Jabiru Aircraft
Pilot Operating Handbook
Model J230-D
JP-FM-09
Revision:
0
12 April 2007
Page 16
2
AIRPLANE AND SYSTEMS DESCRIPTIONS
2.1 ENGINE
Manufacturer:
Jabiru Aircraft Pty Ltd
Model:
3300A
2.2 PROPELLER
Manufacturer:
Jabiru Aircraft Pty Ltd
Model:
C000262-D60P53
Type:
Wooden, Fixed Pitch
Number of blades:
2
Diameter:
1524 mm (60 in)
Pitch
1346 mm (53 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
Forward Limit:
99-mm (3.9”, 10%MAC) aft of datum up to & including 600
kg (1320lb)
Aft Limit
277-mm (10.9”, 28 %) aft of datum at all weights
Datum
Wing Leading Edge
Levelling Means
Longitudinal
Spirit Level placed on the lower section of the door frames
(left or right side).
Lateral
Spirit Level placed on the flap drive cross tube (inside the
fuselage, in the roof of the cabin behind the seats)
Arms
Arm for Front Seat Station
12-mm forward of datum