Pipistrel 1001 AT 912 LSA, Pilot Operating Handbook

Page: 116 / 182

5-8
PAGE
ALPHA Trainer LSA
Pilot Operating Handbook
POH-162-00-40-001
PAGE REV. 0
SECTION 5
PERFORMANCE DATA
5.6. TAKE-OFF
5.6.1. TAKE-OFF PERFORMANCE
Conditions Weight: MTOM ( 1212 lbs / 550 kg)
Power: throttle full open
Flaps: (+1)
Runway: dry, paved and level
Wind: calm
Conditions
DISTANCE
[ft] / [m]
SL
15° C/ISA
Ground roll (MTOM)
555 / 170
50 ft / 15 m obstacle
870 / 265
NOTE: In order to meet the data for takeoff runway lenght over 50 ft / 15m
obstacle maintain Vx (58 KIAS) after takeoff.
CAUTION: Soft (grass) runways increase the published takeoff performance
data by 20%.
Takeoff performance may vary depending on the wind, temperature, elevation
and wing/propeller surface condition.
CAUTION: Calculating take-off performance in hot atmosphere, it is
mandatory to consider the takeoff runway length prolongs as follows:
L = 1,10 • (Lh + Lt - L0).
Abbreviations are as follows:
Lh = takeoff runway length at present elevation, ISA standard conditions.
Lt = takeoff runway length at sea level at same temperature/wind as on the
given location.
L0 = zero wind takeoff runway length at 15°C at sea level.
e.g. if outside temperature is 25°C and you are on 500 m elevation, your
takeoff runway length will be: L = 1,10 • (Lh + Lt - L0) = 1,10 • (205 m + 215 m -
180 m) = 264 meters.