The AMOC Block 4 Test assesses knowledge on aircraft electrical systems, focusing on measuring current, conductivity, and the function of components such as relays and generators. It's designed for professionals enhancing their understanding of typical and emergency power systems in aircraft.
Silver
Gold
Copper
Boron
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Current varying switch
Multiple position switch
Electrically operated mechanical switch
Fuse that withstands large current flow for short time
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115/200 VAC, four-phase, 400 hertz
115/220 VAC, three-phase, 400 hertz
115/200 VAC, three-phase, 800 hertz
115/200 VAC, three-phase, 400 hertz
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Aircraft battery
Transformer Rectifiers
Generator Control Unit
DC Bus Bars
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Hydraulic Motor
Auxiliary Power Unit (APU)
Air Turbine Motor (ATM)
Emergency Activation Unit (EAU)
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Transformer Rectifier
Inverter
Emergency Generator
Integrated Drive Generator (IDG)
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In-flight inspection lights
Exterior lights
Navigation / Position lights
Formation lights
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Size, Material, Radar Range, Reflection angle
Size, Material, Radar Power, Reflection angle
Size, Material, Radar Range, Refraction angle
Size, Material, Radar Range, Reflection arc
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Pulse Repetition Frequency (PRF), Pulse Width (PW), Pulse Depth (PD)
Pulse Reception Frequency (PRF), Pulse Width (PW), Pulse Duration (PD)
Pulse Repetition Frequency (PRF), Pulse Width (PW), Pulse Duration (PD)
Pulse Repetition Frequency (PRF), Pulse Girth (PG), Pulse Duration (PD)
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Active Electronically Scanned Array (AESA)
Phased Array
Parabolic Antenna
Duplexer
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Pulsed-Doppler Radar
Millimeter Wave Radar (MMW)
Synthetic Aperture Radar (SAR)
Radar Altimeter
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Radar altimeter
Rendezvous beacon
Terrain Avoidance
Terrain Following
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Reconnaissance and Surveillance
Search and Rescue
Ground Mapping
Weapons Implementation
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Visual
Dead Reckoning
Radio
Radar
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Heading
Course
Angle of attack
Bearing
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Target Point
Fixed Point
Initial Point
Offset Aim Point
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Automatic Direction Finding (ADF)
VHF omni-directional Range (VOR)
Tactical Air Navigation (TACAN)
Distance Measuring Equipment (DME)
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Instrument Landing System
Microwave Landing System
Global Position System
Pilot Landing System
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1
2
3
4
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Traffic Alert and Collision Avoidance System (TCAS) II
Enhanced Ground Proximity Warning System
Offensive Avionics Systems
Ground Proximity Warning System
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100
200
300
400
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1-10 MHz
2-30 MHz
3-30 MHz
4-40 MHz
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20-200 MHz
30-300 MHz
40-400 MHz
50-500 MHz
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Station Keeping Equipment
AFSATCOM
Have Quick
Interphone Systems
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Interphone System and Global Positioning System
Multifunctional Information Distribution System and Radio Systems
Joint Tactical Information Distribution System and Radio Navigation System
Joint Tactical Information Distribution System and Multifunctional Information Distribution System
Station Keeping Equipment
Navigation System
Interphone Systems
Transmitting Homing Signal
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20 min
30 min
40 min
2 hrs
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Electronic support
Electronic countermeasures
Electronic attack
Electronic protection
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Evasion/avoidance
Deception/confusion devices
Radar jamming
Destruction
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Chaff
Flare
Decoys
DIRCM
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Spot, swept spot, total
Total, spot, focused
Barrage, spot, swept spot
Barrage, focused, spot
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LO technology
Modern technology
Stealth technology
RAM technology
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Combination Unit
Pressure Relief Valve
Cabin Pressure Regulator
Power Control and Distribution Unit
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Prevents over pressure
Prevents excessive cabin pressure
Prevents excessive negative pressure
Transfers emergency air to backup air in the event of a primary power loss
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COMBAT EDGE
Fighter Canopy Seals
Hydraulic Control Unit
Hydraulic Pressure Unit
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Heat Exchanger
Pressurization System
Cabin Pressure Regulator
Aircraft Instrument System
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Isobaric range
Isotonic range
Himalayan range
Differential range
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Blast valve
Dump valve
Manifold Shutoff Valve
Emergency Shutoff Valve
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OBOGS
COBRA JUDGY
COMBAT EDGE
STRYKER TRIDENT
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Pitot / Static System
Central Air Data Computer (CADC)
Gyroscopic Flight Instruments
Attitude Indicator
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Rate of Turn Indicator
Altitude Indicator
Airspeed Indicator
Vertical Velocity Indicator (VII)
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Indicated Airspeed
True Airspeed Indicator
Groundspeed
Maximum Allowable Airspeed Indicator
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Rotation Go-Around Subsystem
Flight Director System
Central Air Data Computer (CADC)
Navigation Instruments
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Attitude Indicator (AI)
Altitude Director Indicator (ADI)
Attitude Heading Reference System (AHRS)
Flight Director System
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Pitch and bank steering bars
Attitude Director Indicator (ADI)
Turn and slip indicator
Rate of turn indicator
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Head Up Display (HUD)
Horizontal Situation Indicator (HSI)
Attitude Heading Reference System (AHRS)
Radio Magnetic Indicator (RMI)
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Flight Director System
Stall Warning System
Vertical Tape Indicators
Multi-Functional Displays (MFD's)
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Stealth, LO (Low Observable)
Low Light Level TV, Steerable TV Set
LANTIRN, Litening II/ER/AT
SAS, AILS
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