FAA Aviation Mechanic Airframe (AMA) flashcards
289 free flashcards. Tap a card to flip it.
Bourdon Tube Pressure Gauge
Flip cardA pressure-sensing mechanism using a curved, flattened, sealed tube that straightens proportionally to internal pressure, driving a pointer through a gear sector and pinion linkage.
- Common in hydraulic, oil, and pneumatic pressure gauges
- Tube straightens as pressure increases
- Motion transmitted via linkage/gear sector to pointer
Memory trick: Bourdon tube bends back to tell you the pressure trend
True Airspeed (TAS) Correction
Flip cardTAS is CAS corrected for nonstandard density altitude; as altitude increases, air density decreases, so TAS exceeds CAS by roughly 2% per 1,000 feet.
- TAS > CAS at altitude due to lower air density
- Rule of thumb: add ~2% of CAS per 1,000 ft altitude
- Exact values require a flight computer or airspeed correction chart
Memory trick: Thinner air, faster TAS — climb and the gap grows.
Poultice (Crevice) Corrosion
Flip cardCorrosion that occurs when moisture and debris are trapped in a tight crevice, such as a lap joint or under a fitting, forming a localized corrosive cell that can bulge the surrounding structure.
- Occurs in faying surfaces, seams, and under fasteners
- Caused by trapped moisture and contaminants
- Corrosion products expand and can bulge or pillow the skin
- Prevented by proper sealing and drainage
Memory trick: Poultice = like a wet bandage trapped against skin, festering underneath
Eddy Current Inspection
Flip cardA nondestructive inspection method using induced electrical currents to detect surface and near-surface flaws in conductive materials, often without removing paint.
- Works only on electrically conductive materials
- Can detect cracks around fastener holes without disassembly
- Sensitive to material conductivity changes, thickness, and flaws
Memory trick: 'Eddy Currents Swirl Through Paint' — no strip needed for surface cracks.
Fuel Tank Vent System
Flip cardA vent line or valve that allows outside air to enter or leave a fuel tank so internal pressure stays close to ambient pressure.
- Prevents tank collapse from vacuum as fuel is used
- Prevents overpressure as altitude decreases
- Often includes a check valve and vent line routed outboard
Memory trick: Vent lets the tank breathe with the sky.
Wheel Bearing Inspection
Flip cardExamination of landing gear wheel bearings for damage such as spalling, pitting, corrosion, or overheating discoloration during scheduled inspections.
- Bearings must be cleaned and repacked with approved grease
- Spalling/pitting requires rejection
- Bluish discoloration may indicate overheating damage
- Bearings are matched sets and not interchanged with new rollers
Memory trick: Pits and spalls mean the bearing falls (out of service).
Thermocouple Lead Wire
Flip cardLead wire connecting a thermocouple probe to its indicator must be made of the same dissimilar metal alloys as the thermocouple itself to avoid introducing false junctions that alter the generated voltage.
- Thermocouples generate voltage from junction of two dissimilar metals
- Common EGT thermocouple types: chromel-alumel or iron-constantan
- Mismatched lead wire alloys create parasitic junction voltages
- No external power source is needed; thermocouples are self-generating
Memory trick: Match the metals like matching puzzle pieces — mismatched alloys create a false extra junction that lies to the gauge.
Negative Pressure Relief Valve
Flip cardA spring-loaded valve that opens to admit outside air into the cabin when outside pressure exceeds cabin pressure, preventing structural damage from inward pressure loads.
- Opens during rapid descent scenarios
- Prevents fuselage crush from negative differential
- Works opposite to positive pressure relief valve
Memory trick: Negative valve = guards against the cabin getting 'sucked in'
Magnetic Drip Stick
Flip cardA calibrated stick inserted through a tank sump opening that uses a magnetic float to physically indicate fuel quantity, serving as a manual backup to electronic fuel gauges.
- Inserted through a calibrated tank access point
- Magnet engages internal float at fuel surface
- Provides manual cross-check for capacitance systems
Memory trick: 'Drip stick dips down to find where the fuel sits.'
System Relief Valve
Flip cardA pressure-limiting valve set to open at a pressure slightly above normal system operating pressure, protecting components from damage due to overpressure.
