Jabiru Aircraft
Pilot’s Operating Handbook
Model J120-C
JP-FM-10
Revision:
0
28 Nov 2007
Page 16 of 50
2
SECTION 2 – AIRPLANE & SYSTEMS DESCRIPTION
2.1
Engine
Manufacturer:
Jabiru Aircraft Pty Ltd
Model:
Jabiru 2200-B
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:
64L Useable
Grade:
Avgas 100LL
Avgas 100/130
MOGAS with minimum Octane Rating of 95 RON
1
may be used.
Do not use fuel additives such as Octane Boosters.
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
Error! Reference source not found.
for additional details.
2.5
CENTRE OF GRAVITY LIMITS
Forward Limit:
1601-mm (63.03”, 20%MAC) aft of datum up to & including
420 kg (926lb)
1661-mm (63.39”, 26.1%MAC) aft of datum at 500kg
(1190lb)
Linear variation between points.
Aft Limit
1695-mm (66.73”, 29.5%) aft of datum at all weights
Datum
1403mm fwd of RHS Wing Leading Edge
Levelling Means