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Cheat sheet

FAA A&P Cheat Sheet

General

23%of exam

Airframe

38%of exam

StructuresControlsHydraulicsLanding GearProtection

Powerplant

38%of exam

EnginesFuel IgnitionLubricationPropellersEngine Inspection

Quick Facts

Tests
AMG, AMA, AMP
Questions
260 listed
AMG
60 questions
AMA
100 questions
AMP
100 questions
Time
2 hours each
Pass
70% each
Vendor
PSI
Standard
Mechanic ACS

Three Tests

G first, then A and P

AMG: 60AMA: 100AMP: 100All: 70%

AMG vs AMA/AMP

AMG

  • General base
  • 60 listed
  • Both ratings use

AMA/AMP

  • Rating specific
  • 100 listed each
  • Separate AKTRs

Base vs rating

Authorization Picker

  1. Need identityFTN(IACRA)
  2. Experience path8610-2(FAA signed)
  3. School pathAMTS document
  4. Military pathCOE(Authorized tests)
  5. Failed testAKTR(Retake proof)
  6. O&P readyDME(After writtens)

Test Logistics

AMG
General knowledge
AMA
Airframe knowledge
AMP
Powerplant knowledge
FTN
FAA tracking number
AKTR
Knowledge test report
DME
Oral practical examiner
PSI
Testing vendor
Validation
Unscored possible items

Ohm Law

E over I times R

E = I x RI = E/RR = E/I

Approved vs Acceptable

Approved

  • FAA accepted
  • Needed for majors
  • Return support

Acceptable

  • Useful reference
  • May need approval
  • Not always enough

Authority matters

Record Picker

  1. Major repairForm 337
  2. Major alterationForm 337
  3. Routine maintenanceLog entry
  4. AD appliesCompliance record
  5. Return to serviceSignature entry
  6. Unknown methodApproved data

Eligibility

Age
18 minimum
English
Read write speak
One rating
18 months
Both ratings
30 months concurrent
AMTS
147 school path
JSAMTCC
Military pathway
8610-2
Mechanic application
Retest
30 days or endorsement

W&B Math

Weight times arm makes moment

Moment: W x ACG: moment/weightArm: distance

AD vs SB

AD

  • Mandatory
  • FAA rule
  • Track recurrence

SB

  • Manufacturer issued
  • Normally advisory
  • Can support data

Required vs recommended

Electricity

Current
Electron movement
Voltage
Electrical pressure
Resistance
Current opposition
Ohm
E = I x R
Power
P = E x I
Series R
Adds directly
Parallel R
Total decreases
Voltmeter
Connect parallel
Ammeter
Connect series
AWG
Lower is larger

Weight Balance

Datum
Reference plane
Arm
Distance from datum
Moment
Weight x arm
CG
Total moment/weight
Forward CG
More nose down
Aft CG
Less stability
Tare
Deduct container weight
Ballast
Correct CG location

Records Data

Part 43
Maintenance rules
Part 65
Mechanic certification
Part 91
Owner inspection duties
AD
Mandatory compliance
SB
Manufacturer recommendation
337
Major alteration/repair
Approved data
Acceptable for approval
Log entry
Work return record

Materials Corrosion

Alclad
Pure aluminum coating
Galvanic
Dissimilar metals
Pitting
Small deep cavities
Intergranular
Grain boundary attack
Filiform
Under paint tracks
Exfoliation
Layered lifting
Passivation
Protective oxide
Torque
Specified tightening

Control Axis

Aileron roll, elevator pitch, rudder yaw

Aileron: rollElevator: pitchRudder: yaw

Deicing vs Anti-Icing

Deicing

  • Removes ice
  • Cycles after buildup
  • Boots common

Anti-icing

  • Prevents ice
  • Before accumulation
  • Heat/fluid common

Remove vs prevent

Airframe Troubleshooter

  1. Heavy controlsRigging check
  2. Loose controlsFreeplay limits
  3. Soft brakesBleed system
  4. Gear unsafeSwitches/locks
  5. Low pressurePump/relief check
  6. Ice concernAnti/deice system

Structures

Monocoque
Skin carries loads
Semimonocoque
Skin plus frame
Longeron
Lengthwise member
Stringer
Stiffens skin
Bulkhead
Fuselage frame
Spar
Primary wing beam
Rib
Airfoil shape
Doubler
Reinforcement patch
Edge distance
Hole margin
Rivet pitch
Fastener spacing

