Aviation Mechanic - General, Airframe, and Powerplant › I. General › Task I. Regulations, Maintenance Forms, Records, and Publications

AM.I.I.R5

Risk management

Determination of component applicability to a given aircraft.

Practice questions Ask the tutor

Study note

Get a short, cited explanation of this element written from the FAA handbooks: the core idea, the numbers that matter, common test traps, and a quick self-check.

From the FAA library

Aviation Maintenance Technician Handbook - Airframe p. 9-32
Chapter 9: Aircraft Electrical System › DC Generators & Controls › DC Generator Maintenance
systems. These procedures are for familiarization only. Always follow the applicable manufacturer’s instructions for a given generator system. In general, the inspection of the generator installed in the aircraft should include the following items: 1. Security of generator mounting ... contact with the commutator bars. The degree of such sparking should be determined. Excessive wear warrants a detailed inspection and possible replacement of various components. [Figure 9-52] Manufacturers usually recommend the following procedures to seat brushes that…
Aviation Maintenance Technician Handbook - Powerplant p. 4-13
Chapter 4: Engine Ignition & Electrical Systems › Types of DC Generators › DC Generator Maintenance
systems. These procedures are for familiarization only. Always follow the applicable manufacturer’s instructions for a given generator system. In general, the inspection of the generator installed in the aircraft should include the following items: 1. Security of generator mounting ... contact with the commutator bars. The degree of such sparking should be determined. Excessive wear warrants a detailed inspection and possible replacement of various components. [Figure 4-24] Manufacturers usually recommend the following procedures to seat brushes that…
14 CFR Part 91 — General Operating and Flight Rules Open
14 CFR § 91.1065 Initial and recurrent pilot testing requirements.
aircraft to be flown by the pilot, the aircraft powerplant, major components and systems, major appliances, performance and operating limitations, standard and emergency operating procedures, and the contents of the accepted operating manual or equivalent, as applicable; (3) For each ... type of aircraft to be flown by the pilot, the method of determining compliance with weight and balance limitations for takeoff, landing and en route operations; (4) Navigation and use of air navigation aids appropriate to the operation or pilot…