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CL 650 > Limitations > Flashcards

Limitations Flashcards

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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
Airspeed and Mach flaps 20 30 45
231 197 189
26
Airspeed and Mach Maximum landing gear extended speed
250/.7
27
Airspeed and Mach Maximum landing gear operating speed
197/0.6 M
28
Airspeed and Mach Maximum tire speed
182
29
Airspeed and Mach Turbulent air penetration speed
280/0.75
30
Air Conditioning and Pressurization. Maximum Differential
9.2
31
Air Conditioning and Pressurization. Negative relief
-0.5
32
Air Conditioning and Pressurization. Differential taxi and takeoff. Also differential for landing.
0.2
33
Air Conditioning and Pressurization. Differential landing
0.2
34
Oxygen. Maximum number of passengers
14
35
APU starting limits
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
Runway Requirements. Width
75
37
Runway Requirements. Slope +-
2%
38
Runway Requirements. Ops review required if…
Contaminated: Less than 5800
39
Autoflight Minimum Altitude for autopilot. After takeoff
320 feet
40
Autoflight Minimum Altitude for autopilot. Category I ILS or LPV (GS ≤ 3.5°)
80 feet
41
Autoflight Minimum Altitude for autopilot. Precision approach (GS > 3.5° and < 4.5°)
160 feet
42
Autoflight Minimum Altitude for autopilot. Visual or IAP to MDA
320 feet
43
5G non-tolerant aircraft operating in the contiguous U.S. airspace, the following operations are prohibited
Autopilot operations on approach below 1000 ft AGL Autothrottles operations on approach below 1000ft AGL AOM 12.9
44
AC Generator load limit 0 to 20,000 Main & APU
30 kVA
45
AC Generator Load Limits 20,001 to 35,000 Main & APU
30kVA 0 for the APU
46
AC Generator Load Limit Above 35,000
Main 25kVA 0 for the APU
47
Batteries Minimum voltage for engines start or APU start:
22V
48
DC TRU load limit: Maximum continuous
100A
49
Fuel pressure fueling Main tank per tank.
4860
50
Fuel quantities. Pressure fueling Auxiliary
7168
51
Fuel quantities Pressure fueling Tail
3112 lbs
52
Fuel quantities Pressure fueling Total
20,000 Gravity fueling (aircraft level) reduce pressure fueling weight by 7%. 15,722 lbs
53
Fuel imbalance Taxi, Takeoff landing
400 lbs
54
Fuel imbalance Inflight
800 lbs
55
Minimum go-around fuel. Per tank
500 lbs
56
Fuel temperature Limitations Do not take off if engine fuel temperature is below?
5°C
57
Fuel Jettison limitations
Flap setting for fuel jettison: 0 Do not jettison fuel in known lightning conditions
58
Fuel transfer
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
Determine Auxiliary tank quantity (lb). Greater than 1200. Less than 1200
2.75 x tail tank qty 2.2 x tail tank qty
60
Fuel transfer When do you NOT manually transfer tail tank fuel?
With more than 7000 lb of fuel in the auxiliary tank.
61
Ice and Rain Protection Icing conditions exist on the ground when operating on contaminated, runway surfaces, or the following conditions are present: ground
•SAT at 10°C or below • Visible, moisture, (i.e. rain, snow, or visible the less than 1 sm)
62
Ice and Rain Protection Icing conditions exist on the ground when operating on contaminated, runway surfaces, or the following conditions are present: in flight
•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
Ice and rain protection Flight in freezing rain is
Prohibited
64
Ice and rain protection If the engine, cow or wing anti-ice system are selected on.
Close, bleed air 10th stage valves for takeoff and land.
65
Ice and rain protection Time and temperature limit on probes
Two minutes when TAT is 15°C or greater.
66
Display unit operating temperature
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
Landing gear Brakes, time limit
Minimum turn time: 15 min
68
APU Maximum altitude for start
20,000 ft
69
APU Minimum temperature for start on ground
-40°C
70
APU Maximum temperature during start ITT
974°C
71
APU Maximum operating altitude
20,000 ft
72
APU Single engine inflight restart
APU use prohibited
73
Maximum altitude for bleed air use from the APU.
15,000 ft
74
APU Maximum speed for start and operation
290 KIAS
75
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
5,6,7
76
Minimum temperature for Start engines
-40°C. AOM 4.2.1.2
77
Engine Start cycles limitations
Three consecutive engine starter cycles with five minutes cooling between additional cycles. Start cycle is limited to 60 seconds
78
ITT for engine starts on the ground
120°C or less for all ground starts
79
Dry motoring limits for engine
first 90 sec 5 minutes off Second and subsequent 30 sec 5 minutes off
80
Thrust reversers below 60kts maximum N1
60% N1
81
Continuous Ignition is used when?
* 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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