Limitations Flashcards

1
Q

Maneuver Speed

A

204 KIAS

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2
Q

Aquaplaning Speed (Take-off)

A

107 GS

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3
Q

Aquaplaning Speed (Landing)

A

92 GS

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4
Q

Maximum Tire Speed

A

182 GS

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5
Q

Cracked Windshield Speed

A

210 KIAS

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6
Q

Turbulent Penetration Speed

A

210 KIAS

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7
Q

Maximum Holding Speed

A

230 KIAS

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8
Q

Minimum Holding Speed - Icing

A

190 KIAS

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9
Q

Minimum Holding Speed - Non Icing

A

180 KIAS

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10
Q

Maximum Operating Speed: 0- 8 000 ft

A

245 KIAS

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11
Q

Maximum Operating Speed: 10 000 ft

A

282 KIAS

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12
Q

Maximum Operating Speed: 18 000 ft

A

286 KIAS

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13
Q

Maximum Operating Speed: 20 000 ft

A

275 KIAS

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14
Q

Maximum Operating Speed: 25 000 ft

A

248 KIAS

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15
Q

Maximum Flap Speed - Flap 0

A

VMO

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16
Q

Maximum Flap Speed - Flap 5

A

200 KIAS

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17
Q

Maximum Flap Speed - Flap 10

A

181 KIAS

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18
Q

Maximum Flap Speed - Flap 15

A

172 KIAS

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19
Q

Maximum Flap Speed - Flap 35

A

158 KIAS

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20
Q

Minimum Flap Speed - Flap 0 (Non Icing)

A

180 KIAS

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21
Q

Minimum Flap Speed - Flap 5 (Non Icing)

A

160 KIAS

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22
Q

Minimum Flap Speed - Flap 10 (Non Icing)

A

150 KIAS

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23
Q

Minimum Flap Speed - Flap 15 (Non Icing)

A

140 KIAS

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24
Q

Minimum Flap Speed - Flap 35 (Non Icing)

A

135 KIAS

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25
Q

Minimum Flap Speed - Flap 0 (Icing)

A

190 KIAS

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26
Q

Minimum Flap Speed - Flap 5 (Icing)

A

170 KIAS

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27
Q

Minimum Flap Speed - Flap 10 (Icing)

A

160 KIAS

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28
Q

Minimum Flap Speed - Flap 15 (Icing)

A

150 KIAS

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29
Q

Minimum Flap Speed - Flap 35 (Icing)

A

140 KIAS

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30
Q

VLO

A

200 KIAS

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31
Q

VLE

A

215 KIAS

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32
Q

Alternate Gear Extension Speed (all Doors open)

A

185 KIAS

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33
Q

Alternate Gear Extension Speed (Any Door open)

A

185 KIAS

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34
Q

Approved Configuration - Take Off

A

5, 10 or 15

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35
Q

Approved Configuration - Cruise

A

0

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36
Q

Approved Configuration - Approach

A

5, 15 or 35

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37
Q

Approved Configuration - Landing

A

15 or 35

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38
Q

Maximum Bank Angle for V2 (V2 ICE) and VGA (VGA ICE)

A

15°

20° add 5 knots

25° add 10 knots

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39
Q

Maximum Bank Angle for VFTO (VFTO ICE) or VREF (VREF ICE)

A

25°

30° add 5 knots

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40
Q

CAT II

A
  • Minimum RVR = 300m
  • Minimum DH = 100ft
  • A/P Disengage = 80ft
  • DUAL FD by 1100ft RA
  • Flaps 15 only
  • MAX NP only
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41
Q

CAT III HGS

A
  • Minimum RVR = 200m
  • Minimum DH = 50ft
  • Flaps 15 only
  • MAX NP only
  • Runway slope not greater than 1%
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42
Q

Low Visibility Take-Off (LVTO)

A
  • When RVR is below 550m
  • Minimum RVR = 75m
  • Guided Take-Off (RVR below 125m) limited to Flaps 5 only
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43
Q

Practice CAT II Approach

A
  • Ceiling at or above 400ft
  • Visibility at or above 2000m
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44
Q

Visual Approach Requirements

A
  • Circling minima or Visibility of 3000m (where no circling minimas exist)
  • VMC and Runway in Sight
  • ATC clearance received
  • At night, a means to determine the approach slope is required (ILS, PAPI)
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45
Q

Swing Over

A
  • Can only be accepted above 1500ft AGL
  • Both Pilots have positively identified the new runway
  • Go around has been clarified with ATC
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46
Q

