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CRJ Limitations Flashcards

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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

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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

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3
Q

-200 Engine Starter Cranking Limits

Start 3

A

Maximum time on : 1 Minute

Followed by: 5 Minutes OFF

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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.

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5
Q

During landing, maximum reverse thrust is prohibited…

A

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

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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*
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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.
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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

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9
Q

Maximum Zero Fuel Weight- 700

A

62,300 lbs

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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.

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11
Q

Maximum Zero Fuel Weight- 900

A

70,750 lbs.

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12
Q

Double Engine Failure

A
  1. Continuous Ignition……. On

2. Airspeed……. 240 KIAS/0.70 minimum

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13
Q

Maximum Landing Weight- 700

A

67,000 lbs.

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14
Q

Maximum Gear Retracted Speed

A

200 KIAS

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15
Q

Maximum Landing Weight- 900

A

75,100 lbs.

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16
Q

Enroute use of slats/flaps…..

A

Is prohibited.

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17
Q

-200 Engine Starter Cranking Limits

Start 1 and 2

A

Maximum time on : 1 Minute

Followed by: 10 seconds OFF

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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.

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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

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20
Q

Prior to Shutdown the engines shown be…..

A

Operated at or near idle for 2 minutes

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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.

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22
Q

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

A

800lbs

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23
Q

Maximum Taxi and Ramp Weight- 700

A

75,250 lbs

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24
Q

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

A

The climb and approach phases of flight is not permitted.

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25
Maximum Gear Extension Speed
220 KIAS
26
-200 APU Start Cycles on Battery | Starts 1-4
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
27
Vfe
Maximum speed at which the aircraft maybe flown with the flaps extended
28
To protect the flight compartment CRT Displays....
The maximum permissible time for ground operations with DC power only is 5 minutes.
29
Visible Mositure
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
30
Stab Trim Runaway | -200
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
31
-200 | Upon Start the engine should not exceed.....
900 ITT degrees C
32
Maximum operating altitude -700/900
41,000 ft
33
APU Bleed Air Limitations | Air Conditioning
Bleed air extraction from the APU is not permitted above: - 200: 15,000 ft - 700/-900: 25,000ft
34
Maximum operating Altitude- 200
36,000 ft.
35
Maximum 90 degree crosswind for landing from a Cat II approach
15 knots
36
Maximum permissible fuel imbalance between the left and right wing tanks for all phases of flight except takeoff in the -200
800lbs
37
Stab Trim Run Away | -700
1. Control Wheel.... Asume Manual Control and Override Runaway 2. Stab Trim Disc....... Push, hold and release
38
Turbulence Penetration Speed
280 KIAS or 0.75M whichever is slower.
39
Maximum direct tailwind for takeoff and landing
10 knots
40
Minimum brake cooling time is...
15 minutes, and all BTMS indicators must be green and are not increasing.
41
Maximum Taxi and Ramp Weight-900
85,000 lbs.
42
-700/-900 Engine Starter Cranking Limits | Start 1 and 2
Maximum time on : 90 seconds | Followed by: 10 seconds OFF
43
-700/-900 Engine Starter Cranking Limits | Start 3
Maximum time on : 90 seconds | Followed by: 5 Minutes OFF
44
-200 APU Start | The 2-minute delay must be observed between cranking attempts to.....
Allow for cooling of the starter and start contractor and APU fuel drainage.
45
With the APU door not closed or the door position is unknown:
The airplane must be limited to: -200: 300 KIAS -700/-900: 220 KIAS Or the APU must remain in operation
46
Maximum slats and/or Flaps extended altitude...
15,000ft
47
Maximum Takeoff Weight- 700
75,000 lbs.
48
Maximum Takeoff Weight-900
84,500 lbs.
49
Engine Limitations | Red
Maximum and Minimum Limitations
50
Maximum 90 degree crosswind for takeoff and landing
27 knots
51
- 200 APU Start using DC Ground Power
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
Operation of the Wing and Cowl Anti-Ice System(s): Ground Contamination or Visible Moisture, During Takeoff OAT 10C or below
Cowl Anti Ice on.
53
Maximum headwind for landing from Cat II approach
16 knots
54
Minimum altitude for flight spoiler deployment;
1,000 ft AGL
55
Maximum permissible fuel imbalance between the left and right wing tanks for all phases of flight expect takeoff in the -700/-900
800lbs.
56
Maximum Zero Fuel Weight- 200
44,000 lbs.
57
Continuous engine Ignition must be used during the following:
- 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
Maximum Airspeed for Windshield Wiper Operation
220 KIAS
59
Engine Limitations Amber
Caution Range
60
Operation of the Wing and Cowl Anti-Ice System(s): | Ice Annunciated Inflight
Wing and Cowl anti-ice
61
Ground Contamination
Runways, Ramps or taxiways with surface snow, ice, slush or standing water
62
Other Emergency Checklists
- 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
Maximum Taxi and Ramp Weight- 200
53,250 lbs.
64
Visible Moisture present below 400 ft AGL and OAT 10 C or below
Activate cowl anti-ice for takeoff
65
-700/-900 | The APU starter motor duty cycle is limited to.....
Not more than three starts/starter attempts in one hour with a two minute delay between cranking attempts.
66
Use of Speed Mode, flight director or autopilot coupled, during approach......
Is not permitted.
67
During all starts, do not exceed.......
75% N1 for 2 minutes after start, or until all operating indications are in the normal range, whichever is longer.
68
The taxi lights must be switched OFF.....
Whenever the airplane is stationary in excess of 10 minutes.
69
RVSM Required Equipment List
- 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
Oil Pressure at Take Off Power
45 PSI minimum
71
After a cold start, the engines must remain......
At idle until oil pressure returns to normal range.
72
Operation of the Wing and Cowl Anti-Ice System(s): Ground Contamination or Visible Moisture, While taxiing OAT 5C or below
Wing and Cowl Anti-Ice on
73
Vfo
The maximum speeds at which it is safe to extend the flaps
74
Engine Limitations Due to Wind Direction: | Greater than 30 degrees in either direction of the airplane nose greater than 30 kts wind speed
Apply maximum of idle/taxi thrust before brake release, then TOGA thrust
75
Braking Loss/ Asymmetry
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
Visible Moisture below 400 ft AGL with OAT 5 C or below activate;
Both cowl and wing anti-ice for takeoff.
77
Smoke/Fumes
1. Oxygen Masks ( if required)..... Don and 100% 2. Crew Communication ...... Establish 3. Immediate Action Items Complete, Assign PF *Without associated CAS message*
78
Maximum Gear Extended Speed
220 KIAS
79
Maximum Landing Weight- 200
47,000 lbs.
80
APU Bleed Air Limitation Engine Start during Ground Operations
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
Engine Limitations Due to Wind Direction: | Greater than 30 degrees in either direction of the airplane nose between 5 and 30 kts wind speed
Apply maximum of 75% N1 before brake release, then TOGA thrust.
82
Engine Limitations Green
Normal Operating Range
83
Maximum permissible fuel imbalance between the left and right wing tanks for take off in the -700/-900
300lbs
84
Maximum Takeoff Weight- 200
53,000 lbs.
85
-200 Flap Speeds
``` Vfe. Vfo Flaps 8. 230. 200 Flaps 20. 220. 200 Flaps 30. 185 Flaps 45. 175 ```
85
-700/-900 | Flap Speeds
Vfe/Vfo ``` Flaps 1. 230 Flaps 8. 230. Flaps 20. 220. Flaps 30. 185 Flaps 45. 175 ```

CRJ Limitations (1 decks)

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