AIRCRAFT
SA 160
AIRCRAFTA I R C R A F T
Symphony
Figure 5-12
LANDING DISTANCE (FOR SHORT FIELDS)
CONDITIONS:
WEIGHT975 kg (2150lbs)
FLAPS40°
APPROACHSPEEDAT 50 FT65 KIAS
PAVED, DRY RUNWAY, ZEROWIND
NOTES:
1. THE LANDING PROCEDURE FOR SHORT FIELDS IS DESCRIBED IN SECTION 4.
2. DECREASE DISTANCES BY 10% FOR EVERY 10 KNOTS OF HEADWIND. FOR OPERATION
WITH TAILWINDS UP TO 10 KNOTS, INCREASE DISTANCES BY 10% FOR EVERY 2 KNOTS.
3. INCREASE GROUND ROLL ON DRY GRASS SURFACE BY 35%.
4. FOR EACH DEGREE OF RUNWAY SLOPE INCREASE GROUND ROLL BY 15%.
5. WITH FLAPS UP (V 74 KIAS), INCREASE LANDING DISTANCE BY 45%.
APP
EXAMPLE:
WEIGHT 2150 lbs
AIRTEMPERATURE 33 °C
AIRFIELDPRESSURE ALTITUDE 1000 ft
HEADWINDCOMPONENT 10 kts
READ VALUE AT ISA+20 °C BECAUSE THE STANDARD
TEMPERATURE IN 1000 FT IS 13 °C. 13°+20°=33 °C
TOTAL OVER50FT OBSTACLE 2461 ft
THECORRECTION FORHEADWIND:
10kts /10kts x 10%=10%DECREASE
GROUNDROLL 901 ft
GROUNDROLL 1001 ft
TOTAL OVER50FT OBSTACLE 2215 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
Pressure
Altitude
ft
ISA-10 °C
ISA ISA+10 °C ISA+20 °C
ISA+30 °C
MSL 2182 869 2280 902 2346 935 2395 968 2461 1001
1000 2264 902 2329 935 2395 968 2461 1001 2526 1033
2000 2313 935 2379 968 2444 1001 2510 1033 2575 1066
3000 2379 951 2444 984 2510 1033 2575 1066 2641 1099
4000 2428 984 2493 1017 2575 1066 2641 1099 2707 1132
5000 2493 1017 2559 1050 2641 1083 2707 1132 2789 1165
6000 2543 1050 2625 1083 2707 1132 2772 1165 2854 1198
7000 2608 1083 2690 1115 2772 1165 2854 1198 2936 1247
8000 2674 1115 2756 1148 2838 1198 2936 1247 3018 1280
5-24
SECTION 5
PERFORMANCE
Feb 25, 2005