# Proposed AD 2003-NM-191-AD: Boeing Model 727, 727-100C, 727-200F, and 727C Series Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2004-03-31
- Products: Boeing
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: November 18, 2003, 68 FR 64998
- Comments due: January 20, 2004
- Became: [AD 2004-03-31](https://openairdocs.org/ad/2004-03-31)
- Docket: 2003-NM-191-AD
- FR document: 03-28738
- Official PDF: https://openairdocs.org/files/sha256/f2/a1/f2a1bdba7e1dcde964c75f1f500a93b5d6297d1abbad5a903d5e5c5d6deb59b7 (from https://www.govinfo.gov/content/pkg/FR-2003-11-18/pdf/03-28738.pdf)
- Federal Register: https://www.federalregister.gov/documents/2003/11/18/03-28738/airworthiness-directives-boeing-model-727-727-100c-727-200f-and-727c-series-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1E0723E60851E68886256DE2005BB5EE.0001
- Page: https://openairdocs.org/proposed/2003-NM-191-AD

## Summary

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Boeing Model 727, 727-100C, 727-200F, and 727C series airplanes. This proposal would require repetitive open-hole high frequency eddy current inspections for cracks in the fuselage skin, strap (bearstrap), and doubler at the forward and aft hinge fittings for the main deck cargo door, and repair of any cracks found. This action is necessary to detect and correct such cracks, which could reach critical crack length and result in rapid decompression of the airplane. This action is intended to address the identified unsafe condition.

## Notices in this docket

- Nov 18, 2003: Notice of proposed rulemaking (NPRM). (first notice), FR document 03-28738, comments due Jan 20, 2004 (https://www.federalregister.gov/documents/2003/11/18/03-28738/airworthiness-directives-boeing-model-727-727-100c-727-200f-and-727c-series-airplanes)

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