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Challenger 350 Terry's > Challenger 350 > Flashcards

Challenger 350 Flashcards

1
Q

Max Tow Limit

A

120°

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2
Q

which doors are Monitored by the door warning system?

A

M E C A B Main Emergency Cargo. Aft Equipment Bay Battery

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3
Q

What happens when you turn on the battery switches

A

All busses are powered. IRS begins aligning. CVR turns on.

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4
Q

What is the function of the APU

A

Air and Electric

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5
Q

Where does the APU receive it’s fuel

A

Right collector tank

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6
Q

When will the passenger door caution turn amber

A

Left engine run switch on.

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7
Q

Max Fuel Load Pressure refueling. Over wing refueling

A

Pressure -14,150 Over Wing - 13,000

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8
Q

Take off thrust for the HTF7350 engine

A

7,372

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9
Q

Which EICAS message requires prompt action

A

Amber

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10
Q

Synoptic Colors: Amber, Green, White, Red

A

Amber- Component Failure. Green - Normal with flow. White - Normal without flow, Red - Exceedence

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11
Q

When will the FDR begin recording

A

Beacon on or Weight off Wheels

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12
Q

When will the emergency lights illuminate

A

Loss of right main bus power.

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13
Q

What is the purpose of the PTU

A

Gear retraction with loss of pressure in Left hydraulic system; Left Engine driven pump failure.

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14
Q

What controls the Landing gear

A

PSEU - Proximity Sensing Electronic Unit.

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15
Q

Which Primary flight control surface is not hydraulic

A

Ailerons

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16
Q

Which spoilers act as Multi- Function Spoilers

A

1,2 And 7,8

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17
Q

When are EICAS messages inhibited in flight

A

Takeoff - Airspeed above 80 kts until 400 feet. Landing - Below 400 feet until less than 40 kts.

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18
Q

Hydraulic Pressure for EDP and DCMP

A

EDP - 3,000 psi. DCMP - 2,800 psi

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19
Q

Standby Indicator battery life

A

3.5 hours

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20
Q

When will the Buss Tie open

A

2 or more generators online.

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21
Q

Which busses will remain powered during loss of all generators.

A

Essential busses and Battery busses.

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22
Q

How long will the Essential Busses and Battery busses last on battery power only

A

1 hour

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23
Q

When will the Auxiliary busses load shed

A

Single generator operation in flight.

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24
Q

Engine Fire and APU fire are controlled by what component

A

FIREX-CU Fire Detection and Extinguishing Control Unit.

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25
Q

Trim Air Only which valves open and which close

A

Right Flow Control Valve opens Left Flow Control Valve closes. Pre-cooler Crossover Valve closes.

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26
Q

Cabin Delta P warning Cass message comes on when

A

Cabin pressure > 9.2 psi or < - .5 psi

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27
Q

Takeoff and return to base pressurization becomes active when

A

At 6,000 feet or 10 minutes.

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28
Q

After crossing the Holding fix in the FMS, what is displayed next to 6L

A

Exit Hold

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29
Q

What is the minimum width required to make a 180 degree turn with a 5 foot safety margin

A

58 feet

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30
Q

What is the purpose of the Scavenge Ejectors

A

Transfer fuel from the Lowest inboard section of the wing to the Collector Tank.

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31
Q

Which pneumatic system uses HP air

A

Wing Anti-Ice

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32
Q

How many Ice detectors are required to generate an ICE DETECTED CAS Message

A

One

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33
Q

What EICAS Message will be displayed with Ice Detected. Anti-Ice System is off. Anti-Ice System on

A

Off - ICE DETECTED in Amber. On - ICE DETECTED in Cyan

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34
Q

Following and aborted start how long must you dry motor the engine

A

30 seconds

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35
Q

Below What Temperature must the Engine Ani-Ice be on with snow etc

A

10° C OAT

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36
Q

Maximum APU altitude using Bleed Air

A

20,000 feet

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37
Q

Maximum APU altitude using Electric

A

30,000 Feet

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38
Q

Maximum APU altitude Running

A

37,000 Feet

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39
Q

Maximum APU altitude Starting

A

30,000 Feet

40
Q

Maximum speed to start APU

A

285

41
Q

Maximum Altitude using the APU to Start The Left engine on the ground

A

9,000

42
Q

What does IASC stand for

A

Integrated Air System Controller

43
Q

How many Igniters does the engine have

A

2

44
Q

When should you Manually select Engine Ignition ON

A

Contaminated Runways, moderate or heavy rain, moderate or heavy Turbulence, In the vicinity of Thunder storms

45
Q

What happens with an ENGINE FIRE

A

MW illuminates, 3 Chimes, ENG FIRE CASE Message, Red FIRE on N1, Aural ENGINE FIRE.

46
Q

Pressing EMER DEPRESS does what in Manual and what in Auto mode.

A

Auto mode - 2,500’ fpm up to 14,000 + - 100’ Manual mode - 3,000’ fpm up to 14,500’ + - 500’

47
Q

What is the power source for the Left DCMP? What is the power source for the Right DCMP?

A

Left DCMP - Right Main Bus. Right DCMP - Left Essential Bus

48
Q

Where is the Fuel/Hydraulic heat exchanger located

A

In Each Wing Fuel Tank.

