Aircraft Operations. Volume II - Construction of Visual and Instrument ...

Part I — Section 4, Chapter 3, Appendix C I-4-3-App C-29
Table I-4-3-App C-4. Calculations associated with the construction of
the holding and racetrack template
DATA
SI UNITS NON-SI UNITS
IAS 405 km/h 220 kt
Altitude 3 050 m 10 000 ft
T 1 min 1 min
Temperature ISA + 15°C ISA + 15°C
CALCULATIONS USING SI UNITS CALCULATIONS USING NON-SI UNITS
Line Parameter Formula Value Formula Value
1 K Conversion factor for 1.1960 Conversion factor for 1.1958
3 050 m and ISA + 15°C
10 000 ft and ISA + 15°C
(see Part I, Section 2,
(see Part I, Section 2,
Chapter 1, Appendix)
Chapter 1, Appendix)
2 V V = K × IAS* 484.38 km/h V = K × IAS* 263.08 kt
* The true airspeed may also be deduced from
Part II, Section 1, Chapter 1, Appendix A.
* The true airspeed may also be deduced from
Part II, Section 1, Chapter 1, Appendix A.
3 v v= V ÷ 3 600 0.1346 km/s v = V ÷ 3 600 0.07308 NM/s
4 R R = 943.27 ÷ V, or 3°/s,
whichever is less
1.95°/s R = 509.26 ÷ V, or 3°/s,
whichever is less
1.94°/s
5 r r = V ÷ 62.83 R 3.96 km r = V ÷ 62.83 R 2.16 NM
6 h in thousands of metres 3.05 in thousands of feet 10
7 w w = 12h + 87 123.6 km/h w = 2h + 47 67 kt
8 w′ w′ = w÷ 3 600 0.03433 km/s w′ =w÷ 3 600 0.0186 NM/s
9 E45 E45 = 45w′ ÷R 0.792 km E45 = 45w′ ÷R 0.431 NM
10 t t = 60T 60 s t = 60T 60 s
11 L L=vt 8.08km L=vt 4.38NM
12 ab ab = 5v 0.67 km ab = 5v 0.37 NM
13 ac ac = 11v 1.48 km ac = 11v 0.80 NM
14 gi1 =gi3 gi1 =gi3 =(t–5)v 7.40km gi1 =gi3 =(t–5)v 4.02NM
15 gi2 =gi4 gi2 =gi4 = (t + 21)v 10.90 km gi2 =gi4 = (t + 21)v 5.92 NM
16 Wb Wb =5w′ 0.17 km Wb= 5w′ 0.09 ΝΜ
17 Wc Wc = 11w′ 0.38 km Wc =11w′ 0.20 ΝΜ
18 Wd Wd =Wc +E45 1.17 km Wd =Wc +E45 0.64 NM
19 We We =Wc +2E45 1.96 km We =Wc +2E45 1.07 NM
20 Wf Wf =Wc +3E45 2.75 km Wf =Wc +3E45 1.50 NM
21 Wg Wg =Wc +4E45 3.55 km Wg =Wc +4E45 1.93 NM
23/11/06