Description / Abstract:
This SAE Aerospace Information Report (AIR) discusses past and
present approaches for monitoring the landing gear structure and
shock absorber, methods for transient overload detection,
techniques for measuring the forces seen by the landing gear
structure, and methods for determining the fatigue state of the
landing gear structure. This AIR covers the landing gear structure
and shock absorber. It does not include the landing gear systems or
landing gear wheels, tires and brakes. Landing gear tire condition
and pressure monitoring are detailed in AIR4830 and ARP6137,
respectively.