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Jabiru Aircraft
Pty Ltd
CASA APPROVED SECTION
Airworthiness Limitations
Jabiru J160-C
REVISION
0
Dated 6th April 2012
Issued By: RAS
Page: 233 of 233
C:\Aero_Craft_Australia\Jabiru\Jabiru_Documents_Edited\Generic_Tech_Mannual\Generic_Tech_Rev1_Unsigned.docx
Print Date: 8/05/2012 1:11:00 PM
23.4 CONTROL SURFACE BALANCING
The J160-C primary control surfaces are balanced during construction. In service there should
be no reason to rebalance the controls. Balance checks of the controls are only required after
repair or refinishing or at the 5000-hourly major airframe inspection.
Table 25
– Control Surface Balancing Limits
Control
Hinge Moment Limits
Weight Limits
Manual Section
Rudder
17500g.mm
+/- 4000g.mm
2100g
+/- 100g
Aileron
94000g.mm
+/- 4000g.mm
1150g
+/- 100g
Elevator
259000g.mm
+/- 4000g.mm
4600g
+/- 100g
23.4.1.1 CABLES
Cables must be inspected as detailed in Section 4.16.
Table 26
– Mandatory Inspection Times
Description
Part No.
Interval (Hours)
Rudder Cable
PC01404
1000
Elevator Cable
PC3A001
1000
Aileron Cable (2)
PC01614
1000
23.4.2 MANDATORY REPLACEMENT
The following components MUST be replaced at the intervals described hereunder.
Table 27
– Mandatory Replacement Times
Description
Part No.
Interval (Hours)
Rudder Cable
PC01404
10 000
Elevator Cable
PC3A001
10 000
Aileron Cable (2)
PC01614
10 000