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Qlink subjects > Q400 Limitations > Flashcards

Q400 Limitations Flashcards

0
Q

Vmo - 10,000’

A

282 kts

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1
Q

Vmo - 8,000’

A

245 kts

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2
Q

Vmo - F180

A

286 kts

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3
Q

Vmo - F200

A

275 kts

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4
Q

Vmo - F250

A

248 kts

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5
Q

Starting Limits

A

Start 1 - 70 sec on - 2 mins off
Start 2 - 70 sec on - 2 mins off
Start 3 - 70 sec on - 30 mins off

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6
Q

Maximum Number of Occupants

Flight Crew

A

2

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7
Q

Maximum Number of Occupants

Observers?

A

1

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8
Q

Maximum Number of Occupants

Observer?

A

1

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9
Q

Maximum Number of Occupants

Cabin Passengers

A

74

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10
Q

Maximum Number of Occupants

Infants?

A

6

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11
Q

Maximum Number of Occupants

Total

A

85

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12
Q

Weight Limit - Forward Baggage Compartment

A

413 kg

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13
Q

Weight Limit - Aft Baggage Compartment 1

A

1724 kg

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14
Q

Weight Limit - Aft Baggage Compartment 2

A

454 kg

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15
Q

Weight Limit - Aft Baggage Compartment 1 and 2 Combined

A

1724 kg

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16
Q

Manoeuvring Limit Load Factors

Flaps Retracted

A

+2.5 & -1.0 g

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17
Q

Manoeuvring Limit Load Factors

Flaps Extended

A

+2.0 & -0.0 g

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18
Q

Maximum Operating Altitude

A

25000 ft

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19
Q

Maximum Operating Altitude for Take off and Landing

A

10000 ft

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20
Q

Maximum runway slope for Take off and Landing

A

+/- 2%

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21
Q

Maximum Temperature

A

+50 DegC or IAS +35 whichever is lower

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22
Q

Ambient Temperature - Flight and Ground

Minimum Temperature

A

-54 degC

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23
Q

Crosswind and Tailwind

Hard Dry Runway

A

32 kts crosswind - 10 kts tailwind

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24
Q

Crosswind and Tailwind

Contaminated runway
Stand Water, Slush or Loose Snow

A

14 kts crosswind - Nil Tailwind

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25
Q

Crosswind and Tailwind

Contaminated runway
Compacted Snow

A

20 kts Crosswind - Nil Tailwind

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26
Q

Setting takeoff power prior to brakes release, with the nose of the aircraft more than 45 deg out of the wind, is prohibited for wind speeds greater than:

A

8 kts

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27
Q

Vmca - Flap 0

A

113 kts

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28
Q

Vmca - Flap 5

A

98 kts

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29
Q

Vmca - Flap10

A

95 kts

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30
Q

Vmca - Flap 15

A

91 kts

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31
Q

Vmcl - Flap 5

A

100 kts

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32
Q

Vmcl - Flap 10

A

99 kts

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33
Q

Vmcl - Flap 15

A

96 kts

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34
Q

Vmcl - Flap 35

A

92 kts

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35
Q

Vmcg

A

Flap 5, 10 & 15 - 89 kts

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36
Q

Manoeuvring Speed (Va)

A

204 kts

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37
Q

Turbulence Penetration Speed (Vb)

A

210 kts

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38
Q

Max Flap Extension Speed

Flap 5

A

200 kts

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39
Q

Max Flap Extension Speed

Flap 10

A

181 kts

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40
Q

Max Flap Extension Speed

Flap 15

A

172 kts

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41
Q

Max Flap Extension Speed

Flap 35

A

158 kts

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42
Q

Max Landing gear Operation Speed (Vlo) - (Gearspeed)

A

200 kts

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43
Q

Max Landing gear Extended Speed (Vle)

A

215 kts

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44
Q

Max Tyre Speed

A

182 kts

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45
Q

Max tq - MTOP

A

106%

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46
Q

Max Tq - NTOP

A

90.3% (90 or 91 indicated)

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47
Q

Max Tq - Transient

A

135% (20 sec max)

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48
Q

Max Tq - Reverse

A

35%

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49
Q

Max Tq - Max Continous

A

100%

50
Q

Max ITT - MTOP

A

880 degC

51
Q

Max ITT - NTOP

A

822 degC (varies with temp -check graph)

52
Q

Max ITT - Max Continous

A

880 degC

53
Q

Max ITT - Starting

A

920 degC

54
Q

Max ITT - Transient

A

920 degC

55
Q

Max ITT - Reverse

A

880 degC

56
Q

Max Np

A

MTOP, NTOP, Max Cont, and Max Reverse

1020 rpm

57
Q

Max Np - Transient

A

1173 rpm

58
Q

Max Continuous Np overspeed

A

1071 rpm

59
Q

Oil Press PSID

MTOP, NTOP, Max Cont, and Max Reverse

A

61 to 72 psi

60
Q

Oil Press PSID - Starting

A

100 psi Max

165 psi, discing with oil temp < 0 deg

61
Q

Oil Press - Transient

A

44 to 61 psi

72 to 100 psi

62
Q

Oil Temp

MTOP, NTOP, Max Cont, and Max Reverse

A

0 to 107 degC

63
Q

Min Oil Temp

Starting

A

-40 degC

64
Q

Max Oil Temp - Transient

A

125 degC - 5 sec max for torque values above flight idle and less than 55%

65
Q

Ground operations with wind speeds greater than 50 kts must:

A

be reported to maintenance within 24 hrs

66
Q

Max power setting for Ground Static Operation with 36 to 50 kts (gusts to 55 kts)

