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Aviation > Q400 Limitations > Flashcards

Q400 Limitations Flashcards

1
Q

Length of wing span

A

93’ 3”

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2
Q

Propellor diameter

A

13’ 6”

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3
Q

Dimension of propellor clearance to ground

A

3’ 3”

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4
Q

Dimension of nose to propellor

A

36’ 10”

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5
Q

Fuselage length

A

107’ 9”

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6
Q

Fuselage height

A

27’ 4”

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7
Q

Inner gear turn radius

A

4’ 9”

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8
Q

Outer gear turn radius

A

33’ 10”

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9
Q

Nose gear turn radius

A

50’ 7”

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10
Q

Wing tip turn radius

A

64’ 9”

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11
Q

Nose turn radius

A

54’ 10”

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12
Q

Elevator turn radius

A

62’ 9”

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13
Q

HGW Aircraft serial numbers

A

4181 and 4186

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14
Q

HGW Ramp weight

A

64700

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15
Q

HGW Take off weight

A

64500

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16
Q

HGW Landing weight

A

61750

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17
Q

HGW Zero fuel weight

A

57000

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18
Q

EGW Ramp weight

A

65400

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19
Q

EGW Takeoff weight

A

65200

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20
Q

EGW Landing weight

A

62000

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21
Q

EGW Zero fuel weight

A

58000

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22
Q

CG HGW fwd limit up to 53000lbs

A

13.8% mac

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23
Q

CG HGW fwd limit 53000lbs - 64500lbs

A

13.8% - 17.4% mac

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24
Q

CG HGW aft limit

A

36% mac

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25
Q

CG EGW fwd limit up to 53000lbs

A

13.8% mac

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26
Q

CG EGW fwd limit 53000lbs - 65200lbs

A

13.8% - 17.7% mac

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27
Q

CG EGW aft limit

A

36% mac

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28
Q

Maneuvering Limit load factor flaps retracted

A

+2.5G / -1G

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29
Q

Maneuvering Limit load factor flaps extended

A

+2G / -0G

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30
Q

Min fuel imbalance

A

600lbs

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31
Q

Vmo up to 8000’

A

245 kias

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32
Q

Vmo 10000’

A

282 kias

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33
Q

Vmo 18000’

A

286 kias

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34
Q

Vmo 20000’

A

275 kias

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35
Q

Vmo 25000’

A

248 kias

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36
Q

Min speed flaps 0º

A

175 kias

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37
Q

Min speed flaps 5º

A

160 kias

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38
Q

Min speed flaps 10º

A

150 kias

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39
Q

Min speed flaps 15º

A

145 kias

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40
Q

Vfe 5º

A

200 kias

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41
Q

Vfe 10º

A

181 kias

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42
Q

Vfe 15º

A

172 kias

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43
Q

Vfe 35º

A

158 kias

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44
Q

Va

A

204 kias

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45
Q

VLo

A

200 kias

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46
Q

VLe

A

215 kias

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47
Q

Rough Air Speed

A

210 kias

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48
Q

Alternate gear extension speed

A

185 kias

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49
Q

Max operating altitude

A

25000’

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50
Q

Max takeoff/landing altitude

A

10000’

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51
Q

Approach category and CAT minimums

A

category C CAT1

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52
Q

Max/Min runway slope

A

+2/-2%

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53
Q

Max tailwind takeoff flaps 10º-15º

A

20 kts

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54
Q

Max tailwind takeoff flaps 5º

A

10 kts

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55
Q

Max tailwind landing flaps 35º

A

20 kts

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56
Q

Max tailwind landing flaps 10º-15º

A

10 kts

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57
Q

Final segment flap setting limit

A

15º

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58
Q

Minimum runway width

A

100’

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59
Q

Minimum runway width plowed runway

A

75’

60
Q

Minimum runway width plowed taxiway

A

50’

61
Q

X-wind component hard, dry, or wet runway

A

32 kts

62
Q

Dry loose snow height takeoff/landing limit

A

4” takeoff / 5.1” landing

63
Q

X-wind component dry loose snow

A

18 kts (R)

64
Q

X-wind component standing water, slush, wet snow

A

14 kts (R)

65
Q

Standing water limit

A

1/4”

66
Q

Standing slush limit

A

1/2”

67
Q

Wet snow limit

A

3/4”

