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Crj200 > Crj200 Limitations > Flashcards

Crj200 Limitations Flashcards

1
Q

What type of engines are on the CRJ200

A

GE CF34-3B1 Both engines produce 8,729 pounds of thrust

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2
Q

What uses 14 stage bleed air?

A

Engine cowl and Wing anti ice and thrust reversers

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3
Q

What is the Max ramp and taxi weight?

A

53,250lbs

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4
Q

What is the max take off weight?

A

53,000

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5
Q

What is the max landing weight?

A

47,000lbs

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6
Q

What is the maximum zero fuel weight?

A

44,000lbs

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7
Q

What is the minimum flight weight?

A

30,000lbs

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8
Q

Max cargo weight?

A

3500lbs

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9
Q

If cargo is carried …flight must be within X min of a suitable airport?

A

45min

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10
Q

Max Turbulent air speed

A

280kts or m.75 which ever is lower

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11
Q

Max operating speed

A

.85 or 335kts

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12
Q

Max relief differential pressure

A

8.7psi

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13
Q

Max altitude for single pack operations

A

25,000ft

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14
Q

Maximum negative differential pressure

A

-.5 psi

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15
Q

Maximum differential pressure for taxi, take off and landing?

A

1 psi

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16
Q

Minimum cabin altitude C ALT while in manual mode?

A

-1500ft

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17
Q

Minimum for auto pilot to be engaged.

A

600ft

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18
Q

Auto pilot must be disconnected on a visual or non-precision approach by?

A

400ft

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19
Q

Auto pilot must be disconnected on a precision approach (ILS) by ?

A

80ft

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20
Q

On the FMS what function must be used when gps sensors are unavailable.

A

FMS auto tune

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21
Q

Aircraft not equipped with a gps sensor shall not use…

A

FMS navigation (white needles) on a missed approach

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22
Q

On a GPS or GNSS Approach what would cause a missed approach past the FAF on the PFD

A

NO APPR

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23
Q

When can you not use the VNAV or Snowflake during IMC or VMC AT NIGHT?

A

Temp at the arrival airport is less than 0 Deg Celsius

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24
Q

When conducting a GNSS NDB or VOR approaches …what should you monitor.

A

ADF OR VOR as the primary source for the final track guidance

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25
Q

What do you need to check for before you commence a GPS Approach on the FMS

A

RAIM is available at the ETA

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26
Q

Where else should you check and see if RAIM is available?

A

At your Alternate airport and at the ETA

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27
Q

What equipment must you have for a SCDA Approach?

A

2 Barometric Altimeters
1 rad alt
1 GPS

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28
Q

What mode is prohibited on the HGS

A

F/D mode

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29
Q

When can you use Aii mode?

A

Never..it is prohibited

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30
Q

On the HGS when is VMC mode authorized?

A

Cruise, Final and visual approach and landing only

31
Q

On the HGS …when is rolling takeoffs only approved?

A

RVR 1200 or higher

32
Q

On the HGS what mode is only approached for landing with flaps 45 or less?

A

PRI

33
Q

When using the HGS …on a A mode approach…when must the autopilot be disconnected by?

A

Before reaching 650ft

34
Q

What are the RVSM required equipment?

A 
Auto pilot 
Altitude alerting system 
Altitude reporting transponder
Air data computer or ADC
Barometric Altimeter x2 
TCAS
35
Q

What is the maximum altitude for APU use?

A

37,000ft

36
Q

Make load for each TRU in flight is?

A

100amps

37
Q

Maximum airspeed with ADG deployed?

A

VMO

38
Q

Max altitude for slats/flaps?

A

15,0000

39
Q

Minimum altitude for spoilers?

A

300 ft

40
Q

Max fuel when pressure fueling?

A

14,518lbs

41
Q

Max fuel in each wing and the centre tank when pressure fueling ?

A

4760lbs each side and 4988lbs in the centre

42
Q

What is the minimum fuel temp for takeoff?

A

5 deg c

43
Q

Max take off fuel imbalance in the centre tank?

A

500lbs
Unless each main wing tank is is above 4,400lbs
Or
Each wing tank is 2,000lbs and allowable zfw is reduced By the way of the fuel in the centre tank in excess of 500 pounds and the centre of gravity in this condition is verified within the limits.

44
Q

What is the max fuel imbalance between the main tanks?

A

800 lbs

45
Q

What is the minimum fuel in each wing tank for goal round?

A

450lbs

46
Q

What is the normal hydraulic pressure?

A

2800 to 3200 psi

47
Q

What is the normal hydraulic system quantity?

A

45% to 85%

48
Q

What bleed valves must be closed for takeoff and landing if the wing and the ice and or cowl anti-ice is on?

A

L and R 10th stage

49
Q

What is the maximum operating speed for the windshield wipers?

A

220 kts

50
Q

When operating in super cool and large droplet icing what must be on?

A

Wing and cowls and leave icing conditions when side icing occurs

51
Q

When you were on the ground when was the Cowl anti-ice be on for taxi and takeoff?

A

When the OAT is 10deg or below and visible moisture in any form is present below 400 feet.
Runaway ramps in taxiways are contaminated and
any presence of precipitation.

52
Q

When does the wing anti- ice need to be on for taxi prior to take off?

A

When the OAT is 5 deg or below
Or when type 2,3,4 anti ice fluids have been used
When going to de ice
Single engine taxi out

53
Q

When is the wing anti ice needed for take off?

A 
When the OAT is 5 deg or below
And
Visible moisture below 400 AGL
Or
Contaminated runway
Or
Precipitation
54
Q

After type 2,3,4 device fluid has been used…when should the wings be selected on?

A

Just prior to thrust increase for takeoff

55
Q

In flight…what temps can icing be encountered during visible moisture?

A

From TAT of 10 deg or less unless SAT is -40

56
Q

When the ICE Message appears ..what should you do?

A

Turn wings on (below 230 kts) and cowls on

57
Q

Maximum landing gear extension?

A

250kts

58
Q

Maximum landing gear retraction?

A

200kts

59
Q

What is the tire limit Speed?

A

182kts gs

60
Q

What is the minimum brake cooling time? Between landing and the next takeoff.

A

15 mins

61
Q

During all engine starts how long must you wait before high thrust?

A

Do not exceed 75% or 2 min

62
Q

No starter cut out happens what should you do?

A

Hit the engine stop button.

63
Q

What is the maximum time on for the starter?

A

1 min followed by 10 secs off

64
Q

An engine start from shut off to idle, what are you looking for on engine parameters?

A

Below 120 ITT AND 20% n2

65
Q

On a engine start, if you need to dry motor what is the maximum time on followed by the maximum time off?

A

90 seconds on, five minutes off

66
Q

What is the minimum oil pressure at idle?

A

25 psi

67
Q

When must continuous engine ignition be used?

A 
On takeoff and landing on contaminated runways
high crosswind components
Flight through moderate or heavy rain
In the vicinity of thunderstorms
In moderate or heavy turbulence
Takeoff after deicing


68
Q

Flex thrust must not be lower than

A

85% N1

69
Q

When should reduce thrust for takeoff not be used?

A 
The antiskid system is in operative
The wing and Cowls are on
Contaminated runway
Wind shear reports
On wet runways unless wet data is used
Aero data requires special departure procedure
70
Q

FMS generated FLX 1 must be …

A

Greater than or equal to aerodata calculated FLX N1 Value

71
Q

Max operating altitude for APU

A

37,000ft

72
Q

Max starting altitude for APU

A

30,000ft

73
Q

Bleed air extraction is not permitted above…

A

15,000 ft

Crj200 (1 decks)

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