Limitations Flashcards

(60 cards)

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
Main Generator Limit up to FL410 is _____ AMPS.
400 AMPS
26
Main Generator Limit above FL410 is _____ AMPS.
300 AMPS
27
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.
30 PSI
28
The use of engine synchronization is prohibited during ________ & _________, and ________ ________ _______, or FADEC ADC or N1 reversionary operations.
Takeoff Landing Single Engine Operations
29
Minimum Flight Crew for All Operations?
2 - Pilot and Copilot
30
During taxi, takeoff and landing when the belted toilet seat is occupied, the aft divider sliding doors must be ______ _____ .
latched open
31
Maximum Operating Mach above 30,650 feet?
.92 indicated
32
Maximum Operating Mach with the Mach Trim Off?
.82 indicated
33
Maximum Altitude to Operate the APU
31,000 feet
34
Use of the baggage compartment is/is not authorized with the cabin unpressurized?
is not
35
The baggage compartment smoke detection system must be ____________ if baggage is to be carried in the compartment.
operational
36
Live animals ____ ____ be carried in the baggage compartment.
may not
37
What is the maximum operating altitude with the baggage compartment unpressurized?
41,000 feet
38
What is the maximum weight that can be carried in the baggage compartment?
700 lbs
39
What is the maximum floor loading distribution in the baggage compartment?
170 lbs per square foot
40
What is the maximum weight that can be carried in the ski holding compartment?
75 lbs
41
What is the autopilots minimum use height in cruise?
1000 ft. AGL
42
What is the autopilots minimum use height during a precision approach (Category I ILS) ?
170 ft. AGL
43
What is the autopilots minimum use height during a nonprecision approach?
400 ft. AGL
44
Autopilot coupled operation with single operational or displayed attitude and heading source is ____________?
prohibited
45
The Citation X is approved for Category ____ and ____ operations?
I | II
46
Autopilot coupled ILS approaches with the flaps up are ____________?
prohibited
47
Crew oxygen mask must be _______, _______ and _______ _____ prior to flight.
checked adjusted correctly stowed
48
Crew oxygen mask are not approved for sustained operation at a cabin altitude greater than _______ feet.
40,000
49
Passenger oxygen mask are not approved for sustained operation at a cabin altitude greater than _______ feet.
25,000
50
Maximum Flap Extended Speed - VFE 5° ?
250 KIAS
51
Maximum Flap Extended Speed - VFE 15° ?
210 KIAS
52
Maximum Flap Extended Speed - VFE Full?
180 KIAS
53
Maximum Slat Extended Speed?
250 KIAS
54
What is the maximum tire ground speed?
182 knots
55
What is the length of the Citation X…..?
72.34 feet
56
What is the width of the Citation X….?
63.64 feet
57
What is the height at the tail….?
19.15 feet
58
What is the cabin length?
23 feet
59
What is the cabin height?
5 feet 8 inches
60
What is the cabin width?
5 feet 7 inches