68
Q

Max ambient temp limit

A

50ºC or ISA +35

69
Q

Min ambient temp limit

A

-54ºC

70
Q

Display warmup period

A

> 3hrs ≤-15ºC

71
Q

Static takeoff limit

A

X-wind >45º >8kts

72
Q

Taxi limitation single engine and reverse thrust

A

Not authorized except exiting runway on single engine landing

73
Q

Tank aux pumps for takeoff and landing

A

ON

74
Q

Fuel heater temp limit

A

0ºC - 71ºC

75
Q

Min oil pressure

A

44psi

76
Q

Normal oil pressure

A

61 - 72psi

77
Q

Transient minimum pressure

A

44 - 61psi

78
Q

Min oil temp for start

A

-40ºC

79
Q

Min oil temp above flight idle

A

0ºC

80
Q

Min oil temp ground idle

A

-40ºC

81
Q

Max oil temp continuous

A

107ºC

82
Q

Max oil temp PLA DISC - FLT idle

A

125ºC

83
Q

Min oil temp above ground idle

A

0ºC

84
Q

Min oil temp above ground idle icing conditions

A

takeoff 55ºC / ≥3 min of flight 65ºC

85
Q

APU must be…

A

Shut down prior to takeoff, attended with pax onboard, attended while pressure refueling.

86
Q

APU N/A

A

during flight or gravity refueling

87
Q

APU ambient temperature min/max ambient temp limit

A

-35ºC / +50ºC or ISA +35

88
Q

APU installed louvers temp limit

A

21ºC

89
Q

APU starter limits

A

60sec ON 2min OFF
60sec ON 2min OFF
60sec ON 30min OFF
Thereafter maintenance required

90
Q

Propellor manufacturer and model

A

Dowty Aerospace R408

91
Q

Powerplant manufacturer and model

A

Pratt and Whitney PW150A

92
Q

Powerplant ambient limit

A

-54ºC / +50 or ISA+35ºC

93
Q

Bypass doors open, MTOP, MCP ambient temp limit

A

ISA +25

94
Q

Max altitude for air start

A

20000’

95
Q

Automatic takeoff power uptrim

A

10% torque

96
Q

MTOP

A

5071 SHP / 106% TRQ

97
Q

NTOP

A

4580 SHP / 90.3% TRQ

98
Q

MCP

A

100% TRQ

99
Q 
MTOP settings (limited to...)
TRQ %
ITT ºC
NL %RPM
NH %RPM
NP RPM (max continuous overspeed)
Oil press range
Oil temp range
A 
Limited to 5min
TRQ: 106% 
ITT: 880ºC 
NL: 100%rpm 
NH: 100%rpm 
NP: 1020rpm (max continuous overspeed 1071)
Oil Press: 61-72psi
Oil Temp: 0º-107ºC
100
Q 
NTOP settings 
TRQ %
ITT ºC
NL %RPM
NH %RPM
NP RPM (max continuous overspeed)
Oil press range
Oil temp range
A 
TRQ: 90.3% 
ITT: Variation with ambient air temp 
NL: Variation with ambient air temp 
NH: Variation with ambient air temp  
NP: 1020rpm (max continuous overspeed 1071)
Oil Press: 61-72psi
Oil Temp: 0º-107ºC
101
Q 
MCP settings
TRQ %
ITT ºC
NL %RPM
NH %RPM
NP RPM (max continuous overspeed)
Oil press range
Oil temp range
A 
TRQ: 100% 
ITT: 880ºC 
NL: 100%rpm 
NH: 100%rpm 
NP: 1020rpm (max continuous overspeed 1071)
Oil Press: 61-72psi
Oil Temp: 0º-107ºC
102
Q

Starting settings
Max ITT ºC (time limit)
Max oil press (disc’ing below 0ºC)
Min oil temp

A

ITT: 920ºC (20sec)
Max Oil press: 100psi (165psi when disc’ing below 0ºC)
Min Oil temp: -40ºC

