Jabiru Aircraft
SECTION 2
CASA APPROVED
Model J160-C
LIMITATIONS
JP-FM-06
Revision:
0
1
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1 Dec 2008
Page 2-7
2.9
CENTRE OF GRAVITY LIMITS
Forward Limit:
180-mm (7.09”, 18.2%MAC) aft of datum up to & including
440 kg (970lb)
233-mm (9.17”, 23.5%MAC) aft of datum at 540kg
(1190lb)
Linear variation between points.
Aft Limit
292-mm (11.50”, 29.5%) 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 across the fuselage between the left
and right side lower door frames.
Arms
Arm for Front Seat Station
297-mm aft of datum
Arm for Baggage On Shelf
920-mm aft of datum
Fuel Station
451-mm aft of datum
Table 2.7
Summary of Contents for J160-C
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