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CJ Type > CJ Systems Questions > Flashcards

CJ Systems Questions Flashcards

1
Q

List the items in the nose equipment area

A

Alcohol Reservoir
Pneumatic Bottle
Brake fluid reservoir
Oxygen Bottle
Antiskid Components

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2
Q

All drain holes in pressurized and unpressurized areas have check valves T/F

A

False
Open drain holes in unpressurized areas
Drain holes with check valves in pressurized areas

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3
Q

What is the maximum baggage limitation in lbs for the nose compartment

A

400 lbs

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4
Q

List the door(s) that are part of the DOOR NOT LOCKED annunciator light circuitry

A

Cabin door. Aft fuselage.

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5
Q

How would you verify that the cabin door is closed and locked prior to taxi

A

There is a door closed window

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6
Q

The locking pin on the emergency exit door must be removed before flight T/F

A

T

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7
Q

During a preflight how do you verify that the hydraulic service door is closed and locked

A

IDK

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8
Q

What is the maximum baggage limitation of the aft cabin compartment

A

400 lbs

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9
Q

List the items in the tail fuselage/baggage compartment

A

Environmental
Electrical Distribution
Flight Control Linkages
Fire Extenguishing Bottles
Battery
Hydraulic Fluid Reservoir
Engine Plug Storage

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10
Q

Disconnecting the batter is mandatory whenever you leave the airplane parked for more than 24 hours T/F

A

True

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11
Q

What type of engines are on the CJ1 and what is the maximum thrust rating

A

Williams FJ44-1A Engines
1,900 lbs per engine

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12
Q

What is the purpose of the TT2 sensor

A

located in bypass duct
Monitors air temperature and adjusts fuel schedule to optimum levels at maximum N2 setting

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13
Q

What are the 6 major engine sections

A

Intake and fan
Compressor
Diffuser
Combustion Turbine
Exhaust
Accessory drive

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14
Q

When will the emergency fuel shut-off mechanism actuate

A

When you press the Engine Fire Pushbutton

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15
Q

What are the items on the accessory gear drive

A

Fuel pump/Fuel control unit (FCU)
Oil pump
Starter-Generator
Hydraulic pump
N2 tachometer-generator

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16
Q

At what pressure differential will the FUEL FLTR BYPASS annunciator light illuminate

A

Bypass imminent-4.5 PSID illuminates FUEL FLTR BYPASS annunciator light
Bypass will occur at 10 PSID

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17
Q

The contents of the fire bottles will do damage to the engine if inadvertently fired into an engine that is not on fire T/F

A

False

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18
Q

During an engine start, when will the start sequence terminate

A

45% N2

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19
Q

What are the GPU requirements for the CJ1

A

Requires a 28 volt, 800-1100 amp GPU

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20
Q

In order to perform a wind-milling emergency air re-start, what speed is required

A

240 KIAS

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21
Q

What is the capacity of the fuel tanks

A

3200 lbs

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22
Q

The electric boost pump is a back-up to the engine driven fuel pump T/F

A

False, it is a back up to the primary ejector pump

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23
Q

When will the electric boost pumps run automatically if the boost pump switches are in the NORM position

A

Engine Start
Crossfeed
Low Fuel Pressure-On when low pressure switch drops through 4.65 psi

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24
Q

It is possible to transfer fuel from one tank to the other tank while the airplane is sitting on the ramp, master switch ON and engines not running T/F

A

True

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25
Q

During normal operation, fuel is delivered to the engine-driven fuel pump from the primary ejector pump at what psi

A

6-8 psi

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26
Q

What cockpit annunciator light(s) will be illuminated when you are properly transferring fuel

A

CROSSFEED and FUEL BOOST ON

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27
Q

What is the minimum fuel temperature (Jet A) for takeoff

A

-29 C

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28
Q

The maximum fuel imbalance is 200 lbs (800 lbs in emergency) T/F

A

False. Max imbalance in emergency is 600 lbs

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29
Q

AVGAS is an approved fuel for the CJ1 T/F

A

False

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30
Q

Fuel additive is required for the CJ1 each time you refuel T/F

A

True

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31
Q

With the loss of DC power, the hydraulic system bypass valve fails to the open position T/F

A

True

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32
Q

When does the HYD PRESS ON annunciator light illuminate

A

Landing Gear
Speedbrakes
Thrust Attenuators
Flaps

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33
Q

What kind of hydraulic fluid is used in the CJ1

A

MIL-H-83282

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34
Q

What is the emergency gear extension procedure

A

Pilot slows aircraft to 150 kts
Pilot moves gear handle to EXTEND position
Pilot pulls Tee Handle out and rotates it 45 degrees to lock handle out
Pilot yaws aircraft
Pilot pulls collar to utilize use of nitrogen air
Extension
Downlimit msw’s close and three green lights illuminate

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35
Q

If the speed brakes are extended and there is a loss of DC power, what will the speedbrakes do

A

the safety valves will spring-load open allowing the speed brakes to BLOW TO TRAIL

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36
Q

How will you know if a thrust attenuator unlocks in flight at a cruise power setting

