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CRJ 200 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max cargo weight (comp 61)

A

3500 lbs

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2
Q

Turb Penetration Speed

A

280kias or M.75. Whichever is lower

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3
Q

Max operating Speed

A

M .85

335 KIAS

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4
Q

Max pressure diff for taxi,takeoff and landing

A

0.1 PSI

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5
Q

Max altitude for single pack operation

A

25 000 ft

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6
Q

Max cabin differential pressure

A

8.7 PSI

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7
Q

Autopilot minimum engage alt

A

600ft

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8
Q

Minimum autopilot altitude NPA or visual

A

400’

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9
Q

Minimum autopilot altitude for precision approach

A

80’

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10
Q

Minimum autopilot for any A mode approach on HGS

A

650’

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11
Q

Individual main AC GEN Limits

A

0-35k’ - 30kVa

>35k - 25kVa

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12
Q

APU Gen load limits

A

0-37k’ - 30 kVa

>37k - APU not allowed

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13
Q

Max. Continuous London each TRU in flight

A

100 amps

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14
Q

Max time allowed on DC power on ground

A

5 mins - to protect crt displays

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15
Q

Max speed with ADG deployed

A

250kias

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16
Q

Max time above 250 Kias with ADG during relight

A

Up to 330kias - 12 mins

Max 331-335 for 4 mins

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17
Q

Maximum flaps and slats altitude

A

15,000’

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18
Q

Vfo and Vfe for Flap 8

A

Vfo - 200

Vfe - 230

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19
Q

Vfo and Vfe for Flap 20

A

Vfo - 200

Vfe - 230

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20
Q

Vfo and Vfe for Flap 30

A

Vfo - 185

Vfe - 185

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21
Q

Vfo and Vfe for Flap 45

A

Vfo - 170

Vfe - 170

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22
Q

Spoilers must not be used at a minimum landing speed of vref for flap setting +…

A

17 kias

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23
Q

Min altitude for spoilers

A

300’ AGL

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24
Q

Approach cannot be commenced or flaps extended from 0 unless which following conditions are met for precision, NPA and visuals

A

For any approach: Basically RVR must be at or above landing limits for entire approach (not fluctuating) until after landing

Cat1 ILS non-coupled using HGS in A1 mode is table 2 approach ban CARs limits

Visuals: no restriction

Restrictions do not apply if u can fly approach, missed approach and divert to alternate with flaps in landing position and conduct and approach with 1000lbs remaining

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25
Q

Min engine fuel temp for takeoff

A

5c

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26
Q

During flight and takeoff min bulk fuel temp for Jet A

A

Takeoff: -30c

In flight: -40c

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27
Q

Takeoff with fuel in excess of 500lbs in centre tank not permitted unless:

A

Each main wing is above 4400 lbs OR

Each wing tank is above 2000lbs AND CofG is in allowable envelope and allowable ZFW is reduced by each lb above 500lb in centre tank

28
Q

Max fuel imbalance

A

800 lbs

29
Q

Min fuel in each wing for go around

A

450 lbs

30
Q

Normal hydraulic pressure

A

2800-3200 PSI

31
Q

Normal hydraulic qty:

A

45-85% with respective hyd pump on.

May indicate higher quantity with pump off

32
Q

Max wiper speed

A

220kias

33
Q

Max landing gear extension, down and locked and retraction speeds

A

VLE - 250 kias
Vgear down and locked - 250 kias
Retraction - 200 kias

34
Q

Tire limit speed

A

182 kias

35
Q

Brake cooling min time between landing or reject before takeoff

A

15 mins

36
Q

Min BTMS for takeoff

A

05 or less and stable and decreasing

37
Q

Min oleo showing

A

Any chrome

38
Q

Max time taxi lights on while stationary

A

10 mins

39
Q

How long must engine remain at idle after start

A

Till oil pressure in green and not above 75% N1 until 2 mins or all indications in normal range - whichever is longer

And

If N2 is 57% or less with oat <= -20c

40
Q

Max N2 split at ground idle

A

2%

41
Q

Starter cranking limits (must not be engaged if N2 >55%)

A

START—-max time On—–followed by:

1—-1min—-10s off
2—-1min—-10s off
3+—-1min—-5 min off

Ground and airborne

42
Q

N2 and ITT for moving thrust from shutoff to idle

A

20% N2 and <120c ITT on ground

<90c ITT for airborne

43
Q

Dry motoring cycle (thrust levers SHUT OFF)

A

Ground and Air

START—-max time on—-followed by:

1—-90s—-5min
2+—-30s—-5min

44
Q

Min oil temp for start

A

-40c

45
Q

Max continuos oil temp and max permissible (15 min max)

A

Max cont: +155c

Max transient +163c

46
Q

Min idle oil pressure

A

25 PSI

47
Q

Minimum oil pressure at takeoff power

A

45psi

48
Q

Max continuous oil pressure

A

115 psi

49
Q

Maximum oil pressure transient after cold start

A

156PSI/130 PSI at idle

May only be above 115 psi for max 10 mins. Thrust levers must not be above idle until normal range

50
Q

Min thrust reverser speed

A

60kias except emergency

51
Q

Min N1 for flex takeoff

A

85% N1

52
Q

Max APU altitude

A

37 000’

53
Q

Max APU starting altitude

A

30 000’

54
Q

Min temp for starting cold soaked APU

A

-40c

55
Q

APU start using battery power

Max Time on and followed by

A

START—-Max time on—-followed by
1—-30s—-2 min off
2—-30s—-20 min off
3+ refer to chart

56
Q

APU start using DC ground power

Max Time on and followed by

A

START—-Max time on—-followed by
1—-15s—-2 min off
2—-15s—-20 min off
3+ refer to chart

57
Q

Max APU bleed air

A

15 000’

58
Q

Max operating engine N2 if both engines to be started with APU

A

70%

59
Q

Max pressure altitude for takeoff and landing

A

10 000’

60
Q

Max operating altitude

A

FL410

61
Q

Maximum ambient temp for takeoff and landing

A

50c

62
Q

Min ambient temp for takeoff

A

-40c

63
Q

Max crosswind for dry, wet and contaminated rwy

A

Dry/damp: 27kts
Wet: 22kts
Contaminated: 15kts

64
Q

Wind limits for cat II/iii

A

Xwind: 13
Headwind: 19kts
Tailwind: 10kts

65
Q

Max tailwind for takeoff and landing

A

10kts

66
Q

Min battery voltage for start (APU and engine)

A

22v

CRJ 200 (1 decks)

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