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CRJ > 200 Limitations > Flashcards

200 Limitations Flashcards

1
Q

Max Ramp Weight (200)

A

53,250 lbs

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2
Q

Max Takeoff Weight (200)

A

53,000 lbs

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3
Q

Max Landing Weight (200)

A

47,000 lbs

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4
Q

Max Zero Fuel Weight (200)

A

44,000 lbs

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5
Q

Min Flight Weight (200)

A

30,000 lbs

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6
Q

Max Cargo Weight - Comp 61 (200)

A

3500 lbs

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7
Q

Flight must be within ____ minutes of a suitable airport if cargo is carried in the cargo compartment (200)

A

45 min

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8
Q

Max turbulent air speed

A

280 KIAS or M .75 (whichever is lower)

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9
Q

Max Operating Speed (200)

A

M .85 or 335 KIAS

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10
Q

Max relief differential pressure

A

8.7 PSI

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11
Q

Max negative differential pressure

A

-0.5 PSI

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12
Q

Max differential pressure for taxi, takeoff and landing

A

0.1 PSI

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13
Q

Min cabin altitude in MANUAL mode

A

-1,500 ft

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14
Q

Max altitude for single PACK ops (200)

A

25,000 ft

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15
Q

Normal minimum autopilot altitude

A

600 AGL

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16
Q

Min autopilot altitude for visual and non-precision approaches

A

400 AGL

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17
Q

Min autopilot altitude for precision approaches

A

80 AGL

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18
Q

Max pressure altitude for FMS calculated thrust setting (200)

A

36,000 ft

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19
Q

Min altitude for true north operations

A

10,000 ft

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20
Q

Min RVR for rolling takeoff when HGS guidance is used

A

1200 RVR

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21
Q

Min autopilot altitude during an “A” mode approach with the HGS

A

650 ft

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22
Q

Max individual AC generator load [Main Generator] (200)

A

0 to 35,000 ft - 30 kVA

Above 35,000 ft - 25 kVA

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23
Q

Max individual AC generator load [APU Generator] (200)

A

30 kVA

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24
Q

Max APU altitude (200)

A

37,000 ft

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25
Q

Max continuous load on each TRU (200)

A

100 AMPS

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26
Q

Max time on ground with DC power only

A

5 min (to protect CRT displays)

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27
Q

Max airpseed with ADG deployed

A

Vmo/Mmo

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28
Q

Max altitude for SLATS/FLAPS operation

A

15,000 ft (enroute use of slats/flaps prohibited)

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29
Q

Flaps 8 (200)

A

Vfo - 200 KIAS

Vfe - 230 KIAS

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30
Q

Flaps 20 (200)

A

Vfo - 200 KIAS

Vfe - 230 KIAS

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31
Q

Flaps 30 (200)

A

185 KIAS

32
Q

Flaps 45 (200)

A

170 KIAS

33
Q

Min altitude for use of flight spoilers

A

300 AGL

34
Q

Min engine fuel temperature for takeoff

A

5 C

35
Q

Bulk Fuel Takeoff Limit [Jet A]

A

-30 C

36
Q

Bulk Fuel Freezing Point [Jet A]

A

-40 C

37
Q

Takeoff with a fuel load in excess of 500 lbs in the centre tank is not permitted unless:

A

-Each main wing tank is above 4400 lbs; or

-Each wing tank is above 2000 lbs and the allowable zero fuel weight is reduced by the weight of the fuel in the centre tank in excess of 500 lbs

38
Q

Max fuel imbalance between main tanks (200)

A

800 lbs

39
Q

Min fuel in each wing tank for go-around (200)

A

450 lbs (wings level and max climb attitude of 10 deg nose up)

40
Q

Prolonged ground operation with any hydraulic system operating should be avoided when ambient temperatures are greater than ___

A

40 C

41
Q

Normal hydraulic system pressure

A

2800 to 3200 PSI

42
Q

Normal hydraulic system quantity

A

45% to 85%

43
Q

Max airpseed for windshield wiper operations (200)

A

220 KIAS

44
Q

Max Landing Gear Speed [Extension] (200)

A

250 KIAS

45
Q

Max Landing Gear Speed [Retraction]

A

200 KIAS

46
Q

Tire Limit Speed (200)

A

182 kt ground speed

47
Q

Min brake cooling time between landing or rejected takeoff and subsequent takeoff

A

15 min

48
Q

Taxi Light limitation

A

Must be switched off when stationary for more than 10 min

49
Q

The starter must not be engaged if indicated N2 rpm exceeds ___ (200)

A

55%

50
Q

Starter Cranking Limits (200)

A

1 min on, 10 sec off

1 min on, 10 sec off

3rd and subsequent - 1 min on, 5 min off

51
Q

ITT limits to move from SHUT OFF to IDLE on start

A

ITT must be 120 C or less for all ground starts

ITT must be 90 C or less for all air starts

52
Q

Dry Motoring Cycle (200)

A

1st - 90 sec on, 5 min off

2 and subsequent - 30 sec on, 5 min off

53
Q

Min oil temperature for starting

A

-40 C

54
Q

Max continuous oil temperature

A

155 C

55
Q

Max permissible oil temperature

A

163 C (15 min transient)

56
Q

Min idle oil pressure

A

25 PSI

57
Q

Min takeoff oil pressure

A

45 PSI

58
Q

Max continuous oil pressure (200)

A

115 PSI

59
Q

Transient oil pressure is limited to ___ minutes

A

10 min

60
Q

Min N1 EICAS FLX value

A

85%

61
Q

Wet runway FLX data is only available when OAT is warmer than ___

A

10 C

62
Q

Min temperature for starting cold soaked APU on ground

A

-40 C

63
Q

APU max starting altitude (200)

A

30,000 ft

64
Q

Bleed air extraction from the APU is not permitted above ____ (200)

A

15,000 ft

65
Q

Bleed air extraction from the APU for engine starting is not permitted above _____

A

13,000 ft

66
Q

APU max RPM (200)

A

107%

67
Q

With the APU DOOR not CLSD or DOOR postion unknown the APU must remain in operation OR the airplane must be limited to ___ KIAS (200)

A

300 KIAS

68
Q

Max pressure altitude for takeoff and landing (200)

A

10,000 ft

69
Q

Max operating altitude

A

41,000 ft

70
Q

Max ambient temperature for takeoff and landing (200)

A

50 C

71
Q

Max tailwind

A

10 kts

72
Q

Max runway slope

A

+/- 2%

73
Q

Max runway slope [CAT II/III]

A

+/- 1%

74
Q

Min runway width

A

100 ft

75
Q

Flight maneuvering load limits [Flaps Retracted]

A

-1.0 to 2.5 G

76
Q

Flight maneuvering load limits [Flaps Extended]

A

0 to 2.0 G

CRJ (2 decks)

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