Figures Flashcards
1
Q
TORA Safety factor (no stopway or clearway)
A
1.25
2
Q
Dry grass (class B surface correction) takeoff
A
1.2
3
Q
Min Vmc at Vr
A
1.05
4
Q
Min use of tailwind reported
A
150%
5
Q
Wet grass (class b surface correction) takeoff
A
1.3
6
Q
TORA safety factor (stopway and / or Clearway)
A
1
7
Q
Max use of headwind reported
A
50%
8
Q
Wet paved (class b surface correction) takeoff
A
1
9
Q
TODA safety factor (stopway and / or clearway)
A
1.15
10
Q
Max slope (greater required authority approval)
A
2%
11
Q
Per 1% upslope class b take off
A
5%
12
Q
ASDA safety factor (stopway and / or Clearway)
A
1.3
13
Q
Min Vs1 at V2
A
1.2
14
Q
Class b screen height
A
50ft
15
Q
Min Vs1 at Vr
A
1.1
16
Q
Min climb gradient (MEP after take off)
A
4%
17
Q
Min gradient at 1500’ (MEP) after takeoff one engine out
A
0.75%
18
Q
Min Vmc at V2
A
1.1
19
Q
IMC less than 15° track change (max domain width)
A
600m
20
Q
Initial semi width
A
60m + 1/2 wingspan
21
Q
Height where gradient must be measurably positive (MEP) one engine out takeoff
A
400ft
22
Q
IMC greater than 15° track change (max domain width)
A
900m
23
Q
Max initial semi width
A
90m
24
Q
Engine failure not assumed below (MEP)
A
300ft
25
VMC >15° track change (max domain width)
600m
26
Vmc <15° track change (max domain width)
300m
27
Half width divergence rate
0.125
28
Climb gradient (MEP en-route engine fail)
0.5%
29
MEP NTOFP all engine climb gradient safety factor
0.77
30
Half width divergence rate
1/8th (0.125)
31
Descent gradient (MEP en-route engine failure)
0.5%
32
SEP min height above safe forced landing site (glide calculation)
1000ft
33
Minimum height before turning (departure sector)
50ft
34
Max planned altitude rate of climb (SEP & MEP)
300fpm
35
MEP en-route min height above destination aerodrome
1000ft
36
Max angle of bank in a turn (departure sector)
15°
37
Class b per 1% downslope landing
5%
38
Class b landing safety factor
1.43
39
Class b landing barrier height
50ft
40
Class b max grass length
20cm
41
Class b min barrier height on authority approval
35ft
42
Class b how much LDA that can be used
70%
43
Class b grass surface correction for landing
1.15
44
Class b wet surface correction for landing
1.15
45
Class b landing safety factor
0.7
46
MEP balked landing min climb gradient all engine
2.5%
47
MEP one engine out min Vs1 climb speed
1.2
48
Class B Vref min
1.3
49
SEP glide gradient en route engine fail
0.5%
50
MEP balked landing power / thrust available after what time
8 seconds
51
MEP balked landing climb speed all engine
Vref
52
Stall speed class b
Vs
53
Stall speed in the landing / approach configuration class b
Vs0
54
Stall speed in the take off configuration Class B
Vs1
55
Min control speed in the landing configuration
Vmcl
56
Min control speed in the given configuration
Vmc(A)
57
Min control speed on or near the ground
Vmcg
58
Speed at which rearward pressure is applied to controls shortly after which the nosewheels lift off the ground
Vr
59
Speed at which the main wheels leave the ground
Vlof
60
Min take off speed at screen height
V2 min
61
Speed at which an engine / major system failure would occur and recognised at the worst time
Vef
62
Max break energy speed to absorb aircraft momentum
Vmbe
63
Min landing speed at screen / barrier height
Vref
64
Threshold speed
Vth
65
Minimum unstick speed
Vmu
66
Max tyre speed
V tyre
67
Stall reference speed in the landing / approach configuration class A
Vsr0
68
Stall reference speed in the take off configuration (class A)
Vsr1
69
Stall reference speed Class A
Vsr
70
Class B min Vs1 at Vr
1.1
71
Class A min Vmc at V2min
1.1
72
Class A min Vmc at Vr
1.05
73
Class a min Vmu at Vlof (aero limit n-1)
1.05
74
Class A min Vmu at Vlof (Geo limit all engine)
1.08
75
Class a Vmu at Vlof (aerolimit all engines)
1.1
76
Class A min Vsr1 at V2min
1.13
77
Class B min Vs1 at V2min
1.2
78
Class A min Vmu at Vlof (geometric limit n-1)
1.04
79
Class A take off screen height dry
35 ft
80
