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Dash 8 > Limitations > Flashcards

Limitations Flashcards

0
Q

MLW 300

A

42000LBS

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1
Q

MLW 200

A

34500LBS

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2
Q

MTOW 200

A

37300LBS

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3
Q

MTOW 300

A

43000LBS

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4
Q

Max Ramp Weight 200

A

37500LBS

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5
Q

Max Ramp Weight 300

A

43200LBS

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6
Q

Gear Operating Speed 200

A

158KTS

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7
Q

Gear Operating Speed 300

A

163KTS

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8
Q

Max Operating Speed @ 0-14,000’ 200

A

242KTS

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9
Q

Max Operating Speed @ 15,000’ 200

A

239KTS

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10
Q

Max Operating Speed @ 20,000’ in a 200

A

223KTS

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11
Q

Max Operating Speed @ 25,000’ in a 200

A

207KTS

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12
Q

What kinds of operations is the Dash 8 eligible for?

A

Day/Night VFR IFR Ops in icing conditions

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13
Q

MZFW for the 200

A

32000LBS

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14
Q

MZFW for the 300

A

39500LBS

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15
Q

Max Operating Speed @ 0-17,000’ in a 300

A

243KTS

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16
Q

Max Operating Speed @ 20,000’ in a 300

A

232KTS

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17
Q

Max Operating Speed @ 25,000’ in a 300

A

214KTS

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18
Q

Manoeuvring Speed in a 200

A

164KTS

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19
Q

Manoeuvring Speed in a 300

A

177KTS

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20
Q

Caution associated with Va

A

Rapid and large alternating control inputs in combination with changes in pitch, roll or yaw may result in structural failure at any airspeed, even below Va

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21
Q

Vturb - 200

A

180KTS

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22
Q

Vturb -300

A

190KTS

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23
Q

Vfe F15 - 200

A

148KTS

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24
Q

Vfe F15 - 300

A

150KTS

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25
Q

Vfe F35 - 200

A

130KTS

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26
Q

Vfe F35 - 300

A

138KTS

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27
Q

Gear Extended Speed - 200

A

172KTS

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28
Q

Gear Extended Speed - 300

A

173KTS

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29
Q

Max Speed with Gear Doors Open (Alternate Gear Extension)

A

140KTS

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30
Q

Max Crosswind

A

36KTS

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31
Q

MTOP 200 Tq / ITT / Np / Oil Px / Oil Temp Are there any limits to this setting

A

107.5% (max 111%) 800°C 1212RPM 55-65psi 45-115°C Yes, 5 mins

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32
Q

MTOP 300 Tq / ITT / Np / Oil Px / Oil Temp Are there any limits to this setting

A

100% (max 105.6%) 800°C 1212RPM 55-65psi 45-115°C Yes, 5 mins

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33
Q

NTOP 200 Tq / ITT / Np / Oil Px / Oil Temp

A

99.5% (includes 2% static increase) Inflight limit is 97.5% 770°C 1212RPM 55-65psi 45-115°C

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34
Q

NTOP 300 Tq / ITT / Np / Oil Px / Oil Temp

A

92% (includes static increase of 2%) Inflight limit is 90% 765°C 1212RPM 55-65psi 45-115°C

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35
Q

MCP 200 Tq / ITT / Np / Oil Px / Oil Temp

A

97.5% for 1200Np 114.2% for 1024Np or lower 800°C 1212RPM 55-65psi 45-115°C

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36
Q

MCP 300 Tq / ITT / Np / Oil Px / Oil Temp

A

90% for 1200Np 96% for 1125Np or lower 800°C 1212RPM 55-65psi 45-115°C

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37
Q

Starting Limits (With reference to Temp)

A

> 800°C - 20secs 840-900°C - 12secs 900-950°C - 5secs

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38
Q

Max Oil Px on starting

A

200psi

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39
Q

Min Oil Temp for Starting

A

-40°C

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40
Q

Transient Power - 200 How long is this allowed?

A

125% 840°C 1320RPM 200psi 125°C 20secs

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41
Q

Transient Power - 300 How long is this allowed?

A

115% 840°C 1320RPM 200psi 125°C Limited to 20secs

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42
Q

Max Reverse - 200

A

90% 770°C

43
Q

Max Reverse - 300

A

90% 765°C

44
Q

Oil Px Limits

A

Normal: 55-65psi Abnormal: 40-55psi (if Nh is BLW 75%) <40psi requires shutdown

45
Q

Oil Temp Limits

A

Normal: 45-115°C Abnormal: 115-125°C limited to 20mins

46
Q

Prior to unfeathering the propeller and for power settings above flight idle, what is the minimum oil temp?

47
Q

What is the minimum oil temp for adequate inlet splitter anti-icing?

48
Q

Starter Cranking Limits

A

1: 1min on / 2min off 2: 1min on / 2min off 3: 1min on / 30min off

49
Q

What is the normal range for the propeller?

A

780-1212RPM

50
Q

What is the propeller restricted range?

A

500-780RPM

51
Q

What is the Maximum refuelling Px?

52
Q

What actions must be taken when refuelling is taking place and people on board?

A

Turn off the fasten seat belt signs Turn off Wx radar Do not transmit on HF SATCOM de-powered Cabin lights illuminated Emergency lights armed Do not start the APU

53
Q

What is the useable fuel in the Mains / Auxs and Cabin Tanks?

A

5678LBS (planned 5400LBS) 4566LBS (planned 4400LBS) 1500LBS per 2xTanks

54
Q

Maximum main tank fuel imbalance

55
Q

Maximum fuel temperature?

