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Limitations Flashcards

1
Q

Runway Requirements.
Length

A

4500

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2
Q

Crosswind
Dry or wet runway

A

24 kt

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3
Q

Maximum Crosswind
Contaminated Runway Condition
Fair/Medium
Poor

A

15 Kt Fair/Medium
10 Kt Poor

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4
Q

Tailwind

A

10 kt

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5
Q

RVSM speed limitation
Maximum cruise Mach number

A

M 0.83

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6
Q

RVSM
Equipment that must be operational:
6 items

A

Autopilot (1)
Altitude alerting devices (2)
AFDs displaying primary altimeters (2)
ATC altitude reporting transponder (1)
Air Data computers (ADC) (2)
Pitot probe heaters (2) on probes linked to the ADC in use

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7
Q

Fuel:
45-minute IFR Reserve

A

2019

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8
Q

Fuel:
Hot Spare

A

8500

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9
Q

Fuel:
Emergency

A

1500

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10
Q

Fuel:
Inclement Weather

A

6500-8500

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11
Q

Wi-Fi Limitations:
The use of KA SAT GND TX/KA BAND GND TX feature is prohibited when

A

During deice operations
One hundred feet of less from a building higher than the aircraft

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12
Q

Maximum takeoff weight is limited by the most restrictive of the following

A

Max certificated T/O weight.
Max runway-limited T/O weight.
Tire speed and brake energy limit weights.
Max takeoff weight (climb limited).
Obstacle clearance, en route, and landing weight limitations.

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13
Q

Landing weight is limited by the most restrictive of the following.

A

Max certificated landing weight.
Max landing weight (i.e., runway length plus obstacle).
Max landing weight (i.e., climb limited)

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14
Q

Max ramp & taxi weight

A

48,300 lbs

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15
Q

Max takeoff weight

A

48,200 lbs

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16
Q

Max landing weight

A

38,000 lbs

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17
Q

Max zero fuel weight

A

32,000 lbs

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18
Q

Baggage compartment limit

A

900 lbs

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19
Q

Altitudes
Operating

A

41,000

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20
Q

Altitudes
Pressure altitude Takeoff, landing

A

10,000

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21
Q

Altitudes
Flaps extended

A

15,500

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22
Q

Altitudes
Landing gear extended

A

20,000

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23
Q

Altitudes
Minimum for use of flight spoilers

A

300

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24
Q

Temperatures
Minimum takeoff
Maximum takeoff/landing

A

-40°C
ISA +35

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25
Q

Airspeed and Mach
flaps 20
30
45

A

231
197
189

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26
Q

Airspeed and Mach
Maximum landing gear extended speed

A

250/.7

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27
Q

Airspeed and Mach
Maximum landing gear operating speed

A

197/0.6 M

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28
Q

Airspeed and Mach
Maximum tire speed

A

182

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29
Q

Airspeed and Mach
Turbulent air penetration speed

A

280/0.75

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30
Q

Air Conditioning and Pressurization.
Maximum Differential

A

9.2

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31
Q

Air Conditioning and Pressurization.
Negative relief

A

-0.5

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32
Q

Air Conditioning and Pressurization.
Differential taxi and takeoff. Also differential for landing.

A

0.2

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33
Q

Air Conditioning and Pressurization.
Differential landing

34
Q

Oxygen.
Maximum number of passengers

35
Q

APU starting limits

A

3 attempts in 1 hour
3 30-second start attempt of continuous cranking, followed by 20 minutes of cooling time.
2 additional 30-second attempt of continuous cranking.
Using ground power, accomplish the following:
2 15-second start attemps of continuous carking, followed by 20-minutes of cooling time.
2 additional 15-second attempt of continuous cranking. in either case, if start is not successful, do not attempt additional start for at least 35 minutes.

