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Challenger 300 > CL30 Limitations > Flashcards

CL30 Limitations Flashcards

1
Q

Max Taxi and Ramp Weight

A

39,000 lb

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2
Q

Max Takeoff Weight

A

38,850 lb

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3
Q

Max Landing Weight

A

33,750 lb

(5,100 lb less than Max Takeoff)

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4
Q

How much fuel must you burn before landing if you took off at Max Takeoff Weight?

A

5,100 lb

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5
Q

Max Zero Fuel Weight

A

27,200 lb

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6
Q

Maxumum Usable Fuel (lb) - Pressure Refuel

A

14,150 lb Total

(7,075 lb / Side)

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7
Q

Maxumum Usable Fuel (lb) - Gravity Refuel

A

13,000 lb Total

(6,500 lb / Side)

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8
Q

Maximum Fuel imbalance

A

Varies from 250 - 600 lb

250 lbs with Total fuel more than 13,700 lbs

600 lbs with Total fuel less than 4,700 lbs

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9
Q

Minumum Fuel for Go-Around

A

500 lb per side

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10
Q

Maximum Bulk Fuel Temp for TakeOff

A

50 C

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11
Q

Minimum Bulk Fuel Temps for Takeoff

A

-30 (Jet A)

  • 35 (Jet 1)
  • 40 (Jet B)
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12
Q

Fuel X-Flow Position For TakeOff

A

Power and Gravity X-Flow Must be OFF

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13
Q

Maximum Operating Altitude

A

45,000 ft

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14
Q

Maximum Takeoff and Landing Altitude

A

10,000 ft

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15
Q

Minimum Altitude for Autopilot Useage

(Climb, Enroute or Descent)

A

700 ft AGL

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16
Q

Minimum Altitude for Autopilot Useage

(Visual or Non Precision)

A

200 ft AGL

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17
Q

Minimum Altitude for Autopilot Useage

(Precision Approach with Glidepath of 3.5 or less)

A

80 ft AGL

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18
Q

Minimum Altitude for Autopilot Useage

(Precision Approach with Glidepath 4.5 or less)

A

160 ft AGL

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19
Q

Maximum Altitude with Yaw Damper OFF

A

31,000 ft

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20
Q

Maximum Gear Extension Altitude

A

18,000 ft

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21
Q

Maximum Flaps Extension Altitude

A

18,000 ft

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22
Q

Minimum Altitude for Spoilers

A

500 ft AGL

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23
Q

Maximum Altitude With the APU Running

A

37,000 ft

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24
Q

Maximum Altitude with APU GEN

A

30,000 ft

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25
Q

Maximum Altitude with ECS Bleed

A

20,000 ft

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26
Q

Maximum Altitude for Engine (APU) Start

A

20,000 ft

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27
Q

Maximum Altitude for Crew/PAX O2 Masks

A

40,000 ft

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28
Q

Maximum Tailwind Component

A

10 knots

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29
Q

Maximum Demonstrated Crosswind (Takeoff)

A

28 knots for Takeoff

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30
Q

Maximum Demonstrated Crosswind (Landing)

A

24 knots for landing

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31
Q

Maximum Demonstrated Crosswind (NWS Inop)

A

15 knots

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32
Q

Maximum Demonstrated Crosswind (On AHRS Channel Inop)

A

15 kntos

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33
Q

Vmo (Up to 8,000 ft)

A

300 KIAS

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34
Q

Vmo (8,001 - 29,475 ft)

A

320 KIAS

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35
Q

Mmo (Above 29,475 ft)

A

0.83 Mach

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36
Q

Vra (Rough Air Penetration Speed)

A

265 KIAS / 0.75 Mach

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37
Q

VLO ret

A

200 KIAS

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38
Q

VLO ext

A

250 KIAS

39
Q

VLE (Operations with the Gear Extended)

A

250 KIAS

40
Q

VFE (10/20)

A

210 KIAS

41
Q

VFE (30)

A

175 KIAS

42
Q

Tire Speed Limit

A

182 KIAS

43
Q

Minimum Spoiler Speed

A

VAPP + 8 KIAS

44
Q

Thrust Reverse IDLE Only

A

Below 40 KIAS

45
Q

Use of Engine Anti-Ice In Flight

A

SAT (Static Air Temperature) is 10 to -40 C with visible moisture, or when ICE DETECTED CAS message is displayed.