56
Q

Minimum fuel temperature for takeoff

57
Q

What are the notes associated with the Auxillary tanks? (There are 3)

A

1: Main tanks must be full prior to refilling Aux tanks 2: Aux fuel transfer not permitted during takeoff 3: Fuel XFR from Aux to Mains should be commenced immediately ATO

58
Q

At what quantity in the Aux tanks can Cabin fuel XFR be started

59
Q

Minimum HYD QTY for dispatch

A

No 1: 1.5QTS No 2: 3.0QTS

60
Q

What is the time limit for operation of the PTU in a non-ARPS aircraft Why

A

5mins The hydraulic circuit in a non-ARPS aircraft is very small and therefore prone to overheating of the fluid

61
Q

Min dispatch Px for the Sick Pusher

A

0°C - 940psi 20°C - 1000psi 40°C - 1060psi

62
Q

Min dispatch Px for O2

A

2 crew - 1300psi 3 crew - 1800psi Cabin portable - 1100psi

63
Q

How long should protective breathing equipment supply O2

64
Q

Tyre Px - 200

A

Nose: 102psi Mains: 94psi

65
Q

Tyre Px - 300

A

Nose: 62psi Mains: 101psi

66
Q

Max operating ambient temperature for ops and APU

A

48.9°C or ISA+35 whichever is lower

67
Q

Minimum operating temperature

68
Q

APU Starter Cranking Limits

A

Same as Engines

69
Q

After a failed APU start attempt, how long is the APU automatically disabled for?

70
Q

What is the recommended period between APU starts Why

A

5mins Allows excess fuel to drain

71
Q

Limitations of the AFCS (11) DOG CHES BEEF

A

1: Use of VOR w/out DME is not permitted in NAV & APP mode 2: The AP must not be manually overpowered 3: AP & FD approaches are approved for angles of 2.5°-4°. G/S angles > 3° approved for F15 only 4: Approved for CAT I only 5: With AP engaged, the pilot must be seated at the controls with seatbelt fastened 6: An AP APPR must not be commenced with an engine inop 7: AP must be disengaged in severe icing 8: AP BCS APP not permitted 9: Min height for AP engagement is 1000’ 10: AP must be disengaged by 200’ ABV RWY elev 11: APP mode is not permitted with: F35 F5 with AP engaged BLW 1500’ F0 with AP engaged BLW 500’

72
Q

Limitations of the DC On the ground In the air

A

Ground: 0.7 Air: 1.0

73
Q

Limitations of a TRU Ground Air

A

Ground: 1.0 Flight: 1.0

74
Q

AC Generator Limitations

A

Ground (up to 10°C) - 1.0 Ground (above 10°C) - 0.33 Flight - 1.0

75
Q

Inverter Limitations

A

Ground and Flight - 1.0

76
Q

EFIS Limits

A

1: ILS not permitted when in composite 2: Primary radar display must be monitored during flight conditions that require the radar 3: OM for the EFIS must be carried on the aircraft 4: If aircraft is only fitted with 1x DME, selecting #2 VOR in MAP mode is prohibited

77
Q

Ditching Dam Px

A

1400psi @ 21°C

78
Q

Load Factors Flap 0 Flap Extended

A

0 - +2.5g / -1.0g Extended - 2.0g / 0.0g

79
Q

Max Operating Altitude

80
Q

Max Altitude for Takeoff and Landing

81
Q

Maximum RWY slope

82
Q

Maximum downwind component

A

10KTS (measured at a height of 10m)

83
Q

Continuous operation with fuel heater outlet temperature indication of what is prohibited

A

Below 11° C or above 57° C

84
Q

Engine and Prop ground operating limitations

A

Max Tq 92.5% Max Tq with propeller feathered 48% Min NH - 66% Propeller continuous operation between 500 and 780 rpm is prohibited. Extended operation with propeller rpm in excess of 780 must only be carried out with airplane headed directly into wind.

85
Q

Max Altitude with gear and flap extended

86
Q

Max tyre speed

87
Q

Normal Cabin Diff

A

5.5 +/- 0.3psi

88
Q

Max Cabin Diff

89
Q

Max Cabin Diff for Taxi/Takeoff/Landing

90
Q

Max Cabin Altitude

91
Q

Definition of Icing conditions

A

Icing conditions exist when the SAT on the ground and for take-off is 10°C or below, or SAT in flight is 5°C or below, and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, or ice crystals). Icing conditions also exist when the SAT on the ground and for take-off is 10°C or below when operating on ramps, taxiways or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.

92
Q

Limitation for use of HF

A

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.

93
Q

Max tyre speed

94
Q

Normal Cabin Diff

A

5.5 +/- 0.3psi

95
Q

Max Cabin Diff

96
Q

Max Cabin Diff for Taxi/Takeoff/Landing

97
Q

Max Cabin Altitude

98
Q

Definition of Icing conditions

A

Icing conditions exist when the SAT on the ground and for take-off is 10°C or below, or SAT in flight is 5°C or below, and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, or ice crystals). Icing conditions also exist when the SAT on the ground and for take-off is 10°C or below when operating on ramps, taxiways or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.

99
Q

Limitation for use of HF

A

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.

101
Q

Max Takeoff Power (MTOP) limit

102
Q

Transient time limits

103
Q

Max Tq with the prop feathered

104
Q

Minimum flight idle Nh

105
Q

Wet RWY limitations

A

All the following are prohibited * Takeoff with 0°F * Antiskid inop * Unpaved/Gravel RWY * Auto Fx inop * Any downwind component

106
Q

Engine - 300

A

PW123E 2140 with up trim of 2380 SHP

107
Q

Engine - 200

A

PW123D 1950 with up trim of 2150 SHP

Dash 8 (7 decks)

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