HK 36 TC with Rotax 912 S3
Flight Manual
Performance
Doc. No. 3.01.12-E
Rev. 1
06 Oct 2003
Page 5 - 10
5.3.7 FUEL CONSUMPTION, CRUISING SPEED, ENDURANCE, RANGE
NOTE
The specifications for endurance and range apply to a full
tank and do not include any reserve. The range specifica-
tions apply to flight in still air with a well-maintained and
correctly adjusted powered sailplane.
%
Conditions:
- Pressure altitude . . . . . . . . . . . . . . . . . . . . 1800 m (5900 ft)
Prop.
speed
Manif.
press.
Fuel flow
Cruising speed
Endur-
ance
Range
Fuel tank
capacity
RPM
inHg
lit./
hr
US
gal/
hr
km/h
kts
mph h:mm
km
NM
stat.
miles liters
US
gal
2000
22
16.8
4.4
170
92
106
3:10
4:35
545
775
295
420
335
480
55
79
14.5
20.9
2200
22.7
19.6
5.2
180
97
112
2:45
3:55
495
705
265
380
305
435
55
79
14.5
20.9
2260
23.3
23.2
6.1
190
103
118
2:15
3:15
440
630
235
340
270
390
55
79
14.5
20.9
