Figures Flashcards

1
Q

TORA Safety factor (no stopway or clearway)

A

1.25

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2
Q

Dry grass (class B surface correction) takeoff

A

1.2

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3
Q

Min Vmc at Vr

A

1.05

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4
Q

Min use of tailwind reported

A

150%

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5
Q

Wet grass (class b surface correction) takeoff

A

1.3

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6
Q

TORA safety factor (stopway and / or Clearway)

A

1

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7
Q

Max use of headwind reported

A

50%

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8
Q

Wet paved (class b surface correction) takeoff

A

1

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9
Q

TODA safety factor (stopway and / or clearway)

A

1.15

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10
Q

Max slope (greater required authority approval)

A

2%

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11
Q

Per 1% upslope class b take off

A

5%

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12
Q

ASDA safety factor (stopway and / or Clearway)

A

1.3

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13
Q

Min Vs1 at V2

A

1.2

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14
Q

Class b screen height

A

50ft

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15
Q

Min Vs1 at Vr

A

1.1

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16
Q

Min climb gradient (MEP after take off)

A

4%

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17
Q

Min gradient at 1500’ (MEP) after takeoff one engine out

A

0.75%

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18
Q

Min Vmc at V2

A

1.1

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19
Q

IMC less than 15° track change (max domain width)

A

600m

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20
Q

Initial semi width

A

60m + 1/2 wingspan

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21
Q

Height where gradient must be measurably positive (MEP) one engine out takeoff

A

400ft

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22
Q

IMC greater than 15° track change (max domain width)

A

900m

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23
Q

Max initial semi width

A

90m

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24
Q

Engine failure not assumed below (MEP)

A

300ft

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25
Q

VMC >15° track change (max domain width)

A

600m

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26
Q

Vmc <15° track change (max domain width)

A

300m

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27
Q

Half width divergence rate

A

0.125

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28
Q

Climb gradient (MEP en-route engine fail)

A

0.5%

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29
Q

MEP NTOFP all engine climb gradient safety factor

A

0.77

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30
Q

Half width divergence rate

A

1/8th (0.125)

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31
Q

Descent gradient (MEP en-route engine failure)

A

0.5%

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32
Q

SEP min height above safe forced landing site (glide calculation)

A

1000ft

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33
Q

Minimum height before turning (departure sector)

A

50ft

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34
Q

Max planned altitude rate of climb (SEP & MEP)

A

300fpm

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35
Q

MEP en-route min height above destination aerodrome

A

1000ft

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36
Q

Max angle of bank in a turn (departure sector)

A

15°

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37
Q

Class b per 1% downslope landing

A

5%

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38
Q

Class b landing safety factor

A

1.43

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39
Q

Class b landing barrier height

A

50ft

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40
Q

Class b max grass length

A

20cm

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41
Q

Class b min barrier height on authority approval

A

35ft

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42
Q

Class b how much LDA that can be used

A

70%

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43
Q

Class b grass surface correction for landing

A

1.15

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44
Q

Class b wet surface correction for landing

A

1.15

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45
Q

Class b landing safety factor

A

0.7

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46
Q

MEP balked landing min climb gradient all engine

A

2.5%

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47
Q

MEP one engine out min Vs1 climb speed

A

1.2

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48
Q

Class B Vref min

A

1.3

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49
Q

SEP glide gradient en route engine fail

A

0.5%

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50
Q

MEP balked landing power / thrust available after what time

A

8 seconds

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51
Q

MEP balked landing climb speed all engine

A

Vref

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52
Q

Stall speed class b

A

Vs

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53
Q

Stall speed in the landing / approach configuration class b

A

Vs0

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54
Q

Stall speed in the take off configuration Class B

A

Vs1

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55
Q

Min control speed in the landing configuration

A

Vmcl

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56
Q

Min control speed in the given configuration

A

Vmc(A)

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57
Q

Min control speed on or near the ground

A

Vmcg

58
Q

Speed at which rearward pressure is applied to controls shortly after which the nosewheels lift off the ground

A

Vr

59
Q

Speed at which the main wheels leave the ground

A

Vlof

60
Q

Min take off speed at screen height

A

V2 min

61
Q

Speed at which an engine / major system failure would occur and recognised at the worst time

A

Vef

62
Q

Max break energy speed to absorb aircraft momentum

A

Vmbe

63
Q

Min landing speed at screen / barrier height

A

Vref

64
Q

Threshold speed

A

Vth

65
Q

Minimum unstick speed

A

Vmu

66
Q

Max tyre speed

A

V tyre

67
Q

Stall reference speed in the landing / approach configuration class A

A

Vsr0

68
Q

Stall reference speed in the take off configuration (class A)

A

Vsr1

69
Q

Stall reference speed Class A

A

Vsr

70
Q

Class B min Vs1 at Vr

A

1.1

71
Q

Class A min Vmc at V2min

A

1.1

72
Q

Class A min Vmc at Vr

A

1.05

73
Q

Class a min Vmu at Vlof (aero limit n-1)

A

1.05

74
Q

Class A min Vmu at Vlof (Geo limit all engine)

A

1.08

75
Q

Class a Vmu at Vlof (aerolimit all engines)

A

1.1

76
Q

Class A min Vsr1 at V2min

A

1.13

77
Q

Class B min Vs1 at V2min

A

1.2

78
Q

Class A min Vmu at Vlof (geometric limit n-1)

