US-2024-20-07
Equipment / Furnishings - Emergency Float Kit Activation Handle - Repetitive Inspections / Replacement
EASA
•
US
•
Effective Date:
2024-12-05
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Applicability
AIRBUS HELICOPTERS/AIRBUS HELICOPTERS DEUTSCHLAND/APICAL INDUSTRIES INC./BELL TEXTRON CANADA LTD (BTCL)/BELL TEXTRON INC. (BTI)/LEONARDO S.p.A. HELICOPTERS/MD HELICOPTERS INC (MDHI)/ROBINSON HELICOPTER COMPANY/SIKORSKY
- AS 350 / EC 130/EC 120 B/BO 105/EC135/635/MBB-BK 117/EASA STC 10016829 /EASA STC 10028171/EASA STC 10069698/FAA STC SR00780LA/FAA STC SR00831LA/FAA STC SR00856LA /FAA STC SR00932LA/FAA STC SR01459LA/FAA STC SR01535LA/FAA STC SR01687LA/FAA STC SR01779LA /FAA STC SR01855LA /FAA STC SR01902LA/FAA STC SR02049LA/FAA STC SR02244LA/FAA STC SR02484LA/STC EASA.IM.R.S.01013/STC EASA.IM.R.S.01107/STC EASA.IM.R.S.01114/STC EASA.IM.R.S.01115/STC EASA.IM.R.S.01135/STC EASA.IM.R.S.01199 /STC EASA.IM.R.S.01202/STC EASA.IM.R.S.01225 /STC EASA.IM.R.S.01226/STC EASA.IM.R.S.01241/STC EASA.IM.R.S.01334/206/407/210/212/412/AB212/AB412/369/500N/R44 (Raven)/R66/S-76
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:
2024-11-29
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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