Crashworthy data Compliant with FAA Helicopter Regulations. Identify if separate or recorder Part 91.609. integrated with ruggedized recorder. Engine and Aircraft Compliant with existing FAA requirements Provide information on Usage and what options/systems are Maintenance Data available. (HUMS) Removable or With cabin exposed, capable of ~80 KIAS N/A Sliding cabin doors for forward flight. on both sides Aircrew doors Ability to jettison doors while on the ground N/A jettison capability during emergency situations. Ergonomic Adjustable Seat and/or Pedals to Identify adjustment ranges adjustments accommodate pilots. of seat and pedals. Aircrew Cockpit Cockpit, seat, and seatbelt are compatible Provide a 3-view drawing Area with (current) DoN Aviation Life Support of cockpit from eye point System (ALSS) flight gear and NVD view (with dimensions or equipment. scaling). aircrew one aircrew member to move N/A restraint system about the cabin safely while cabin is exposed with open or removed doors. aircrew restraint attachment points designed to withstand a limit load of 3,600 lbs. with an ultimate load of 5,400 lbs. The ultimate load of 5,400 lbs. is considered to be acting as follows: For sidewall mounted attachments (those mounted on vertical cabin frames, bulkheads or any structure along the cabin sidewalls) the ultimate load shall act through a 180° hemispherical cone of action oriented about the vertical axis. For cabin overhead mounted attachments the ultimate load acts through a 180° cone of action oriented about the aircraft lateral axis. NVD HUD Interface Interface should be compliant with If capability for interface Compatible with applicable FAA requirements exists. Please describe DOD, NVD HUD what can be displayed. (monocle) Describe your platforms ability to meet the following parameters:
Crashworthy data recorder Compliant with FAA Helicopter Regulations. Part 91.609. Identify if separate or integrated with ruggedized recorder. Engine and Aircraft Usage and Maintenance Data (HUMS) Compliant with existing FAA requirements Provide information on what options/systems are available. Removable or Sliding cabin doors on both sides With cabin exposed, capable of ~80 KIAS for forward flight. N/A Aircrew doors jettison capability Ability to jettison doors while on the ground during emergency situations. N/A Ergonomic adjustments Adjustable Seat and/or Pedals to accommodate pilots. Identify adjustment ranges of seat and pedals. Aircrew Cockpit Area Cockpit, seat, and seatbelt are compatible with (current) DoN Aviation Life Support System (ALSS) flight gear and NVD equipment. Provide a 3-view drawing of cockpit from eye point view (with dimensions or scaling). aircrew restraint system one aircrew member to move about the cabin safely while cabin is exposed with open or removed doors. aircrew restraint attachment points designed to withstand a limit load of 3,600 lbs. with an ultimate load of 5,400 lbs. The ultimate load of 5,400 lbs. is considered to be acting as follows: For sidewall mounted attachments (those mounted on vertical cabin frames, bulkheads or any structure along the cabin sidewalls) the ultimate load shall act through a 180° hemispherical cone of action oriented about the vertical axis. For cabin overhead mounted attachments the ultimate load acts through a 180° cone of action oriented about the aircraft lateral axis. N/A NVD HUD Interface Compatible with DOD, NVD HUD (monocle) Interface should be compliant with applicable FAA requirements If capability for interface exists. Please describe what can be displayed. Describe your platforms ability to meet the following parameters:
N6134017R9999_TH-XX_RFI__06.01.2017_RDM_Final_6-1-2017.docx