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CRJ POH Chapter 3 Limitations > Limitations and Immediate Action Items Test > Flashcards

Limitations and Immediate Action Items Test Flashcards

1
Q

Maximum Taxi and Ramp Weight

A

53,250 lbs

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2
Q

Maximum Takeoff Weight

A

53,000 lbs

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3
Q

Maximum Landing Weight

A

47,000 lbs

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4
Q

Maximum Zero Fuel Weight

A

44,000 lbs

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5
Q

Minimum Operating Weight Empty

A

25,480 lbs

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6
Q

Maximum Pressure Altitude for takeoff and landing

A

8,000 ft

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7
Q

Maximum Operating Altitude

A

36,000 ft

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8
Q

Minimum Ambient Temperature for Takeoff

A

-40°C

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9
Q

Definition of Icing Conditions COWL

A

Icing Conditions exist when the OAT (on the ground and for takeoff) or TAT (inflight) is 10°C or
below, and:
• Visible moisture in any form (such as clouds, fog, mist, rain, snow, sleet, or ice crystals), is present in flight, or below
400 feet AGL for ground operations, or
• When operating on surfaces that are wet or contaminated.

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10
Q

When must COWL anti-ice be on

A

Cowl Anti-Ice must be ON for all ground and flight operations when icing conditions exist except when the inflight SAT
is -40°C or below, or ICE is annunciated by the ice detection system.

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11
Q

Definition of Icing Conditions WING

A

Icing conditions exist when the OAT (takeoff) is 5°C or TAT (inflight) is 10°C or below, and:
• Visible moisture in any form (such as clouds, fog, mist, rain, snow, sleet or ice crystals) is present in flight, or below
400 feet AGL for takeoff, or
• The runway is wet or contaminated.

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12
Q

When must WING anti-ice be on

A

Wing Anti-Ice must be ON for takeoff and flight operations when ICE is annunciated by the ice detection system, or
when icing conditions exist and the airspeed is less than 230 KIAS except when the inflight SAT is -40°C or below. In addition, Wing Anti-Ice must be ON for the final two minutes prior to takeoff during all ground operations 5°C
OAT or below unless Type III or IV anti-icing fluid has been applied.

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13
Q

Tactile Check - When-Why-How

A

OAT is 5°C or less or wing fuel temperature is 0°C or less or the atmospheric conditions have been conducive to frost formation.
Ice and frost may continue to adhere to wing surfaces for some time at OAT above 5°C
Tactile check wing leading edge, wing forward upper surface, wing rear upper surface

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14
Q

Do not hold in icing conditions with ____ and/or _____ extended

A

Slats / Flaps

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15
Q

Continued operation in areas where SLD icing conditions exist is__________

A

Prohibited

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16
Q

All contaminated performance data will be for _______ takeoffs

A

Static

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17
Q

Maximum Tailwind for takeoff and landing

A

10 kts

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18
Q

Maximum Crosswind for takeoff and landing

A

27 kts

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19
Q

Maximum 90 degree Crosswind for landing from a Category II approach

A

15 kts

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20
Q

Maximum headwind for landing from a Category II Approach

A

17 kts

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21
Q

Maximum weight in the cargo compartment

A

3,500 lbs

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22
Q

Flights must be within _______ minutes of a suitable airport with cargo in the cargo compartment

A

45

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23
Q

EICAS Limit Markings Red/Amber/Green

A

Maximum and Minimum Limitations/Caution Range/Normal Operating Range

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24
Q

Maximum ITT for start

A

900°C

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25
Q

Maximum N2 split at idle

A

2%N2

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26
Q

Maximum ITT for all air starts

A

90°C

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27
Q

Maximum ITT allowed to advance the thrust levers to idle for all ground starts

A

120°C

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28
Q

Oil pressure Steady-state idle

A

25 PSI minimum

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29
Q

Oil pressure Takeoff Power

A

45 PSI minimum

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30
Q

Minimum oil temperature for engine starting

A

-40°C

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31
Q

During ALL starts, do not exceed ________N1 for _______ minutes after start, or until all operating indications are in the normal range, whichever is _________

A

75%/2/longer

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32
Q

Operate engines at or near idle for ______ minutes prior to shutdown

A

2

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33
Q

Airplane Cold Soak Define:

A

Before the first flight of the day, when the airplane is cold soaked at an ambient temperature of -30°C or below for more than 8 hours

34
Q

Airplane Cold Soak Operational

A

The engines must be dry motored for 60 seconds and fan rotation must be verified before an engine start is initiated.
Thrust revers must be actuated until deploy and stow cycles are less than 5 seconds

35
Q

Continues ignition must be used during:

A

Takeoff and landing on contaminated runways
Takeoffs with high crosswinds (15 kts or greater)
Flight through moderate or heavier precipitation
Flight through moderate or heavier turbulence
Flight in the vicinity of thunderstorms

