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

I-4-3-App C-28 Procedures — Aircraft Operations — Volume II
23/11/06
Table I-4-3-App C-3. Calculations associated with the construction of
the 80°-260° procedure turn template
DATA
SI UNITS NON-SI UNITS
IAS 405 km/h 220 kt
Altitude 1 850 m 6 000 ft
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 1.1244 Conversion factor for 1.1231
1 850 m and ISA + 15°C
6 000 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 455.38 km/h V = K × IAS 247.08 kt
3 v v= V ÷ 3 600 0.1265 km/s v = V ÷ 3 600 0.0686 NM/s
4 R R = 943.27 ÷ V, or 3°/s,
whichever is less
2.07°/s R = 509.26 ÷ V, or 3°/s,
whichever is less
2.06°/s
5 r r = V ÷ 62.83 R 3.5 km r = V ÷ 62.83 R 1.91 NM
6 h in thousands of metres 1.85 in thousands of feet 6
7 w w = 12h + 87 109.2 km/h w = 2h + 47 59 kt
8 w′ w′ = w÷ 3 600 0.03 km/s w = w ÷ 3 600 0.0164 NM/s
9 E E = w′÷R 0.0145 km/° E = w′ ÷R 0.00796 NM/°
10 ab ab = 5v 0.63 km ab = 5v 0.34 NM
11 de, d1e1, d2e2 de =d1e1 =d2e2 = 10v 1.27 km de =d1e1 =d2e2 = 10v 0.69 NM
12 We2 We2 = 15w′ + 85 E 1.68 km We2 = 15w′ + 85 E 0.92 NM
13 Wg Wg =15w′ + 130 E 2.34 km Wg =15w′ + 130 E 1.28 NM
14 Wh Wh = 15w′ + 175 E 2.99 km Wh = 15w′ + 175 E 1.64 NM
15 Wi Wi = 15w′ + 220 E 3.64 km Wi = 15w′ + 220 E 2.00 NM
16 Wj Wj = 15w′ + 265 E 4.29 km Wj = 15w′ + 265 E 2.36 NM
17 Wk Wk =15w′ + 255 E 4.15 km Wk =15w′ + 255 E 2.28 NM
18 Wl Wl = 15w′ + 300 E 4.80 km Wl = 15w′ + 300 E 2.63 NM
19 Wm Wm =15w′ + 345 E 5.45 km Wm =15w′ + 345 E 2.99 NM