- Opens at a preset maximum pressure
- Routes excess fluid back to reservoir
- Distinct from thermal relief valves, which protect isolated segments
Memory trick: Relief valve = the 'pressure cop' that stops things from blowing up.
Thermal Relief Valve
Flip cardA small relief valve installed to protect a length of tubing that can be isolated by shutoff valves on both ends, relieving pressure caused by fluid thermal expansion.
- Protects trapped, isolated fluid segments
- Opens at a lower pressure than the main system relief valve
- Common near landing gear and other valve-isolated sections
Memory trick: Thermal relief = the 'pressure release valve on a soda bottle left in the sun.'
Cabin Pressure Differential
Flip cardThe difference between the pressure inside a pressurized cabin and the ambient pressure outside the aircraft at altitude; it is a critical structural design limit.
- Differential = cabin pressure − outside ambient pressure
- Exceeding max differential can cause structural damage
- Typical transport aircraft max differential is around 8–9 psi
Memory trick: Differential is what's left after subtracting outside from inside.
Electrically Heated Windshield System
Flip cardA windshield anti-ice/anti-fog system using embedded conductive heating film with a temperature sensor and controller to regulate power and prevent overheating.
- Conductive film embedded in laminated windshield
- Controller regulates power based on windshield temperature
- Prevents overheating, cracking, or delamination
Memory trick: Controller = the windshield's thermostat, not its ice-spotter
Torque Link (Scissor) Assembly
Flip cardA hinged linkage connecting the upper strut cylinder to the lower piston, transmitting torque to prevent piston rotation while allowing strut compression/extension.
- Prevents wheel/piston from rotating within the cylinder
- Allows telescoping motion of the shock strut
- Also used to actuate shimmy dampers or steering feedback in some designs
Memory trick: Torque link scissors keep the strut from spinning like a loose bolt
Open-Center Hydraulic System
Flip cardA hydraulic system in which fluid flows continuously from the pump through all selector valves (in series) and back to the reservoir until a valve is actuated to direct flow to a subsystem.
- Selector valves are wired in series
- Pump delivers constant flow, not constant pressure
- Common on older and lighter aircraft with fixed-displacement pumps
Memory trick: Open-center: 'Open road' — fluid keeps cruising until a valve redirects it.
Follow-Up (Feedback) Servo Actuator
Flip cardA hydraulic power control unit in which actuator piston movement is mechanically fed back to reposition the metering valve toward neutral, stopping motion at the commanded position.
- Provides proportional, precise control surface positioning
- Metering valve returns to neutral as actuator reaches commanded position
- Common in transport aircraft primary flight control systems
Memory trick: Follow-up servo 'checks its work' by feeding position back to the valve.
Wing Ice Inspection Light
Flip cardA light fixture aimed at the wing leading edge to allow the flight crew to visually check for ice buildup during night operations.
- Provides illumination only, no heating
- Used on aircraft lacking automatic ice detectors
- Mounted on fuselage or wing to shine on leading edge
Memory trick: 'Ice light just lets the pilot LOOK, not COOK.'
Stress Corrosion Cracking (SCC)
Flip cardCracking caused by the combined action of sustained tensile stress and a corrosive environment on a susceptible metal, propagating perpendicular to the applied stress.
- Requires sustained (static) tensile stress, not cyclic loading
- Common in high-strength steel and aluminum alloys under residual or applied stress
- Cracks propagate transgranularly or intergranularly, often with little visible deformation
Memory trick: 'Stress + corrosion = a silent crack sneaking through.'
Outflow Valve
Flip cardA pneumatically or electrically controlled valve that regulates the rate of air leaving a pressurized cabin to maintain a scheduled cabin altitude.
- Positioned by the cabin pressure controller
- Modulates continuously during flight
- Works with a separate safety relief valve for overpressure protection
Memory trick: Outflow valve is the cabin's exhaust throttle.
Drag Brace (Drag Strut)
Flip cardA structural landing gear member oriented fore-and-aft that absorbs taxi, takeoff, and landing drag loads and transfers them into the airframe.
