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CRJ Memory Items & Limitations (PSA) > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum 90 degree crosswind for landing and takeoff

A

27 knots

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2
Q

Maximum 90 degree crosswind for landing from a Category II Approach

A

15 knots

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3
Q

Maximum headwind for landing from a Category II Approach

A

16 knots

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4
Q

Maximum direct tailwind for takeoff and landing

A

10 knots

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5
Q

Maximum operating altitude <-701>, <-900>

A

41,000 ft.

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6
Q

Note: Takeoff or landing

A

Except in emergency, takeoff or landing will not be attempted whenever peak wind value exceeds 50 knots. Crosswind components, not including gust factor, are limited to AFM maximum demonstrated as listed above. Crosswind and tailwind components may be further limited by runway conditions or Operations specifications (See POH 3.12.3)

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7
Q

Maximum Taxi and Ramp Weight

A

701: 75,250 lbs.
900: 85,000 lbs.

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8
Q

Maximum Takeoff Weight

A

701: 75,000 ft.
900: 84,500 ft.

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9
Q

Maximum landing weight

A

701: 67,000 lbs.
900: 75,100 lbs.

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10
Q

Maximum zero fuel weight

A

701: 62,300 lbs.
900: 70,750 lbs.

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11
Q

Turbulence Penetration Speed

A

280 KIAS/.75M, whichever is lower

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12
Q

Maximum gear extension speed

A

220 KIAS

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13
Q

Maximum gear extended speed

A

220 KIAS

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14
Q

Maximum gear retraction speed

A

200 KIAS

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15
Q

Maximum airspeed for windshield wiper operation

A

250 KIAS

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16
Q

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

A

250 KIAS <701>, <900>

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17
Q

Maximum Cruise Mach in RVSM Airspace

A

0.82M

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18
Q

Tire Limit Ground Speed <701>

A

182 knots

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19
Q

Tire Limit Ground Speed <900>

A

195 knots

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20
Q

Flaps 1 <701>, <900>

A

230 KIAS

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21
Q

Flaps 8 <701>, <900>

A

230 KIAS

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22
Q

Flaps 20 <701>, <900>

A

220 KIAS

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23
Q

Flaps 30 <701>, <900>

A

185 KIAS

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24
Q

Flaps 45 <701>, <900>

A

170 KIAS

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25
Q

Flaps Note: <701>, <900>

A

The Vfe and Vfo speeds are equal

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26
Q

Operation in Icing Conditions: TAXI

A

CONDITION: Ground Contamination or Visible Moisture
TEMPERATURE: OAT 10*C or Below
IAS: N/A
ANTI-ICE: COWL

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27
Q

Operation in Icing Conditions: TAKEOFF

A

CONDITION: Ground Contamination or Visible Moisture
TEMPERATURE: OAT 10C or Below (5C or Below)
IAS: N/A
ANTI-ICE: Cowl (Wing & Cowl)

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28
Q

Operation in Icing Conditions: IN FLIGHT

A

CONDITION: Visible Moisture
TEMPERATURE: From TAT 10C to SAT -39C
IAS: >= 230 (<230)
ANTI-ICE: Cowl (Wing + Cowl)

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29
Q

Operation in Icing Conditions: ICE ANNUNCIATED INFLIGHT

A

CONDITION: On
TEMPERATURE: N/A
IAS: N/A
ANTI-ICE: Wing & Cowl

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30
Q

Define Ground Contamination

A

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

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31
Q

Define Visible Moisture

A

Visible moisture or precipitation in any form (such as fog with visibility of one mile or less, mist, rain, snow, sleet, and ice crystals or clouds inflight)

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32
Q

Visible Moisture below 400 feet AGL with OAT 10*C or below:

A

Activate cowl anti-ice for takeoff. If OAT 5*C or below activate both cowl and wing anti-ice for takeoff.

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33
Q

Engine Indications: RED, AMBER, GREEN

A

RED: Maximum or minimum limitations
AMBER: Caution range
GREEN: Normal operating range

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34
Q

During all starts,

A

Do not exceed 75% N1 for 2 minutes after start or until all operating indications are in the normal range, whichever is longer.

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35
Q

At shutdown, operate engines

A

At or near idle for 2 minutes prior to shutdown.

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36
Q

To ground start, ITT

A

Must be below 120*C before attempting to ground start the engine.

37
Q

To airstart, ITT

A

Must be below 90*C before attempting to airstart engine.

