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dhc8-102 limitations > Limitations > Flashcards

Limitations Flashcards

1
Q

Max ramp weight

A

35200lb

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2
Q

Max Take off weight

A

35000 lb

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3
Q

Max Landing weight

A

33900

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4
Q

Max Zero fuel weight

A

31700

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5
Q

Load factor limits

A

Flap up : +2.5g / -1g

Flaps down: +2g / 0g

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6
Q

Max operating Altitude

A

25,000 ft

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7
Q

Max altitude for T/O and Landing

A

10,000

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8
Q

Max runway slope T/O and Landing

A

+2% uphil

-2% downhill

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9
Q

Max Tail wind component ( With sup 3)

A

10kt (20Kt)

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10
Q

Max ambiant air temperature limit

A

48,9 or ISA +35 wichever is lower

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11
Q

Min ambient temperature

A

-54 C

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12
Q

Approved T/O Flaps setting

A

5 / 15

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13
Q

Max Altitude with landing gear and/or flaps extended

A

15,000

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14
Q

Vmo 0-14000

A

242 kt

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15
Q

Vmo 15,000’

A

239 kt

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16
Q

Vmo 20’000

A

223 kt

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17
Q

Vmo 25’000

A

207 kt

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18
Q

Vfe Flaps 5

A

148 kt

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19
Q

Vfe Flaps 15

A

148 kt

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20
Q

Vfe Flaps 35

A

130 kt

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21
Q

Va

A

163 kt

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22
Q

Vlo

A

158 kt

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23
Q

Vle

A

172 kt

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24
Q

Rough air airspeed

A

180 kt

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25
Q

Alt Landing gear extension

A

140 kt

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26
Q

Max tire GS

A

139 kt

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27
Q

Max propeller unfeathering

A

165 kt

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28
Q

Starter cranking limits

A

1 minute - 2 min off
1 minute - 2 min off
1 minute - 30 minutes off

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29
Q

Min voltage for GPU or APU engine start

A

24 V

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30
Q

Min Voltage for Battery start

A

22 V

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31
Q

Minimum NH ground operations

A

60%

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32
Q

Max torque with prop feathered

A

50%

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33
Q

Propeller restricted range

A

Continuous ops between 500-780 is prohibited

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34
Q

Propeller Ground limitation

A

Extended ops in excess of 780 must be carried out with airplane facing wind

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35
Q

Min oil temperature for unfeathering or power above idle

A

0 degres

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36
Q

Min oil temp for engine inlet splitter ice protection

A

Temp below -45 could result in ice build up

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37
Q

Pre heat engine prior to start

A

-40 or below

38
Q

Complete Engine shut down

A

Oil pressure below 40 PSI

39
Q

Max T/O max Torque

A

105%

40
Q

Max T/O max ITT

A

816 deg

41
Q

Max T/O max NH

A

100%

42
Q

Max T/O max NP

A

1212RPM

43
Q

Max T/O Oil pressure

A

55-65

44
Q

Max T/O Oil temp

A

45-115

45
Q

Normal T/O max torque

A

92%

46
Q

Normal T/O max ITT

A

785 deg

47
Q

Normal T/O max NH

A

100 %

48
Q

Normal T/O max NP

A

1212 RPM

49
Q

Normal T/O Oil pressure PSI

A

55 to 65 PSI

50
Q

Normal T/O Oil temp

A

45-115 deg

51
Q

Max continuous max Torque

A

90%

52
Q

Max continuous max ITT

A

800 deg

53
Q

Max continuous max NH

A

100%

54
Q

Max continuous max NP

A

1212 RPM

55
Q

Max continuous Oil pressure

A

55 to 65 PSI

56
Q

Max continuous Oil temperature

A

45-115 deg

57
Q

Starting max ITT

A

950 deg
Between 816-850 max 20 seconds
Between 850-950 max 5 seconds

58
Q

Starting max Oil pressure

A

200 PSI

59
Q

Starting oil temperature

A

Min -40 to start

60
Q

Transcient max Torque

A

125%

61
Q

Transcient max ITT

A

850 deg

62
Q

Transcient max NH

A

102%

63
Q

Transcient max NP

A

1320 RPM

64
Q

Transcient max oil temp

A

125 deg max

65
Q

Maximum Reverse max Torque

A

90%

66
Q

Maximum Reverse max ITT

A

785 deg

67
Q

Maximum Reverse max NH

A

100%

68
Q

Maximum Reverse max NP

A

1212 RPM

69
Q

Maximum Reverse Oil pressure

A

55-65 PSI

70
Q

Maximum Reverse Oil temp

A

45-115 deg

71
Q

Max usuable fuel

A

5678 lb

72
Q

Approved fuel

A

Jet A, Jet A1, Jet B, JP-4

73
Q

Fuel heater outlet temperature

A

11-57 deg

74
Q

Max fuel imballance

A

600 lb

75
Q

Electrical load DC Gen on ground

A

0.7

76
Q

Electrical load DC Gen in flight

A

1.0

77
Q

Electrical load TRU gnd and flt

A

1.0

78
Q

Electrical load AC Gen per phase GND

A

Below 10 deg : 1.0

10 deg and above : 0.33

79
Q

Electrical load AC Gen per phase FLT

A

1.0

80
Q

Inverters ground and flight

A

1.0

81
Q

Normal cabin ∆P

A

5.5 PSI (+/- 0.3)

82
Q

Maximum cabin ∆P

A

5.95 PSI

83
Q

Maximum Taxi, T/O and landing ∆P

A

0.5 PSI

84
Q

Maximum cabin altitude pressurized

A

8000 ft

85
Q

Lenght

A

73 ft 01 in

86
Q

Width

A

85 ft

87
Q

Height

A

24 ft 05 in

88
Q

Propeller Diameter

A

13 ft

89
Q

Propeller tip to ground

A

3 ft 01in

90
Q

Hstab Width

A

26 ft

91
Q

Normal 180 radius

A

60 ft

92
Q

Maximum structural design weight

A

21400

dhc8-102 limitations (3 decks)

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