Fire Protection and Flammability Testing able support the maximum flight and landing load expected
AIR8635
Provide basis for conducting Fire Protection and Flammability Testing with ability to support the maximum flight and landing load expected during a recognize a fire condition.
Rationale: The basis for a structural element to support a select design load during a recognized engine fire condition has a similarity foundation in applicable FAA FAR 29 and FAR 25 Advisory Circular guidance material as well as that applicable for Powerplant Installation and Propulsion Systems.