38
Q

Idle Engine Oil Pressure

A

Steady-state idle 25 psi minimum

39
Q

Takeoff Power Engine Oil Pressure

A

Takeoff power 45 psi minimum

40
Q

Continuous engine ignition must be used during the following:

A
  • Takeoff and landing on contaminated runways
  • Takeoff with high crosswind components (15 knots or greater)
  • Flight through moderate or heavier intensity rain
  • Flight through moderate or heavier intensity turbulence
  • Flight in the vicinity of thunderstorms
41
Q

ENGINE OPERATING LIMITS:
Wind 30* on either direction of airplane nose; no wind speed limit
OR
>30* in either direction of the airplane nose; <5 knots wind speed

A

No limitations - TOGA thrust may be applied before brakes released

42
Q

ENGINE OPERATING LIMITS:
Wind >30* on either direction of airplane nose; between 5 and 30 knots wind speed

A

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

43
Q

ENGINE OPERATING LIMITS:
Wind >30* on either direction of airplane nose; >30 knots wind speed

A

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

44
Q

Engine Starter Cranking Limits <701>, <900> (Ground Only)

A

1st start: 90 seconds with 10 seconds off
2nd start: 90 seconds with 10 seconds off
3rd and subsequent start: 90 seconds with 5 minutes off

45
Q

Engine Starter Cranking Limits <701>, <900> (Flight Only)

A

1st start: 2 minutes with 10 seconds off
2nd and subsequent starts: 1 minute with 5 minutes off

46
Q

Starter Note: Cannot be engaged above what RPM

A

The starter must not be engaged if indicated N2 RPM exceeds 45% (inflight or on the ground)

47
Q

At initiation of thrust lever movement from SHUT OFF to IDLE:

A
  • ITT must be 120*C or less for all ground starts
  • ITT must be 90*C or less for all air starts
48
Q

Oil Pressure Note:

A

Note: After cold start, engine must remain at idle until oil pressure returns to normal range.

49
Q

Fuel Imbalance <701>, <900>

A

Maximum permissible fuel imbalance between the left and right wing tanks for:
- Takeoff: 300 lbs.
- All other phases of flight: 800 lbs.

50
Q

Takeoff with center tank fuel load

A

Takeoff with a fuel load in excess of 500 lbs. in the center tank is not permitted unless each wing tank is above 4,400 lbs. Powered cross flow and gravity cross flow must be OFF for takeoff.

51
Q

APU start cycles are permitted: <701>, <900>

A

The APU starter motor duty cycle is limited to not more than three (3) starts/start attempts in one (1) hour with a two (2) minute delay between cranking attempts

52
Q

APU Bleed Air Limitation: AIR CONDITIONING

A

Bleed air extraction from the APU is not permitted above: <701>, <900> 25,000 ft.

53
Q

APU Bleed Air Limitations: ENGINE START DURING GROUND OPERATIONS

A

Each engine may be started using the APU as a bleed air source.

54
Q

APU Door Open Limitations

A

With the APU door not closed or the door position is unknown:
- The airplane is limited to 220 KIAS <701>, <900>
OR
- The APU must remain in operation

55
Q

During Approach

A

Use of SPEED MODE (DES or IAS), with flight director or autopilot coupled, during approach is not permitted.

56
Q

During climb and approach

A

Use of VNAV, with flight director or autopilot coupled, during the climb and approach phases of flight is not permitted.

57
Q

VISUAL or NON-PRECISION:
Autopilot Prohibited at altitudes below 600 ft. AGL, except when performing the following:

A
  • For visual non-precision approaches, the minimum height for autopilot use is 400 ft AGL.
58
Q

For Precision Approaches <701>, <900>:
Operation of the Autopilot is prohibited at altitudes below 600 ft. AGL, except when performing the following:

A

For precision approaches (PAR/ILS), the minimum height for autopilot use is 80 ft. AGL unless:
- The glide path angle is greater than 3.5 degrees and less than or equal to 4.0 degrees and the airport elevation is less than or equal to 4000 feet the minimum height for autopilot is 120 ft. AGL
- ILS approaches with a glide path angle of greater than 4.0 degrees is prohibited.

59
Q

For Precision Approaches <900>:
Operation of the Autopilot is prohibited at altitudes below 600 ft. AGL, except when performing the following:

A

<900> For precision approaches (PAR/ILS) or approach procedures with vertical guidance, the minimum height for autopilot use with one engine operating is 110 ft. AGL

60
Q

RVSM Required Equipment List

A
  • Autopilot with Altitude Hold (must be operational)
  • Altitude Alerting System (must be operational)
  • Altitude Reporting Transponder (2) (One (1) must be operational)
  • Air Data Computers (2) (Two (2) must be operational)
61
Q

Ground Operation: Permissible DC Electrical System Loads

A

To protect the flight compartment CRT displays, the maximum permissible time for ground operation with DC power only is 5 minutes.