- Resists fore-and-aft loads
- Works with side brace (lateral loads) and trunnion (pivot)
- Often incorporates a downlock mechanism
- Failure can allow gear to collapse rearward or forward
Memory trick: Drag brace drags the fore-aft load away.
Fretting Corrosion
Flip cardA form of wear corrosion caused by small-amplitude repetitive motion between two tightly fitted surfaces, producing fine oxide debris and surface damage.
- Occurs at hinge points, bolted joints, bearing fits
- Produces reddish-brown powder on aluminum, black on steel
- Can lead to fatigue crack initiation if undetected
Memory trick: Fretting = friction + vibration = fine dust
Spar Web (Box Beam)
Flip cardThe vertical sheet metal member connecting the upper and lower spar caps in a box beam spar, primarily designed to carry shear loads while the caps carry bending loads.
- Spar caps carry tension/compression bending loads.
- Web carries shear loads, similar to an I-beam web.
- Webs are often reinforced with vertical stiffeners to prevent buckling.
Memory trick: Caps = Compression/tension, Web = shear — 'Caps Bend, Web Shears'
Transformer-Rectifier Unit (TRU)
Flip cardA device that steps down AC voltage using a transformer and converts it to DC using rectifier diodes, commonly used in AC-primary electrical systems to supply DC buses and charge the battery.
- Combines a step-down transformer with a rectifier
- Converts 115V AC to 28V DC typically
- Used on aircraft where AC generators are the primary power source
Memory trick: TRU = 'Turn to DC, Reduce voltage, Use it' — transform then rectify.
Lead-Acid Specific Gravity
Flip cardA hydrometer measurement of electrolyte density used to determine the state of charge of a lead-acid battery.
- Fully charged: approx. 1.275–1.300
- Discharged: drops toward 1.150–1.200
- Readings must be corrected for electrolyte temperature
Memory trick: Heavy acid = healthy battery; watery acid = weak battery.
Redundant Wire Bundle Separation
Flip cardA wiring installation practice of physically separating wire bundles for redundant systems so that a single localized fault cannot disable both systems.
- Protects against single-point failures like chafing, fire, or mechanical damage
- Applies to critical/redundant flight control and electrical systems
- Often required by design standards for essential and backup circuits
Memory trick: Never put both parachutes in the same bag — separate redundant bundles.
Torque Wrench Extension Calculation
Flip cardWhen using an extension on a torque wrench, the wrench setting must be adjusted using TW = TA x [L / (L+A)] to compensate for the increased effective lever arm, ensuring the correct final torque is applied to the fastener.
- L = wrench handle length, A = extension length
- TA = desired actual torque at the fastener
- Wrench reading (TW) is set lower than TA when using an extension
Memory trick: Longer arm, lighter reading — extension multiplies force, so dial down the setting
Multiple-Disc Brake
Flip cardA brake assembly using several alternating rotating and stationary discs compressed by hydraulic pistons to create braking friction, common on transport aircraft.
- Rotating discs are splined to the wheel
- Stationary discs are keyed to the torque tube
- Provides greater surface area and heat capacity
- Used on most large jet transport main gear
Memory trick: Many discs, many hands squeezing together = multiple-disc brake.
Self-Locking Nut Temperature Limits
Flip cardSelf-locking nuts use either a fiber insert or an all-metal locking feature to resist loosening from vibration; the type selected depends on the operating temperature of the installation location.
- Fiber-insert (nylon) locknuts limited to about 250°F
- All-metal locknuts suitable for higher temperature areas like engine/exhaust zones
- Both resist nut rotation from vibration but by different mechanisms
- Not used where the nut is expected to be removed and reinstalled excessively without inspection
Memory trick: Fiber melts near fire — use all-metal near heat.
Squat Switch (Weight-on-Wheels Switch)
Flip cardA switch mounted on the landing gear strut that senses strut compression to signal whether the aircraft is on the ground or in the air, used for gear/spoiler interlock logic.
- Senses strut compression from aircraft weight
- Prevents gear retraction while on ground
- Enables systems like spoilers/reversers only when confirmed on ground
Memory trick: Squat down = strut compresses = switch says 'we're on the ground'
Rectifier
Flip cardA device, typically using diodes, that converts alternating current (AC) into direct current (DC) in an aircraft alternator system.