103
Q 
Transient settings (limited to...) 
TRQ %
ITT ºC
NL %RPM
NH %RPM
NP RPM 
Oil press range
Oil temp limit (time limit)
A 
Limited to 5min
TRQ: 135% 
ITT: 920ºC 
NL: 102.3%rpm 
NH: 101.3%rpm 
NP: 1173rpm 
Oil Press: 44-61psi and 72-100psi
Oil Temp: 125º (5sec max for TRQ values >FLT idle <55%)
104
Q 
Max reverse settings
TRQ %
ITT ºC
NL %RPM
NH %RPM
NP RPM 
Oil press range
Oil temp range
A 
TRQ: 35% 
ITT: 880ºC 
NL: 100%rpm 
NH: 100%rpm 
NP: 1020rpm 
Oil Press: 61-72psi
Oil Temp: 0º-107ºC
105
Q

Starter cranking limits

A

70sec ON / 2min OFF
70sec ON / 2min OFF
70sec ON / 30min OFF

106
Q

Wide cut fuel types are…

A

Prohibited

107
Q

Usable fuel

A

5862lbs / tank

108
Q

Max engine torque on ground

A

100%

109
Q

Max engine NH on ground

A

64.2%

110
Q

Max X-wind at 30º

A

50kts (mx action required)

111
Q

Max power setting when maneuvering on ground

Wind speed: 9-20kts

A

FLT Idle (momentarily increase for acceleration)

112
Q

Max power setting when maneuvering on ground

Wind speed: 21-35kts

A

FLT Idle

113
Q

Max power setting when maneuvering on ground

Wind speed: 36-50kts

A

Flight Idle (disc when static)

114
Q

Max power setting when STATIC on ground

Wind speed: 9-20kts

A

≤60ºPLA

115
Q

Max power setting when STATIC on ground

Wind speed: 21-35kts

A

FLT Idle

116
Q

Max power setting when STATIC on ground

Wind speed: 36-50kts

A

DISC

117
Q

Power lever aft of flight idle in flight is…

A

Prohibited

118
Q

Min SATºC for engine relight

A

-40ºC

119
Q

Max batt load meter reading for takeoff

Min batt temp for takeoff

A
  1. 1

- 20ºC

120
Q

Max load air/ground for AC/DC gen and TRU

A

1.0

121
Q

Max altitude for extending landing gear and flaps

A

15000’

122
Q

Max tire speed

A

182kts groundspeed

123
Q

Normal cabin press diff limit

A

5.46 +/- 0.1psi

124
Q

Max cabin press diff limit

A

5.95psi

125
Q

Max cabin press diff limit taxi/takeoff/landing

A

0.5psi

126
Q

Max cabin altitude

A

8000’

127
Q

Observe brake cooling between

A

Landing/rejected takeoff and subsequent takeoff

128
Q

Airframe mode select switch in icing conditions

A

FAST

129
Q

Icing conditions exist when?

A

SAT is ≤10ºC on ground visible moisture or contaminated runways or ≤5ºC in flight with visible moisture

130
Q

Autopilot engaged approaches approved for all flap configurations with a height limitation of ___ for
Flap 0º

A

1000’agl

131
Q

Autopilot must be disengaged

A

Severe icing
Severe turbulence
200’agl
1000’agl or FAF which ever is lower during SE approach

132
Q

Autopilot cannot be engaged until

A

1000’agl on takeoff or missed approach

133
Q

Autopilot is not approved for

A

Approaches other than CAT1

VOR without DME function

134
Q

Autopilot and FD approved for glideslope angles between…

A

2.5º-4º

135
Q

Use of VS mode

A

Prohibited for climb (R)

136
Q

Max flight time to suitable airport for landing if cargo is in FWD/AFT or either

A

1hr

137
Q

Cockpit speakers configuration

A

HOT MIC OFF Pilot/Copilot

Observer audio panel INT/RAD Centered

138
Q

ISIS flight time limitation

A

45min

139
Q

PFD MFD ED cycle limitation

A

Once every 24hrs

140
Q

Oxygen required for dispatch portable bottle

A

1600psi

141
Q

Oxygen required for dispatch 3 crew

A

1450psi

142
Q

Oxygen required for dispatch 2 crew

A

1050psi

143
Q

Derived dip down for RNAV approaches

A

MDA +50’

144
Q

VNAV vertical path angle limits enroute and approach

A

6º enroute

4º approach

145
Q

Route of flight limitation

A

within 1hr of a suitable airport with still air normal speed one engine inoperative

146
Q

Takeoff alternate distance

A

250NM

147
Q

Landing light limitation

A

5min (R)

Aviation (3 decks)

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