AM.II.F.R1
Risk managementRelieving system pressure prior to system servicing or disassembly.
From the FAA library
- Chapter 9: Flight Manuals and Other Documents › Preventive Maintenance › Examples of Preventive Maintenance
tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or flight deck interior when removal or disassembly of any primary structure or operating system is not required; applying preservative or protective material to components where ... disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices; repairing upholstery and decorative furnishings of the cabin, flight deck, or balloon basket interior when…
- 14 CFR Part 43, Appendix A to Part 43—Major Alterations, Major Repairs, and Preventive Maintenance
wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. (10) Applying preservative or protective material to components where ... disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when…
- Chapter 13: Aircraft Landing Gear Systems › Wheel Inspection › Off Aircraft Wheel Inspection
wheels are relatively soft. Any nick or deformation causes a stress concentration that can easily lead to wheel failure. Disassembly of the Wheel Disassembly of the wheel should take place in a clean area on a flat surface, such ... aside for cleaning and inspecting. The tie bolts can then be removed. Do not use an impact tool to disassemble the tie bolts. Aircraft wheels are made of relatively soft aluminum and magnesium alloys. They are not designed to receive…