Alloy Iron Castings, Ductile, Sand, Corrosion Resistant 22Ni (2.5 - 3.0C) As Cast
Torque Tightening Threaded Fasteners
NUT, PLAIN HEX - THIN, UNS S66286 MJ THREAD, METRIC
Bolts & Screws, UNS G87400 Tensile Strength 860 MPa & 1000 MPa Procurement Specification, Metric
Aluminum Alloy Die Forgings (7050-T74) Solution Heat Treated and Overaged
Aluminum Alloy, Castings 7.0Si - 0.32Mg (356.0-T6) Solution and Precipitation Heat Treated
Plating, Electroless Nickel
Specification for Aero and Aero-Derived Gas Turbine Engine Lubricants
Aluminum Alloy, Rolled or Cold Finished Bars and Rods (7075-T651) Solution and Precipitation Heat Treated
Aluminum Alloy, 2024, Bar, Rod, and Wire; Rolled, Drawn, or Cold Finished
Fittings, Tube, Fluid Systems, Separable, High Pressure Beam Seal, 5000/8000 psi, General Specification For
Technical Guidelines for Aerospace and High Performance Electronic Systems Containing Lead-free Solder and Finishes
SAE ITC Guidance for Selection of Metallic Material Specifications & Standards Used for New Designs
Amendment Record No. TS95-AR for Technical Specification No. TS95
Landing Gear Safety Criticap Processes
Information on Hard Landings
This document provides information on the current practices used by commercial and military operators in regards to hard landings (or overload events designated as hard landings). Since detailed information on inspections would be aircraft specific, this AIR provides only a general framework. Detailed information and procedures are available in the maintenance manuals for specific aircraft.
Because hard landings potentially affect the entire aircraft, guidelines are listed here for non-landing gear areas. But, the primary focus of the document is the landing gear and related systems. The document may be considered to be applicable to all types of aircraft.
This document does NOT provide recommended practices for hard landing inspections, nor does it provide recommendations on the disposition of damaged equipment. Refer to ARP 4915 and ARP 5600.