AD 2005-05-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Eagle | Various | Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagle 150B Airplanes |
Unsafe Condition
Binding of the co-pilot rudder pedal assembly due to premature wear of the bushing, which could result in loss of co-pilot rudder and brake control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the co-pilot rudder pedal assembly welded design, part number (P/N) 2720D07-02, for cracks. If cracks are found, replace the assembly with a new bolted design co-pilot rudder pedal assembly, P/N 2720D07-10. If no cracks are found, modify the rudder pedal assembly following Eagle Aircraft Optional Service Bulletin SB 1096, dated September 16.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Inspect within 30 days after April 22, 2005 (the effective date of this AD).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Model Eagle 150B airplanes, manufacturer serial numbers (MSN) 016 through 042, equipped with a co-pilot rudder pedal assembly welded design, part number (P/N) 2720D07-02, and certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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