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XJT CRJ-200 > Limitations > Flashcards

Limitations Flashcards

0
Q

What is the maximum takeoff weight of the CRJ 200?

A

53,000 lbs

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1
Q

What is the maximum ramp weight of the CRJ 200?

A

53,250 lbs

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2
Q

What is the maximum landing weight of the CRJ 200?

A

47,000 lbs

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3
Q

What is the maximum zero fuel weight of the CRJ 200?

A

44,000 lbs

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4
Q

What is the cargo compartment loading weight limited to?

A

3,500 lbs

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5
Q

What is maximum airport pressure altitude for takeoff and landing?

A

10,000 ft PA

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6
Q

What is the maximum operating altitude?

A

41,000 ft

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7
Q

What is the maximum ambient air temperature approved for takeoff and landing?

A

ISA +35 degrees Celsius

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8
Q

What is the minimum ambient temperature approved for takeoff?

A

-40 degrees Celsius

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9
Q

Why should you restrict your rotation rate to 3 degrees per second?

A

It can lead to excessively high pitch attitudes and angles of attack near the ground, leading to reduced stall margins resulting in stick shaker and pusher, and possibly loss of control.

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10
Q

On the ground, when must the cowl anti-ice be ON?

A

With OAT less than 10 degrees Celsius and visible moisture present, or operating on runways, ramps or taxiways with surface snow, ice, standing water or slush present.

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11
Q

On the ground, when the cowl and wing anti-ice are selected ON, what caution messages might be posted, and when should they disappear?

A

L (R) COWL A/ICE caution messages. They should disappear when engine thrust is increased. If more than 78% N2 is needed to extinguish the messages, then maintenance action is required.

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12
Q

In flight, when should cowl anti-ice be selected ON?

A

When TAT is 10 degrees Celsius or below, and visible moisture in any form is encountered (eg clouds, rain, snow, sleet, ice crystals), except when SAT is -40 degrees Celsius or below. It must also be switched on when ICE is annunciated by the ice detection system.

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13
Q

On the ground, when must wing anti-ice be selected on if Type II, III or IV anti-icing fluids have NOT been applied?

A

During final taxi prior takeoff (during single-engine taxi, this is considered the period after the second engine has been started), when the OAT is 5 degrees Celsius or below, regardless of weather conditions.

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14
Q

Why should thrust reverser use on wet and contaminated surfaces be avoided while taxiing?

A

Thrust reverser use in these conditions could result in wing contamination from reverse jet blast.

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15
Q

When must wing anti-ice be selected ON for takeoff, assuming Type II, III or IV anti-ice fluids have been applied to the wing? When exactly should this be done?

A

When the OAT reads under 5 degrees Celsius or below, and visible moisture in any form (clouds, fog, mist) is present below 400 ft, or the runway is wet or contaminated, or in the presence of any precipitation (snow, rain, sleet, ice crystals). The wing anti-ice should only be selected ON just prior to thrust increase for takeoff.

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16
Q

What other anti-ice system must always be selected ON when wing anti-ice is selected ON for takeoff?

A

Cowl anti-ice

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17
Q

In flight, when must wing anti-ice be selected on?

A

If the TAT is 10 degrees Celsius or below, and visible moisture in any form is encountered (clouds, rain, snow, sleet, ice crystals) except when the SAT is -40 degrees Celsius or below, or if the airspeed is less than 230 KIAS.

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18
Q

Are we permitted to operate the CRJ-200 in areas where SLD icing conditions exist?

A

No

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19
Q

How can one detect if the aircraft has entered an area where SLD icing exists?

A

Ice accretion on the flight compartment side windows.

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20
Q

What actions are necessary if ice accumulates on the flight compartment side windows?

A

Wing and cowl anti-icing must be selected ON in SLD icing conditions. Leave icing conditions as soon as possible.

