FSC 1520: Aircraft, Rotary Wing
The following documents are a part of this series:- AN-9254 - Detail Weight Statement (Rotorcraft Only)
- MIL-D-23222 - Demonstration Requirements for Helicopters
- MIL-D-8778 - Data for Evaluation and Development of Rotary Wing Aircraft
- MIL-DTL-32742 - Handling Qualities for Military Rotorcraft
- MIL-H-8501 - Helicopter Flying and Ground Handling Qualities, General Requirements for (No Superseding Document)
- MIL-P-27881 - Preparation for Delivery of H-21 Helicopter for Domestic and Overseas Shipment and Storage Of
- MIL-S-8698 - Structural Design Requirements, Helicopters (Asg) (No Superseding Document)
- MIL-STD-250 - Aircrew Station Controls and Displays for Rotary Wing Aircraft (No Superseding Document)
- MIL-STD-3063 - Rotorcraft Structural Integrity Program (RSIP)
- MIL-T-8679 - Test Requirements, Ground, Helicopter (No Superseding Document)
- MS-33572 - Instrument, Pilot, Flight, Basic, Standard Arrangement for Helicopters
- MS-33575 - DIMENSION, BASIC, COCKPIT, HELICOPTER (USE MIL-STD-1333 FOR ARMY and NAVY AND DH2-2 FOR AIR FORCE)
- MS-87017 - Switches (Arrangement and Functions) Grip Assembly, Cyclic Controller, for Installation in Helicopters (No Superseding Document)