Safety_of_Flight_(SOF)_Requirements_12_Apr_2016.pdf

Testing Requirements for Safety Of Flight 12 April 2016

Due to Email limitations, SOF data shall be provided on CD and sent to:

PM Air Warrior (POC listed in Synopsis) 6726 Odyssey Dr, Huntsville, AL 35806

Data shall be in the form of Test Reports with the raw data provided. The SOF data must be for the equivalent hardware to be flown in Phase 2. Equivalent hardware may be demonstrated by

a) Part number of test items matching part number for Phase 2

b) If Phase 2 hardware has a different part number than the hardware used in SOF testing then the vendor must provide Qualification by Similarity reports. The Qual by Sim must show a clear linkage between part numbers and the differences between the items. The report can include drawings and analysis.

Test Procedure All Tests are in accordance with MIL-STD- 810G unless noted otherwise

Combined Environment (Temp/Alt/Humidity)

520.3 Procedure III

Tailored for operational temperature, humidity, and altitude. A minimum of ten cycles is required. The procedure may be tailored to include the Low Pressure (altitude) Storage/Air Transport testing and Low Temperature Storage testing at the beginning of the first cycle.

Operational Temperature: - 32oC (-25oF) to +52oC (+125oF);

Altitude 20000 ft MSL;

Transportation /Storage Temp: -60oC (-80oF) to + 85oC (+185oF)

Vibration 514.6, Procedure I Cat 24;

Man-Mounted

Explosive Atmosphere 511.5, Procedure I ;

Components shall have maximum input voltage applied to them and shall be operated continuously at their maximum loads

Altitude 20000 ft MSL

CE 101 Power Leads 30 Hz to 10 kHz

Per: MIL-STD-461 & ADS-37A-PRF

CE 102 Power Leads, 10kHZ to 10 MHz

Per: MIL-STD-461 & ADS-37A-PRF

RE 102; 10kHz to 18 GHz

Per: MIL-STD-461 & ADS-37A-PRF

Center of Mass and CG for head born weight

Per AVNS-DTL-10868B(draft) Must show display is frangible if the weight and center of mass of the display & helmet exceeds the requirements in Para 3.1.2.