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Aircraft Service Manual
Jabiru Aircraft
Pty Ltd
JTM001-1
J120, J160, J170, J200/J400, J230/J430, J250/J450 Variants
REVISION
1
Dated: Nov 2011
Issued By: SW
Page: 31 of 233
4
INSPECTION & SERVICING
4.1
BASIC INSPECTION PROCEDURE
Remove the engine cowlings and i
nspect the engine bay in “dirty” condition.
Clean the engine bay, propeller and aircraft exterior.
Carry out the inspections listed in Table 8.
Test and re-assemble the aircraft. Test fly if required.
4.2
MANDATORY INSPECTIONS & LIFED ITEMS
4.2.1 AIRFRAME
At intervals of 5000 hours the Jabiru (all models) airframe must be subject to an overall condition
inspection by Jabiru Aircraft or an aircraft maintainer authorised by Jabiru Aircraft. As part of this
inspection, wing struts must be disassembled, inspected for damage using appropriate NDT methods
(such as dye-penetrant testing).
Jabiru aircraft do not have an overall airframe life limitation.
4.2.2 UNDERCARRIAGE
Main undercarriage bolts and nose leg pivot bolts shown in Figure 8 are to be changed every 500
hours TIS.
Figure 8
– Undercarriage
7 Bolts & nuts in total to be replaced.