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CRJ-900 > Limitations > Flashcards

Limitations Flashcards

0
Q

Aircraft Approach Category

A

Category D

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1
Q

Flight Deck Door

A

The flight deck door must be kept closed and locked at all times during flight except to permit access and egress in accordance with the FOM and this CFM.
• Any time the flight deck door is opened in flight, a challenge and response closing and locking verification must be used to verify that the door is closed and locked.
• Any time one of the required flight crew leaves the flight deck, another crewmember must be present in the flight deck to ensure that the required crewmember is not locked out of the flight deck.

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2
Q

Max Ramp Weight

MRW

A

85,000

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3
Q

Max T/O Weight

MTOW

A

84,500

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4
Q

Max Landing Weight

MLW

A

75,100

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5
Q

Max Zero Fuel Weight

MZFW

A

70,750

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6
Q

Minimum Flight Weight

A

45,000

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7
Q

Max Cargo Weight

Aft

A

3,650 (Company)

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8
Q

Max Cargo Weight

Fwd

A

1,700

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9
Q

Max Cruise Mach in RVSM

A

.82 Mach

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10
Q

Vfe

Flaps 1

A

230

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11
Q

Vfe

Flaps 8

A

230

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12
Q

Vfe

Flaps 20

A

220

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13
Q

Vfe

Flaps 30

A

185

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14
Q

Vfe

Flaps 45

A

170

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15
Q

Vle

Landing Gear Extended (cruise down and locked)

A

220

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16
Q

Vlr

Landing Gear Retraction

A

200

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17
Q

Max Airspeed Turbulent Air Penetration

A

280 or .75, whichever is lower

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18
Q

Windshield Wiper Speed

A

250

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19
Q

Max Tire Speed

A

195 (ground speed)

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20
Q

Max Speed for ADG

A

Vmo/Mmo

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21
Q

Max Tailwind

A

10 Kts

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22
Q

Max X-Wind (Dry)

T/O

A

35 Kts

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23
Q

Max X-Wind (Dry)

Landing

A

32 Kts

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24
Q

Max X-Wind (Wet)

Landing or T/O

A

27 Kts

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25
Q

Max X-Wind
Landing
(Fair)

A

20 Kts

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26
Q

Max X-Wind
Landing
(Poor)

A

15 Kts

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27
Q

Max X-Wind (Dry)
Landing or T/O
High Mins

A

CA-25

FO-15

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28
Q

Max Pressure Altitude for T/O and Ldg

A

9,600

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29
Q

Max Operating Altitude

A

41,000

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30
Q

Max temp for T/O and Ldg

A

ISA +35

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31
Q

Min Temp for T/O and Ldg

A

-40

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32
Q

Max flight time with cargo

A

60 minutes

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33
Q

Taxi Lights (aircraft stationary)

A

10 minutes

34
Q

Wheel Brake Cooling Limits

A

Brake cooling times must be observed between a landing or a low- energy rejected takeoff (RTO) and a subsequent takeoff to ensure that sufficient brake energy is available to bring the airplane to a complete stop if the subsequent takeoff is rejected. See “Brake Cooling Requirements - Brake Cooling Requirements - BTMS Inoperative on page 4-167.

35
Q

Max Relief Differential Pressure

36
Q

Max Negative Differential Pressure

37
Q

Max Differential Pressure

Taxi T/O Landing

38
Q

Max Single Pack Operation

39
Q

Door opening with regards to pressurization

A

The airplane must be completely depressurized prior to opening any of the airplane doors.

40
Q

Max Altitude for using EMG DEPRESS

A

15,000 ft for possible ear damage

41
Q

Auto Pilot Useage

A

Prohibited below 600 ft except:

  • Visual/non precision-400 ft
  • ILS (both engines)- 80 ft
  • ILS (single engine)- 110 ft

Operations with an ILS glidepath angle that exceeds 3.5 degrees are prohibited.

42
Q

RVSM airspace and transponder usage

A

When in RVSM, the autopilot must be coupled to the same side transponder

43
Q

Max Individual AC Generator Loading

0-41,000 ft

44
Q

Max load on each TRU

In flight

45
Q

Max time on DC power

Ground ops

A

5 minutes

CRT display cooling

46
Q

Circuit Breaker Reset

In flight

A

A circuit breaker must not be reset or cycled (i.e. opened or closed) unless doing so is consistent with explicit procedures specified in this manual or unless, in the judgement of the pilot in command, that resetting or cycling of the circuit breaker is necessary for the safe completion of the flight.

47
Q

Setting the MDA

A

The next highest 10 foot increment must be selected if the altitude is not at a 10 foot increment.