VMC

A
  • Horizontal Distance to Cloud 1500m
  • Vertical Distance to Cloud 1000ft

Visibility:

Below 10 000 ft = 5 Km

Above 10 000 ft = 8 km

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47
Q

Commander’s Landing

A

ILS

DH+100ft

Required Minimum + 700m

          Non Precision Approach

DH + 200ft

Required Minimum + 1000m

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48
Q

Maximum Ramp Weight

A

29 089 kg

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49
Q

Maximum Takeoff Mass

A

28 998 kg

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50
Q

Maximum Landing Mass

A

28 009kg (26 308kg for Steep Approach)

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51
Q

Maximum Zero Fuel Mass

A

26 308 kg

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52
Q

Maximum Warderobe Load

A

72 kg

53
Q

Maximum Load Fwd Compartment (Hold 1)

A

413 kg

54
Q

Maximum Load Aft Cargo Compartment (Hold 2)

A

1043 kg

55
Q

Maximum Load Aft Cargo Compartment (Hold 3)

A

454 kg

56
Q

Maximum Load G3 Galley

A

340 kg

57
Q

Maximum Load G4 Galley

A

360 kg

58
Q

Maximum Operating Altitude

A

25 000 ft

59
Q

Maximum Take Off and Landing Altitude

A

10 000 ft

60
Q

Maximum Ambient Temperature Limit (Flight Enevelope)

A

+ 50° or ISA + 35° whichever is lower

61
Q

Minimum Ambient Temperature Limit (Flight Envelope)

A
  • -54° C
62
Q

Load Factor - Flaps Retracted

A

+ 2.5G / - 1G

63
Q

Load Factor - Flaps Extended

A

+ 2G / -0G

64
Q

Maximum Crosswind (Wet and Dry Runway)

A

32 kts

65
Q

Maximum Crosswind - A/P CAT II

A

18 kts

66
Q

Maximum Crosswind - HGS CAT III

A

15 kts

67
Q

Maximum Crosswind - Take Off LCY

A

32 kts

68
Q

Maximum Crosswind - Landing LCY

A

25 kts

69
Q

Maximum Tailwind - Dry and Wet Runway

A

20 kts

70
Q

Maximum Headwind - A/P CAT II or HGD CAT III

A

24 kts

71
Q

Maximum Tailwind - A/P CAT II or HGD CAT III

A

10 kts

72
Q

Maximum Tailwind - LCY

A

5 kts

73
Q

Maximum Oxygen Pressure - 2 Crew

A

1050 psi

74
Q

Maximum Oxygen Pressure - 3 Crew

A

1450 psi

75
Q

Normal Cabin Pressure Differential Limit

A

5.46 psi +/- 0.1 psi

76
Q

Maximum Cabin Pressure Differential Limit

A

5,95 psi

77
Q

Maximum Cabin Pressure Differential Limit during Taxi, Take-Off and Landing

A

0,5 psi

78
Q

Maximum Cabin Altitude (Pressurized Flight)

A

8 000 ft

79
Q

Maximum Cabin Altitude (Unpressurized Flight)

A

10 000 ft

80
Q

Icing Conditions

A
  • SAT on ground and for take off is 10° or below or SAT in flight is 5°or below and visibility moisture in any form is present, like fog, haze with visibility of less than 1 SM or if there is rain or snow present
  • SAT on ground and for take off is 10° or below when operating on ramps, taxiways and runways where surface snow, ice, standing water or slush may be ingested
81
Q

Engine Intake Bypass Door Maximum Temperature

A

ISA + 25° C

82
Q

Maximum Window Heat Temperature

A

Do not select NORM when SAT is greater than 20° C.

83
Q

Autopilot Disengagement - Non Precision Approach

A

200 ft AGL

84
Q

Autopilot Disengagement - CAT I

A

160 ft AGL

85
Q

Autopilot Disengagement - A/P CAT II

A

80 ft ARTE

86
Q

Autopilot Disengagement - HGS CAT III

A

At or above 1 000 ft AGL

87
Q

Autopilot Disengagement - OEI

A

At or above 1 000 ft AGL

88
Q

Maximum Load Meter reading before Take Off

A

0.1

89
Q

Maximum Load Meter reading before Engine Start

A

0.4

90
Q

Minimum Battery Temperature before Take Off

A
  • -20° C
91
Q

Minimum Power Up Voltage

A

23V DC

92
Q

Maximum Time for Essential Services

A

45 Minutes

93
Q

Maximum Altitude for Engine Restart

A

20 000 ft

94
Q

Automatic Take Off Power Up Trim

A

10 %

95
Q

Maximum ITT

A
  • 880° C
  • 920° C (transient) during Engine Start
96
Q

Maximum NP (RPM)

