2a651 Cdc 3

1. 3. (402) The main fuel control allows the engine to safely accelerate, reducing the possibility of

Flameout.

Turbine seizure.

Overtemperature.

Compressor shift.

2. 4. (402) The purpose of a fuel/oil cooler in a fuel system is to

Heat the fuel and cool the oil.

Cool the fuel and cool the oil.

Heat the fuel and heat the oil.

Cool the fuel and heat the oil.

3. 27. (409) What term is used to indicate that air is being mixed with the oil in the oil pump to create pockets of air?

Aeration.

Induction.

Convection.

Compression.

4. 48. (415) What are microscopic metallic particles in the oil system called?

Wear metals.

Friction metals.

Precious metals.

Transformation metals.

5. 1. (401) What is the composition of JP–8 fuel?

Gasoline and kerosene.

Diesel fuel and AV GAS.

Diesel fuel and kerosene.

Gasoline and diesel fuel.

6. 5. (403) What type of fuel control uses items such as thermocouples, relays, amplifiers, and solenoids to help control a jet engine?

Pneumatic.

Fuel injection.

Hydromechanical.

Electrohydromechanical.

7. 6. (403) On fuel controls that require setting during an engine trim, calibration and/or adjustment screws must be

Replaced.

Die marked.

Safety sealed and/or lockwired.

Apply a thread locking compound.

8. 51. (416) What is the term for the process of producing voltage in a conductor when it passes through a magnetic field?

Static.

Electronics.

Mutual induction.

Electromagnetic induction.

9. 28. (409) In an engine oil tank, which device separates the air from the oil?

Aerator.

Deaerator.

Check valve.

Bypass valve.

10. 23. (407) In addition to the visual inspection the T–56 engine fuel nozzle also requires what type of inspection?

Nondestructive.

Spray pattern.

Pre-torque.

Ultrasonic.

11. 40. (413) The valve that allows fluid to flow in only one direction is the

Check.

Relief.

Bypass.

Pressurizing.

12. 9. (404) Which F100-PW–220 engine fuel system component controls pressurization of the core engine fuel system?

N2 sensor.

P&D valve.

Fuel nozzle.

Fan inlet Tt2.5 sensor.

13. 15. (405) On an F108-CF–100 engine, the fuel injectors contain

Only primary fuel flow passages.

Only secondary fuel flow passages.

Both primary and secondary fuel flow passages.

Primary, secondary, and auxiliary fuel flow passages.

14. 18. (407) On the T56 engine, how many and what type of fuel pumps are contained in the fuel pump and filter assembly?

3 gear; 1 boost.

2 gear; 2 boost.

2 gear; 1 boost.

1 gear; 2 boost.

15. 24. (408) Which type of oil cooler operates on the same principle as a radiator in an automobile?

Air.

Fuel.

Hydraulic.

Pneumatic.

16. 25. (408) When an engine is not operating, static preload for a carbon oil seal is provided by

Air pressure.

Oil pressure.

Spring pressure.

Hydraulic pressure.

17. 32. (410) On an F100-PW–220 engine, the air/oil coolers are mounted on the fan duct and use

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.

18. 83. (433) Once the cooling airflow has done its job of cooling the turbine section, where does it go?

Through a heat exchanger.

Out the turbine case bleed holes.

Into the gas stream to exit the engine.

Back to the compressor to be used again.

19. 33. (410) On an F100-PW–220 engine, what component permits oil to bypass the oil filter during cold weather starts?

Oil relief valve.

Filter bypass valve.

Filter poppet valve.

Oil pressure transmitter tap.

20. 53. (416) Which part of a generator acts as an automatic switching device, changing alternating current to direct current?

Brushes.

Slip rings.

Commutator.

Permanent magnet.

21. 16. (406) What supplies the AE2100D3 FADEC with power until engine RPM is sufficient for the alternator stator to take control?

Airplane 28 VDC power supply.

NIU.

MIL-STD–1553B data bus.

Mission computer.

22. 66. (423) The JFS is basically a

Piston-type starter.

Pneumatic-type starter.

Small gas turbine engine.

Cartridge-pneumatic starter.

23. 8. (404) On an F100-PW–220 engine, the MFC is capable of operating in how many modes?

One.

Two.

Three.

24. 47. (415) Who is responsible for ensuring that the OAP operates properly?

Project monitor.

