SAMPLE
5-6
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
5.3.2
Endurance and Range
The table below shows fuel consumption, endurance and range at given
engine speed.
Altitude [ft
ISA]
3000 ft
Fuel quantity
[l]
88
USgal
23,2
Engine
speed [rpm] 4500 4800 5000 5300 5500
Fuel consumption
[l/h]
12
14
15
18
20
[km/h]
120
160
170
180
190
IAS
KIAS 65
86
92
97
103
[km/h]
116 147 155 163 170
CAS
KCAS
63 79 84 88 92
Endurance [hh:mm]
07:18
06:14
05:51
04:48
04:24
[km]
850
924
909 796
748
Range
[NM]
458
499
491
430
403
5.3.3
Effect of rain on flight performance and characteristics
Neither flight performance nor characteristics are substantially affected by
rain or accumulation of insects on the airplane surface..
5.3.4
Demonstrated crosswind performance
Max. permitted cross wind velocity
for take-off and landing .............................. 5 m/s
10 kts
Max. permitted head wind velocity
for take-off and landing ............................ 12 m/s
23 kts
5.3.5
Optimum glide speed
Optimum glide speed ............................ 120 km/h IAS
65 KIAS
5.3.6 Ceiling
Service ceiling ...................................... 3000 m
10.000 ft
