AD 2009-24-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna | Aircraft Company Model 525A | Airworthiness Directives; Cessna Aircraft Company Model 525A Airplanes |
Unsafe Condition
Fatigue cracks found in thrust attenuator paddles, which could result in in-flight departure of the thrust attenuator paddles. This failure could lead to rudder and elevator damage and result in loss of control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect the left and right thrust attenuator paddle assemblies to determine if there are any missing, loose, or damaged fasteners and to determine if there are any cracks in the paddle. Replace loose or damaged fasteners and replace cracked thrust attenuator paddles found during any inspection.
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Compliance Time
Within the next 60 days after December 15, 2009, or within the next 30 hours time-in-service after December 15, 2009, whichever occurs first. Repetitively inspect thereafter at intervals not to exceed 150 hours time-in-service.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Aircraft Company Model 525A airplanes, serial numbers 0001 through 0244, that are 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 6, 2026
Rights: U.S. Government Public Domain
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