Logistics commander

Propulsion flight chief.

Laboratory supervisor.

25. 2. (401) At room temperature, how many times longer will it take water to settle out of JP–8 than out of gasoline?

Two.

Three.

Four.

Five.

26. 11. (404) On the F100-PW–220 engine, which component controls the augmentor fuel control?

Fuel pump.

Fuel pump controller.

Signature elimination probe.

DEEC.

27. 12. (404) Core engine fuel flow sequence on an F100-PW–220 engine starts at the main fuel pump and then goes through the

Main fuel control, fuel/oil cooler, pressurizing and dump valve, and fuel nozzles.

Fuel/oil cooler, pressurizing and dump valve, main fuel control, and fuel nozzles.

C. augmentor fuel pump, augmentor fuel control, fuel/oil cooler, pressurizing and dump valve,and fuel nozzles.

D. augmenter fuel control augmentor fuel pump, fuel/oil cooler, pressurizing and dump valve, andfuel nozzles.

28. 29. (409) Which type of oil system stores the oil in a tank fitted to the side of the engine?

Wet sump.

Dry sump.

Hot tank.

Cold tank.

29. 52. (416) On a simple AC generator, which item takes the current from the slip rings to operate the electrical device?

Brushes.

Commutator.

Rotating loop.

Permanent magnet.

30. 43. (413) Which RGB component prevents oil in the oil tank from draining into the RGB rear case?

Shutoff valve.

Oil pump and filter.

Oil pump check valve.

Oil pump bypass valve.

31. 50. (415) The SEM/EDX analysis process differs from conventional oil analysis in which major aspect?

SEM/EDX samples must be sent off-site for analysis.

SEM/EDX particles must be oil free for analysis to take place.

SEM/EDX provides results concerning equipment and components condition.

SEM/EDX samples can only be obtained in an intermediate maintenance shop.

32. 77. (428) Discharge air used for aircraft engine anti-icing to heat-critical areas is taken from which engine area?

Turbine.

Augmentor.

Compressor.

Combustion.

33. 80. (430) On an F110-GE–129 engine, the anti-icing system prevents detrimental formation and accumulation of ice on front frame struts, forward centerbody, and

Ring cowl.

C-D duct.

Fan inlet guide vane flaps.

Variable exhaust nozzle flaps.

34. 10. (404) Which stage of compressor air drives the augmenter fuel pump on an F100-PW–220 engine?

7th.

10th.

13th.

14th.

35. 45. (414) The journeyman must be aware of which hazardous property of modern jet engine oil?

Toxicity.

Viscosity.

Alkalinity.

Corrosiveness.

36. 46. (415) The primary benefit of identifying an impending failure through the OAP is

Improved safety.

Increased component life.

Reduced maintenance cost.

Increased equipment availability.

37. 22. (407) When the null orifice on the T56 engine TD valve is set at zero, how much fuel will the valve bypass?

0%.

10%.

20%.

30%.

38. 13. (405) Operational control of the F108-CF–100 engine is achieved by the use of the power lever, fuel shut-off lever, and

Fuel pump.

Oil/fuel heat exchanger.

Air/fuel heat exchanger.

PMC.

39. 34. (411) What is used to check the oil level in a F108-CF–100 engine?

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.

40. 82. (432) What does a high-altitude stall sound like?

"Choo-choo.”

An explosion.

Popping corn.

Severe tearing of metal.

41. 68. (423) What engine section houses the JFS combustion section?

Geartrain.

Turbine plenum.

Generator control unit.

Gas generator and accessory drive assembly.

42. 7. (404) When in the primary mode, what controls the operation of the F100-PW–220 engine?

MEC.

PMG.

DEEC.

43. 92. (438) In the mechanical blockage-type thrust reverser, when the reverser is not in use, what happens to the doors?

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 enginenacelle.

44. 44. (413) How many scavenge oil pumps are located in the RGB?

1.

2.

3.

4.

45. 88. (436) What AE2100D3 engine component continuously monitors the LVDT signal and controls the compressor IGV position?

NIU.

FPMU.

LVIT.

FADEC.

46. 98. (440) What are the two main types of augmentor (afterburner) ignition systems?

Torch igniter and hot streak.

Hot streak and fuel injection.

Pilot burner ring and hot streak.

Torch igniter and pilot burner ring.

