Figure 36 – Shockwatch Indicator - Jabiru j160 Technical Manual

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Aircraft Technical Manual
JTM001-5
As all possible circumstances cannot be listed here, the following is provided as guidance only. A
critical, trained eye is required and inspections should include, but not be limited to, these items.
-
Overall undercarriage: check for bent or damaged nuts, bolts etc. Check for damaged spats or
spat mounting hardware.
Nose leg – check for bends / cracks. Check rubber has not cracked & rubber shaft is straight.
-
Check nose wheel yoke & nose wheel housing on firewall have not bent.
-
Main undercarriage: check inboard and outboard bolts and clamps for damage and security.
Carefully inspect the leg for cracking or other damage.
Brakes: check for bent discs, loose or damaged hardware. Check security of brake lines – i.e.
-
they are strapped to the undercarriage leg and are not rubbing against any sharp objects such as
screws etc.
-
Fuselage: check structure surrounding undercarriage mount points for damage including de-
lamination, cracking, buckling etc.
-
Propeller tip: check for indications of impact.
-
Wings: check for free-play at attachments as detailed in Section 5.12.
Where a tripped indicator is found during maintenance it must be recorded in the aircraft logbook.
The indicator must be re-set before the aircraft is returned to service.
If the indicator trips repeatedly it is recommended that the operator contact Jabiru Aircraft or our
representative to determine a suitable program of additional preventative maintenance.
Indicator – set,
ready to use.
Indicator – Tripped,
indicating high g-
force peak. Note
visible red dot
This document is controlled while it remains on the Jabiru server. Once this no longer applies the document becomes uncontrolled.
ISSUE
1
2
3
Jabiru Aircraft
J120, J160, J170, J200/J400, J230/J430, J250/J450 Variants
Figure 36 – ShockWatch Indicator (all J-Series)
4
5
Dated: 29th October 2014
Pty Ltd
Re-set tool: use to
re-set indicator after
is has tripped
Issued By: AS
Page: 79 of 298

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