49
Q

How Long do the Emergency lights illuminate

A

15 with normal ambient temperatures 10 minutes if Cold

50
Q

Oxygen Quantity Outside panel. Inside on MFD in cockpit

A

Outside - 1,850 psi. Inside 5,439 Liters.

51
Q

At what altitude will the EPAV drop the passenger masks in auto

A

14,500’ + - 500’

52
Q

When will the DCMP Hydraulic pumps run continuously

A

With Flaps beyond 10 degrees

53
Q

Minimum fuel for Go-Around

A

1,000 Lbs

54
Q

Edit…I need to check this…I think it’s supposed tp be LP not HP..air is used for what systems, and what is the Max psi

A

Engine Starting, Environmental and Pressurization. Max psi is 50.

55
Q

Pressure Relief valves are set to what psi

A

Over Pressure 9.4 psi. Under Pressure - .5 psi

56
Q

Cabin Altitude Caution CAS message.

A

8,500’ Cabin Altitude

57
Q

Cabin Altitude Red CAS Message

A

9,400’ Cabin Altitude

58
Q

Aircraft Batteries

A

24V NICAD 44 amp/hr

59
Q

Max Generator Loads with 2 Generators on the ground

A

400 amps

60
Q

Max Generator Loads with 1 Generator in flight

A

500 Amps

61
Q

Max Generator Load Transient

A

600 amps for 5 minutes.

62
Q

CVR lasts for how many hours

A

2 Hours

63
Q

FDR lasts for how many hours

A

25 Hours

64
Q

PMA - Permanent Magnet Alternator Powers what?

A

FADEC above 45% N2

65
Q

Aux Hydraulic pump pressure

A

2,500 - 3350 psi

66
Q

Pushing the Fire Switch does What 6 things

A
  1. Shuts down FADEC. 2. Arms Squibs. 3. Closes Fuel Shut-Off. 4. Closes Pneumatic Shut-off. 5. Closes Hydraulic Shut-off. 6. Generator selected Offline
67
Q

Ram Air Valve can only be opened below

A

10,000 feet

68
Q

In order to get To To on the flight director, you must have.

A

V speeds and Flaps set to takeoff

69
Q

Max Altitude with Yaw Damper off

A

31,000 feet

70
Q

Which EICAS message requires Immediate action

A

RED

71
Q

Total Circuit Breaker panels

A

4 in Cockpit, 1 in Galley, 2 in aft equipment bay.

72
Q

Nose wheel steering. Tiller and Rudder pedals.

A

Tiller - 65° Rudder Pedals - 7°

73
Q

Doors that must be unlocked for flight.

A

B O C A. Battery, Outflow, Cargo, Aft Equipment bay

74
Q

Apu Planned Fuel burn

A

150 Lbs per hour.

75
Q

Air Conditioning / Bleed panel is normally.

A

All on or All off.

76
Q

Configuration Warning.

A

PDFAST - Pretty Damn fast… Parking brake, Disconnect X Two, Flaps, Autopilot, Spoilers, Trims

77
Q

EICAS shows messages in what order?

A

Order of Importance, Order of Occurrence

78
Q

ROLS is what?

A

Remote Oil Level Sensor.

79
Q

Oil must be checked when?

A

5 minutes to 30 minutes after shut-down.

80
Q

What is the EPAV?

A

Electro Pneumatic Actuating Valve. ( Oxygen Control)

81
Q

How long do the Aft Equipment bay light stay on?

A

20 Minutes. After 15 Minutes the Lights will flash for 10 seconds and then turn off.

82
Q

Where are the Fire Extinguishers located?

A

Cockpit, Coat Closet and Lavatory.

83
Q

Where is the Therapeutic O2 Outlet located?

A

Behind the VIP Seat just ahead of the Emergency exit. The mask is in a drawer under the Divan.

84
Q

How much fuel is required to keep the Fuel Hydraulic cooler completely Submersed.

A

2,800 Pounds, 1,400 per side.

85
Q

Standby Instrument is powered by which bus?

A

Right Essential bus.

86
Q

Ditching switch available below what altitude?

A

15,000 feet

87
Q

Ditching switch only in what mode?

A

Auto

88
Q

What does the Ditching switch do?

A

Depressurizes the cabin, Disables the ECS (Flow Control Valves) and closes the Outflow valve.

89
Q

Emergency Depress Switch. Auto and Manual Modes.

A

Auto Mode: 2,500 FPM to 14,000’ + - 100’ Manual Mode: 3 000 FPM to 14,500’ + - 100’

90
Q

Emergency Depress Switch. Auto and Manual Modes.

A

Auto Mode: 2,500 FPM to 14,000’ + - 100’ Manual Mode: 3 000 FPM to 14,500’ + - 100’

91
Q

Oxygen Masks auto deploy at What altitude?

A

14,500’ + - 500 feet.

92
Q

At What altitude will Cabin Oxygen masks stop delivering Oxygen?

A

9,500’ + - 500 feet.

93
Q

When connecting External power to the aircraft, when will the Avail light come on?

A

When the Power is the correct Voltage and Polarity.

94
Q

HP air Provides air for which system? What psi is HP Air?

A

Anti-Ice; 36 psi.

95
Q

With less than 1,000 lbs of fuel per side, limit flight to less than.

A

30 Minutes.

96
Q

What happens when Engine Run switch is positioned to On?

A

Fuel Pumps On and FADEC is initialized.

Challenger 350 Terry's (1 decks)

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