Limitations Flashcards

1
Q

Maximum Ramp Weight

A

36,400 lbs

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2
Q

Maximum Takeoff Weight

A

36,100 lbs

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3
Q

Maximum Landing Weight

A

31,800 lbs

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4
Q

Maximum Zero Fuel Weight

A

24,400 lbs

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5
Q

Maximum Altitude for Takeoff and Landing

A

14,000 feet

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6
Q

Maximum Tailwind Component

A

10 knots

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7
Q

Minimum Altitude for In-Flight use of the Speedbrakes

A

500 feet AGL

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8
Q

Maximum Asymmetric Fuel

A

400 lbs

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9
Q

Maximum Emergency Asymmetric Fuel

A

800 lbs

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10
Q

Minimum Wing Fuel Per Tank for Takeoff

A

500 lbs

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11
Q

Takeoff in High Idle is…..

A

Prohibited (except for touch and go)

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12
Q

Maximum Operating Altitude

A

51,000 ft.

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13
Q

Unusable Fuel Quantity - Wings/Center Tank

A
  1. 81 gallons in each wing tank

2. 2 gallons in the center tank

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14
Q

Maximum Single Point Refueling PSI

A

55 psi

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15
Q

Maximum Single Point Defueling PSI

A

-10 psi

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16
Q

Center tank to wing transfer must be initiated prior to _______ lbs per side wing fuel?

A

3100 lbs

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17
Q

Simultaneous use of crossfeed and center-to-wing tank transfer is prohibited when the wing fuel quantity is ________ lbs or less per side?

A

2900 lbs

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18
Q

How many FADEC’s must be operational for takeoff?

A

All 4 must be operational

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19
Q

Both Air Data Computers Must be Operational for Takeoff: True or False

A

True

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20
Q

What is the minimum start duct pressure (EICAS) prior to ground start?

A

25 psi

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21
Q

FADEC automatic overspeed shutdowns are set at ______ % N1 and _______ % N2.

A

105% N1

105.6% N2

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22
Q

Minimum fan speed for takeoff is _______ ?

A

73.6% N1

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23
Q

ENGINE AIR TURBINE STARTER LIMITS
____ consecutive normal starts followed by ____ minutes cooling are permitted. One ____ second motoring cycle is equivalent to one normal start.

A

3
25
30

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24
Q

Do not engage the air turbine starter above ____ % N2 RPM. Air turbine starter drive shaft damage can occur.

A

25%

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25
Q

Main Generator Limit up to FL410 is _____ AMPS.

A

400 AMPS

26
Q

Main Generator Limit above FL410 is _____ AMPS.

A

300 AMPS

27
Q

If a ground pneumatic cart is being used for engine start, it must be capable of maintaining a minimum air pressure of _____ PSI, as displayed in the EICAS, prior to initiating the start.

A

30 PSI

28
Q

The use of engine synchronization is prohibited during ________ & _________, and ________ ________ _______, or FADEC ADC or N1 reversionary operations.

A

Takeoff
Landing
Single Engine Operations

29
Q

Minimum Flight Crew for All Operations?

A

2 - Pilot and Copilot

30
Q

During taxi, takeoff and landing when the belted toilet seat is occupied, the aft divider sliding doors must be ______ _____ .

A

latched open

31
Q

Maximum Operating Mach above 30,650 feet?

A

.92 indicated

32
Q

Maximum Operating Mach with the Mach Trim Off?

A

.82 indicated

33
Q

Maximum Altitude to Operate the APU

A

31,000 feet

34
Q

Use of the baggage compartment is/is not authorized with the cabin unpressurized?

A

is not

35
Q

The baggage compartment smoke detection system must be ____________ if baggage is to be carried in the compartment.

A

operational

36
Q

Live animals ____ ____ be carried in the baggage compartment.

A

may not

37
Q

What is the maximum operating altitude with the baggage compartment unpressurized?

A

41,000 feet

38
Q

What is the maximum weight that can be carried in the baggage compartment?

A

700 lbs

39
Q

What is the maximum floor loading distribution in the baggage compartment?

A

170 lbs per square foot

40
Q

What is the maximum weight that can be carried in the ski holding compartment?

A

75 lbs

41
Q

What is the autopilots minimum use height in cruise?

A

1000 ft. AGL

42
Q

What is the autopilots minimum use height during a precision approach (Category I ILS) ?

A

170 ft. AGL

43
Q

What is the autopilots minimum use height during a nonprecision approach?

A

400 ft. AGL

44
Q

Autopilot coupled operation with single operational or displayed attitude and heading source is ____________?

A

prohibited

45
Q

The Citation X is approved for Category ____ and ____ operations?

A

I

II

46
Q

Autopilot coupled ILS approaches with the flaps up are ____________?

A

prohibited

47
Q

Crew oxygen mask must be _______, _______ and _______ _____ prior to flight.

A

checked
adjusted
correctly stowed

48
Q

Crew oxygen mask are not approved for sustained operation at a cabin altitude greater than _______ feet.

A

40,000

49
Q

Passenger oxygen mask are not approved for sustained operation at a cabin altitude greater than _______ feet.

A

25,000

50
Q

Maximum Flap Extended Speed - VFE 5° ?

A

250 KIAS

51
Q

Maximum Flap Extended Speed - VFE 15° ?

A

210 KIAS

52
Q

Maximum Flap Extended Speed - VFE Full?

A

180 KIAS

53
Q

Maximum Slat Extended Speed?

A

250 KIAS

54
Q

What is the maximum tire ground speed?

A

182 knots

55
Q

What is the length of the Citation X…..?

A

72.34 feet

56
Q

What is the width of the Citation X….?

A

63.64 feet

57
Q

What is the height at the tail….?

A

19.15 feet

58
Q

What is the cabin length?

A

23 feet

59
Q

What is the cabin height?

A

5 feet 8 inches

60
Q

What is the cabin width?

A

5 feet 7 inches