AD 2003-24-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Eurocopter | France Model AS332C, L, L1, and L2 | Airworthiness Directives; Eurocopter France Model AS332C, L, L1, and L2 Helicopters |
Unsafe Condition
Cracks detected in the pilot or co-pilot anti-torque pedal adjustment lever (P/N 332A27.2344.20) that have not been modified in accordance with MOD 0726179, which could lead to failure of the lever, loss of braking ability on the ground, or loss of yaw control in flight, and subsequent loss of control of the helicopter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the pedal unit adjustment lever for cracks using a dye-penetrant inspection at specified intervals. Replace any cracked lever with an airworthy lever before further flight. Modify the pedal unit and replace the adjustment levers in accordance with Eurocopter Alert Service Bulletin No. 67.00.20, dated June 8, 2001, as a terminating action for the AD requirements.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 hours time-in-service (TIS) for helicopters with 4,450 or more hours TIS, and for helicopters with less than 4,450 hours TIS, on or before accumulating 4,500 hours TIS. Pedal unit modification must be completed before March 1, 2004.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Eurocopter France Model AS332C, L, L1, and L2 helicopters with a pilot or co-pilot anti-torque pedal adjustment lever (P/N 332A27.2344.20) that has not been modified in accordance with MOD 0726179.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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