Hydraulic vs Pneumatic

Hydraulic

  • Liquid power
  • Incompressible
  • High force

Pneumatic

  • Air power
  • Compressible
  • Lower weight

Fluid vs air

Controls Rigging

Aileron
Roll control
Elevator
Pitch control
Rudder
Yaw control
Trim tab
Control force relief
Cable tension
Use tension chart
Turnbuckle
Cable adjustment
Control stop
Travel limiter
Flutter
Destructive oscillation

Airframe Systems

Hydraulic
Incompressible fluid power
Pneumatic
Compressed air power
Accumulator
Stores pressure
Relief valve
Limits pressure
Selector valve
Routes flow
Oleo strut
Shock absorption
Anti-skid
Prevents wheel lock
Bleed air
Engine compressor air

Protection Avionics

Pitot
Impact pressure
Static
Ambient pressure
Altimeter
Static pressure
Airspeed
Pitot plus static
ELT
Emergency transmitter
Position lights
Navigation lights
Fire detection
Heat sensing
Deicing
Remove ice
Anti-icing
Prevent ice

Four Stroke

Suck squeeze bang blow

IntakeCompressionPowerExhaust

Detonation vs Preignition

Detonation

  • Explosive burn
  • After spark
  • Pressure spike

Preignition

  • Early ignition
  • Hot spot
  • Before spark

Explosion vs early fire

Powerplant Troubleshooter

  1. Rough mag checkIgnition system
  2. High CHTCooling/mixture
  3. High EGTMixture/induction
  4. Low oil pressureOil system
  5. Poor accelerationFuel metering
  6. Vibration after propTrack/balance

Engine Basics

Intake
Charge enters
Compression
Charge squeezed
Power
Combustion drives piston
Exhaust
Gases leave
Detonation
Explosive combustion
Preignition
Early ignition source
EGT
Exhaust gas temperature
CHT
Cylinder head temperature
Turbine
Continuous combustion
Compressor
Raises air pressure

Fixed vs Constant Speed

Fixed pitch

  • Angle fixed
  • RPM varies
  • Simple prop

Constant speed

  • Governor controlled
  • RPM selected
  • Blade angle varies

Fixed angle vs governed

Fuel Ignition

Carburetor
Venturi fuel metering
Mixture
Fuel/air ratio
Idle cutoff
Stops fuel flow
Vapor lock
Fuel vapor blockage
Carb ice
Venturi temperature drop
Magneto
Self-contained ignition
E-gap
Magneto timing point
Impulse coupling
Starting spark boost
Spark plug
Ignites mixture
Hot start
Vapor-rich condition

Lubrication Propellers

Wet sump
Oil in engine
Dry sump
Separate oil tank
Scavenge pump
Returns oil
Pressure pump
Supplies bearings
Oil cooler
Removes heat
Governor
Controls blade angle
Fixed pitch
Blade angle fixed
Constant speed
Maintains selected RPM
Feather
Minimum drag angle
Blade track
Tip path check

Engine Inspection

Compression test
Cylinder sealing
Borescope
Internal visual
Oil screen
Metal evidence
Hot section
Turbine inspection area
FOD
Foreign object damage
TBO
Overhaul interval
Run-up
Operational check
Leak check
Fluid escape check

Common Traps

One test myth

Three separate AKTRs No combined score

FTN vs authorization

FTN identifies you 8610-2 authorizes path

Validation questions

May appear Not scored

AD vs SB

AD is mandatory SB usually advisory

Series vs parallel

Series resistance adds Parallel resistance drops

Deice vs anti-ice

Deice removes ice Anti-ice prevents ice

Detonation vs preignition

Detonation after spark Preignition before spark

Major vs minor

Major needs approval Minor needs entry

Last Minute

  1. 1.AMG 60; AMA/AMP 100 each
  2. 2.Each test: 2 hours
  3. 3.Each test: 70% pass
  4. 4.FTN first; PSI schedules
  5. 5.Keep every AKTR
  6. 6.O&P follows passed writtens
  7. 7.AD mandatory; SB usually advisory
  8. 8.Major work needs approved data
  9. 9.Moment = weight x arm
  10. 10.Series adds; parallel drops
  11. 11.Hydraulic liquid; pneumatic air
  12. 12.Detonation after; preignition before
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