- Uses diodes that allow current flow in only one direction
- Found in brushless AC alternator systems
- Different from an inverter, which converts DC to AC
Memory trick: Rectifier = one-way valve for electrons
Y-Connected Three-Phase Voltage
Flip cardIn a wye (Y) connected three-phase AC system, line voltage equals phase voltage times the square root of 3 (approximately 1.732).
- Line voltage = Phase voltage × 1.732
- Y connection provides both line and phase voltage access via neutral
- Common in aircraft brushless AC alternators
Memory trick: Y-connection: multiply phase voltage by 1.732 to get the line voltage.
Electrothermal Propeller Deicing
Flip cardA system using electrical heating elements on propeller blades, cycled by a timer to shed ice in sections while limiting electrical power demand.
- Heating elements bonded to blade leading edges
- Timer cycles power to limit electrical load
- Centrifugal force helps throw off loosened ice
Memory trick: Cycle to save power, spin to shed the ice
Fuel Filter/Water Separator
Flip cardA component installed in the fuel system that removes water and solid contaminants from fuel before it reaches the engine.
- Has a drainable sump for removing collected water
- Prevents ice formation and pump/injector damage
- Should be drained regularly per maintenance schedule
Memory trick: Filter/separator is the fuel system's water trap.
Landing Gear Retraction Sequence
Flip cardThe proper order of switch actuation and mechanical events during gear retraction, verified during a functional/rigging check: weight off wheels, downlock release, gear retraction, and uplock engagement.
- Squat switch must sense weight-off-wheels before retraction
- Downlocks must release before gear can move
- Gear retracts into wheel well after downlock release
- Uplocks secure gear up and extinguish position light
Memory trick: Weight off, lock off, gear goes, lock on.
Kollsman Window / Pressure Altitude
Flip cardThe altimeter setting window; setting it to 29.92 in Hg standard pressure causes the altimeter to indicate pressure altitude, used above 18,000 ft MSL.
- 29.92 in Hg is standard sea-level pressure
- Used above 18,000 ft MSL for common altitude reference
- Local altimeter setting is used below 18,000 ft MSL
Memory trick: 29.92 = the standard 'reset button' above 18,000 feet
Pump Unloading Valve
Flip cardA pressure control valve used with fixed-displacement pumps that diverts pump output to the reservoir at low resistance once system pressure reaches the cutout setting.
- Used with constant-delivery pumps
- Cutout: diverts flow to reservoir at set high pressure
- Cut-in: restores normal delivery at a lower set pressure
Memory trick: Unloading valve = pump treadmill, spins free once it's 'full.'
Variable Displacement Pump
Flip cardAn engine-driven hydraulic pump that automatically varies piston stroke to match system demand while maintaining constant pressure.
- Self-regulates output without external relief valve
- Contrasts with fixed displacement pumps needing a separate pressure regulator
- Common on large transport aircraft hydraulic systems
Memory trick: Variable pump breathes in and out with demand.
Maintenance Record Retention (91.417)
Flip card14 CFR 91.417 specifies retention periods for aircraft maintenance records, distinguishing between routine maintenance/AD compliance records and permanent records like total airframe time.
- AD compliance/routine maintenance records: 1 year or until superseded/repeated
- Total time in service, major repairs/alterations, life-limited parts status: retained for life of the airframe
- Records must be transferred with the aircraft upon sale
Memory trick: 'One year, unless it's forever' — routine vs permanent records
Radiographic (X-ray) Inspection
Flip cardAn NDT method that passes penetrating radiation through a part to produce an image revealing internal flaws, voids, or corrosion without disassembly.
- Uses X-ray or gamma radiation and film or digital detector
- Effective for internal defects in honeycomb, bonded, and thick structures
- Requires strict radiation safety controls and trained/certified personnel
Memory trick: 'X-ray sees through the skin like looking through a wall.'
Cable Tension Rigging
Flip cardProcess of adjusting flight control cable tension to manufacturer specifications using a tensiometer, accounting for ambient temperature.
