This quiz assesses knowledge on jet fuel systems, focusing on fuel types, handling, and engine control mechanisms. It is crucial for understanding safe aircraft operation and maintenance, targeting skills in aerospace and mechanical engineering.
Aeration
Induction
Convestion
Compression
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Flameout
Turbine seizure
Overtemp
Compressor shift
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Gasoline and kerosene
Diesel fuel and kerosene
Diesel fuel and AV gas
Gasoline and diesel fuel
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Mec
Pmg
Deec
Tsfc
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Nondestructive
Spray pattern
Pre-torque
Ultrasonic
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Wear metals
Friction metals
Precious metals
Transformation metals
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Static
Electronics
Mutual induction
Electromagnetic induction
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Piston type starter
Pneumatic type starter
Small gas turbine engine
Cartridge pneumatic starter
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Through the heat exchanger
Out the turbine case bleed holes
Into the gas stream to exit the engine
Back to the compressor to be used again
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Pneumatic
Fuel injection
Hydromechanical
Hydroelectromechanical
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Replaced
Dye marked
Safety sealed or lockwired
Apply a thread locking compound
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Check
Relief
Bypass
Pressurizing
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Secondary fan airflow as a coolant
Secondary fan airflow as an oil heater
Primary core engine airflow as a coolant
Primary core engine airflow as an oil heater
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N2 sensor
P&D valve
Fuel nozzle
Fan inlet sensor
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Air
Fuel
Hydraulic
Pneumatic
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Air pressure
Spring pressure
Oil pressure
Hydraulic pressure
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Aeration
Deaeration
Check vavle
Bypass valve
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Only primary fuel flow passages
Only secondary fuel flow passages
Both primary and secondary fuel flow passages
Primary, secondary, and auxiliary fuel flow passages
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Airplane 28 VDC power supply
NIU
MIL-STD-1553B data bus
Mission computer
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Fuel pump
Fuel pump controller
Signature elimination probe
DEEC
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3 gear 1 boost
2 gear 2 boost
2 gear 1 boost
1 gear 2 boost
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Oil relief valve
Filter bypass valve
Filter poppet valve
Oil pressure transmitter tap
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1
2
3
4
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Brushes
Commutator
Rotating loop
Permanent magnet
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Ring-cowl
C-D duct
Fan inlet guide vane flaps
Variable exhaust nozzle flaps
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Shutoff valve
Oil pump and filter
Oil pump check valve
Oil pump bypass valve
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Turbine
Augmentor
Combustion
Compressor
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1
2
4
5
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Project monitor
Logistics commander
Propulsion flight chief
Laboratory supervisor
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Choo choo
An explosion
Popping corn
Severe tearing of metal
Wet sump
Dry sump
Hot tank
Cold tank
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Fuel pump
Oil heat exchanger
Air fuel exchanger
PMC
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Toxcicity
Viscosity
Alkalinity
Corrosiveness
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Brushes
Slip rings
Commutator
Permanent magnet
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NIU
FPMU
LVIT
FADEC
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They retract into the engine mount strut
They are stored behind each engine in the wing
They form the inner exhaust cone during forward thrust operation
They retract around the engine exhaust cone, usually forming the rear section of the engine nacelle
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7th
10th
13th
14th
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0%
10%
20%
30%
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Thermostat
Flap actuator
Size of the core
Regulating valve
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Sight gauge on the oil tank
Flight station oil level gauge
Filler cap with a graduated gauge
Graduated marking on the outside of the tank
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Samples must be sent off-site for analysis
Particles must be free of oil for analysis to take place
Provides results concerning equipment and components condition
Samples can only be obtained in an intermediate maintenance shop
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ESS PTO
Engine PTO
Hydraulic motor
Electric motor mounted on the aircraft
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Ground start
Speed sensitive
Fuel enrichment
Secondary fuel pump pressure
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TD valve
Speed sensitive control
TD potentiometers
TD amplifier
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Four speed switch
Electrical power
Hydraulic decoupler
50 percent engine cutout switch assembly
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Fuel control
Fuel spray bars
Fuel manifolds
Fuel/oil cooler
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Torch igniter and hot streak
Hot streak and fuel injection
Pilot burner ring and hot streak
Torch igniter and pilot burner
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Improved safety
Increased component life
Reduced maintenance cost
Increased equipment availability
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Quiz Review Timeline (Updated): Jan 16, 2023 +
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