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Jason Various > Limitations - Q400 > Flashcards

Limitations - Q400 Flashcards

1
Q

Maximum Number of Occupants

A

Standard - 85 (74, 3, 2 + 6)
84 - 89 (78, 3, 2 + 6)

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2
Q

Max Ramp Weight

A

S - 29,089
84 - 29,665

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3
Q

Max Brakes Release Weight

A

S - 28,998
84 - 29,574

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4
Q

Max Landing Weight

A

S - 28,009
84 - 28,123

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5
Q

Max Zero Fuel Weight

A

S - 25,855
84 - 26,308

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6
Q

Forward Baggage (Locker 11)

A

413

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7
Q

Aft Baggage (Hold 41)

A

S - 1707
84 - 1270

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8
Q

Aft Baggage (Hold 42)

A

S - 453
84 - 454

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9
Q

Aft Baggage (Hold 41 and 42 combined)

A

S - 1707
84 - 1270

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10
Q

Manoeuvring Limit Load Factors

A

Flap retracted +2.5 g / -1.0 g
Flap extended +2.0 g / 0.0 g

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11
Q

Maximum operating altitude

A

25,000

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12
Q

Maximum operating altitude for takeoff and landing

A

10,000

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13
Q

Maximum operating ambient temperature limit

A

50°C or ISA +35°C whichever is lower

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14
Q

Minimum operating ambient temperature limit

A

-54°C

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15
Q

Maximum Runway Slopes

A

+2% - -2%

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16
Q

Crosswind and Tailwind Component - Hard Dry Runway

A

32 / 10 (10-20kts tailwind permitted per Flight Manual Supplement)

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17
Q

Crosswind and Tailwind Components - Standing Water, Slush, Loose Snow

A

14

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18
Q

Crosswind and Tailwind Components - Compacted Snow

A

20

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19
Q

Taxi Speed limits

A

Normal - 25 / 15
Narrow (15 - 18m width) - 15 / 10

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20
Q

Manoeuvring Speed (VA)

A

204

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21
Q

Turbulence Penetration Speed (VB)

A

210

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22
Q

Maximum Flap Extended Speed (VFE) F5 -

A

200

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23
Q

Maximum Flap Extended Speed (VFE) F10 -

A

181

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24
Q

Maximum Flap Extended Speed (VFE) F15 -

A

172

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25
Q

Maximum Flap Extended Speed (VFE) F35 -

A

158

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26
Q

Maximum Landing Gear Operation Speed (VLO)

A

200

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27
Q

Maximum Landing Gear Extended Speed (VLE)

A

215

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28
Q

Alternate Gear Extension Speed

A

185

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29
Q

Maximum Tyre Speed (Groundspeed)

A

182

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30
Q

Engine Maximum Operating Temperature

A

50°C or ISA+35 whichever is lower

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31
Q

Engine Minimum Operating Temperature

A

-54°C

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32
Q

Engine Maximum Airstart Altitude

A

20,000ft

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33
Q

Engine Automatic Takeoff Power Uptrim

A

10% torque (nominal)

34
Q

With bypass doors open, MTOP and MCP power settings are limited to a maximum ambient temperature of

35
Q

MTOP

36
Q

NTOP

A

90.3 / 822

37
Q

Max Continuous

38
Q

Starting ITT

A

920 - 20 seconds

39
Q

Transient

40
Q

Max Reverse

41
Q

Starting Time Limits

A

70 on 2 min off
70 on 2 min off
70 on 30 min off

42
Q

Minimum SAT for engine relight is

43
Q

Total usable fuel

44
Q

Maximum fuel imbalance between contents of main fuel tanks

45
Q

Tank Aux Pumps for takeoff and landing.

46
Q

Takeoff and continuous in-flight operation with the fuel heater outlet temperature indication
below 0°C or above 71°C

A

Prohibited

47
Q

Minimum Hydraulic Fluid Quantity for Dispatch

A

40%, 40%, 45%

48
Q

Oxygen - Standard Flight Crew Fixed

A

S - 1300psi, Jump - 1800psi
84 - 1050psi, Jump - 1450psi

49
Q

Oxygen - Cabin Portable

50
Q

Pressurisation - Normal cabin pressure differential limit

A

5.46 ±0.1 psi

51
Q

Pressurisation - Maximum cabin pressure differential limit

52
Q

Pressurisation - Maximum cabin pressure differential limit during taxiing, takeoff and landing

53
Q

Pressurisation - Maximum cabin altitude (pressurised flight)

54
Q

Maximum altitude with the landing gear and/or flap extended

A

15,000 ft.