A

Disc

67
Q

Hyd Qnty for dispatch

A

System 1, 2 and 3 - 50%

68
Q

Min Dispatch - O2

Crew Fixed System

A

1300 psi

69
Q

Min Dispatch - O2

Cabin Crew Supp O2 - 121 lt

A

1600 - 1800 @ 21 deg

70
Q

Min Dispatch - O2

Supp O2 - 311 lt

A

1600 psi at 21 degC

71
Q

Normal Press Differential Limit

A

5.46 psi

72
Q

Max Press Differential Limit

A

5.95 psi

73
Q

Max Cabin Press Differential Limit during Taxiing, Take-off and Landing

A

0.5 psi

74
Q

Max Cabin Alt (for pressurised flight)

A

8000 ft

75
Q

Max Tyre Pressure - Main Wheels

A

140 psi

76
Q

Max Tyre Pressure - Nose Wheels

A

92 psi

77
Q

The Crew Fixed Oxygen system is capable of supplying at least _____ min of protective breathing O2 to each crew member

A

15

78
Q

Gravity refuelling is not permitted when:

A

the APU is running

79
Q

Continuous operation of the APU throughout the refuelling process, requires:

A

sufficient fuel in the left main fuel tank

80
Q

The fuel truck must be parked at least ______ mt ( _____ ft) from the APU exhaust outlet

A

9.2 mt (30 ft)

81
Q

In the case of fuel spillage at the adaptor or the fuel tank vents:

A

refuelling must be stopped immediately

82
Q

At ports not accustomed to refuelling Dash8 aircraft:

A

the re-fueller must be advised that the APU will be running.

83
Q

Pressure Error Correction (PEC) for a precision approach is

A

20 ft

84
Q

Max battery load meter reading for take-off is

A

0.1

85
Q

Min battery temperature for take-off is?

A

-20 degC

86
Q

When Ice is detected the AIRFRAME MODE selector must

A

be positioned to FAST or SLOW

87
Q

During auto pilot operation, a pilot must:

A

be seated at the controls with seat belts fastened

88
Q

In severe Icing conditions, the autopilot:

A

must be disengaged

89
Q

In APP mode, use of the VOR without:

A

associated DME is not permitted

90
Q

With one engine inoperative, the Autopilot must be disengaged:

A

prior to extension of the landing gear or 1000 ft, whichever occurs first

91
Q

Autopilot and Flight director only approaches are approved for glideslope angles of:

A

2.5 to a max of 4 deg

92
Q

On approach the autopilot must be disengaged by ______ ft above runway elevation

A

200

93
Q

After take off or go-round, the minimum height for autopilot engagement is

A

1000 ft agl

94
Q

The AFCS is approved for autopilot approaches to:

A

CAT 1 limits only

95
Q

Unless the baggage compartments are empty, the aircraft must not be operated more than:

A

1 hours flight time from an airport suitable for landing.

96
Q

When the ADF is used as the prime means of navigation or for confirming position, use of the:

A

HF transmitter is prohibited!

97
Q

What distance = 1 hr flight time with OEI

A

276 nm

98
Q

With the Integrated Standby Instrument fitted, what is the maximum fight duration that can be flown from a airport suitable for landing?

A

1 hr flight time

99
Q

The DHC8 Model 402 is eligible for _____ and _____ VFR, _____ and operation in_______ _______

A

day and night, IFR, icing conditions

100
Q

Minimum Flight crew is

A

Two pilots

101
Q

The Engine Model in the Q400 is

A

Pratt and Whittney - PW 150A

102
Q

Minimum operating Temperature is

A

-54 degC

103
Q

Maximum airstart altitude is

A

20000 ft

104
Q

Automatic Take-offpower uptrim is?

A

10% tq (nominal)

105
Q

Maximum Torque for ground operations is?

A

100%

106
Q

Minimum NH is?

A

64.2 %

107
Q

With wind speeds of 36 to 50 kts (gusts of 55 kts) and the nose of the aircraft more that 30 deg out of the wind, the max pwr setting is

A

Disc

108
Q

With wind speeds of 21 to 35 kts and the nose of the aircraft more that 30 deg out of the wind, the max pwr setting is

A

flight idle

109
Q

With wind speeds of 9 to 20 and the nose of the aircraft more that 30 deg out of the wind, the max pwr setting is?

A

60 deg PLA

110
Q

Minimum SAT for engine relight is

A

-40 degC

111
Q

What inflight operation of the power levers is prohibited

A

aft of the FLT IDLE gate

112
Q

Q400 total usable fuel?

A

11724 lbs / 5318 kg

113
Q

Max Fuel imbalance

A

600 lbs / 272 kg

114
Q

The AUX pumps must be ON for?

A

Take off and landing.

115
Q

Continuous operation with the fuel heater outlet temperature indication:

A

below 0 degC and above 71 degC is prohibited

116
Q

Fuel weights are based on a specific gravity of:

A

0.795 at 15 degC

117
Q

The engine Intake bypass doors must be ______ for engine operation in icing conditions

A

open

118
Q

During ground operations in icing conditions the _______ _______ and the _______ _______ _______ must also be on

A

pitot static and the stall warning heat

119
Q

The max permitted WED of contaminate is?

A

15 mm

120
Q

The maximum permitted depth of contaminant is?

A

60mm

121
Q

For WED greater then 3mm:

A

Power levers aft of disc is prohibited

122
Q

Minimum oil temp to ensure engine inlet ice protection is?

A

55 degC

123
Q

Minimum oil temperature required to ensure engine air inlet ice protection, in flight and within 3 minutes of setting take-off power, is?

A

65 degC

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