![background image](http://html1.mh-extra.com/html/jabiru/j170-c/j170-c_pilot-operating-handbook_3124307016.webp)
Jabiru Aircraft
Pilot Operating Handbook
Model J170-C
JP-FM-08
Revision:
0
3 April 2007
Page 16
2
AIRPLANE AND SYSTEMS DESCRIPTIONS
2.1 ENGINE
Manufacturer:
Jabiru Aircraft Pty Ltd
Model:
2200B
2.2 PROPELLER
Manufacturer:
Jabiru Aircraft Pty Ltd
Model:
C000262-D60P42
Type:
Wooden, Fixed Pitch
Number of blades:
2
Diameter:
1524 mm (60 in)
Pitch
1067 mm (42 in)
Max RPM:
3300
2.3 FUEL
Capacity:
135L Total Useable (2 OFF 67.5L Wing Tanks)
Grade:
Avgas 100LL
Avgas 100/130
MOGAS with minimum Octane Rating of 95 RON may be used.
Refer to Section 3 for additional details.
2.4 ENGINE OIL
Jabiru Aircraft approves lubricating oils of any brand name conforming to specifications MIL-L-
6082 for straight mineral oil and MIL-L-22851 for ashless dispersant oil.
Refer to Section 3 for additional details.
2.5 OPERATING WEIGHTS AND LOADING
Max Take-Off & Landing Weight:
600 kg (1323 lb)
Maximum Baggage
18kg behind each seat – 36kg total
Forward Limit:
180-mm (7.09”, 18.2%MAC) aft of datum up to & including
440 kg (970lb)
255-mm (10.0”, 25.8%MAC) aft of datum at 600kg
(1323lb)
Linear variation between points.
Aft Limit
287-mm (11.3”, 29.0%) aft of datum at all weights
Datum
Wing Leading Edge
Levelling Means
Longitudinal
Spirit Level placed on the lower section of the door frames