- Tensiometer measures cable tension in pounds
- Rigging charts list correct tension per temperature
- Improper tension causes control stiffness or slack
Memory trick: Hot day, loose cable — temperature sets the tension target
Pitting Corrosion
Flip cardLocalized corrosion that forms small cavities or pits on a metal surface due to a breakdown of the protective oxide layer, often leaving powdery deposits.
- Appears as isolated small holes/cavities
- Common starting point for stress corrosion cracking
- Caused by moisture, salt, or chemical exposure
- Detected visually or with a fine probe/depth gauge
Memory trick: Pitting = pockmarks, like tiny craters on the moon.
Honeycomb Panel Moisture (Pillowing)
Flip cardA bulging pattern in the outer skin of a honeycomb sandwich panel caused by trapped moisture expanding within the core cells.
- Visible as a 'pillowing' or quilted pattern matching the cell pattern
- Detected/confirmed with a coin tap test or moisture meter
- Can lead to core degradation, disbonding, and freeze-thaw damage
Memory trick: 'Pillowing = the core is soaked and puffing up like a pillow.'
Pressurized Reservoir
Flip cardA hydraulic reservoir supplied with bleed air or system pressure to maintain positive pressure at the pump inlet.
- Prevents pump cavitation at altitude
- Uses bleed air or system pressure
- Common on transport category aircraft
Memory trick: Push fluid to the pump so it never runs dry — pressurize!
Pneumatic Deicer Boot Distributor Valve
Flip cardA timed valve in a pneumatic deicing system that directs pressurized air sequentially to different sections of rubber boots to inflate and deflate them, breaking off ice.
- Powered typically by an engine-driven vacuum/pressure pump
- Boots inflate in a specific sequence to avoid ice bridging
- Deflated by vacuum between cycles for aerodynamic smoothness
Memory trick: Distributor valve is the boot system's traffic cop.
Acceleration/Deceleration Error (ANDS)
Flip cardA magnetic compass error occurring on east/west headings in which acceleration causes an apparent turn toward north and deceleration causes an apparent turn toward south, due to compass card pendulosity and magnetic dip.
- ANDS = Accelerate North, Decelerate South
- Error is most pronounced on east/west headings
- No error occurs on north/south headings during acceleration
- Caused by pendulous mounting of the compass card combined with vertical dip component
Memory trick: ANDS: Accelerate North, Decelerate South — remember it like a compass speeding north when you step on the gas.
Deicing Boot Distributor Valve
Flip cardA timer-driven valve in a pneumatic deicing system that sequences bleed air pressure and vacuum to inflatable boot tube sections to shed ice.
- Creates the alternating inflate/deflate cycle
- Works with an ejector for vacuum during deflation
- Powered by engine bleed air pressure for inflation
Memory trick: Distributor 'deals the cards' of air to each boot section in order
Windshield Anti-Ice Fluid System
Flip cardA system that sprays isopropyl alcohol-based fluid onto the windshield to prevent ice and frost formation by lowering the freezing point of surface moisture.
- Uses alcohol-based fluid, often isopropyl alcohol
- Fluid is pumped from a reservoir to spray bars at the windshield base
- Alternative to electric or bleed-air heated windshields
Memory trick: Alcohol lowers the freeze point, like antifreeze on glass.
Structural Repair Manual (SRM)
Flip cardA manufacturer-published document providing approved data on allowable damage limits, repair procedures, and materials for aircraft structure.
- Provides blend-out and allowable damage limits
- Used to determine if damage is repairable or requires replacement
- Considered approved data for repairs when followed exactly
- Specific to aircraft make/model
Memory trick: SRM = 'Skin Repair Menu' — the recipe book for fixing dents
Truss-Type Fuselage
Flip cardA fuselage structure built from welded steel tubing arranged in triangular (truss) patterns that carries all structural loads, with the covering providing shape only.
- Triangular tubing arrangement resists loads efficiently
- Common on early and light fabric-covered aircraft
- Covering (fabric/sheet) is non-structural
- Also called a Pratt or Warren truss configuration
Memory trick: Triangles in tubing = truss taking the tension.
Pressure Reducer (Reducing) Valve
Flip cardA hydraulic valve that reduces main system pressure to a lower, regulated value for a subsystem such as wheel brakes.
