Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

CRJ Limitations > CRJ Limitations > Flashcards

CRJ Limitations Flashcards

1
Q

On the initiation of thrust lever movement from shut off to idle:

A

ITT must be 120C or less for all ground starts

ITT must be 90C or less for all air starts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Operation of the Wing and Cowl Anti-Ice System(s):
Visible Moisture - Inflight
TAT 10 C to SAT -39C
Less than 230 IAS

A

Wing and Cowl Anti-Ice

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

-200 Engine Starter Cranking Limits

Start 3

A

Maximum time on : 1 Minute

Followed by: 5 Minutes OFF

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Engine to Engine N2 split at ground idle power should not be greater than…..

A

2% N2. If N2 is 57% or less with an OAT of -20C or warmer, do not accelerate above idle.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

During landing, maximum reverse thrust is prohibited…

A

Below 75 KIAS, and reverse idle should be achieved bu 60 KIAS.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Cabin ALT Message or Emergency Descent Procedure

A
  1. Oxygen Masks….. Don and 100%
  2. Crew Communication ………. Establish
  3. Captain assumes Pilot Flying Duties
    * If cabin pressure is verified to be uncontrollable and the airplane structural integrity is in doubt, it is preferable to maintain at or below the speed at which the malfunction occurred and avoid high maneuvering loads*
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Operation with the autopilot engaged is prohibited….

A

Below 600ft AGL, except when performing the following;

  • For visual and non-precision approaches, the minimum height for the autopilot use is 400ft AGL
  • For precision approaches, the minimum height for autopilot use is 80 ft AGL
  • -900 For precision approaches or approach procedures with vertical guidance, the minimum height for autopilot use with one engine operating is 110 ft AGL.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Operation of the Wing and Cowl Anti-Ice System(s):
Visible Moisture - Inflight
TAT 10 C to SAT -39C
Greater than or equal to 230 IAS

A

Cowl Anti- Ice

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Maximum Zero Fuel Weight- 700

A

62,300 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

To ensure adequate maneuver margins, Flight spoilers must not be extended….

A

Inflight at air speeds below the recommended reference speed plus 17 KIAS.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Maximum Zero Fuel Weight- 900

A

70,750 lbs.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Double Engine Failure

A
  1. Continuous Ignition……. On

2. Airspeed……. 240 KIAS/0.70 minimum

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Maximum Landing Weight- 700

A

67,000 lbs.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Maximum Gear Retracted Speed

A

200 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Maximum Landing Weight- 900

A

75,100 lbs.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Enroute use of slats/flaps…..

A

Is prohibited.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

-200 Engine Starter Cranking Limits

Start 1 and 2

A

Maximum time on : 1 Minute

Followed by: 10 seconds OFF

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Engine Limitations Due to Wind Direction:
Within 30 degrees on either direction of the airplane nose- no wind speed limit
Or
Greater than 30 degrees in either direction of the airplane nose less than 5 kts of wind

A

No limitations- TOGA thrust maybe applied before brakes released.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Operation of the Wing and Cowl Anti-Ice System(s):
Ground Contamination or Visible Moisture, While taxiing
OAT 10C or below

A

Cowl Anti-Ice one

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Prior to Shutdown the engines shown be…..

A

Operated at or near idle for 2 minutes

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Takeoff with a fuel load in excess of 500 lbs in the center tank……

A

Is not permitted unless each wing tank is above 4,400 lbs. Powered crossflow and gravity crossflow must be OFF for takeoff.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Maximum permissible fuel imbalance between the left and right wing tanks for take off in the -200

A

800lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Maximum Taxi and Ramp Weight- 700

A

75,250 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

Use of VNAV, flight director or autopilot coupled, during….

A

The climb and approach phases of flight is not permitted.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

Maximum Gear Extension Speed

A

220 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

-200 APU Start Cycles on Battery

Starts 1-4

A

1 Max Time on 30 seconds Followed by 2 minutes off
2 Max Time on 30 seconds Followed by 20 minutes off
3 Max Time on 30 seconds Followed by 2 minutes off
4 Max Time on 30 seconds Followed by 40 minutes off

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

Vfe

A

Maximum speed at which the aircraft maybe flown with the flaps extended

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

To protect the flight compartment CRT Displays….

