โ† All AMT Flashcard Decks

Airframe Systems & Components Flashcards

7 cards from real AMT practice questions. Tap to flip, then mark Knew It or Still Learning โ€” missed cards come back until you master them.

Read the first 7 Airframe Systems & Components flashcards as text
  1. In a pressurized aircraft fuselage, the structure must be designed to withstand which primary stress?

    Answer: Tensile hoop stress

    Internal pressurization creates tensile hoop stress that attempts to expand the fuselage diameter, requiring the skin to resist being pulled apart.

  2. What is the purpose of a bleed air system on a turbine-powered aircraft?

    Answer: To supply hot compressed air from the engine for cabin pressurization and anti-ice

    Bleed air is extracted from engine compressor stages and used for cabin pressurization, air conditioning, anti-icing, and pneumatic systems.

  3. Which rivet is most appropriate for use in areas that are accessible from one side only?

    Answer: Cherry (blind) rivet

    Blind rivets, such as Cherry rivets, are designed to be installed from one side when the back side is inaccessible.

  4. A semi-monocoque fuselage structure derives most of its strength from:

    Answer: A combination of skin, stringers, frames, and bulkheads working together

    Semi-monocoque construction shares loads between the stressed skin and the internal framework of stringers, frames, and bulkheads.

  5. What does a negative dihedral (anhedral) wing configuration primarily provide?

    Answer: Decreased lateral stability for improved maneuverability

    Anhedral reduces the natural lateral stability (dihedral effect), which is desirable in highly maneuverable or swept-wing high-speed aircraft.

  6. When must a Required Inspection Item (RII) on an air carrier aircraft be re-inspected?

    Answer: When the item was not inspected by an authorized inspector or was found defective and repaired

    An RII must be reinspected if it was not properly inspected by an authorized RII inspector or if it was found defective and subsequently repaired.

  7. What is the purpose of a bonding jumper on an aircraft fuel system component?

    Answer: To provide an electrical ground path that prevents static charge buildup

    Bonding jumpers provide a continuous electrical path to dissipate static electricity, preventing sparks that could ignite fuel vapors.