Airframe Mechanic Certification Cheat Sheet 2026
The 30 highest-yield Airframe Mechanic Certification facts, distilled from real exam questions. Print it, save it as a PDF, or study it here — free, no sign-up.
100 questions
120 min time limit
70% to pass
- During an inspection of a control cable passing over a pulley, a single broken wire is discovered. According to FAA AC 43.13-1B, what action is required? → The entire control cable assembly must be replaced.
- During a walk-around inspection, a pilot notices excessive freeplay in the aileron. As an A&P mechanic, your first action should be to: → Inspect the control system per the AMM to identify the source of freeplay
- What action must be taken when a mechanic discovers a condition that may make an aircraft unairworthy but is not specifically listed in the maintenance manual? → Refer the condition to an IA or repair station for a determination of airworthiness
- What is the purpose of a fire sleeve on aircraft tubing? → Provide fire-resistant protection for fluid-carrying lines
- What is 'stress corrosion cracking' (SCC)? → Cracking resulting from the combined effects of tensile stress and corrosive environment
- A 'pilot hole' in sheet metal work is: → A small-diameter starter hole drilled before final-size drilling
- A mechanic discovers a crack in an aircraft structure that is NOT listed in the approved repair manual. What is the correct course of action? → Obtain an FAA-approved repair data or DER-approved repair before proceeding
- What does EGT (Exhaust Gas Temperature) measure in a turbine engine? → Temperature of exhaust gases at a specified turbine stage
- What does the 'T' designation (such as T3, T4, T6) indicate in aluminum alloy nomenclature? → The temper (heat treatment condition) of the alloy
- When laying out rivet rows, the transverse pitch (row spacing) should be at minimum: → 75% of the rivet pitch within the row
- What type of corrosion forms as a white powdery deposit on aluminum aircraft structures? → Oxidation corrosion
- When assembling a large transport category aircraft's empennage to the fuselage, the horizontal stabilizer incidence is set by: → Shimming or adjusting the rear spar attach point per maintenance manual data
- Which component prevents reverse flow in a hydraulic or pneumatic line? → Check valve
- What type of stress acts perpendicular to the cross-section of a structural member and tends to pull it apart? → Tension
- When performing an inspection using a borescope, what is the primary advantage over direct visual inspection? → It allows internal inspection of areas inaccessible without disassembly
- What is the primary cause of hot section deterioration in a turbine engine? → Thermal cycling and oxidation from extreme combustion temperatures
- When is a logbook entry for an inspection considered complete per 14 CFR Part 43.11? → When the date, aircraft total time, and mechanic signature/certificate number are recorded
- What is the purpose of a fuselage bulkhead? → To carry concentrated loads and maintain fuselage cross-sectional shape
- A fuel control unit (FCU) on a turbine engine primarily schedules fuel flow based on: → Compressor inlet temperature and pressure, throttle position, and RPM
- What color dye is used to identify 100LL aviation gasoline (avgas)? → Blue
- When a technician finds that a turnbuckle in a control cable system is improperly safetied, what is the correct action? → Remove the existing safety wire, verify thread engagement, and re-safety properly
- What is 'corrosion' in the context of aircraft metals? → Electrochemical deterioration of metal by reaction with the environment
- What does 'grain direction' mean when working with aircraft sheet metal? → The direction the metal crystals were aligned during rolling
- What color coding identifies MIL-PRF-5606 hydraulic fluid? → Red
- Which type of load causes a structural member to twist about its longitudinal axis? → Torsional load
- A doubter (doubler) plate installed over a cracked fuselage skin repair serves primarily to: → Restore original strength and stop-drill the crack
- What is the function of a propeller governor? → Maintain a selected RPM by varying propeller pitch
- What condition does a cracked or chafed pitot tube indicate regarding airworthiness? → The pitot tube must be replaced before flight
- Which of the following cable materials is NOT recommended for primary flight control systems due to its susceptibility to corrosion? → Both B and C
- Under 14 CFR Part 91.417, how long must an aircraft owner or operator retain records of inspections and major alterations? → Indefinitely, as part of the permanent aircraft record
Turn these facts into recall:
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