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C5 E145 Nov 2020 > Limitations (w Notes) > Flashcards

Limitations (w Notes) Flashcards

1
Q

Minimum Total Air Temperature in Cruise Flight Above 25,000 ft.

A

-45°C

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2
Q

Max. Ramp Weight (MRW)

A

XR: 53,351 lbs
LR: 50,044 lbs

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3
Q

Max. Takeoff Weight (MTOW)

A

XR: 53,131 lbs
LR: 49,823 lbs

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4
Q

Max. Landing Weight (MLW)

A

XR: 44,092 lbs
LR: 43,651 lbs

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5
Q

Max. Zero Fuel Weight (MZFW)

A

XR: 40,785 lbs
LR: 40,564 lbs

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6
Q

V LO for retraction

A

200 KIAS

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7
Q

V LO for extension

A

250 KIAS

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8
Q

V LE

A

250 KIAS

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9
Q

V A

A

200 KIAS

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10
Q

Max. Flap Extension Speed - Flaps 9°

A

250 KIAS

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11
Q

Max. Flap Extension Speed - Flaps 9°

Above 10,000 ft. and Y/D Diseng.

A

250 KIAS

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12
Q

Max. Flap Extension Speed - Flaps 18°

A

200 KIAS

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13
Q

Max. Flap Extension Speed - Flaps 18°

Above 10,000 ft. and Y/D Diseng.

A

200 KIAS

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14
Q

Max. Flap Extension Speed - Flaps 22°

A

200 KIAS

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15
Q

Max. Flap Extension Speed - Flaps 22°

Above 10,000 ft. and Y/D Diseng.

A

180 KIAS

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16
Q

Max. Flap Extension Speed - Flaps 45°

A

160 KIAS

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17
Q

Max. Flap Extension Speed - Flaps 45°

Above 10,000 ft. and Y/D Diseng.

A

145 KIAS

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18
Q

Maximum Takeoff and Landing Tailwind Component

A

10 kt

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19
Q

Maximum Usable Fuel Quantity Per Tank (Wing)

A

844.9 US Gal (5717 lb)

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20
Q

Unusable Quantity Per Tank (Wing)

A

5.8 US Gal (39 lb)

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21
Q

Maximum Usable Fuel Quantity (Ventral Tank)

A

275.3 US Gal (1863 lb)

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22
Q

Unusable Quantity (Ventral Tank)

A

3.1 US Gal (21 lb)

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23
Q

Maximum Permitted Imbalance Between Tanks

A

800 lb

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24
Q

Minimum Fuel Tank Temperature

A

-40°C

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25
Q

Maximum Fuel Tank Temperature

A

52°C

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26
Q

Minimum Temperature for APU Operation

A

-54°C

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27
Q

Maximum Altitude for APU Start

A

30,000 ft

28
Q

Maximum Altitude for APU Operation

A

37,000 ft

29
Q

Maximum Rotor Speed for APU Operation

A

108%

Note: automatically shut down at 104% rotor speed

30
Q

Minimum Battery Temperature for APU Start

A

-20°C

31
Q

Maximum APU EGT Start Temperature

A

884°C

32
Q

APU Max. Continuous EGT Temperature

A

680°C

33
Q

APU Max EGT Temperature

A

717°C for 5 minutes max.

34
Q

APU Starter Limits

A

Between Three Consecutive Attempts… 1 Minute Off

Between Two Series of Three Consecutive Attempts… 30 Minutes Off

35
Q

Engine Type

A

XR: Rolls-Royce AE3007A1E

LR: Rolls-Royce AE3007A1P

36
Q

Engine Max N1

A

100%

37
Q

Engine Max N2

A

XR: 105%
LR: 102.4%

38
Q

Engine Max ITT on Start

A

800°C

39
Q

Engine Max ITT (Takeoff Modes)

A

XR: 970°C
Note: Takeoff thrust limited to 5 min.

LR: 948°C

992°C
Note: Temps between 971°C and 992°C limited to 90 sec.