A

1.04

79
Q

Class A take off screen height dry

A

35 ft

80
Q

Class A min Vsr0 at Vref

A

1.23

81
Q

Class A min Vsr1 at V2min (4 engine turboprops)

A

1.08

82
Q

Factor applied to TOR dry

A

1.15

83
Q

Factor applied to TOD dry

A

1.15

84
Q

Class A take off screen height wet

A

15 ft

85
Q

The greater of TODn-1 wet or TOD dry

A

TOD wet

86
Q

The greater of TOD n-1 dry or 1.15 TODn dry

A

TOD dry

87
Q

Factor applied to TORn wet

A

1.15

88
Q

The greater of TORn-1 dry or 1.15 TORn dry

A

TOR dry

89
Q

The greater of TORn-1 wet or 1.15 TORn wet

A

TOR wet

90
Q

Class A NTOFP no turns but be commenced below

A

50ft

91
Q

Class A NTOFP angle of bank must no exceed 15° below

A

400ft

92
Q

Class A NTOFP max angle of bank below 400ft

A

15°

93
Q

Class A NTOFP no turns but be commenced below … if greater then 50ft

A

1/2 wingspan

94
Q

Class A NTOFP max angle of bank 200-400ft (authority approval)

A

20°

95
Q

Class A NTOFP above 15° angle of bank obstacle clearance is

A

50ft

96
Q

Class A NTOFP max angle of bank above 400ft

A

25°

97
Q

Class A NTOFP authority approval for max angle of bank increased to 30° height range

A

400-1500ft

98
Q

Class A NTOFP authority approval for max angle of bank increase to 20° height range

A

200-400ft

99
Q

Class A NTOFP max angle of bank 400-1500ft (authority approval)

A

30°

100
Q

Class A NTOFP safety factor for 4 engine (one engine out)

A

1%

101
Q

Class A NTOFP safety factor for 3 engine (one engine out)

A

0.9%

102
Q

Class A NTOFP safety factor for twin (one engine out)

A

0.8%

103
Q

Class A NTOFP min % gradient in the 1st segment (4 engine)

A

0.5%

104
Q

Class A NTOFP min % gradient in the 1st segment (3 engine)

A

0.3%

105
Q

Class A NTOFP min % gradient in the 1st segment (twin engine)

A

0.0%

106
Q

Class A NTOFP min % gradient in the 2nd segment (4 engine)

A

3%

107
Q

Class A NTOFP min % gradient in the 2nd segment (3 engine)

A

2.7%

108
Q

Class A NTOFP min % gradient in the 2nd segment (twin engine)

A

2.4%

109
Q

Min height for end of segment 2

A

400ft

110
Q

Min height for start of segment 3

A

400ft

111
Q

Class A NTOFP min % gradient in the 3rd segment (4 engine) used for acceleration only

A

1.7%

112
Q

Class A NTOFP min % gradient in the 3rd segment (3 engine) used for acceleration only)

A

1.5%

113
Q

Class A NTOFP min % gradient in the 3rd segment (twin engine) used for acceleration only

A

1.2%

114
Q

Class A NTOFP min % gradient in the 4th segment (4 engine)

A

1.7%

115
Q

Class A NTOFP min % gradient in the 4th segment (3 engine)

A

1.5%

116
Q

Class A NTOFP min % gradient in the 4th segment (twin engine )

A

1.2%

117
Q

Class A min speed used for determining baulked climb requirement

A

1.13 Vsr0

118
Q

Class A min baulked climb % gradient

A

3.2%

119
Q

Class A NTOFP min net % gradient in the 2nd segment (twin engine)

A

1.6%

120
Q

Class A min speed used for determining discontinued approach climb requirement

A

1.41

121
Q

Class A max speed used for determining baulked climb requirement

A

1.23Vsr0

122
Q

Class A min speed used for determining baulked climb requirement

A

Vmcl

123
Q

Class A min discontinued approach climb % gradient (4 engine)

A

2.7%

124
Q

Class A min discontinued approach climb % gradient (3 engine)

A

2.4 %

125
Q

Class A discontinued approach climb % gradient (twin engine)

A

2.1%

126
Q

Max use of LDA for turbojet

A

60%

127
Q

Class A min discontinued instrument approach climb % gradient with decision height below 200ft

A

2.5%

128
Q

Class A mad decision height for discontinued instrument approach climb % gradient

A

200ft

129
Q

Alternate LDA safety factor turboprop

A

1.43

130
Q

Alternate LDA safety factor turbojet

A

1.67

131
Q

Max use of LDA for turboprop

A

70%

132
Q

Max runway slope without consideration

A

2%

133
Q

Tailwind factor (landing)

A

150%

134
Q

Headwind factor (landing)

A

50%

135
Q

Number of alternate airfield with full landing compliance when only forecast wind comparable

A

2

136
Q

Number of alternate airfield with full landing compliance when still wind compatible

A

1

137
Q

Alternate landing screen height with authority

A

35ft

138
Q

Min depth (mm) to be classed as contaminated

A

3mm

139
Q

Min runway coverage to be classed as contaminated

A

25%

140
Q

Dry landing distance factor for contamination

A

115%

141
Q

Contaminated landing distance factor if published and accepted by authority

A

115%