Tecnam P92-JS - CLIMB PERFORMANCE

FLIGHT MANUAL
Date: Issue 3: 25
th
May 2010
5-9
P92-JS
S E C T I O N 5
PERFORMANCE
CLIMB PERFORMANCE
CLIMB RATE IN CLEAN CONFIGURATION
CONDITIONS:
- Flaps: 0°
- Engine: full throttle
- V
Y
= 70KIAS for 550kg MTOW
- V
Y
= 73KIAS for 600kg MTOW - R/C residual 100 ft/min.
12000
14000
8000
10000
4000
6000
2000
-2000
PRESSURE ALTITUDE (ft)
RATE OF CLIMB (ft/m')
10
TEMPERATURE (deg.C)
-20 -10
0
20
200
30
400
0
1400
1000
600 800
1200
0
2000
4000
ISA
550 kg
500
450
8000
6000
10000
14000
12000
16000
600 kg
 Example:
Given
Find
O.A.T. = 17°C
Rate of climb = 700 ft/min
Pressure altitude = 5600 ft
Weight = 550 Kg