47. 30. (409) Which type of oil system design places the oil cooler in the pressure subsystem?

Wet tank.

Dry tank.

Hot tank.

Cold tank.

48. 38. (413) The amount of ram air passing through the oil cooler core is regulated by the

Thermostat.

Flap actuator.

Size of the core.

Regulating valve.

49. 67. (423) Which item initially rotates the JFS?

ESS PTO.

Engine PTO.

Hydraulic motor.

Electric motor mounted on the aircraft.

50. 49. (415) Oil sampling intervals should not vary by more than

5 percent.

10 percent.

15 percent.

20 percent.

51. 56. (419) Which unit of an AC ignition system develops 20,000 volts?

Inverter.

Capacitor.

Generator.

Transformer.

52. 59. (420) On early ignition systems, what is the purpose of compositors in an ignition system?

Prevent the points from arcing.

Cause a voltage to jump across the spark gap in the ignition unit.

Step up voltage high enough to break down the air gap of the igniter plug.

Hold back the current flow until the voltage is high enough to be rectified.

53. 75. (427) On the T56 engine, which switch energizes the starter control valve to the OPEN position?

Ground start.

Speed-sensitive.

Fuel enrichment.

Secondary fuel pump pressure.

54. 76. (427) Which T56 engine component functions as an on-off control for the air supply that is sent to the starter?

Air turbine.

Ground start switch.

Starter control valve.

Secondary fuel pump pressure switch

55. 14. (405) The F108 engine fuel pump contains a low-pressure stage (centrifugal boost stage) and a high-pressure

Gear stage.

Gerotor stage.

Axial boost stage.

Sliding vane stage.

56. 26. (409) The F100-PW–100 engine oil pressure varies with N2 speed, engine inlet oil temperature, and

Oil jet pressure.

Fan turbine speed.

Oil nozzle condition.

Number of oil jets used.

57. 37. (413) Which type of oil pump is used on the T56 engine?

Gear.

Float.

Gerotor.

Centrifugal.

58. 54. (417) What provides the PTO shaft that is used to drive the CSD?

Engine fittings.

Aircraft fittings.

Engine adapter.

Aircraft adapter.

59. 63. (421) What is the output of the AE2100D3 alternator stator?

1 to 20 VAC.

20 to 40 VAC.

40 to 60 VAC.

60 to 80 VAC.

60. 65. (422) The OSG on the cartridge-pneumatic starter consists of the

Shaft and piston.

Igniter and cable.

Flyweights and piston.

Flyweights and igniter.

61. 72. (424) On the F–15 secondary power system, what is used to stop the JFS starting cycle when the aircraft engine has accelerated to starter cutout speed?

Four-speed switch.

Manual decoupler.

Hydraulic decoupler.

50 percent engine cutout switch assembly.

62. 90. (438) What are the two types of thrust reversers?

Aerodynamic blockage and convergent-divergent.

Aerodynamic blockage and mechanical blockage.

Divergent-convergent and mechanical blockage.

Convergent-divergent and mechanical blockage.

63. 20. (407) On the T56 engine, what compares the desired throttle setting from the coordinator with the actual TIT signal from the thermocouples

TD valve.

Speed-sensitive control.

TD potentiometers.

TD amplifier.

64. 35. (412) Approximately how many GPM does the AE2100D3 PUAD lube and scavenge pump provide at engine PTO?

3.

5.

7.

9.

65. 57. (419) A simple DC ignition system consists of vibrator,

Igniter plugs, and transformer.

Igniter plugs, and AC to DC converter.

AC to DC converter, and transformer.

AC to DC converter, transformer, and igniter plugs.

66. 55. (418) The slide-type resistor in the EGT circuit is used to

Adjust the thermocouples.

Calibrate the EGT indicator in the flight station.

Compensate for minor voltage buildups in the circuit.

Compensate for differences in temperatures at altitude.

67. 17. (406) What component is controlled by the AE2100D3 FADEC through the ENGINE START switch for normal engine shutdown or by the fire control handle for emergency shutdown?

Servo valve.

Fuel check valve.

Electric shutoff valve.

Latching shutoff valve.

68. 60. (420) The T56 engine speed-sensitive control lets electrical current flow to the fuel and ignition system at

16% RPM.

30% RPM.

65% RPM.

94% RPM.

69. 99. (441) The F100 engine augmentor's primary nozzle actuator is driven by cables from the

T5 amplifier.

