2A651H EOC Pretest 1
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- 1.Which functions form a maintenance group?
- A.
Operations, aircraft maintenance, flying
- B.
Maintenance, operations, QA
- C.
QA, support, aircraft maintenance
- D.
Maintenance operations, maintenance, aircraft maintenance, and QA
- 2.Who monitors flying and maintenance schedules, and maintains visibility of fleet health?
- A.
Operations Support Center
- B.
Logistics Support Squadron
- C.
Operations Support Squadron
- D.
Maintenance Operations Center
- 3.When you are assigned to an equipment maintenance squadron as an engine troop, to what flight will you most likely be attached?
- A.
Maintenance
- B.
Accessories
- C.
Fabrication
- D.
Munitions
- 4.When you are assigned to an aircraft maintenance squadron as an engine troop, to what flight will you most likely be attached?
- A.
Debrief
- B.
Specialist
- C.
Deployment
- D.
Training
- 5.What does the fifth position of the AFSC 3A652 represent?
- A.
Career field subdivision
- B.
Specific AFSC
- C.
Career field
- D.
Skill level
- 6.What type of training is provided to help you learn the knowledge portion of your job?
- A.
OJT
- B.
Task qualification
- C.
CDCs
- D.
NCOA
- 7.How many months must you have in the AF before you attend Airman Leadership School (ALS)?
- A.
24
- B.
36
- C.
48
- D.
18
- 8.Which program's purpose is to ensure safe and healthy working conditions for all AF employees?
- A.
MSDS
- B.
AFOSH
- C.
ORM
- D.
Flight-line saftey
- 9.Air Force Occupational Safety and Health (AFOSH) standards are located within Air Force publication series?
- A.
55
- B.
66
- C.
91
- D.
92
- 10.Which Air Force instruction defines quality maintenance and requires maintenance personnel to display integrity and comply with all written guidance?
- A.
21-110
- B.
00-20-1
- C.
00-20-2
- D.
21-101
- 11.The compressor bleed air supplied by small gas turbine (SGT) engines is not used for the
- A.
Heating the fuel supplied to the engines
- B.
Starting the main engines.
- C.
Pressurizing the aircraft.
- D.
Air-conditioning system.
- 12.What component contains the alternating current (AC) generator located on C-130 type aircraft that incorporates the gas turbine compressor (GTC)?
- A.
GTC compressor section.
- B.
GTC accessory gearbox
- C.
Air turbine motor.
- D.
Right wheel well.
- 13.This statement applies when either the auxiliary power unit (APU) or the gas turbine compressor (GTC) is installed on C-130 aircraft.
- A.
GTC can only be operated while the aircraft is flying.
- B.
APU can only be operated while the aircraft is on the ground
- C.
APU can be operated whether the aircraft is on the ground or flying.
- D.
GTC can be operated whether the aircraft is on the ground or flying
- 14.After combustion, the resulting hot gases flow through the bottom of the C-130 aircraft’s auxiliary power unit (APU) combustion can and into the
- A.
Deswirl ring.
- B.
Turbine torus.
- C.
Exhaust flange.
- D.
Turbine plenum
- 15.What type of energy does the C-130 aircraft’s auxiliary power unit (APU) turbine section converts the hot gases produced by the combustion section into?
- A.
Electric
- B.
Hydro
- C.
Pneumatic
- D.
Mechanical
- 16.Which switch, within the multiple centrifugal switch assembly, opens a circuit to stop the C- 130 aircraft auxiliary power unit’s (APU) ignition unit?
- A.
15
- B.
65
- C.
95
- D.
110
- 17.This C-130 aircraft auxiliary power unit (APU) component calibrates the exhaust gas temperature (EGT) indicator to the thermocouple.
- A.
Thermocouple resistor.
- B.
Pneumatic thermostat.
- C.
EGT thermocouple
- D.
EGT power supply
- 18.What type of sump system is an auxiliary power unit (APU) considered if the oil is not stored within the engine itself?
- A.
Wet
- B.
Dry
- C.
Reserve
- D.
Emergency
- 19.The acceleration control valve compares these two inputs to schedule the proper fuel-flow to the atomizer during a C-130 aircraft’s auxiliary power unit (APU) acceleration.
- A.
RPM and EGT
- B.
CDP and fuel pressure
- C.
CIT and RPM
- D.
EGT and fuel pressure
- 20.Which component does the thermostat bleed air pressure away from during the C-130 aircraft auxiliary power unit’s (APU) start and acceleration?
- A.
Load control valve.
- B.
Acceleration control diaphragm.
- C.
Pneumatic thermostat.
- D.
Compressor discharge solenoid.
- 21.What component provides the mounting pad for the bottom surface of the AE2100D3 air inlet housing?
- A.
PUAD
- B.
GMAD
- C.
FPMU
- D.
Inlet scroll case
- 22.What type of compressor rotor assembly is used on the AE2100D3 engine?
- A.
14-stage axial-flow
- B.
5-stage axial, 1-stage centrifugal
- C.
14-stage dual spool compressor
- D.
14-stage axial-flow, 1-stage centrifugal
- 23.How many fuel nozzles are in the AE2100D3 engine?
- A.
8
- B.
12
- C.
16
- D.
18
- 24.The AE2100D3 GMAD supplies the pads and drives for the AC generator, hydraulic pump, PGB lube and scavenge pump, propeller overspeed governor (OSG) and high-pressure pump, and the
- A.
FPMU
- B.
Starter
- C.
PCU
- D.
Alternator stator
- 25.The AE2100D3 starter control valve is spring-loaded to what position?
- A.
Opened
- B.
Closed
- C.
Fixed
- D.
Actuated
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