A

The maximum permissible time for ground operations with DC power only is 5 minutes.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

Visible Mositure

A

Visible moisture or precipitation in any form.

Such as fog with visibility one mile or less, mist, rain, snow, sleet, and ice crystals or clouds in flight

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

Stab Trim Runaway

-200

A
  1. Control Wheel….. Assume Manual control and override Runaway
  2. Both Stab Trim Disc’s……. Push, hold and release
  3. Captain assumes PF Duty
  4. Stab Ch1 cb (2f5)……. Open
  5. Stab CH2 cb (4A1) …… Open
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

-200

Upon Start the engine should not exceed…..

A

900 ITT degrees C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
32
Q

Maximum operating altitude -700/900

A

41,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
33
Q

APU Bleed Air Limitations

Air Conditioning

A

Bleed air extraction from the APU is not permitted above:

  • 200: 15,000 ft
  • 700/-900: 25,000ft
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
34
Q

Maximum operating Altitude- 200

A

36,000 ft.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
35
Q

Maximum 90 degree crosswind for landing from a Cat II approach

A

15 knots

36
Q

Maximum permissible fuel imbalance between the left and right wing tanks for all phases of flight except takeoff in the -200

A

800lbs

37
Q

Stab Trim Run Away

-700

A
  1. Control Wheel…. Asume Manual Control and Override Runaway
  2. Stab Trim Disc……. Push, hold and release
38
Q

Turbulence Penetration Speed

A

280 KIAS or 0.75M whichever is slower.

39
Q

Maximum direct tailwind for takeoff and landing

A

10 knots

40
Q

Minimum brake cooling time is…

A

15 minutes, and all BTMS indicators must be green and are not increasing.

41
Q

Maximum Taxi and Ramp Weight-900

A

85,000 lbs.

42
Q

-700/-900 Engine Starter Cranking Limits

Start 1 and 2

A

Maximum time on : 90 seconds

Followed by: 10 seconds OFF

43
Q

-700/-900 Engine Starter Cranking Limits

Start 3

A

Maximum time on : 90 seconds

Followed by: 5 Minutes OFF

44
Q

-200 APU Start

The 2-minute delay must be observed between cranking attempts to…..

A

Allow for cooling of the starter and start contractor and APU fuel drainage.

45
Q

With the APU door not closed or the door position is unknown:

A

The airplane must be limited to:
-200: 300 KIAS
-700/-900: 220 KIAS
Or the APU must remain in operation

46
Q

Maximum slats and/or Flaps extended altitude…

A

15,000ft

47
Q

Maximum Takeoff Weight- 700

A

75,000 lbs.

48
Q

Maximum Takeoff Weight-900

A

84,500 lbs.

49
Q

Engine Limitations

Red

A

Maximum and Minimum Limitations

50
Q

Maximum 90 degree crosswind for takeoff and landing

A

27 knots

51
Q
  • 200 APU Start using DC Ground Power
A

1 Max Time on 15 seconds Followed by 2 minutes off
2 Max Time on 15seconds Followed by 20 minutes off
3 Max Time on 15 seconds Followed by 2 minutes off
4 Max Time on 15 seconds Followed by 40 minutes off

52
Q

Operation of the Wing and Cowl Anti-Ice System(s):
Ground Contamination or Visible Moisture, During Takeoff
OAT 10C or below

A

Cowl Anti Ice on.

53
Q

Maximum headwind for landing from Cat II approach

A

16 knots

54
Q

Minimum altitude for flight spoiler deployment;

A

1,000 ft AGL

55
Q

Maximum permissible fuel imbalance between the left and right wing tanks for all phases of flight expect takeoff in the -700/-900

A

800lbs.

56
Q

Maximum Zero Fuel Weight- 200

A

44,000 lbs.

