) for the sensor system and subsystems, as well as empty weights, and gross weights, and cg for the aircraft.
The report should include drawings that show the location of the cg for the system and for each subsystem in the system’s reference frame. The sensor system reference frame datum should be clearly marked on all drawings. 14