A

MASTER CAUTION ATTEN UNLOCK

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37
Q

In flight, with the landing gear in the UP position, 1500 psi of pressure is holding the landing gear up T/F

A

False

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38
Q

What is the capacity of the hydraulic brake reservoir

A

1 quart

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39
Q

How would you utilize the emergency brake handle

A

Pulling on the cockpit red lever applies high pressure equally to both main wheel brake units
Releasing that handle stops air flow, relieves brake pressure, and vents brake air overboard
Don’t press on the brake pedals when using the air system and use one single, steady pull on the brake lever

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40
Q

When will the ANTI SKID INOP annunciator light illuminate

A

Antiskid control switch-off
System fault detected by the integrity monitor
PWR BRK LOW PRESS annunciator illuminated

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41
Q

List three functions of the GCU

A

Starter Cutoff
Field relay reset from a dead bus
Voltage regulation
Paralleling/load division
Feeder fault ground fault protection
Reverse current/differential voltage
Field Weakening

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42
Q

To charge the aircraft battery with a ground power unit, the battery master switch must be in the BATT position T/F

A

False

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43
Q

What is the minimum battery voltage required for a battery start

A

24 v

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44
Q

What are the starter-generator limitations

A

Three starts in 30 minutes, with a 30 second rest between each start

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45
Q

List the items on the emergency busses for the CJ1

A

Comm 1
Nav 1
Overhead Flood Lights
Pilot’s and Copilot’s Audio Panels
Voltmeter
Flap Control
RH Pitot Static Heater
Standy Altimeter/airspeed
Standby Gyro (has its own battery pack, not on the emergency bus)
Standby HSI
Copilot AHRS

46
Q

What is the maximum amperage limitation for the starter-generators

A

300 amps

47
Q

The crossed bus allows for logical grouping of items on the right and left main circuit breaker panels T/F

A

False
It’s function is to act like a crosstie between the L and R main DC busses through 225 amp current limiters

48
Q

The battery disconnect switch located inside of the cockpit on the captain’s side oxygen panel can be utilized to disconnect the battery from the hot battery bus after shutdown

A

False, that will drain the battery
It is used to open the battery relay in the event of a Battery Overheat (stuck relay) or stuck start relay

49
Q

The BATT O’TEMP annunciator light will illuminate at what temperature

A

145-160 degrees F: Steady BATT O’TEMP annunciator
160 degrees +: Flashing BATT O’TEMP annunciator

50
Q

At what % N2 will the SG disconnect the start and begin generation

A

45%

51
Q

List all the de-ice systems on the CJ1

A

Surface De-ice (Boots) - bleed air
Captain’s Windshield De-ice - alcohol

52
Q

What is the limitation associated with the pitot-static system

A

Limit operation time to two minutes on the ground

53
Q

When should you select the HIGH setting on the windshield bleed switch

A

For temperatures colder than -18C

54
Q

The windshield bleed valve fails to the closed position T/F

A

False

55
Q

What is the backup to the windshield bleed system and how do you operate it

A

Captain’s Windshield Alcohol De-ice
Continuous 10 minute supply controlled by cockpit on/off switch

56
Q

Regarding the engine anti-ice switches, when should you select the ENG ON position and when should you select the WING/ENG position

A

IDK, I’d imagine I would always just select both

57
Q

With the loss of DC power, the wing crossflow shutoff valve fails to the open position T/F

A

False

58
Q

How is the engine pylon ram air inlet duct heated

A

Electrically heated blankets
Limitation-do not power on the ground for more than 3 minutes

59
Q

What is the temperature limitation associated with the surface de-ice boots

A

-35C

60
Q

What is the minimum airspeed required in sustained icing conditions with the anti-ice systems in the ON position

A

160 kts

61
Q

Primary control static wicks are required for dispatch T/F

A

True

62
Q

All controls have a single manual trim tab with a cockpit position indicator T/F

A

False
Rudder and aileron controls have a single manual trim tab with a cockpit position indicator. Elevator controls have two trim tabs which can be either manually or electrically actuated.

63
Q

The rudder trim tab has a servo-assist function T/F

A

True

64
Q

How would you engage the control lock and what surfaces are locked

A

Pulling aft on the cockpit control lock handle will lock all primary controls in the neutral, and the throttles in the cutoff position

65
Q

The pilot can physically override the autopilot elevator servo

A

True

66
Q

The stick shaker is mechanically linked to the angle of attack probe T/F

A

False

67
Q

How many degrees can you move the nose wheel if you push full-scale right rudder deflection while taxiing?

