AD 2010-12-01
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 could result in in-flight departure of the thrust attenuator paddles, leading to rudder and elevator damage and 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 for loose and damaged fasteners and cracks. Replace loose or damaged fasteners and cracked thrust attenuator paddles found during inspection. Retain the requirements of AD 2009-24-13 until replacement of both thrust attenuator paddles and eight countersunk fasteners with new design thrust attenuator paddles and universal head rivets.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 60 flight hours
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Affected Aircraft
Cessna Aircraft Company Model 525A airplanes, serial numbers 0001 through 0244, 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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