Beech Bonanza A36
Section V
Raytheon Aircraft
I EXAMPLE CALCULATIONS
Examples have been presented on all performance graphs. In
addition, the calculations for flight time, block speed and fuel
required for a proposed flight are listed below. All examples and
I calculations utilize the following conditions:
CONDITIONS
I At Departure:
Outside Air Temperature ................... 15°C (59°F)
I Field Elevation ............................... 5333 ft
Altimeter Setting . . . . . . . . . . . . . . . . . . . . . . . . 29.60 in. Hg
Runway 26L Length ......................... 10,004 ft
I At Destination:
Outside Air Temperature ................... 25°C (77°F)
I Field Elevation ............................... 3605 ft
Altimeter Setting . . . . . . . . . . . . . . . . . . . . . . . . 29.56 in. Hg
Wind. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 190° at 12 kts
I Runway 22 Length. . . . . . . . . . . . . . . . . . . . . . . . . . 13,502 ft
I
I
I
I
I
I
ROUTE
SEGMENT
LEGA
LEG B
LEG C
LEG D
LEGE
5-6
AVERAGE AVERAGE
MAGNETIC MAGNETIC
COURSE VARIATION
155° 12°E
153°
12°E
135° 12°E
132°
11°E
126°
10°E
WIND AT OAT
DIST 11,500 11,500
NM FEET FEET°C
DIR/KTS
51 010°130 -5
40 010°130 -5
74
100°120 0
87
200°120 9
70 200°120 10
November, 2002