Jabiru j430 - Flap Cross Shaft Assembly

Aircraft Technical Manual
Jabiru Aircraft Pty Ltd
JTM001-5
J120, J160, J170, J200/J400, J230/J430, J250/J450 Variants
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ISSUE
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Dated: 29th October 2014
Issued By: AS
Page: 163 of 298
Figure 113 – J200 Family Electric Flap System Sheet 2 (J200/J400, J230/J430, J250/J450)
6.58 FLAP Cross SHAFT ASSEMBLY (all J-Series)
6.58.1 Description
 As shown above the flaps are driven via a shaft which runs from one side of the fuselage to the
other.
 In turn this shaft is an assembly of 2 different sized steel tubes with input and output arms attached.
6.58.2 Flap Cross Shaft Removal
Required Tools:
Tools as required in Section 0
Parts and Material:
Heavy duty tape
Type of Maintenance:
Line Maintenance
Level of Certification:
L2 or LAME (A&P or LSA Repairman / Maintenance)
Return to Service:
L2 or LAME (A&P or LSA Repairman / Maintenance)
1. Remove one wing to allow removal of shaft. Refer to Section 0 for details on wing removal
procedure.
2. Either use heavy duty tape to hold the remaining flap in the up position or remove the flap
from the aircraft.
3. Disconnect the flap drive motor or manual lever from the cross shaft input arm.
4. Remove external flap drive arm from the end of the shaft nearest the remaining wing.