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21
Q

Frost, ice, snow or slush adhering to any critical surface (wings, uper fuselage, horizontal stabilizer, vertical stabilizer, control surfaces and engine inlets) prohibits takeoff, except under what circumstances?

A

Takeoff is permitted with frost adhering to the upper surface of the fuselage, if it is possible to distinguish surface features (markings and lines). Frost in excess of this must be removed from the fuselage. In addition, frost on the underside of the wing fuel tank area that is caused by cold-soaked fuel is permitted, to a maximum thickness of 3 mm.

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22
Q

What are the necessary checks for detecting ice on the wing leading edge, wing forward upper surface, and wing rear upper surface during the external walkaround? When are these checks required?

A

A visual and a tactile check, necessary when the OAT is 10 degrees Celsius or less, the wing fuel temperature is 0 degrees Celsius or less, or the atmospheric conditions have been conducive to frost formation. Note that ice and frost may continue to adhere to wing surfaces for some time even at OATs above 10 degrees Celsius.

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23
Q

What requirements exist for pilot training when conducting a takeoff and the OAT is 5 degrees Celsius or less?

A

The pilot conducting the takeoff and the PIC must have had specific training within the last 12 calendar months for takeoff procedures, ground icing conditions and cold weather operations. If this cannot be met, wing anti-ice must be selected ON just prior to thrust increase for takeoff.

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24
Q

What are the maximum runway slopes approved for takeoff and landing?

A

+ or - 2%

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25
Q

What are the maximum tailwind components for takeoff and landing?

A

10 kts tailwind in either case.

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26
Q

What is the minimum flight crew of the CRJ-200?

A

One pilot and one copilot.

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27
Q

What colours denote maximum and minimum limitations, caution ranges and normal operating ranges?

A

Red, amber and green, respectively.

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28
Q

How long must engines be allowed to run prior to takeoff?

A

Two minutes

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29
Q

How long must engines be run at idle prior to shutdown?

A

At least two minutes to dissipate heat and stabilize internal operating temperatures.

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30
Q

May taxi time be included in the cool-down period prior to shutdown?

A

Yes, if the engine is at or below 80% N2

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31
Q

If the aircraft has been cold-soaked at an ambient temperature of -30 degrees Celsius or below for more than eight hours, what action is required prior to initiating start?

A

The engines must be motored for 60 seconds and fan rotation must be verified before start is initiated.

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32
Q

Under what conditions must the aircraft be exposed to for it to require that the engines must be motored for 60 seconds and that fan rotation must be verified before start is initiated?

A

The aircraft must have been cold-soaked at an ambient temperature of -30 degrees Celsius or below for more than eight hours.

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33
Q

What action is required of the thrust reversers if the aircraft has been cold-soaked at an ambient temperature of -30 degrees Celsius or below for more than eight hours?

A

Thrust reversers must be actuated until the deploy and stow cycles are less than five seconds.

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34
Q

When must continuous engine ignition be used?

A

Takeoff and landing on contaminated runways, takeoff with crosswind components greater than 10 kts, flight through moderate or heavier intensity rain or turbulence, flight in the vicinity of thunderstorms, and engine operation at or near shaker and pusher settings (this requires an operable auto-ignition system).
Memory Hook: CCRTTS: Contamination, Crosswinds, Rain, Turbulence, Thunderstorms, Shaker/Pusher.

35
Q

The starter must not be used if indicated N2 rpm exceeds what value?

A

55%

36
Q

What is the maximum time a starter can be selected on for the first engine start attempt? How long should it be off before attempting again?

A

1 minute, and 10 seconds respectively.

37
Q

Are there any temperature limitations at the initiation of thrust lever movement from SHUT OFF to IDLE?

A

ITT must be 120 degrees Celsius or less for all ground starts.

38
Q

When determining the assumed temperature, and the reduced engine thrust takeoff procedure is used, what takeoff performance data must be used?

A

The takeoff performance data for APR OFF must always be utilized.

39
Q

What limitations exist regarding the use of a reduced engine thrust takeoff procedure?

