SA 160
AIRCRAFTA I R C R A F T
Symphony
AIRCRAFT
5-17
SECTION 5
PERFORMANCE
Feb 25, 2005
EXAMPLE:
WEIGHT 2150lbs
AIRTEMPERATURE 21°C
AIRFIELDPRESSURE ALTITUDE 2000 ft
HEADWIND COMPONENT 13.5 kts
READ VALUE AT ISA+10 °C BECAUSE THE
STANDARD TEMPERATURE IN 2000 FT IS 11°C.
11°+10°=21 °C
Figure 5-6
TAKEOFF DISTANCE (FOR SHORT FIELDS)
CONDITIONS:
FLAPS20°
TAKEOFF POWER SETBEFOREBRAKERELEASE.
PAVED,DRYRUNWAY,ZEROWIND.
NOTES:
1. THE TAKEOFF PROCEDURE FOR SHORT RUNWAYS IS DESCRIBED IN SECTION 4.
2. DECREASE DISTANCES BY 10% FOR EVERY 9 KNOTS OF HEADWIND. FOR OPERATION
WITH TAILWINDS UP TO 10 KNOTS, INCREASE DISTANCES BY 10% FOR EVERY 2 KNOTS OF
TAILWIND.
3. FOR OPERATION ON DRY, GRASS RUNWAY, INCREASE DISTANCES BY 10% OF THE GROUND
ROLL FIGURE.
LIFT-OFF58 KIAS
SPEEDAT 50 ft 62KIAS
WEIGHT975 kg (2150 lbs)
GROUNDROLL 1394 ft
OVER A50FT OBSTACLE 1755 ft
THE CORRECTION FOR HEADWIND:
13.5 kts / 9 kts X 10% = 15% DECREASE
GROUNDROLL 1185 ft
OVER A50FT OBSTACLE 1492 ft
TOTAL
TO
CLEAR
50 FT
OBS
ft
TOTAL
TO
CLEAR
50 FT
OBS
ft
TOTAL
TO
CLEAR
50 FT
OBS
ft
TOTAL
TO
CLEAR
50 FT
OBS
ft
TOTAL
TO
CLEAR
50 FT
OBS
ft
GROUND
ROLL
ft
GROUND
ROLL
ft
GROUND
ROLL
ft
GROUND
ROLL
ft
GROUND
ROLL
ft
PRESS
ALT
ft
ISA-10 °C ISA ISA+10 °C ISA+20 °C
ISA+30 °C
MSL 1050 1378 1148 1476 1230 1591 1329 1690 1411 1788
1000 1115 1444 1214 1558 1312 1657 1394 1772 1493 1886
2000 1198 1542 1296 1640 1394 1755 1493 1870 1575 1985
3000 1312 1673 1427 1804 1526 1919 1624 2034 1722 2149
4000 1460 1837 1558 1952 1673 2083 1772 2198 1870 2329
5000 1575 1985 1690 2116 1804 2231 1903 2362 2001 2477
6000 1706 2133 1821 2264 1936 2395 2051 2526 2149 2657
7000 1854 2297 1969 2444 2083 2575 2182 2690 2297 2822
8000 2001 2477 2116 2608 2231 2740 2329 2871 2444 3002