# Proposed AD FAA-2006-25105: Raytheon Aircraft Company Beech Models 45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2007-06-01
- Products: Raytheon
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: July 31, 2006, 71 FR 43075
- Comments due: September 29, 2006
- Became: [AD 2007-06-01](https://openairdocs.org/ad/2007-06-01)
- Docket: FAA-2006-25105 (https://www.regulations.gov/docket/FAA-2006-25105, where comments are filed)
- Project: 2006-CE-33-AD
- FR document: 06-6581
- Official PDF: https://openairdocs.org/files/sha256/28/42/28424143735549d46a678b0ea8ab6d6d371f51a67e6e2f47c68f11573a61caad (from https://www.govinfo.gov/content/pkg/FR-2006-07-31/pdf/06-6581.pdf)
- Federal Register: https://www.federalregister.gov/documents/2006/07/31/06-6581/airworthiness-directives-raytheon-aircraft-company-beech-models-45-yt-34-a45-t-34a-b-45-and-d45
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CE7067DBACF7CE1F862571BC00704516.0001
- Page: https://openairdocs.org/proposed/FAA-2006-25105

## Summary

We propose to supersede Airworthiness Directive (AD) 62-24-01, which applies to all Raytheon Aircraft Company (Raytheon) Beech Models 45 (YT-34), A45 (T-34A, B45), and D45 (T-34B) airplanes. AD 62-24-01 currently requires you to repetitively inspect, using the dye penetrant method, the front and rear horizontal stabilizer spars for cracks and replace any cracked stabilizer. Since we issued AD 62-24-01, we determined that using dye penetrant inspection method may not detect cracks before failure of the horizontal stabilizer spars. Therefore, we are proposing to require the surface eddy current inspection method to detect cracks in the horizontal stabilizer spars. Consequently, this proposed AD would retain the actions required in AD 62-24-01 and change the required inspection method from dye penetrant to surface eddy current. We are proposing this AD to prevent failure of the front and rear horizontal stabilizer spars caused by fatigue cracks. This failure could result in stabilizer separation and loss of control of the airplane.

## Notices in this docket

- Jul 31, 2006: Notice of proposed rulemaking (NPRM). (first notice), FR document 06-6581, comments due Sep 29, 2006 (https://www.federalregister.gov/documents/2006/07/31/06-6581/airworthiness-directives-raytheon-aircraft-company-beech-models-45-yt-34-a45-t-34a-b-45-and-d45)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.