55
Q

Maximum Flap Position during Alternate Gear Extension

56
Q

APU General

A

Is for ground operations only.
Must be shutdown prior to takeoff.
Must not be operated unattended with passengers on board.
Must not be operated unattended during pressure refuelling.
Must not be operated during gravity refuelling.

57
Q

APU ambient temperature limitations

A

Maximum: 50°C or ISA+35, whichever is lower
Minimum: -35°C

58
Q

APU Start limits

A

1 min on 2 min off
1 min on 2 min off
1 min on 30 min off

59
Q

APU Generator loads

60
Q

Refuelling with the APU running

A

Gravity refuelling is not permitted
Starting or shutting down the APU during refuelling is not permitted
The left main fuel tank must contain sufficient fuel to ensure continuous running of the APU throughout the refuelling process
The fuel truck must be parked at least 9.2 m (30 ft) from the APU exhaust outlet
At ports not accustomed to refuelling Dash 8 aircraft, the re-fueller must be advised that the APU will be running

61
Q

Position Error Correction (PEC)

A

20ft to DA

62
Q

Main, Auxiliary and Standby Battery Takeoff Limitation

A

Load - 0.1
Min battery Temp - -20

63
Q

Automatic Flight Control System (AFCS)

A

The AFCS is approved for autopilot approaches to CAT 1 limits only.
APP mode, autopilot engaged approaches, is approved for:
* Flap 0 (minimum altitude 1000 ft AGL)
* Flap 5, 10, 15 and 35
Other autopilot limitations are as follows:
* The autopilot must be disengaged in severe icing conditions
* During autopilot operation, the pilot flying must be seated at the controls with safety and shoulder harness fastened.
* Use of VOR without associated DME is not permitted in APP mode
* After takeoff or go-around, the minimum height for autopilot engagement is 1000 feet AGL
* On approach (precision or non-precision), the autopilot must be disengaged at or above 200 ft above runway elevation
* Flight in conditions of severe atmospheric turbulence with the autopilot engaged is prohibited
* An autopilot approach must not be commenced or continued with an inoperative
engine.
NOTE
The autopilot must be disengaged at or above 1,000 ft AGL
* Autopilot and flight director only approaches are approved for glideslope angle of 2.5° to a maximum of 4 degrees
* Autopilot approaches have been demonstrated in crosswind components up to 18 knots. This is not considered limiting.

64
Q

Baggage Compartment Fire Extinguishing

A

Unless the forward and aft baggage compartments are empty, the airplane must not be operated further than 1 hour flying time from a suitable airport for landing.

65
Q

Avionics

A

-HOT MIC select switches on the pilot and co-pilot ARCDU must be OFF and the INT/RAD switch on the observers Audio Control Panel must be centred, when using the cockpit speakers.
-With HF Comm installed, use of the HF transmitter is prohibited when the ADF is used as the prime means of navigation or for position confirmation.
- With Integrated Standby Instrument, MS 4—432835 or MS 4—456883, installed, the airplane must not be operated further than 1 hour flying time from a suitable airport for landing.

66
Q

Contaminated Runway Operations

A

Standing Water, Slush or Loose Snow Limitations
For Operation from runways contaminated with standing water, slush, or loose snow:
* The maximum operating altitude for takeoff and landing is 6000 ft MSL
* The maximum permitted WED of contaminant is 15 mm
* The maximum permitted depth of contaminant is 60 mm
* For WED greater than 3 mm, selection of power levers aft of DISC is prohibited
* The maximum crosswind component for takeoff and landing is 14 knots

67
Q

MTOP Time Limit

68
Q

Max Oil Temp between discing and flight idle

69
Q

Minimum Oil Temp for power above flight idle

70
Q

Min Oil Temp for takeoff into icing conditions

A

55
then 65 within 3 minutes

71
Q

Minimum Oil Temp to unfeather Propeller

72
Q

Maximum Oil Temp for completion of flight with a 20% reduction in power

73
Q

Maximum allowable continuous NP overspeed

74
Q

Engine Ground Limit Maximum Torque

75
Q

Engine Ground Limit Minimum NH

76
Q

Maximum Wind Speed with the nose more that 30 degrees out of the wind

77
Q

Normal Oil Pressure

78
Q

Oil Pressure Limit (maximum) Starting

A

100 max
165 if OAT below 0

79
Q

Transient Oil Pressure Limits

A

44-61
72-100
Normal Transient Limits 20 seconds

80
Q

Oil Temp Normal

A

0-107
115 with Power reduced 20%

81
Q

Minimum Oil Temp Starting

82
Q

Maximum Oil Temp Transient

Jason Various (7 decks)

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