Unified control.

Afterburner fuel control.

CENC.

70. 21. (407) Which T56 engine component sends the fuel to the fuel manifold?

TD valve.

Main fuel pump.

TD amplifier.

Fuel control.

71. 31. (410) On an F100 engine, the breather pressurizing valve is internally mounted in the

Oil tank.

Gearbox.

72. (431) The T56 engine anti-icing solenoid valve is

Normally open.

Energized open.

Normally closed.

Deenergized closed.

73. 61. (421) An F100-PW–100 engine augmentor igniter plug ionizes at a minimum rate of how many sparks per second?

25.

30.

45.

90.

74. 70. (424) Oil is supplied to the F–15 JFS through the

Oil tank.

Aircraft filter.

JFS oil system.

CGB oil system.

75. 71. (424) On an F–15, the power to start the engines begins with the JFS and continues through the CGB to the

PTO.

PMG.

ADG.

AMAD.

76. 58. (420) On early ignition systems, the high-energy capacitor-type ignition system does not include a

Vibrator.

Capacitor.

Centrifugal switch.

Gas-filled rectifier.

77. 79. (429) On an F108-CF–100 engine anti-ice system, what is the purpose of the air injector on the air regulator?

Control air velocity at high RPM.

Control air temperature and pressure.

Provide auxiliary airflow during engine start.

Provide controlled airflow during VBV operation.

78. 36. (412) What AE2100D3 component drives the PGB lube and scavenge pump?

Alternator stator.

PGB.

PUAD.

GMAD.

79. 62. (421) From where does the AE2100D3 ignition system receive its electrical power?

Generator.

Alternator stator.

Aircraft battery.

Essential DC bus.

80. 64. (421) What component monitors the AE2100D3 ignition exciters spark rate?

FADEC.

GMAD.

PUAD.

NIU.

81. 94. (439) The F117-PW–100 fan thrust reverser door upper right and left sensors send a signal to which channel or channels of the EEC?

A channel.

B channel.

Both A & B channels.

Both A & C channels.

82. 41. (413) In the power unit oil system, the dual-port oil jet mounted on the front side of the compressor air inlet housing is used to lubricate the

Mid and center sleeve bearings.

Torquemeter and compressor front bearings.

83. 96. (439) How many linear hydraulic actuators are used to deploy and stow the fan thrust on the F117-PW–100 engine?

2.

3.

4.

5.

84. 19. (407) What T56 engine controls the rotary movement of the fuel control metering valve?

Temperature.

Engine speed.

Throttle position.

Compressor inlet pressure.

85. 100. (442) On an F110-GE–129 augmentor variable nozzle, uniform movement and geometric stability of the nozzle is provided by

Mechanical synchronization of the nozzle actuators.

Electrical synchronization of the nozzle actuators.

Pneumatic synchronization of the nozzle actuators.

Hydraulic synchronization of the nozzle actuators.

86. 73. (425) When starting the F–16, which component drives the JFS geartrain, fuel control, and lube pump?

Pneumatic power.

Electrical power.

Hydraulic start motor.

Accessory drive gearbox.

87. 74. (426) How is the AE2100D3 starter control valve actuated?

Electrically.

Pneumatically.

Hydraulically.

Hydro-electrically.

88. 91. (438) One type of aerodynamic blockage thrust reverser uses

A closed nozzle.

The reverser door extension.

A clamshell-type restriction aft of engine.

Vanes inside the duct to create swirling gases.

89. 42. (413) The power section and RGB oil systems are joined together at the

Fuel heater and strainer.

External scavenge oil filter.

External scavenge oil pump.

Scavenge element of the main pump.

90. 95. (439) The core reverser lock proximity sensors are mounted on the

Aft fan duct.

Fwd fan duct.

Actuator.

Control valve.

91. 84. (434) On an F108-CF–100 engine, the variable bleed valves bleed air from the

N1 compressor.

N2 compressor.

First stage fan.

Last stage of compression.

92. 78. (429) On an F108 engine, anti-ice air is ducted from which manifold?

Pneumatic.

Augmentor.

Combustion case.

Compressor case.

93. 87. (436) On the AE2100D3 engine, what type of actuator is the CVG actuator?

Mechanical.

Electrical.

Hydraulic.

Fuel.