36
Q

Starter cranking limits

A

1 min/10 sec, 1 min/10 sec, 1 min/5 min

37
Q

Dry Motor Cycle for engines

A

90 sec/5 min, 30 sec/5 min

38
Q

Maximum fuel imbalance between the left and right wing tank

A

800 lbs

39
Q

Maximum total fuel for pressure refueling

A

14,518 lbs

40
Q

Takeoff with a fuel load in excess of ______ in the center tank is not permitted unless each wing tank is above ________

A

500 lbs / 4,400 lbs

41
Q

Powered Crossflow and gravity crossflow must be ______ for takeoff

A

Off

42
Q

Takeoff with engine fuel temperature indications below ______ is prohibited

A

5°C

43
Q

Minimum Fuel Quantity for a go-around per wing tank, assuming 10 degrees pitch up _________

A

450 lbs

44
Q

APU start (on battery)

A

30 sec/2 min, 30 sec/20 min, 30 sec/2 min, 30 sec/40 min

45
Q

APU start (on DC ground power)

A

15 sec/2min, 15 sec/20 min, 15 sec/2 min, 15 sec/40 min

46
Q

APU maximum starting altitude

A

30,000 ft

47
Q

APU maximum operating altitude

A

36,000 ft

48
Q

Maximum APU RPM

A

107%

49
Q

With the APU door not closed, or the door position is unknown: The airplane must be limited to _____, or _________

A

300 KIAS/The APU must remain in operation

50
Q

Maximum bleed air extraction for air conditioning from the APU is______

A

15,000 ft

51
Q

Maximum engine start altitude with APU bleed air______

A

13,000 ft

52
Q

Minimum Engine Oil Pressure for takeoff ________

A

45 psi

53
Q

Flap position 8 Vfe / Vfo

A

230 KIAS / 200 KIAS

54
Q

Flap position 20 Vfe / Vfo

A

220 KIAS / 200 KIAS

55
Q

Flap position 30 Vfe / Vfo

A

185 KIAS

56
Q

Flap position 45 Vfe / Vfo

A

170 KIAS

57
Q

Gear extension maximum operating airspeed

A

220 KIAS

58
Q

Gear down and locked maximum operating airspeed

A

220 KIAS

59
Q

Gear retraction maximum operating airspeed

A

200 KIAS

60
Q

Maximum Tire Speed ________

A

182 kts

61
Q

Maximum airspeed for windshield wiper operation failed in the non-parked position__________

A

220 KIAS

62
Q

Maximum Turbulence Penetration Speed______

A

280 KIAS or .75M whichever is lower

63
Q

Maximum cruise mach in RVSM airspace

A

.82 M

64
Q

RVSM Required Equipment List

A

Autopilot (1) / Must be operational
Altitude Alerting System (1) / Must be operational
Altitude Reporting Transponder (2) / (1) Must be operaitonal
ADC (2) / (2) Must be operational

65
Q

Minimum Auto Pilot engagement altitude ______ except when performing Non-precision approach_________, Precision approach________

A

600 ft AGL / 400 ft AGL / 80 ft AGL

66
Q

Maximum slats/flaps extension altitude

A

15,000 ft

67
Q

Maximum permissible time on the ground with only DC power

A

5 min

68
Q

Minimum altitude for light spoiler deployment

A

1000 ft AGL

69
Q

Minimum airspeed for flight spoiler use

A

Vref + 17 KIAS

70
Q

Minimum brake cooling time

A

15 minutes and all BTMS indicators are green and not increasing

71
Q

During ladning application of thrust reverse above ______ is not permitted at air speeds below _____. Below _____, reverse thrust must be reduced to idle, not above _______

A

60%N1 / 75 KIAS / 60 KIAS / 30%N1

72
Q

Use of the EMER DEPRESS switch above ______ is prohibited

A

15,000 ft

73
Q

Max altitude for single pack operations

A

25,000 ft

74
Q

Max differential pressure for taxi, takeoff, and landing

A

0.1 psi

75
Q

Maximum relief differential pressure

A

8.7 psi

76
Q

Braking Loss / Asymmetry

A

Wheel Brakes…Release Momentarily
PM will select ANTI-SKID to OFF
Wheel Brakes…Re-apply as required
Reverse Thrust…Apply maximum until stopping assured

77
Q

Cabin Alt

A

Oxygen Masks….Don and 100%
Crew Communication….Establish
Captain assumes PF duties

78
Q

Double Engine Failure

A

CONT IGNITION….On

Airpspeed…240 KIAS minimum

79
Q

Smoke/Fumes

A

Oxygen Masks….Don and 100%

Crew Communication….Establish

80
Q

Stab Trim Runaway

A

Control Wheel…. Assume manual control and override runaway
Both STAB TRIM DISCs….Push, hold, release
Captain assumes PF duties
STAB CH1 cb (2f5)….open
STAB CH2 cb (4a1)….open

CRJ POH Chapter 3 Limitations (14 decks)

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