HORIZONTAL TAIL / HORIZONTAL TAIL GENERAL MAINTENANCE 12-11
CHANGE C1 ICON A5 / MAINTENANCE MANUAL
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Level of Certification
LSA-RM
Task Specific Training Required
No
Special Tools Required
None
Parts Required
None
Aircraft System and Number
09—Horizontal Tail
Consumables
None
The elevator pushrod can be removed separately from the horizontal tail and the air rudder.
1. Remove the aft ME000640 surface plug at the top right side of the VT tip.
2. Remove the MS21043-3 nut, AN3C11A bolt and NAS1149C0332R washers that attach the aft end
of the pitch pushrod to the elevator horn.
3. Working through the aft small circular hole in the top right side of VT tip, remove the AN3C7A
bolt and NAS1149C0332R washer that connects the forward end of the pitch pushrod to the
pitch bellcrank. The bolt is threaded into a nutplate.
4. Slide the final pitch pushrod aft through the hole at the aft end of the VT-HT joint fairing, and
remove it from the aircraft.
VERIFICATION METHOD:
Once the elevator pushrod is completely detached from the aircraft, this task is complete.
RELATED INFORMATION:
"Horizontal Tail Removal" on page 12-11
12.3.1.4 Horizontal Tail Removal
Instructions for removing the Horizontal Tail.
TASK INFORMATION:
Type of Maintenance
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