# Proposed AD FAA-2012-0931: The Boeing Company Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2013-16-17
- Products: Boeing
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: September 6, 2012, 77 FR 54856
- Comments due: October 22, 2012
- Became: [AD 2013-16-17](https://openairdocs.org/ad/2013-16-17)
- Docket: FAA-2012-0931 (https://www.regulations.gov/docket/FAA-2012-0931, where comments are filed)
- Project: 2011-NM-128-AD
- FR document: 2012-21944
- Official PDF: https://openairdocs.org/files/sha256/10/db/10dbe50be7e1fc96bc8d1a0ebe9661a50941081dd661dde1b39b54ffc26a1be9 (from https://www.govinfo.gov/content/pkg/FR-2012-09-06/pdf/2012-21944.pdf)
- Federal Register: https://www.federalregister.gov/documents/2012/09/06/2012-21944/airworthiness-directives-the-boeing-company-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4EEC96FB9980388386257A71005443E3.0001
- Page: https://openairdocs.org/proposed/FAA-2012-0931

## Summary

We propose to adopt a new airworthiness directive (AD) for all The Boeing Company Model 727, 727C, 727-100, 727-100C, 727-200, and 727-200F series airplanes. This proposed AD was prompted by a structural re-evaluation by the manufacturer, which identified elements within the wing trailing edge flap area that qualify as structural significant items (SSI). This proposed AD would require revising the maintenance inspection program to include inspections that will give no less than the required damage tolerance rating for certain SSIs, and repairing cracked structure. We are proposing this AD to detect and correct fatigue cracking of the wing trailing edge structure, which could result in compromised structural integrity of the airplane.

## Notices in this docket

- Sep 6, 2012: Notice of proposed rulemaking (NPRM). (first notice), FR document 2012-21944, comments due Oct 22, 2012 (https://www.federalregister.gov/documents/2012/09/06/2012-21944/airworthiness-directives-the-boeing-company-airplanes)

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