A
  • 1020 RPM
  • 1071 RPM (Maximum continuous)
  • 1173 RPM (transient)
97
Q

Different Torque values

A
  • MTOP = 106%
  • NTOP = 90.3%
  • MCP = 100%
  • MAX Reverse = 35%
  • MAX Transient = 135%
98
Q

MTOP Limitations (in minutes)

A
  • 5 Minutes in normal conditions
  • 10 Minutes in case of an Engine Failure
99
Q

Meaning of Transient (in Time)

A

20 seconds

100
Q

Oil Temperature Limitations for Icing

A

Take Off in Icing Conditions

55°C prior to Take Off and 65°C 3 Minutes after setting Take Off Power

Take Off into Icing Conditions

55°C when entering Icing Conditions and 65°C 3 Minutes after setting Take Off Power

101
Q

Minimum Oil Temperature to Unfeather the Propeller

A

-18°C

102
Q

Engine Starter Cranking Limits

A
  1. 70 seconds ON 2 Minutes OFF
  2. 70 seconds ON 2 Minutes OFF
  3. 70 Seconds ON 30 Minutes OFF
103
Q

Torque Indicator - Green Range

A

0 - 100%

104
Q

Turbine Temperature Indicators (ITT)
- Green Range

A

250 - 880°C

105
Q

Propeller RPM Indicators - Green Range

A

660 - 1020 RPM

106
Q

NH Indicators - Green Range

A

64.2 - 100%

107
Q

NL Indicators - Green Range

A

0 - 100%

108
Q

Oil Temperature Indicators - Green Range

A
  • 0 - 107°C
  • 55°C - 107°C (with Prop Heat ON)
  • 65°C - 107°C (with Prop Heat ON 3 Minutes after Take Off)
109
Q

Oil Pressure Indicators - Green Range

A

61 - 72 psi

110
Q

Fuel Temperature Indicators - Green Range

A

0 - 71°C

111
Q

APU Starter Cranking Limits

A
  1. 60 Seconds ON 2 Minutes OFF
  2. 60 Seconds ON 2 Minutes OFF
  3. 60 Seconds ON 30 Minutes OFF
112
Q

Maximum Total Usable Fuel

A

5318 kg

113
Q

Maximum Fuel in each Wing Tank

A

2 659 kg

114
Q

Maximum Fuel Imbalance

A

272 kg

115
Q

Maximum Parking Brake Pressure for Start Up

A
  • Engine #2 first = 500 psi
  • Engine #1 first = 1 000 psi
116
Q

Maximum Altitude with Landing Gear Extended

A
  • 15 000 ft
  • 20 000 ft (Supplement 94)
117
Q

Airspeed Tolerances

A
  • Between Left & Right Indicator = 2 KIAS
  • Between any Indicator & Stby Indicator = 10 KIAS
118
Q

Altitude Tolerances

A
  • 60 ft below 5 000 ft
  • 170 ft at 25 000 ft
119
Q

Final Reserve Fuel

A

460 kg

120
Q

Standard Taxi Fuel

A

100 kg

121
Q

Contingency Fuel

A

85 kg

122
Q

What is the maximum amount of infants allowed?

A

34

123
Q

What is the most aft CG limit?

A

36% MAC

124
Q

What is the most forward CG limit?

A

13.8 % MAC up to 24 000 kg

17.3% MAC above 24 000 kg

125
Q

Maximum Temperature for MTOP

A

ISA +25°C

126
Q

Maximum Temperature for RDC TOP

A

ISA +35°C

127
Q

Maximum Temperature for Operations with Bleeds ON

A

OAT plus 11°C must not exceed 50°C or ISA +35°C

128
Q

Operation on contaminated runways

A
  • Maximum WED of contamination for take off and landing is 15 mm
  • Maximum depth of contamination is 60 mm
  • Maximum altitude for take off and landing is 6 000 ft MSL
  • Take off with RDC NP is not allowed
  • RDC NP landing not allowed
  • Maximum tailwind 10 kts
  • For Talpa Rwycc 2&3, and for WED greater than 3 mm, selection of power levers aft of DISC not allowed