Class A min Vsr0 at Vref
1.23
81
Class A min Vsr1 at V2min (4 engine turboprops)
1.08
82
Factor applied to TOR dry
1.15
83
Factor applied to TOD dry
1.15
84
Class A take off screen height wet
15 ft
85
The greater of TODn-1 wet or TOD dry
TOD wet
86
The greater of TOD n-1 dry or 1.15 TODn dry
TOD dry
87
Factor applied to TORn wet
1.15
88
The greater of TORn-1 dry or 1.15 TORn dry
TOR dry
89
The greater of TORn-1 wet or 1.15 TORn wet
TOR wet
90
Class A NTOFP no turns but be commenced below
50ft
91
Class A NTOFP angle of bank must no exceed 15° below
400ft
92
Class A NTOFP max angle of bank below 400ft
15°
93
Class A NTOFP no turns but be commenced below ... if greater then 50ft
1/2 wingspan
94
Class A NTOFP max angle of bank 200-400ft (authority approval)
20°
95
Class A NTOFP above 15° angle of bank obstacle clearance is
50ft
96
Class A NTOFP max angle of bank above 400ft
25°
97
Class A NTOFP authority approval for max angle of bank increased to 30° height range
400-1500ft
98
Class A NTOFP authority approval for max angle of bank increase to 20° height range
200-400ft
99
Class A NTOFP max angle of bank 400-1500ft (authority approval)
30°
100
Class A NTOFP safety factor for 4 engine (one engine out)
1%
101
Class A NTOFP safety factor for 3 engine (one engine out)
0.9%
102
Class A NTOFP safety factor for twin (one engine out)
0.8%
103
Class A NTOFP min % gradient in the 1st segment (4 engine)
0.5%
104
Class A NTOFP min % gradient in the 1st segment (3 engine)
0.3%
105
Class A NTOFP min % gradient in the 1st segment (twin engine)
0.0%
106
Class A NTOFP min % gradient in the 2nd segment (4 engine)
3%
107
Class A NTOFP min % gradient in the 2nd segment (3 engine)
2.7%
108
Class A NTOFP min % gradient in the 2nd segment (twin engine)
2.4%
109
Min height for end of segment 2
400ft
110
Min height for start of segment 3
400ft
111
Class A NTOFP min % gradient in the 3rd segment (4 engine) used for acceleration only
1.7%
112
Class A NTOFP min % gradient in the 3rd segment (3 engine) used for acceleration only)
1.5%
113
Class A NTOFP min % gradient in the 3rd segment (twin engine) used for acceleration only
1.2%
114
Class A NTOFP min % gradient in the 4th segment (4 engine)
1.7%
115
Class A NTOFP min % gradient in the 4th segment (3 engine)
1.5%
116
Class A NTOFP min % gradient in the 4th segment (twin engine )
1.2%
117
Class A min speed used for determining baulked climb requirement
1.13 Vsr0
118
Class A min baulked climb % gradient
3.2%
119
Class A NTOFP min net % gradient in the 2nd segment (twin engine)
1.6%
120
Class A min speed used for determining discontinued approach climb requirement
1.41
121
Class A max speed used for determining baulked climb requirement
1.23Vsr0
122
Class A min speed used for determining baulked climb requirement
Vmcl
123
Class A min discontinued approach climb % gradient (4 engine)
2.7%
124
Class A min discontinued approach climb % gradient (3 engine)
2.4 %
125
Class A discontinued approach climb % gradient (twin engine)
2.1%
126
Max use of LDA for turbojet
60%
127
Class A min discontinued instrument approach climb % gradient with decision height below 200ft
2.5%
128
Class A mad decision height for discontinued instrument approach climb % gradient
200ft
129
Alternate LDA safety factor turboprop
1.43
130
Alternate LDA safety factor turbojet
1.67
131
Max use of LDA for turboprop
70%
132
Max runway slope without consideration
2%
133
Tailwind factor (landing)
150%
134
Headwind factor (landing)
50%
135
Number of alternate airfield with full landing compliance when only forecast wind comparable
2
136
Number of alternate airfield with full landing compliance when still wind compatible
1
137
Alternate landing screen height with authority
35ft
138
Min depth (mm) to be classed as contaminated
3mm
139
Min runway coverage to be classed as contaminated
25%
140
Dry landing distance factor for contamination
115%
141
Contaminated landing distance factor if published and accepted by authority
115%