A

Reduced thrust can not be used if normal takeoff fan speed is less than 85% N1, and the reduced engine thrust must not be less than 85% N1. Reduced thrust can not be used if the wing and/or cowl anti-icing bleeds are in use, on runways contaminated with standing water, slush, snow or ice, or when warnings of windshear or downdrafts have been forecast.

40
Q

For reduced thrust takeoffs, what source of outside temperature should be used?

A

The current surface weather. Do NOT use the indicated SAT from the EFIS. This information is not valid on the ground.

41
Q

Can the reduced engine thrust procedure be used on wet runways?

A

Yes, provided the wet runway performance data is used.

42
Q

What is the maximum permissible fuel imbalance between the contents of the main left tank and the main right tank?

A

800 lbs

43
Q

Is any fuel remaining in a tank after the appropriate fuel quantity indicator reads zero considered usable?

A

No

44
Q

Under what conditions can we take off with fuel loads in excess of 500 lbs in the centre tank?

A

If each wing tank is above 4,400 lbs. (See OM 1-4.6 for additional, non-memory conditions)

45
Q

If each wing tank has less than 4,400 lbs of fuel on board, what is the maximum weight of fuel that can be carried in the centre tank?

A

500 lbs

46
Q

What is the minimum fuel quantity for a go around? What is the maximum assumed climb attitude?

A

450 lbs per wing (with the aircraft level) and 10 degrees nose up.

47
Q

What is the maximum time that an APU battery can be used to start an APU initially, on the ground or for a normal in-flight start?

A

On the first and second start attempts, 30 seconds, followed by 20 minutes off, before any other starts are attempted by following the QRH procedure.

48
Q

What is the maximum time ground power can be used to start an APU?

A

15 seconds on the first and second attempts, followed by 20 minutes off before any further attempts are conducted according to the OM and QRH.

49
Q

Why do we allow two minutes between APU start attempts?

A

To allow for cooling of starter and start contactor and for APU drainage.

50
Q

What is the maximum altitude at which APU bleed air can be extracted for air conditioning?

A

15,000 ft

51
Q

What APU bleed air extraction limitation exists regarding engine start during ground operations?

A

No bleed air extraction limitation exists. Each engine may be started using the APU bleed air, then the operating engine’s thrust must not exceed 70% N2.

52
Q

What APU bleed air limitation exists for engine start during flight?

A

During single engine operations, APU bleed air extraction for an engine start is not permitted. During double engine failure conditions, APU bleed air extraction for engine starts is permitted. However, bleed air extraction is limited to 13,000 ft and below.

53
Q

What kind of flight control manipulation can result in structural failure at any speed, including below VA?

A

Rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw (eg large sideslip angles).

54
Q

What are the maximum speeds at which it is safe to extend the flaps?

A

Flaps 0-8 200 KIAS
Flaps 8-20 200 KIAS
Flaps 20-30 185 KIAS
Flaps 30-45 170 KIAS

55
Q

What are the maximum speeds at which the aircraft can be flown with flaps extended?

A

Flaps 8: 215 KIAS
Flaps 20: 215 KIAS
Flaps 30: 185 KIAS
Flaps 45: 170 KIAS

56
Q

What are the maximum speeds at which the landing gear may be extended and retracted, and what is the maximum speed that the aircraft may be flown with the landing gear extended and locked?

A

250, 200 and 250 KIAS respectively.

57
Q

What is the maximum airspeed for turbulence penetration?

A

280 KIAS or 0.75 Mach, whichever is lower.

58
Q

What is the minimum operating limit speed? Any exceptions?

A

Intentional speed reduction below the onset of stall warning, as defined by stick shaker operation, is prohibited unless a lower speed is specifically authorized for flight test or training operations.

59
Q

What is the maximum speed for windshield wiper operation?

A

220 KIAS

60
Q

What are the maximum total, headwind and tailwind components for takeoff or landing?