48
Q

TCAS

A

May deviate from an ATC clearance to comply with an RA

49
Q

Visible Moisture

A

Fog with a visibility of 1 mile or less, rain, snow, sleet, and ice crystals

50
Q

Cowl Anti-Ice

Ground

A

10°C or less with visible moisture or contaminated surface.

Cowl anti-ice on before continuous ignition.

51
Q

Cowl Anti-Ice

Flight

A
  • TAT of 10°C or less in visible moisture (except with SAT -40°C or less)
  • ICE annunciated
52
Q

Wing Anti-Ice

Ground

A

5°C or less with visible moisture or contaminated surface.

If II-IV anti-ice fluid used, wings on just prior to T/O

53
Q

Wing Anti-Ice

Flight

A
  • ICE annunciated
  • In icing conditions with airspeed less than 230

Do not hold in icing with flaps/slats extended

54
Q

Pneumatic System with Anti-Ice usage

A

Wing and/or cowl anti-ice selection is prohibited with the APU as a bleed source in manual mode.

55
Q

Super-Cooled Large Droplet Icing

A

Continued operation in areas where super-cooled large droplet (SLD) icing conditions exist is prohibited.
SLD icing conditions are indicated by ice accretion on the flight compartment side windows.
• The wing anti-icing system must be ON in SLD icing conditions.
• The cowl anti-icing system must be ON in SLD icing conditions.
• Leave icing conditions when side window icing occurs

56
Q

Frost, ice, snow, or slush adhering to any critical surface (wings, winglets, horizontal stabilizer, vertical stabilizer, control surfaces, and engine inlets).

A

Takeoff Prohibited

57
Q

Max Fuel Imbalance

A

T/O-300 lbs

In Flight-800 lbs

58
Q

Max Fuel in Center Tank

A

500 lbs unless more than 4,400 lbs in the wings

59
Q

Min Fuel for a Go-Around

A

600 lbs per wing

Max climb attitude 10° nose up

60
Q

Min Fuel Temp for T/O

61
Q

Fuel Crossflow

A

Powered cross-flow and gravity cross-flow must be off for takeoff.

62
Q

Min ambient temp for APU Starting (cold soaked)

63
Q

APU Start Cycles

A
  • No more than 3 start attempts in 1 hour

- 2 minute delay between starts

64
Q

Max Altitude for APU bleed air Extraction

65
Q

APU bleed air extraction for engine starts

A

No limitation, each engine may be started with it.

66
Q

Max Load on the APU Generator

67
Q

Engine Type

A

GE CF34-8C5

68
Q

Max Fuel Load

A

Pressure- 19,594 lbs

Gravity- 14,810 lbs

69
Q

Engine Warm-up

A
  • Remain at idle until oil pressure at normal range

- Do not exceed 75% N1 until 2 minutes or all indications are in the normal range (whichever takes longer)

70
Q

HIGH PWR SCHEDULE Switch

A

Not permitted

71
Q

Airplane Cold Soaked

A

-30°C for more than 8 hours

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

72
Q

Continuous Ignition

A

• Takeoffs and landings on contaminated runways
• Flight through moderate or heavier intensity rain
• Flight through moderate or heavier intensity turbulence
• Flight in the vicinity of thunderstorms

If continuous ignition and Cowl anti-ice are needed, select the Cowl anti-ice first.

73
Q

Flex T/O

A
  • If wing and/or cowl anti-icing bleeds are in use.
    • On runways contaminated with standing water, slush, snow, or ice.
  • When warnings of windshear or downdrafts have been forecast.
    • When the anti-skid system is inoperative.

The flex thrust procedure may be used on wet runways, provided that wet runway performance data are used.

74
Q

Starter Cranking Limits

A

Starter may not be used if N2 rpm exceeds 45%.

75
Q

Engine Start

Ground

A

1 & 2-90 on 10 sec off

3-5- 90 on, 5 min off

76
Q

Engine Start or Motoring

Flight

A

1- 120 on, 10 sec off

2-5- 60 on, 5 min off

77
Q

Motoring

Ground

A

1- 90 on, 5 min off

2-5- 30 on, 5 min off

78
Q

Thrust Lever

SHUTOFF 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.

79
Q

Thrust Reversers

A
  • Ground use only
  • Full stop landings only, no go-around
  • Takeoff with thrust reverser icons or EICAS warning and/or caution messages displayed is prohibited.
  • Max reverse limited to 75 Kts, idle by 60 Kts
  • With plane stationary, reverse limited to idle
80
Q

Reverse Taxi or Powerback

A

Prohibited

81
Q

Enroute use of Slats/Flaps

A

Prohibited

Do not use above 15,000 ft

82
Q

Flight Spoilers

A
  • Not used below 1,000 ft

- VREF +10 for current weight and flap configuration.

83
Q

Stall Protection System

A

Must remain on for all phases of flight

CRJ-900 (2 decks)

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