US-2024-14-03
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Applicability
COMMANDER (CPAC, INC.)/DAHER AEROSPACE/GARMIN INTERNATIONAL INC./MOONEY INTERNATIONAL CORPORATION/PIPER AIRCRAFT INC./TEXTRON AVIATION INC.
- 112/114/TB/EASA STC 10069439/FAA STC SA01866WI/M20/PA-24 (Comanche)/PA-28 (Archer)/PA-28 (Cadet)/PA-28 (Cherokee)/PA-28 (Dakota)/PA-28 (Warrior)/PA-28R (Arrow)/PA-30 (Twin Comanche)/PA-32 (Cherokee Six)/PA-32 (Piper 6X)/PA-32 (Saratoga)/PA-32R (Lance)/PA-39 (Twin Comanche)/172 (Skyhawk)/172RG/177 (Cardinal)/177RG (Cardinal RG)/182 (Skylane)/19/206/U206 (Super Skywagon)/206H (Stationair)/210 (Centurion)/23 (Musketeer)/24 (Sierra)/33 (Bonanza)/35 (Bonanza)/36 (Bonanza)/F172/F177RG/F182/FR172 (Reims Rocket)/P172D/P206/TP206 (Super Skylane)/R172 (Hawk XP)
Overview
This AD requires replacement of flap control pushrods on certain Airbus A320 family aircraft due to potential wear that could lead to reduced flap control and loss of control.
Compliance
Status:
Active
Publication Date:
2024-07-22
Maintenance Plan
Initial Replacement
Within 3,000 FH or 24 months
No repetive actions required
Estimated Labor:
4.5 - 6.0 hours
Downtime:
Approximately 1 day
Affected Parts
Part Number:
Description
823100-101
Flap Control Pushrod Assembly
NAS6204-25
Pushrod End Flitting
MS21256-6
Self-Locking Nut
Required Actions
-
Replace left and right flap control pushrods with serviceable parts.
-
Accomplish within 3,000 flight hours or 24 months, whichever occurs first.
-
Record compliance in the aircraft maintenance records.
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