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CRJ200 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max allowable weight of the acft at the gate?

A

53,250 lbs

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2
Q

Max TOW

A

53,000 lbs

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3
Q

Max ZFW

A

44,000 lbs

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4
Q

Max Landing Weight

A

47,000 lbs

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5
Q

Min OAT for takeoff?

A

-40 Degrees C

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6
Q

Max tailwind for t/o and landing?

A

10 knots

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7
Q

Max alt

A

FL410

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8
Q

Flight must be w/in 45 min of nearest suitable airport under what conditions?

A

If cargo is carried in cargo compartment.

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9
Q

With BTMS operative, min brake cooling time between landing or rejected t/o and subsequent t/o?

A

15 minutes

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10
Q

Max weight in the cargo compartment?

A

3,500 lbs

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11
Q

Max crosswind on a wet runway?

A

27 knots

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12
Q

Max crosswind on contaminated runway w/braking action less than good?

A

15 knots

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13
Q

Max crosswind if the Capt has less than 100 hours PIC in type?

A

27 knots

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14
Q

Max speed to lower landing gear?

A

250 knots

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15
Q

Max speed to raise landing gear?

A

200 knots

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16
Q

Max speed with landing gear extended?

A

250 knots

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17
Q

Vfo for flaps 8?

A

200 knots

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18
Q

Vfo for flaps 20?

A

200 knots

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19
Q

Vfo for flaps 30?

A

185 knots

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20
Q

Vfo for flaps 45?

A

170 knots

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21
Q

Vfe for flaps 8?

A

215 knots

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22
Q

Vfe for flaps 20?

A

215 knots

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23
Q

Max cargo loading weight

A

3500 lbs

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24
Q

Max airport pressure alt for t/o and landing

A

10,000 ft

25
Q

Max ambient air temp approved for t/o and landing

A

ISA + 35 degrees C

26
Q

Mx action is required if L(R) COWL A/ICE messages are not extinguished above what N2?

A

78%

27
Q

The engine cowl anti-ice system must be ON when:

A

1) When in icing conditions

2) When ICE is annunciated by the ice detection system

28
Q

T/F Aircraft indicated SAT or TAT may not be used on the ground.

A

True

29
Q

Maximum runway slope

A

+/- 2 degrees

30
Q

Minimum flight crew

A

One pilot and one copilot

31
Q

Engines must be running how many minutes prior to takeoff?

A

2 minutes

32
Q

Operate engines at IDLE for a minimum of now many minutes prior to shutdown?

A

2 minutes

33
Q

Taxi-in time with engines below what percent may be included in the two minute cool down period?

A

80% N2

34
Q

Cold Soak definition

A

Before the first flight of the day and the aircraft has been at an ambient temp of -30 degrees C or below for more than eight hours.

35
Q

Cold Soak engine start requirements

A

Motor for 60 seconds AND verify fan rotation.

36
Q

Cold Soak thrust reverser requirements

A

Actuate thrust reversers until the deploy and stow cycles are less than 5 seconds.

37
Q

Starter Cranking Limits

A

First Start: one minute on, 10 seconds off

38
Q

Max N2 for starter use

A

55%

39
Q

Max ITT to initiate all ground starts

A

120 degrees C

40
Q

L and R main fuel tank max fuel imbalance

A

800 lbs

41
Q

Minimum fuel quantity for a go-around

A

450 lbs per wing in a level aircraft

42
Q

APU starting limits using aircraft batteries on the ground or for normal in-flight start

A

1st Start, 30 seconds
2nd Start, 30 seconds followed by 20 minutes off
*A two minutes delay should be observed between cranking attempts to allow for cooling of starter and start contractor and for APU drainage.

43
Q

APU starting limits using ground power

A

1st start, 15 seconds
2nd start, 15 seconds followed by 20 minutes off
*A two minutes delay should be observed between cranking attempts to allow for cooling of starter and start contractor and for APU drainage.

44
Q

Max altitude to use APU bleed air

A

15,000’

45
Q

APU bleed limit for engine start on the ground

A

No bleed air extraction limit, but once started, engines thrust must not exceed 70% N2.

46
Q

APU bleed limit for engine start during flight, single engine

A

APU bleed air extraction for an engine start is not permitted

47
Q

APU bleed limit for engine start during flight during double engine failure

A

APU bleed air extraction for engine starts is permitted 13,000’ and below.

48
Q

Turbulence penetration airspeed

A

280 KIAS or 0.75 mach, whichever is lower

49
Q

Max speed for windshield wiper operations

A

220 KIAS

50
Q

Wind limits for takeoff

A

60 knots or a headwind component of >55 knots

51
Q

(T/F) The ADC source coupled to the active autopilot must be the same as that coupled to the ATC transponder during flight in RVSM airspace

A

True

52
Q

Max alt to extend flaps

A

15,000’

53
Q

Min alt (AGL) to extend spoilers

A

800’ AGL

54
Q

Max flap setting to use spoilers

A

30 degrees

55
Q

Max taxi light operation time when stationary

A

10 minutes

56
Q

Minimum airspeed to use max reverse thrust

A

60 KIAS

57
Q

(T/F) Use of the ISI localizer and back course information is prohibited during back course approaches.

A

True

58
Q

Max ITT allowed during engine start.

A

900 deg C

59
Q

Max N2 split at idle?

A

2%

CRJ200 (2 decks)

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