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Air Nelson/Q300 > Limitations > Flashcards

Limitations Flashcards

1
Q

MTOP (Oil Temperature)

A

45°C to 115°C

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2
Q

Minimum NH on the ground

A

66%

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3
Q

Normal cabin pressure differential limit

A

5.5 + or - 0.3 psi

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4
Q

Starter Cranking Time Limits

A

1 minute on, 2 minutes off for 2 starts, then 30 minutes off after 3rd start.

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5
Q

MTOP Time Limit

A

5 minutes

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6
Q

What FMS based approaches are prohibited?

A

ILS, LOC

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7
Q

AFCS (Glideslope)

A

Only approved for glideslope angles of 2.5° to 4°. Glideslope angles greater than 3° only approved for Flap 15°.

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8
Q

What mode of the AFCS may not be used when using a VOR without associated DME?

A

NAV and APP

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9
Q

Max Continuous (Max NL)

A

104%

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10
Q

Maximum cabin altitude (pressurised flight)

A

8,000 ft.

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11
Q

Maximum load meter reading for ground operation at or above 10°C (AC Generator)

A

0.33

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12
Q

Maximum operating altitude

A

25,000 ft.

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13
Q

NTOP (Max NL)

A

101.7%

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14
Q

Max Fuel Imbalance

A

272 kg

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15
Q

Maximum torque with propeller feathered

A

48%

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16
Q

Vfe 10°

A

154 knots

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17
Q

What are the vertical path angle limits on the FMS?

A

6° in en-route and terminal mode and 4° in approach mode

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18
Q

NTOP (Np)

A

1212 rpm

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19
Q

Transient (Np)

A

1320 rpm

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20
Q

Engine Start Tailwind limits (GPU assisted start)

A

35 knots

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21
Q

Maximum cabin pressure differential limit

A

5.95 psi

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22
Q

Maximum Operating Ambient Temperature

A

Lesser of 48.9°C or ISA + 35

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23
Q

Transient (Max NL)

A

104.3%

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24
Q

Vfe 15°

A

150 knots

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25
Q

Manoeuvring Limit Load Factors (Flaps Extended)

A

+2.0g/0.0g

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26
Q

Starting (Oil Pressure)

A

200 psi

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27
Q

On the AFCS, APP mode is not permitted with:

A

Flaps 35°/ Flaps 5° and autopilot engaged below 1500ft. AGL/ Flaps 0° and autopilot engaged below 500ft. AGL

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28
Q

Maximum Tailwind Component for Take-off and Landing

A

10 knots (20 knots for Air Nelson with Limitations)

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29
Q

Maximum Runway Slope

A

2% up or down

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30
Q

Vfe 5°

A

163 knots

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31
Q

Transient (Max ITT)

A

840°C

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32
Q

Maximum load meter reading for flight operation (AC Generator)

A

1.0

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33
Q

MTOP (Np)

A

1212 rpm

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34
Q

Transient (Max Torque)

A

115%

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35
Q

Vfe 35°

A

138 knots

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36
Q

Operating in Icing Conditions (Engine/Airframe)

A

Engine intake by-pass doors must be open and engine ignition switch at AUTO; When ice is detected, the AIRFRAME AUTO selector must be selected to FAST or SLOW

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37
Q

Engine Start Tailwind limits (Battery start)

A

No tailwind permitted

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38
Q

Useable fuel capacity

A

1287 kg each tank

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39
Q

MTOP (Max NL)

A

104%

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40
Q

When must the autopilot be disengaged on approach?

A

200ft above runway elevation

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41
Q

Icing Conditions (in Flight)

A

SAT in flight 5°C or below and visible moisture in any form is present (e.g. cloud/fog with vis one mile or less, rain, snow, sleet, or ice crystals)

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42
Q

Max Reverse (Np)

A

1212 rpm

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43
Q

May the AFCS be used OEI on an approach?

A

No

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44
Q

Maximum torque on the ground

A

92.5%

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45
Q

Engine

A

PW123

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46
Q

Cargo Compartment 3 Weight

A

181 kg

47
Q

Max Continuous (Max NH)

A

102.7%

48
Q

NTOP (Max ITT); Can this be exceeded?

A

765°C (May be exceeded by 5°C for a maximum of 30 seconds)

49
Q

Max Continuous (Oil Temperature)

A

45°C to 115°C

50
Q

Cargo Compartment 2 Weight

A

454 kg

51
Q

Maximum Ramp Weight

A

19,595 kg

52
Q

Maximum load meter reading for ground operation below 10°C (AC Generator)

A

1.0

53
Q

Maximum load meter reading for ground operation (Inverter)

A

1.0

54
Q

Max Continuous (Max ITT)

A

800°C

55
Q

NTOP (Oil Pressure)

A

55 psi to 65 psi

56
Q

Maximum Zero Fuel Weight

A

17,917 kg

57
Q

NTOP (Max NH)

A

101%

58
Q

Max Reverse (Max ITT)

A

765°C

59
Q

Icing Conditions (Ground)

A

SAT 10°C or below and visible moisture in any form is present (e.g. cloud/fog with vis one mile or less, rain, snow, sleet, or ice crystals) or 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.