- Protects lower-pressure-rated components
- Different function from priority valve (flow priority)
- Maintains constant reduced outlet pressure despite main system fluctuations
Memory trick: Reducer valve = a pressure 'step-down transformer' for brakes.
Nomex Honeycomb Core
Flip cardA lightweight sandwich panel core material made of aramid fiber paper dipped in phenolic resin, valued for corrosion resistance, moisture resistance, and good strength-to-weight ratio compared to aluminum honeycomb.
- Does not corrode like aluminum honeycomb when exposed to moisture.
- Lighter than aluminum honeycomb of similar strength.
- Common in aircraft interior panels, fairings, and control surfaces.
Memory trick: Nomex = 'No More' corrosion in moist conditions
Trip-Free Circuit Breaker
Flip cardA circuit breaker designed to open an overloaded circuit automatically regardless of the position of the operating control.
- Cannot be held closed by the switch during an overload
- Protects wiring from overheating even if crew tries to override it
- Required by 14 CFR for most aircraft circuit protection devices
Memory trick: 'Trip-Free' Frees the circuit even if you fight it
Airspeed Indicator Color Markings
Flip cardStandardized colored arcs and lines on an airspeed indicator denote specific operating speed ranges and limits for safe aircraft operation.
- White arc = flap operating range (Vso to Vfe)
- Green arc = normal operating range (Vs1 to Vno)
- Yellow arc = caution range; red line = Vne (never exceed)
Memory trick: White for wings with flaps down.
Tubeless Tire
Flip cardAn aircraft tire that seals air directly against the wheel rim without using an inner tube.
- Bead seats against rim to form airtight seal
- Lighter and runs cooler than tube-type tires
- Damaged bead or rim can cause leaks
Memory trick: Tubeless = trust the bead, not a tube
Ram Air Emergency Ventilation Valve
Flip cardA backup valve that opens to admit ram air into the cabin for ventilation when the normal pressurization system fails, interlocked to open only at low differential pressure and airspeed.
- Provides emergency ventilation, not full pressurization
- Interlocked with pressure differential and airspeed sensors
- Typically used at lower altitudes where cabin/ambient pressure difference is small
Memory trick: Ram air only opens when it's safe—low pressure, low speed.
Accumulator Precharge Ratio
Flip cardAccumulators are typically precharged with nitrogen to about one-third of the hydraulic system's rated operating pressure.
- Precharge ≈ system pressure ÷ 3
- Too low precharge causes piston to bottom out
- Too high precharge reduces fluid storage capacity
Memory trick: Divide by three to find the nitrogen key.
Hydraulic Fluid Color Coding
Flip cardAircraft hydraulic fluids are dyed distinct colors to help identify fluid type and prevent accidental mixing of incompatible fluids.
- MIL-PRF-5606 mineral-base fluid is red
- Phosphate ester fire-resistant fluid (e.g., Skydrol) is purple
- Never mix fluid types—incompatible seals and chemistry
Memory trick: Purple = phosphate; Red = regular (mineral) fluid
Flux Valve (Flux Gate)
Flip cardA magnetic heading sensor, usually mounted in a wingtip or tail away from magnetic interference, that electrically transmits heading information to remote cockpit indicators via a synchro system.
- Mounted away from magnetic interference sources
- Sends signal through a synchro/autosyn transmission system
- Feeds remote indicators such as RMI, HSI, and autopilot heading systems
Memory trick: Flux valve is the wingtip 'compass spy' radioing heading data to the cockpit
Piccolo Tube Wing Anti-Ice
Flip cardA perforated tube running inside a wing leading edge that distributes hot engine bleed air along its length to prevent ice formation.
- Uses engine bleed air, not electric heat
- Perforations spray hot air against the inner leading edge skin
- Common on transport category turbine aircraft
Memory trick: Piccolo tube plays a tune of hot air along the wing.
Anti-Skid Braking System
Flip cardA system that automatically modulates brake pressure to individual wheels to prevent skidding during heavy braking.
- Uses wheel-speed transducers to detect impending skid
- Releases brake pressure momentarily to restore rolling traction
- Improves stopping distance especially on wet/icy runways
Memory trick: Anti-skid pumps the brakes for you, like ABS in a car