A

60 kts total, with a headwind component not to exceed 55 kts, and a tailwind component not to exceed 10 kts.

61
Q

What are the maximum crosswind components for takeoff and landing?

A

Maximum DEMONSTRATED for Dry: 27 kts, otherwise wet, 27 kts, Contaminated with braking action less than good: 15 kts, or if Captain has less than 100 hrs in type: 27 kts.

62
Q

What are the minimum altitudes for the autopilot?

A

600’ AGL, except for approaches:
Visual and non-precision approaches: 400’ AGL but not lower than 50’ below MDA whichever is higher.
Precision approaches: 80’ AGL, but not lower than 50’ below DA or DH whichever is higher.

63
Q

When is use of the autopilot’s DES submode prohibited?

A

During approach

64
Q

During flight in RVSM airspace, what condition exists regarding the active autopilot and the ATC transponder?

A

Both must be coupled to the same ADC source.

65
Q

What additional action must be taken regarding bleed air if the engine cowl and/or wing anti-ice systems have been selected on during takeoff and landing?

A

The 10th stage valves must be closed.

66
Q

What is the maximum permissible time for ground operations with DC power only? Why?

A

5 minutes, to prevent the CRTs from overheating.

67
Q

When may a circuit breaker be reset or cycled in flight?

A

Never, unless doing so is consistent with explicit procedures specified in the CR2 OM/QRH or unless, in the judgment of the PIC, resetting or cycling of the circuit breaker is necessary for the safe completion of the flight.

68
Q

Are we permitted to use flaps enroute?

A

No

69
Q

Is there a maximum altitude above which we are not permitted to extend flaps?

A

Yes; 15,000 ft

70
Q

To ensure adequate maneuver margins, below what speed must flight spoilers not be extended?

A

The recommended approach speed plus 17 KIAS.

71
Q

What is the minimum altitude for flight spoiler extension?

A

800’ AGL

72
Q

Can flight spoilers be used in conjunction with flaps?

A

Yes, with flap settings 30 or less.

73
Q

When must the Stall Protection System Test be accomplished?

A

Before the first flight of the day.

74
Q

When should the stall protection switches be selected on?

A

For all phases of flight.

75
Q

Engine operation at or near shaker and pusher settings are predicated on which system being operable?

A

The auto-ignition system

76
Q

After how many minutes of the aircraft being stationary must the taxi lights be switched off?

A

10 minutes

77
Q

What indications regarding the thrust reversers would prohibit a takeoff?

A

THRUST REVERSER UNLK light on, REV icon on N1 gauge, L or R REV UNLOCKED caution message.

78
Q

On landing, when is maximum reverse thrust not permitted?

A

Below 60 KIAS reverse thrust must be reduced to idle.

79
Q

What limit exists for the thrust reversers when stationary during the preflight check?

A

They must be reduced to reverse idle.

80
Q

When are we permitted to use thrust reversers to back up the aircraft?

A

Never.

81
Q

When can reverse thrust be used during taxi operations?

A

Never in normal operations, only in emergency situations.

82
Q

With the BTMS operative, what is the minimum cooling time between a landing stop or an aborted takeoff and a subsequent takeoff?

A

15 minutes

83
Q

Pilots must deviate as necessary to comply with a TCAS RA. What exceptions exist?

A

The aircraft performance is limited such as with an engine failure, or conditions are such that it can be seen that there is an obvious error or malfunction in the TCAS.

84
Q

When there is no GPS input, what danger exists regarding the EGPWS?

A

The EGPWS may fail to alert when a terrain threat exists, during ambient surface temperatures below ISA, during non-standard temperature lapse rates, or if incorrect barometric settings are set on the altimeter.

85
Q

When NAV 1 is tuned to a valid ILS frequency, will the ISI display localizer and glideslope deviation? When are we not permitted to use this information?

A

Yes, and we are not permitted to use it during backcourse aproaches.

XJT CRJ-200 (1 decks)

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