Tecnam P92-JS - TAKEOFF PERFORMANCE

FLIGHT MANUAL
Date: Issue 3: 25
th
May 2010
5-7
P92-JS
S E C T I O N 5
PERFORMANCE
TAKEOFF PERFORMANCE (Approved data)
TAKEOFF DISTANCE
CONDITIONS:
- Flaps: 15°
MTOW=550kg
MTOW=600kg
- Engine: full throttle (see Sect.4)
- VR =
47 KIAS
48 KIAS
- Runway: dry, compact, grass
- V
obs
=
56 KIAS
58 KIAS
- Slope: 0° Wind: zero
- V
LO
=
49 KIAS
51KIAS
- R/C  200 ft/min
1. Decrease distances by 10% for each 10 Kts of headwind.
Increase distances by 20 % for each 10 Kts of tailwind
2. For dry and paved runway operation decrease ground
run by 6 %
NOTE
 Example:
Given
Find
O.A.T. = 15°C
TOD = 253m
Pressure-altitude = 2900 ft
MTOW = 600kg
Weight = 450 Kg
TOR = 117 m
Fig. 5-4. TAKEOFF PERFORMANCE