46
Q

Minimum Temp for Takeoff

A

-40 C

47
Q

Minimum Oil Temperature for Starting

A

-40 C

48
Q

After three start attempts, how long must the starter be allowed to cool?

A

15 min cooling period

49
Q

How long should an starter be allowed to cool after a 5 minutes (cranking) attempt?

A

15 min

50
Q

How long must an engine be motored after an aborted start?

A

30 sec

51
Q

Minimum Oil Pressure At IDLE

A

28 psi

52
Q

Minimum Idle N2

A

46.0%

53
Q

Max Ground Start ITT

A

650 C

54
Q

Maximum ITT to Begin a Start

A

350 C

55
Q

Maximum Generator Electrical Load (2 or 3 Gens Operating)

A

400 amps

56
Q

Maximum Generator Electrical Load (1 Gen on the ground)

A

400 amps

57
Q

Maximum Generator Electrical Load (1 Gen in Flight)

A

500 amps

58
Q

Maximum Generator Electrical Load (Transient 5 min)

A

600 amps

59
Q

Maximum APU RPM

A

108%

60
Q

Maximum APU EGT (Start)

A

973 C

61
Q

Maximum APU EGT (Normal)

A

718 C

62
Q

How many start attempts do you get to start the APU?

A

3, followed by a 1 minute cooling period.

63
Q

How much of a cooling period do you need after each of your 3 APU start attempts?

A

1 min

64
Q

How long of a cooling period do you need after the 3rd APU start attempt?

A

20 min

65
Q

How long should you wait to make another APU start, after a successful start.

A

10 min

66
Q

How many successful start attemps can you make with 10 minute cooling intervals before you need to wait an hour?

A

6 attempts

67
Q

How long do you need to wait after 6 successful starting attempts?

A

1 hour

68
Q

Can you use the APU during de/anti-ice operations?

A

No - Use is Prohibited.

69
Q

Is TakeOff with a APU SHUTDOWN CAS Message allowed?

A

No - Takeoff without inspection is prohibited.

70
Q

Five Limitations for use of Thrust Reverse

A
  1. Use on paved surfaces only. 2. Do not deploy in flight. 3. Do not back up the airplane. 4. No use for touch and go landings. 5. Below 40 KIAS - IDLE Only.
71
Q

TRIM AIR ONLY

A

Prohibited on ground.

72
Q

Max Pressurization Differential On Ground

A

0.1 psi

73
Q

Max Pressurization Differential - Landing

A

1.0 psi

74
Q

Max Pressurization Differential (Positive)

A

9.4 psi

75
Q

Max Pressurization Differential (Negative)

A

-0.5 psi

76
Q

Minimum flight weight?

A

23,100 lbs

77
Q

To be used for navigation, the FMS must be recieving:

A
  1. One VOR/DME or 2. Two DMEs or 3. GPS (RAIM must be available)
78
Q

Minimum battery temp for takeoff?

A

-20 C

79
Q

Use of Takeoff Power (time)?

A

5 min

80
Q

Use of APR power (auto)?

A

10 min

81
Q

Use of APR power (manual)?

A

5 min

82
Q

When should you remove the battery?

A

When the temp is expected to be less than -30 C for more than 10 hours.

83
Q

What is the limitation for use of battery or GPU on the ground?

A

If temp is above 40 C, no more than 30 min.

84
Q

Minimum Oil temp for above Idle?

A

5 C

85
Q

Minimum Oil temp for Takeoff?

A

15 C

86
Q

Maximum pressure for pressure refueling?

A

55 psi

87
Q

Maximum pressure for pressure defueling?

A

-8.0 psi

88
Q

Types of operation

A

Day, Night, VMC, IMC Icing

89
Q

What equippment is required for RVSM?

A

Autopilot Altitude Alerting System One Altitude Reporting Transponder Two Air Data Computers

90
Q

Restriction on Holding in Ice

A

No Flaps

91
Q

Side window building ice

A

Assume flight in super cooled large droplets. Wing and Engine anti-ice ON Leave icing conditions as soon as possible.

92
Q

Engine Anti-Ice System On For Takeoff (Ground)

A

OAT 10 C or colder with visible moister (such as fog with vis. of 1 mile or less).

93
Q

Engine Anti-Ice System On For Taxi (Ground)

A

OAT 10 C or colder with surface contaminants

Challenger 300 (2 decks)

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