94. 39. (413) Bleed air flowing through which component increases airflow through the cooler?

Flap actuator.

Oil cooler flap.

Augmentation valve.

Augmentation ejector.

95. 89. (437) The T56 engine component that allows 14th-stage air to close the bleed air valves is the

Balance line.

Bleed air valve.

Speed-sensitive valve.

Speed-sensitive control.

96. 93. (439) On the F117-PW–100 engine, what component controls hydraulic power for actuating both the fan and core thrust reversers?

Control valve.

Electronic engine control.

Hydraulic pump.

Fuel control.

97. 85. (434) On an F108-CF–100 engine, the direction of the variable bleed valve rotation is controlled by the

Flexible shafts.

Feedback cable.

Fuel gear motor.

Ballscrew actuators.

98. 97. (440) What component heats augmentor fuel to provide better vaporization and combustion?

Fuel control.

Fuel spraybars.

Fuel manifolds.

Fuel/oil cooler.

99. 86. (435) On an F110-GE–129 engine, the MEC schedules the variable vane positions by the

Sea-level temperature and actual engine RPM.

Compressor inlet pressure and turbine speed.

Fan discharge temperature and core engine speed.

Turbine discharge pressure and compressor inlet temperature.

100. 69. (424) Which component provides an electrical safety cutoff for the JFS if the power turbine accelerates to a 110 percent overspeed condition?

Overspeed clutch.

Three-speed switch.

Overrunning clutch.

2A651 CDC 3

1. 3. (402) The main fuel control allows the engine to safely accelerate, reducing the possibility of

2.

What first name or nickname would you like us to use?

2. 4. (402) The purpose of a fuel/oil cooler in a fuel system is to

3. 27. (409) What term is used to indicate that air is being mixed with the oil in the oil pump to create pockets of air?

4. 48. (415) What are microscopic metallic particles in the oil system called?

5. 1. (401) What is the composition of JP–8 fuel?

6. 5. (403) What type of fuel control uses items such as thermocouples, relays, amplifiers, and solenoids to help control a jet engine?

7. 6. (403) On fuel controls that require setting during an engine trim, calibration and/or adjustment screws must be

8. 51. (416) What is the term for the process of producing voltage in a conductor when it passes through a magnetic field?

9. 28. (409) In an engine oil tank, which device separates the air from the oil?

10. 23. (407) In addition to the visual inspection the T–56 engine fuel nozzle also requires what type of inspection?

11. 40. (413) The valve that allows fluid to flow in only one direction is the

12. 9. (404) Which F100-PW–220 engine fuel system component controls pressurization of the core engine fuel system?

13. 15. (405) On an F108-CF–100 engine, the fuel injectors contain

14. 18. (407) On the T56 engine, how many and what type of fuel pumps are contained in the fuel pump and filter assembly?

15. 24. (408) Which type of oil cooler operates on the same principle as a radiator in an automobile?

16. 25. (408) When an engine is not operating, static preload for a carbon oil seal is provided by

17. 32. (410) On an F100-PW–220 engine, the air/oil coolers are mounted on the fan duct and use

18. 83. (433) Once the cooling airflow has done its job of cooling the turbine section, where does it go?

19. 33. (410) On an F100-PW–220 engine, what component permits oil to bypass the oil filter during cold weather starts?

20. 53. (416) Which part of a generator acts as an automatic switching device, changing alternating current to direct current?

21. 16. (406) What supplies the AE2100D3 FADEC with power until engine RPM is sufficient for the alternator stator to take control?

22. 66. (423) The JFS is basically a

23. 8. (404) On an F100-PW–220 engine, the MFC is capable of operating in how many modes?

24. 47. (415) Who is responsible for ensuring that the OAP operates properly?

25. 2. (401) At room temperature, how many times longer will it take water to settle out of JP–8 than out of gasoline?

26. 11. (404) On the F100-PW–220 engine, which component controls the augmentor fuel control?

27. 12. (404) Core engine fuel flow sequence on an F100-PW–220 engine starts at the main fuel pump and then goes through the

28. 29. (409) Which type of oil system stores the oil in a tank fitted to the side of the engine?

29. 52. (416) On a simple AC generator, which item takes the current from the slip rings to operate the electrical device?

30. 43. (413) Which RGB component prevents oil in the oil tank from draining into the RGB rear case?