40
Q

Engine Max Continuous ITT

A

XR: 935°C
LR: 901°C

41
Q

Oil Pressure Below 88% N2

A

34 - 110psi* **

Note*: May be exceeded during starts if oil temp is below 21°C. Eng must remain at IDLE until oil pressure is less than 110 psi.

Note**: Operation in oil pressure amber range is permitted between 111-115 psi in all operational modes, time limited to 5 min. or between 116-155 psi in app operational modes, time limited to 2 min. Total time above 110 psi may not exceed 5 min.

42
Q

Oil Pressure At or Above 88% N2

A

48* - 110** psi

Note*: While this is an abnormal condition, operation between 48 and 34 psi is permitted during take off and go-around phases.

Note**: Operation in oil press. amber range is permitted between 111-115 psi in all operational modes, time limited to 5 min. or between 116-155 psi in app operational modes, time limited to 2 min. Total time above 110 psi may not exceed 5 min.

43
Q

Min. Engine Oil Temperature

A

21°C

Note: Min oil temp. for starting is -40°C for lube oil MIL-L-23699D and -54°C for lube oil MIL-L-7808K

44
Q

Max. Engine Oil Temperature

A

126°C

45
Q

Max. Engine Vibration

A

LP Spool: 1.8 IPS
HP Spool: 1.1 IPS

Note: Vibration in amber range below 2.5 IPS is time limited to 5 min. during takeoff or go-around phases or 10 sec. during the remainder flight phases.

46
Q

Takeoff Thrust Modes

A

E T/O
T/O
Alt T/O-1

Note: All takeoff thrust modes are limited to 5 minutes, beginning when takeoff thrust is applied during the takeoff roll.

47
Q

Engine Starter Limits on Ground

A

Starting or Dry Motoring… Up to 5 minutes on, 5 minutes off
-OR-
First through Fourth Cycles… 1 minute on, 1 minute off
Following Cycles… 1 minute on, 5 minutes off

48
Q

Engine Starter Max. Continuous Operation Time in Flight

A

5 minutes on

Note: No cool down time is required shall an in-flight start be reattempted.

49
Q

Engine Warm Up Time

A

Cold Engines*: 4 min
Warm Engines: 2 min

Before takeoff to increase N2 above 83%, engine oil temp. must be at 40°C minimum. In lieu of this limit is acceptable to run the engine for at least 8 minutes in idle or taxi thrust, and check if the temperature is at least 21°C.

Note*: The engine is considered cold if it has been shut down for more than 90 min.

50
Q

Engine Cool Down Time

A

2 min.

51
Q

Maximum Temperature for Anti-Icing Operation

A

10°C

52
Q

Minimum Temperature for Manual Anti-Icing Operation

A

-40°C

53
Q

Holding Configuration

A

Landing Gear… Up
Flaps… Up
Minimum Airspeed… 200 KIAS

54
Q

Max. Airspeed for Windshield Wiper Operation

A

170 KIAS

55
Q

Maximum Load on Main Generator

A

400A

56
Q

Maximum Load on APU Generator

A

Up to 30,000 ft: 400A

Above 30,000 ft: 300A

57
Q

Maximum Battery Temperature for APU Operation

A

70°C

58
Q

Maximum Differential Pressure

A

7.8 psi

59
Q

Maximum Differential Overpressure

A

8.1 psi

60
Q

Maximum Differential Negative Pressure

A

-0.3 psi

61
Q

Maximum Altitude for Flap Extension

A

20,000 ft

62
Q

Autopilot Minimum Decision Altitude During ILS Approach

A

200 ft AGL

63
Q

Autopilot Minimum Engagement High After Takeoff

A

500 ft

64
Q

Autopilot Minimum Use Height

A

XR: 160 ft
LR: 200 ft

65
Q

Autopilot Malfunction Altitude Loss

A

Cruise: 80 ft
Maneuver: 40 ft
ILS Approach: 35 ft

66
Q

Closet Floor Weight Limitation

A

100 lbs

67
Q

Cargo Area Weight Limitation

A

2,646 lbs

Note: No personnel in cargo area with less than 2,000 lbs of fuel on board. Advise Ops if the aircraft has less than 2,000 lbs of fuel.

C5 E145 Nov 2020 (10 decks)

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