EOC 2A651 All Volumes Together!
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EOC most missed questions.
- 1.Which TO covers information concerning the Air Force TO system?
- A.
00-5-1
- B.
00-5-2
- C.
00-20-1
- D.
00-20-2
- 2.What are the type(s) of view(s) available with the rigid borescope?
- A.
Direct
- B.
Axisymetrical
- C.
Direct and lateral
- D.
60 degrees up and 180 degrees down
- 3.The Fluke 8025A multimeter control that is used to set the meter to check for AC and DC is the
- A.
Function selector
- B.
Range-mode pushbutton switch
- C.
Touch-hold pushbutton switch
- D.
Volts,ohms,diode test input jack
- 4.You adjust a micrometer by turning the
- A.
Barrel
- B.
Frame
- C.
Spindle
- D.
Thimble
- 5.What directs the gases onto the first-stage turbine wheel blades in a jet engine?
- A.
Flameholder
- B.
Combustion chamber
- C.
Turbine wheel blades
- D.
Turbine stator
- 6.In a dual-spool compressor, rpm o the N2 compressor are determined by the
- A.
Starter
- B.
Fuel pump
- C.
Fuel control
- D.
Low-pressure turbine
- 7.On the T56 turboprop engine, which compressor section assmebly disperses compressor discharge air and directs it to the combustion chambers?
- A.
Diffuser
- B.
Compressor rotor
- C.
Compressor housing
- D.
Compressor air inlet housing
- 8.The amount of twisting deflection is determined by the
- A.
Torque shaft
- B.
Reference shaft
- C.
Safety coupling
- D.
Pinion input gear
- 9.Which T56 compressor component supports the compressor rear bearing labyrinth seal?
- A.
Compressor rotor
- B.
Air inlet housing
- C.
Compressor diffuser
- D.
First-stage compressor wheel hub
- 10.What are used to retain the turbine buckets in the first-stage wheel of the T56-A-15
- A.
Cotter pins
- B.
Curvic splines
- C.
Cover plate seals
- D.
Anti-rotation pins
- 11.On the AE2100D3, the forward engine mounts are located on the
- A.
Air inlet housing
- B.
Diffuser assembly
- C.
Sides of the PGB
- D.
Aft side of the PGB
- 12.What components mount on the front face of the AGB on the T700 engine?
- A.
Alternator and oil cooler
- B.
Scavenge pump and oil cooler
- C.
Alternator and fuel boost pump
- D.
Scavenge pump and fuel boost pump
- 13.Primary airflow in the F108 engine is through all of the following components except the
- A.
Booster
- B.
Core engine
- C.
Accessory gearbox
- D.
Low-pressure turbine
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