SECTION 2 CHAPTER 6 ANNEX B

CHALLENGING ENVIRONMENT CONTEMPORARY CRASH PROTECTION STANDARD

As discussed in Section 2 Chapter 6, the Authority prescribed challenging environment contemporary crash protection standard is the sum of the following:

design requirements provided by the latest amendment of MIL-STD-1290A, plus

HIC and femur load requirements of FAR or CS 2X.562 (whichever is most demanding) using the FAR/CS appropriate for the type and size of aircraft, plus

equipment requirements specified in the most demanding operational regulations of the FARs, CSs and EU CAT.

This annex presents additional detail on the application of the components of the challenging environment CCPDR.

Design requirements specified in MIL-STD-1290A

MIL-STD-1290A presents a contemporary military crash protection standard requiring minimal supplementation, other than from design standards referred to within MIL-STD-1290A including:

MIL-DTL-27422D–Detail Specification for the Tank, Fuel, Crash-Resistant, Ballistic-Tolerant, Aircraft

MIL-S-58095A–Seat System: Crash-Resistant, Non-Ejection, Aircrew, General Specification for

MIL-S-85510–Seats, Helicopter Cabin, Crashworthy, General Specification for

MIL-H-83796B–Hose Assembly, Rubber, Lightweight, Medium Pressure, General Specification for

MIL-PRF-83282D–Hydraulic Fluid, Fire Resistant

MIL-DTL-25579F–Hose Assembly, High Temperature, Medium Pressure General Specification for

MIL-H-38360B–Hose Assemblies, High Temperature, High Pressure, 3000 psi, Hydraulic and Pneumatic.

JSSG 2010-7 and the Aircraft Crash Survival Design Guide provide additional detailed guidance on the application of crash protection design requirements in the military context.

Head Injury Criteria and Femur Load Requirements

MIL-STD-1290A must be supplemented with FAR or CS 2X.562 (whichever is more demanding) for measuring head injury and femur loads in the design of seats. The associated FAA advisory circulars (ACs 27-1B, 29-2C, 23.562-1 or 25.562-1B as applicable) provide additional guidance on means of compliance for these crash protection design features.

Operational Regulations

MIL-STD-1290A must be supplemented with the operational regulation clauses of the FARs and EU CAT that provide crash protection requirements detailed in Annex A to Section 2 Chapter 6. These operational requirements are equally applicable to, and form part of, the Authority prescribed challenging environment contemporary crash protection design standard.