62
Q

Enroute use of slats/flaps

A

Is prohibited.

63
Q

Maximum slats and/or flaps extended altitude:

A

15,000 ft.

64
Q

Minimum altitude for flight spoilers

A

1,000 ft. AGL

65
Q

Inflight spoilers requirement

A

To ensure adequate maneuver margins, flight spoilers must NOT be extended inflight at airspeeds below the recommended reference speed plus 10 KIAS.

66
Q

Landing with Thrust Reversers

A

During landing, maximum reverse thrust is prohibited below 75 KIAS, and reverse idle should be achieved by 60 KIAS.

67
Q

Taxi Lights Restriction

A

The taxi lights must be switched OFF whenever the airplane is stationary in excess of 10 minutes.

68
Q

Wheel Brake Cooling

A

Minimum brake cooling time is 15 minutes, and all BTMS indicators must be green and are not increasing.

69
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
    (Extreme caution is required during braking to avoid tire damage)
  4. Reverse Thrust —> Apply maximum until stopping is assured
  5. Immediate Actions Items complete.
70
Q

CABIN ALT Msg or EMERGENCY DESCENT PROCEDURE

A
  1. Oxygen masks —> Don and 100%
  2. Crew communication —> Establish
  3. Captain assumes PF duties
71
Q

Cabin Pressure Note

A

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.

72
Q

SMOKE / FUMES

A
  1. Oxygen masks (if required) —> Don and 100%
  2. Crew communications —> Establish

(NOTE: This will be accomplished even without an associated CAS message)

73
Q

STAB TRIM RUNAWAY

A
  1. Control wheel —> Assume manual control and override runaway
  2. STAB TRIM DISC —> Push, hold and release
74
Q

Other Immediate Action Items

A
  • Rudder System Jam
  • Aileron System Jam
  • Elevator System Jam
  • L (R) ENGINE OIL PRESS Msg or Oil Pressure Low
  • Uncommanded Yaw Motion
  • Unreliable Airspeed In-Flight
75
Q

Maximum altitude for single pack operation

A

31,000 ft.

76
Q

Maximum starting altitude

A

37,000 ft.

77
Q

Maximum AC ELECTRICAL load on the engine or APU driven generator

A

40 kVA

78
Q

Maximum DC electrical load on each TRU

A

120 amps

79
Q

If static/standing takeoff data is generated and wind limits prevent a Static/Standing takeoff winds must be entered in ____ OR for aircraft with ACARS inoperative, dispatch must ____ winds into TLR data

A

ACARS, manually insert

80
Q

Maximum fuel quantity for pressure refueling <700, 900>

A

19,594 lbs

81
Q

Maximum Fuel Quantity Gravity Refueling 700 or 900

A

700: 14,580 lbs
900: 14,810 lbs

82
Q

The minimum fuel quantity for go-around per wing tank (with the airplane level) and assuming a maximum airplane climb attitude of ____ nose up is ____ lbs

A

10*, 600 lbs

83
Q

A tactile check of the wing leading edge is required when:

A
  1. The OAT is 10*C or less
  2. The bulk fuel temperature is 0*C or less
  3. The atmospheric conditions have been conducive to frost formation
  4. Ice and frost may continue to adhere to wing surfaces for some time even at outside air temperature above 10*C
84
Q

Do not hold in icing conditions with ____ extended

A

Slats and/or flaps

85
Q

Category II approaches are prohibited when the braking action is reported less than ____

A

Medium

86
Q

Flight must be within ____ minutes of a suitable airport, if cargo is carried in either cargo compartment

A

60

87
Q

Auto Cross Fuel activated at an imbalance of _____ lbs. It deactivates once the lower tank is now _____ lbs fuller than the original full tank.

A

200 lbs / 50 lbs

88
Q

What limitations apply to Reduced Thrust (FLEX) Takeoff?

A
  • Anti-skid must be operative
  • PROHIBITED on contaminated runways
  • PROHIBITED if the airplane has been de-iced
  • PROHIBITED if the wing or cowl anti-ice bleeds are in use
  • PROHIBITED if warnings or windshear or downdrafts have been forecast
  • PROHIBITED with an engine that cannot achieve full-rated thrust
  • PROHIBITED when a special departure procedure specifies full thrust for takeoff

CRJ Memory Items & Limitations (PSA) (3 decks)

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