A

20 degrees

68
Q

To tow the airplane with a tug, the control wheel lock must be disengages T/F

A

True

69
Q

All primary controls are unboosted and mechanically actuated

A

True

70
Q

The captain’s side electric pitch trim can override the copilot’s side electric pitch trim T/F

A

True

71
Q

Oxygen is always available to the pilot and copilot regardless of the position of the Oxygen Control Valve T/F

A

True

72
Q

What is the capacity of the oxygen bottle (in cubic feet)

A

22 cubic feet

73
Q

What type of crew oxygen masks are in the CJ1

A

diluter demand and demand

74
Q

At optimal capacity (green arc), what is the capacity (in psi) of the oxygen bottle

A

1600-1800 psi

75
Q

How do you check to make sure that the oxygen bottle is turned on at the bottle prior to flight

A

Don, 100%, no restriction to breathing

76
Q

A crew member should disconnect the oxygen mask at the connector port on the oxygen control panel after each flight T/F

A

IDK. I don’t think so, and I don’t think that is possible

77
Q

A pressure regulator reduces oxygen pressure to what (in psi)

A

70 psi

78
Q

A portable fire extinguisher located underneath the left side of the copilot’s chair is required for dispatch T/F

A

True

79
Q

When will the passenger oxygen masks in the cabin automatically drop

A

13,500 ft cabin altitude

80
Q

How can the crew drop the passenger oxygen masks without DC power

A

Manual drop

81
Q

With the pressurization source selector in the BOTH position, how many pounds per minute are available to pressurize and condition the cabin

A

8 PPM

82
Q

Selecting the FRESH AIR position on the pressurization source selector will depressurize the cabin T/F

A

True

83
Q

The pylon pre cooler cools the engine bleed air from 800 degrees to what temperature

A

500 F

84
Q

Selecting the EMER position on the pressurization source selector will provide how much air to pressurize the cabin

A

6 ppm

85
Q

The air conditioning compressor will auto-shed when you climb above FL 180 T/F

A

False
It will automatically load shed in the event of a generator failure, however it should be manually secured

86
Q

What is the purpose of the FLOOD position on the environmental panel

A

Evaporators circulate cabin air. Selecting flood on the aft evaporator diverts all air out of a flood cooling vent near top of the pressure bulkhead

87
Q

With the temperature selector in the AUTO position, when will the compressor automatically disengage

A

When the ram-air modulating valve is at approximately 70% or more closed, the compressor is disengaged

88
Q

The AIR DUCT O’HEAT annunciator light will illuminate when the temperature in the duct between the cabin heat exchanger and the aft pressure bulkhead reaches what temperature

A

300 degrees F

89
Q

With the flow divider in the MAX position, what is the distribution of air to the cockpit and to the cabin

A

Crew 90% and Cabin 10%

90
Q

To use the defog fan, select either HI or LO on the defog switch and verify that the compressor is in the AUTO position T/F

A

False, I believe with the selection of high or low automatically turns on the compressor

91
Q

The pressurization can hold a 5,000 ft cabin at the maximum certified altitude of 41,000 ft T/F

A

False, 8000 ft

92
Q

What is the maximum pressure differential that the cabin can hold

A

8.6 psid

93
Q

What is the function of the cabin altitude limit valves

A

Open at a cabin altitude of 13000 ft, allowing cabin ambient air to enter the control line(s), reducing the control vacuum, and closing the outflow valves, thus re-establishing cabin pressure

94
Q

The emergency dump switch requires no DC power to function T/F

A

False, requires DC power and vacuum to function

95
Q

The digital pressure controller will set a maximum climb rate of how many feet per minute

A

fpm x 1000

96
Q

On the ground, what will cause the airplane to go into pre-pressurization mode

A

On the ground with both throttles about 85% N2, both outflow valves slowly close

97
Q

Prior to takeoff, what should you set in the digital pressure controller window

A

Pilot selects destination field elevation plus 200 ft

98
Q

How do you know if the digital pressure controller goes into isobaric mode

A

If the air data sensor/computer information is interrupted, the controller will switch from AUTO to ISOBARIC mode
Yellow caution light appears in top left corner of controller display face

99
Q

If the pressurization system goes into manual mode, how would you climb and descent that cabin

A

Cherry Picker

100
Q

How do you test the digital pressure controller prior to flight

A

Press and hold EXER button

101
Q

Intensity of the cockpit floodlights can be adjusted using a rheostat control T/F

A

True

102
Q

When will the cockpit floodlights automatically turn on

A

IDK

103
Q

When should the navigation lights be turned on

A

IDK

104
Q

Power for the nose baggage compartment light comes from which bus

A

IDK but I think the HOT bus

105
Q

If the nose baggage compartment light switch is left in the ON position and the baggage door is closed and locked, will the light stay on

A

No

106
Q

The rotating beacon is located on top of the vertical stabilizer and should be turned on whenever the engines are running T/F

A

True

107
Q

When flying at night, how would you verify ice accumulation on the wings

A

Wing inspection light

108
Q

Selecting PASS SAFETY on the passenger safety switch does what

A

No smoke, seatbelt & emergency exit lights

109
Q

The landing lights are located on the landing gear assembly and should be turned to the OFF position whenever the landing gear is up T/F

A

IDK, I would say that it doesn’t matter much, the gear is up

110
Q

Taxiing with the landing lights in the RECOG/TAXI position will cause the lights to illuminate in an alternating fashion at a low intensity T/F

A

False

CJ Type (5 decks)

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