60
Q

Max Reverse (Oil Pressure)

A

55 psi to 65 psi

61
Q

Manoeuvring Limit Load Factors (Flaps Retracted)

A

+2.5g/-1.0g

62
Q

Vmo (0-17,000 ft.)

A

243 knots

63
Q

Maximum cabin pressure differential limit during taxiing/take-off/landing

A

0.5 psi

64
Q

Maximum load meter reading for flight operation (TRU)

A

1.0

65
Q

When is lower than normal oil pressure acceptable?

A

Between 40 and 55 psi is allowed at engine speed below 75% NH

66
Q

Cargo Compartment 1 Weight

A

839 kg

67
Q

Maximum Tyre Speed

A

165 knots

68
Q

Engine Start Tailwind limits (APU or Cross Generator assisted start)

A

20 knots

69
Q

Maximum load meter for ground operation (TRU)

A

1.0

70
Q

Time limit for above normal maximum oil temperature

A

115°C to 125°C is time limited to 20 minutes

71
Q

Centre of Gravity Limits

A

15% MAC to 40% MAC

72
Q

MTOP (Max Torque)

A

105.6%

73
Q

What is the general time limit for Transient Limits

A

20 seconds, unless otherwise stated

74
Q

After take-off or go-around, what is the minimum height for autopilot engagement?

A

1000ft. AGL

75
Q

Max Continuous (Oil Pressure)

A

55 psi to 65 psi

76
Q

Max Continuous (Np)

A

1212 rpm with 90% Torque; 1125 rpm with 96% Torque

77
Q

Max Continuous (Max Torque)

A

90% for 1200 Np; 96% for 1125 rpm

78
Q

Maximum Landing Weight

A

19,051 kg

79
Q

Vmo (25,000 ft.)

A

214 knots

80
Q

Minimum Oil Temperature for Start

A

-40°C

81
Q

MTOP (Max NH)

A

102.7%

82
Q

Vlo

A

163 knots

83
Q

MTOP (Max ITT)

A

800°C

84
Q

Vmo (20,000 ft.)

A

232 knots

85
Q

NTOP (Max Torque)

A

92% (90% in flight)

86
Q

AFCS Category

A

Category II Approval but not permitted

87
Q

Minimum oil temperature prior to un-feathering propeller

A

0°C

88
Q

Transient (Oil Temperature)

A

125°C

89
Q

Maximum altitude for air start

A

20,000 ft.

90
Q

Max Reverse (Maximum Torque)

A

90%

91
Q

Starting (Max ITT)

A

840°C to 900°C for 12 seconds; 900°C to 950°C for 5 seconds

92
Q

Maximum altitude for extending landing gear or wing flap

A

15,000 ft.

93
Q

Minimum Operating Ambient Temperature

A

-54°C

94
Q

Minimum flight idle NH

A

66%

95
Q

Max Reverse (Max NL)

A

101.7%

96
Q

MTOP (Oil Pressure)

A

55 psi to 65 psi

97
Q

Alternate Gear Extension Speed

A

140 knots

98
Q

Max Reverse (Max NH)

A

101%

99
Q

Maximum load meter reading for flight operation (DC Generator)

A

1.0

100
Q

Maximum total baggage compartment weight

A

1,134 kg

101
Q

Maximum Crosswind Component

A

36 knots

102
Q

Maximum load meter reading for ground operation (DC Generator)

A

0.7 (may be exceeded for up to 1 minute for internal battery starting of engines)

103
Q

Transient (Max NH)

A

103.7%

104
Q

Maximum Take-off Weight

A

19,505 kg

105
Q

Vle

A

173 knots

106
Q

NTOP (Oil Temperature)

A

45°C to 115°C

107
Q

Bleed air position for take-off and landing

A

OFF

108
Q

Va

A

177 knots

109
Q

Maximum load meter reading for flight operation (Inverter)

A

1.0

110
Q

Maximum operating altitude for take-off and landing

A

10,000 ft.

111
Q

Vra

A

190 knots

112
Q

Max Reverse (Oil Temperature)

A

45°C to 115°C

113
Q

Propeller prohibited range for ground operation

A

500 to 780 rpm

Air Nelson/Q300 (10 decks)

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