31. 50. (415) The SEM/EDX analysis process differs from conventional oil analysis in which major aspect?

32. 77. (428) Discharge air used for aircraft engine anti-icing to heat-critical areas is taken from which engine area?

33. 80. (430) On an F110-GE–129 engine, the anti-icing system prevents detrimental formation and accumulation of ice on front frame struts, forward centerbody, and

34. 10. (404) Which stage of compressor air drives the augmenter fuel pump on an F100-PW–220 engine?

35. 45. (414) The journeyman must be aware of which hazardous property of modern jet engine oil?

36. 46. (415) The primary benefit of identifying an impending failure through the OAP is

37. 22. (407) When the null orifice on the T56 engine TD valve is set at zero, how much fuel will the valve bypass?

38. 13. (405) Operational control of the F108-CF–100 engine is achieved by the use of the power lever, fuel shut-off lever, and

39. 34. (411) What is used to check the oil level in a F108-CF–100 engine?

40. 82. (432) What does a high-altitude stall sound like?

41. 68. (423) What engine section houses the JFS combustion section?

42. 7. (404) When in the primary mode, what controls the operation of the F100-PW–220 engine?

43. 92. (438) In the mechanical blockage-type thrust reverser, when the reverser is not in use, what happens to the doors?

44. 44. (413) How many scavenge oil pumps are located in the RGB?

45. 88. (436) What AE2100D3 engine component continuously monitors the LVDT signal and controls the compressor IGV position?

46. 98. (440) What are the two main types of augmentor (afterburner) ignition systems?

47. 30. (409) Which type of oil system design places the oil cooler in the pressure subsystem?

48. 38. (413) The amount of ram air passing through the oil cooler core is regulated by the

49. 67. (423) Which item initially rotates the JFS?

50. 49. (415) Oil sampling intervals should not vary by more than

51. 56. (419) Which unit of an AC ignition system develops 20,000 volts?

52. 59. (420) On early ignition systems, what is the purpose of compositors in an ignition system?

53. 75. (427) On the T56 engine, which switch energizes the starter control valve to the OPEN position?

54. 76. (427) Which T56 engine component functions as an on-off control for the air supply that is sent to the starter?

55. 14. (405) The F108 engine fuel pump contains a low-pressure stage (centrifugal boost stage) and a high-pressure

56. 26. (409) The F100-PW–100 engine oil pressure varies with N2 speed, engine inlet oil temperature, and

57. 37. (413) Which type of oil pump is used on the T56 engine?

58. 54. (417) What provides the PTO shaft that is used to drive the CSD?

59. 63. (421) What is the output of the AE2100D3 alternator stator?

60. 65. (422) The OSG on the cartridge-pneumatic starter consists of the

61. 72. (424) On the F–15 secondary power system, what is used to stop the JFS starting cycle when the aircraft engine has accelerated to starter cutout speed?

62. 90. (438) What are the two types of thrust reversers?

63. 20. (407) On the T56 engine, what compares the desired throttle setting from the coordinator with the actual TIT signal from the thermocouples

64. 35. (412) Approximately how many GPM does the AE2100D3 PUAD lube and scavenge pump provide at engine PTO?

65. 57. (419) A simple DC ignition system consists of vibrator,

66. 55. (418) The slide-type resistor in the EGT circuit is used to

67. 17. (406) What component is controlled by the AE2100D3 FADEC through the ENGINE START switch for normal engine shutdown or by the fire control handle for emergency shutdown?

68. 60. (420) The T56 engine speed-sensitive control lets electrical current flow to the fuel and ignition system at

69. 99. (441) The F100 engine augmentor's primary nozzle actuator is driven by cables from the

70. 21. (407) Which T56 engine component sends the fuel to the fuel manifold?

71. 31. (410) On an F100 engine, the breather pressurizing valve is internally mounted in the

72. (431) The T56 engine anti-icing solenoid valve is

73. 61. (421) An F100-PW–100 engine augmentor igniter plug ionizes at a minimum rate of how many sparks per second?

74. 70. (424) Oil is supplied to the F–15 JFS through the

75. 71. (424) On an F–15, the power to start the engines begins with the JFS and continues through the CGB to the

76. 58. (420) On early ignition systems, the high-energy capacitor-type ignition system does not include a

77. 79. (429) On an F108-CF–100 engine anti-ice system, what is the purpose of the air injector on the air regulator?