36
Q

Runway Requirements.
Width

37
Q

Runway Requirements.
Slope +-

38
Q

Runway Requirements.
Ops review required if…

A

Contaminated: Less than 5800

39
Q

Autoflight
Minimum Altitude for autopilot. After takeoff

40
Q

Autoflight
Minimum Altitude for autopilot.
Category I ILS or LPV (GS ≤ 3.5°)

41
Q

Autoflight
Minimum Altitude for autopilot.
Precision approach (GS > 3.5° and < 4.5°)

42
Q

Autoflight
Minimum Altitude for autopilot.
Visual or IAP to MDA

43
Q

5G non-tolerant aircraft operating in the contiguous U.S. airspace, the following operations are prohibited

A

Autopilot operations on approach below 1000 ft AGL
Autothrottles operations on approach below 1000ft AGL
AOM 12.9

44
Q

AC Generator load limit
0 to 20,000
Main & APU

45
Q

AC Generator Load Limits
20,001 to 35,000
Main & APU

A

30kVA 0 for the APU

46
Q

AC Generator Load Limit
Above 35,000

A

Main 25kVA 0 for the APU

47
Q

Batteries
Minimum voltage for engines start or APU start:

48
Q

DC TRU load limit:
Maximum continuous

49
Q

Fuel pressure fueling
Main tank per tank.

50
Q

Fuel quantities. Pressure fueling
Auxiliary

51
Q

Fuel quantities
Pressure fueling
Tail

52
Q

Fuel quantities
Pressure fueling
Total

A

20,000 Gravity fueling (aircraft level) reduce pressure fueling weight by 7%.
15,722 lbs

53
Q

Fuel imbalance
Taxi, Takeoff landing

54
Q

Fuel imbalance
Inflight

55
Q

Minimum go-around fuel.
Per tank

56
Q

Fuel temperature Limitations
Do not take off if engine fuel temperature is below?

57
Q

Fuel Jettison limitations

A

Flap setting for fuel jettison: 0
Do not jettison fuel in known lightning conditions

58
Q

Fuel transfer

A

Fuel transfer (left or right tank to auxiliary tank/gravity) must be off for takeoff.
During normal operations, tail tank transfer system must not be used as a center of gravity control device: it must remain selected to the automatic mode.

59
Q

Determine Auxiliary tank quantity (lb). Greater than 1200.
Less than 1200

A

2.75 x tail tank qty

2.2 x tail tank qty

60
Q

Fuel transfer
When do you NOT manually transfer tail tank fuel?

A

With more than 7000 lb of fuel in the auxiliary tank.

61
Q

Ice and Rain Protection
Icing conditions exist on the ground when operating on contaminated, runway surfaces, or the following conditions are present: ground

A

•SAT at 10°C or below
• Visible, moisture, (i.e. rain, snow, or visible the less than 1 sm)

62
Q

Ice and Rain Protection
Icing conditions exist on the ground when operating on contaminated, runway surfaces, or the following conditions are present: in flight

A

•TAT at 10°C or below
• Visible, moisture, (i.e. rain, snow or visibility, less than one sm ), except when SAT is -40°C or below.

63
Q

Ice and rain protection
Flight in freezing rain is

A

Prohibited

64
Q

Ice and rain protection
If the engine, cow or wing anti-ice system are selected on.

A

Close, bleed air 10th stage valves for takeoff and land.

65
Q

Ice and rain protection
Time and temperature limit on probes

A

Two minutes when TAT is 15°C or greater.

66
Q

Display unit operating temperature

A

Do not power display units on ground when flight compartment temperatures exceed 40°C for more than 30 minutes unless at least one air conditioning pack is operating and passenger door is closed.

67
Q

Landing gear
Brakes, time limit

A

Minimum turn time: 15 min

68
Q

APU Maximum altitude for start

69
Q

APU Minimum temperature for start on ground

70
Q

APU Maximum temperature during start ITT

71
Q

APU Maximum operating altitude

72
Q

APU Single engine inflight restart

A

APU use prohibited

73
Q

Maximum altitude for bleed air use from the APU.

74
Q

APU Maximum speed for start and operation

75
Q

During taxi to warm the brakes to prevent them from retaining moisture after takeoff.
Greater than 42,000
36,000-42,0000
Less than 36,000

76
Q

Minimum temperature for Start engines

A

-40°C. AOM 4.2.1.2

77
Q

Engine Start cycles limitations

A

Three consecutive engine starter cycles with five minutes cooling between additional cycles. Start cycle is limited to 60 seconds

78
Q

ITT for engine starts on the ground

A

120°C or less for all ground starts

79
Q

Dry motoring limits for engine

A

first 90 sec 5 minutes off
Second and subsequent 30 sec 5 minutes off

80
Q

Thrust reversers below 60kts maximum N1

81
Q

Continuous Ignition is used when?

A
  • Takeoff or landing on contaminated runways
  • Takeoff with high crosswind
  • Moderate of heavier intensity rain
  • Moderate or heavier intensity turbulence
  • In the vicinity of thunderstorms

CL 650 (15 decks)

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