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CRJ-200 > Limitations > Flashcards

Limitations Flashcards

1
Q

Cat II

Max Headwind
Max X-Wind
Max Tailwind

A

Headwind 16 kts
Crosswind 15
Tailwind 10

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2
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 (Flight Attendant or Flight Observer) must be present in the flight deck to ensure the required Crewmember is not locked out of the flight deck.

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3
Q

Passenger Door

A

4 Pax/1000 lbs

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4
Q

Cargo

A
  • Within 45 minutes of a suitable airport if cargo is carried
  • 3500 lbs max
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5
Q

Max Pressure Altitude for T/O and Ldg

A

10,000 ft

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6
Q

Max Operating Altitude

A

41,000 ft

37,000 ft (Company)

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7
Q

Max Operating Altitude

Single Pack

A

25,000 ft

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8
Q

Max ambient temp for T/O and Ldg

A

ISA +35*

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9
Q

Min ambient temp for T/O

A

-40*

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10
Q

Max Taxi and Ramp Weight

A

53,250 lbs

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11
Q

Maximum T/O Weight

A

53,000 lbs

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12
Q

Max Landing Weight

A

47,000 lbs

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13
Q

Max Zero Fuel Weight

A

44,000 lbs

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14
Q

Minimum Flight Weight

A

30,000 lbs

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15
Q

Max Tailwind

A

10 kts

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16
Q

Max X-Wind

Wet/Dry

A

27 Kts

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17
Q

Max X-Wind

Contaminated

A

15 kts

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18
Q

Cowl Anti Ice

A

Ground
- 10* or below visible moisture or contaminated surfaces.

Flight

  • TAT 10* in icing conditions except when SAT
  • 40* or below.
  • Ice annunciated
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19
Q

Wing Anti-Ice

Ground Ops

A

Icing Conditions Exist

  • OAT 5* or less
  • Visible moisture below 400 ft
  • Contaminated Runway
  • Precip
  1. Must be on for final taxi unless anti ice fluid applied
  2. On for T/O if icing conditions exist
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20
Q

Wing Anti-Ice

Flight Ops

A

TAT 10* or below with visible moisture

  • ICE Annunciated
  • Below 230 kts in icing conditions
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21
Q

Super Cooled Large Droplet Icing

A

Ice accretion on the side windows

  • Wing/Cowl anti-ice on
  • Leave Icing conditions
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22
Q

Vfe

A

8-230
20-230
30-185
45-170

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23
Q

Vfo

A

8-200
20-200
30-185
45-170

24
Q

Vle

25
Q

Vlo Retract

26
Q

Vlo Extend

27
Q

Max Tire Speed

28
Q

Max Turbulent Air Penetration

A

280 or .75

Whichever is lower

29
Q

Max Wiper Speed

A

220

If wiper has failed in the non-parked position, 220 kts max

30
Q

Minimum operating speed limit

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.

31
Q

Engine Type

32
Q

Airplane Cold Soaked

A

FFOD -30* for more than 8 hours

  • Engines motored and fan rotation verified for 60 sec before engine started
  • Reversers actuated until deploy/stow less than 5 sec
33
Q

Continuous Ignition

A

• Takeoff and landings on contaminated runways
• Takeoffs with high cross-wind components (>27 knots, Company)
• Moderate or heavier intensity rain
• Moderate or heavier intensity turbulence
• Vicinity of thunderstorms
Engine operation at or near the shaker and pusher settings is predicated on an operable auto-ignition system

34
Q

Starter limits

Ground or Air

A

No starter above 55% N2

35
Q

Engine Start

A

1st-60s on 10s off
2nd-60s on 10s off
3rd+ 60s on 5m off

36
Q

Thrust lever movement from shutoff to idle

Max ITT

A

Gnd-120*

Air-90*

37
Q

Dry Motor Cycle

A

May be used for ground or air starts

1st-90s on 5m off
2nd+ 30s on 5m off

38
Q

Flex T/O

A
  • Less than 85% N1
  • Engine cannot achieve full rated thrust
  • Anti-ice used
  • Contaminated Rwy
  • Windshear/Downdraft warnings
  • Special Departure Procedure says no
  • Anti-skid inop
  • May be used on WET Rwy is loaded in Aerodata
  • No lower than 85% N1
  • APR Off data used for assumed temp (auto handled by Aerodata)
39
Q

Fuel Limitations

A
  • Max imbalance-800 lbs
  • Fuel remaining when gauge reads 0 is unusable.
  • T/O with more than 500 in the center prohibited unless 4400 lbs in each wing
40
Q

Min fuel for Go-around

A

450 per wing @ 10* nose up

41
Q

Max fuel load

A

14,518-Pressure

13,906-Gravity

42
Q

Min bulk fuel temp

43
Q

Fuel crossflow

A

Gravity and powered crossflow must be OFF for T/O

44
Q

Min temp for APU start

45
Q

APU start cycle

Battery

A

30s-2m off
30s-20m off
30s-2m off
30s-40m off

46
Q

APU start cycle

DC power

A

15s-2m off
15s-20m off
15s-2m off
15s-40m off

47
Q

APU Bleed Air Limitations

A
  • AC-15,000 ft
  • Eng Starts (in air)-13,000 ft
  • Eng Starts (on gnd)- do not exceed 70% N2
48
Q

Max differential Pressure

A

8.7 to -0.5
Ground 0.1
Max at touchdown 1.0

Do not operate past -1500 in manual mode

Low press ground air used-cabin door must be open

49
Q

Max permissible time on gnd with DC power

A

5 min for CRT cooling

50
Q

Max flap altitude

A

15,000 ft

Enroute use prohibited

51
Q

Min fuel for T/O when a T/O alternate is listed

52
Q

Flight spoilers

A

Not permitted below 1,000 ft

Vref+17 kts

Prohibited with flaps greater than 30*

53
Q

Thrust Reversers

A
  • Gnd only
  • Full stop Ldg only
  • T/O prohibited with unlk light, Rev icon, Unlk caution msg
  • not permitted below 60 kts, at idle below 60 kts.
54
Q

Taxi lights

A

10 min max when stationary

55
Q

Auto Pilot

A

-DES submode prohibited durning appch
-not below 600’
-visual/non precision 400’
Precision 80’
-autopilot on same side as transponder while in RVSM

CRJ-200 (1 decks)

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