# Proposed AD FAA-2010-0327: Cessna Aircraft Company Model 525A Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2010-12-01
- Products: Cessna
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: March 30, 2010, 75 FR 15629
- Comments due: May 14, 2010
- Became: [AD 2010-12-01](https://openairdocs.org/ad/2010-12-01)
- Docket: FAA-2010-0327 (https://www.regulations.gov/docket/FAA-2010-0327, where comments are filed)
- Project: 2010-CE-012-AD
- FR document: 2010-7024
- Official PDF: https://openairdocs.org/files/sha256/a1/12/a112869bf7673523af6583816e4f87093620b7ea6358bbb8817d321fd3f512e7 (from https://www.govinfo.gov/content/pkg/FR-2010-03-30/pdf/2010-7024.pdf)
- Federal Register: https://www.federalregister.gov/documents/2010/03/30/2010-7024/airworthiness-directives-cessna-aircraft-company-model-525a-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/777F9C0CDF77E8B8862576F6005217B6.0001
- Page: https://openairdocs.org/proposed/FAA-2010-0327

## Summary

We propose to supersede Airworthiness Directive (AD) 2009-24- 13, which applies to certain Cessna Aircraft Company (Cessna) Model 525A airplanes. AD 2009-24-13 currently requires you to repetitively inspect the thrust attenuator paddle assemblies for loose and damaged fasteners and for cracks. AD 2009-24-13 also requires you to replace loose or damaged fasteners and replace cracked thrust attenuator paddles found during any inspection. Since we issued AD 2009-24-13, Cessna has developed new design thrust attenuator paddles and universal head rivets as terminating action for the repetitive inspections. Consequently, this proposed AD would retain the requirements of AD 2009-24-13 until replacement of both thrust attenuator paddles and the eight countersunk fasteners with new design thrust attenuator paddles and universal head rivets. We are proposing this AD to detect and correct loose and damaged fasteners and cracks in the 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.

## Notices in this docket

- Mar 30, 2010: Notice of proposed rulemaking (NPRM). (first notice), FR document 2010-7024, comments due May 14, 2010 (https://www.federalregister.gov/documents/2010/03/30/2010-7024/airworthiness-directives-cessna-aircraft-company-model-525a-airplanes)

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