57
Q

Continuous engine Ignition must be used during the following:

A
  • Takeoff and Landing on contaminated Runways
  • Takeoff with high crosswind components (15 kts or greater)
  • Flight through moderate or heavier intensity rain
  • Flight through moderate or heavier intensity turbulence
  • Flight in the vicinity of thunderstorms
58
Q

Maximum Airspeed for Windshield Wiper Operation

A

220 KIAS

59
Q

Engine Limitations

Amber

A

Caution Range

60
Q

Operation of the Wing and Cowl Anti-Ice System(s):

Ice Annunciated Inflight

A

Wing and Cowl anti-ice

61
Q

Ground Contamination

A

Runways, Ramps or taxiways with surface snow, ice, slush or standing water

62
Q

Other Emergency Checklists

A
  • Rudder System Jam
  • Aileron System Jam
  • Elevator System Jam
  • L(R) Engine Oil Pressure Message or Oil Pressure Low
  • Uncommanded Yaw Motion
  • Unreliable Airspeed In-Flight
63
Q

Maximum Taxi and Ramp Weight- 200

A

53,250 lbs.

64
Q

Visible Moisture present below 400 ft AGL and OAT 10 C or below

A

Activate cowl anti-ice for takeoff

65
Q

-700/-900

The APU starter motor duty cycle is limited to…..

A

Not more than three starts/starter attempts in one hour with a two minute delay between cranking attempts.

66
Q

Use of Speed Mode, flight director or autopilot coupled, during approach……

A

Is not permitted.

67
Q

During all starts, do not exceed…….

A

75% N1 for 2 minutes after start, or until all operating indications are in the normal range, whichever is longer.

68
Q

The taxi lights must be switched OFF…..

A

Whenever the airplane is stationary in excess of 10 minutes.

69
Q

RVSM Required Equipment List

A
  • Autopilot with altitude hold….Must be Operational
  • Altitude Alerting System….Must be Operational
  • Altitude Reporting Transponder (2) ….One Must be Operational
  • Air Data Computers (2)…. Both Must be Operational
70
Q

Oil Pressure at Take Off Power

A

45 PSI minimum

71
Q

After a cold start, the engines must remain……

A

At idle until oil pressure returns to normal range.

72
Q

Operation of the Wing and Cowl Anti-Ice System(s):
Ground Contamination or Visible Moisture, While taxiing
OAT 5C or below

A

Wing and Cowl Anti-Ice on

73
Q

Vfo

A

The maximum speeds at which it is safe to extend the flaps

74
Q

Engine Limitations Due to Wind Direction:

Greater than 30 degrees in either direction of the airplane nose greater than 30 kts wind speed

A

Apply maximum of idle/taxi thrust before brake release, then TOGA thrust

75
Q

Braking Loss/ Asymmetry

A
  1. Wheel Brakes…… Release Momentarily
  2. PM will select ANTI-SKID to OFF
  3. Wheel Brakes……… Re-Apply as required
  4. Reverse Thrust …….. Apply Maximum until stopping assured
  5. Immediate Action Items Complete
76
Q

Visible Moisture below 400 ft AGL with OAT 5 C or below activate;

A

Both cowl and wing anti-ice for takeoff.

77
Q

Smoke/Fumes

A
  1. Oxygen Masks ( if required)….. Don and 100%
  2. Crew Communication …… Establish
  3. Immediate Action Items Complete, Assign PF

Without associated CAS message

78
Q

Maximum Gear Extended Speed

A

220 KIAS

79
Q

Maximum Landing Weight- 200

A

47,000 lbs.

80
Q

APU Bleed Air Limitation

Engine Start during Ground Operations

A

Each engine may be started using the APU as bleed air source.
-200
If both engines are to be started using the APU bleed air, the operating engine’s thrust must not exceed 70% N2.

81
Q

Engine Limitations Due to Wind Direction:

Greater than 30 degrees in either direction of the airplane nose between 5 and 30 kts wind speed

A

Apply maximum of 75% N1 before brake release, then TOGA thrust.

82
Q

Engine Limitations

Green

A

Normal Operating Range

83
Q

Maximum permissible fuel imbalance between the left and right wing tanks for take off in the -700/-900

A

300lbs

84
Q

Maximum Takeoff Weight- 200

A

53,000 lbs.

85
Q

-200 Flap Speeds

A 
Vfe.               Vfo
Flaps 8.          230.              200
Flaps 20.       220.               200
Flaps 30.                  185
Flaps 45.                   175
85
Q

-700/-900

Flap Speeds

A

Vfe/Vfo

Flaps 1.           230
Flaps 8.          230.              
Flaps 20.       220.               
Flaps 30.       185
Flaps 45.        175

CRJ Limitations (1 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions