Aircraft Hardware and Fasteners
Bolts, nuts, washers, rivets, locking devices, seals, clamps and access-panel hardware.
Source: AMT-SIM original reference
Reference notes
Aircraft hardware is selected for strength, vibration resistance, corrosion resistance and traceability. Bolts and nuts clamp parts, washers spread load, rivets form permanent joints, and approved locknuts, cotter pins or safety wire resist rotation.
O-rings and gaskets seal fluid and pressure boundaries. Adel clamps support wires and hoses. Dzus fasteners secure removable access panels. Do not substitute automotive or hardware-store parts without approved data.
Inspect threads, heads, holes, grip length, locking feature and installation direction. Torque and secure the assembly according to the applicable maintenance data.
Books, manuals and source material
Aviation Maintenance Technician Handbook - General (FAA-H-8083-30B)
Federal Aviation Administration · FAA-H-8083-30B, General
Official FAA handbook covering mathematics, physics, materials, tools, electricity, human factors and maintenance practices.
Open source resourceAcceptable Methods, Techniques, and Practices - Aircraft Inspection and Repair
Federal Aviation Administration · FAA Advisory Circular AC 43.13-1B, with changes
FAA-accepted practices for inspection, repair, structures, hardware, electrical work and systems when applicable.
Open source resourceA&P Technician General Textbook Reference
Jeppesen · A&P Technician General - use the learner's licensed edition and assigned chapter/pages
Course textbook reference for general knowledge topics. AMT-SIM stores citations and study links, not unauthorized textbook reproductions.
Reference this title in the licensed or school-provided copy.
Related Learning
This reference is an AMT-SIM study aid. Use current approved data and instructor guidance for real maintenance.