# Proposed AD FAA-2004-18788: Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Comment period closed
- Products: Boeing
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: August 6, 2004, 69 FR 47808
- Comments due: September 20, 2004
- Docket: FAA-2004-18788 (https://www.regulations.gov/docket/FAA-2004-18788, where comments are filed)
- Project: 2003-NM-203-AD
- FR document: 04-17988
- Official PDF: https://openairdocs.org/files/sha256/45/ac/45acdebf525728073e6be28a422a34ed3f1a9efe7cc7fca05017e2d82607bbf3 (from https://www.govinfo.gov/content/pkg/FR-2004-08-06/pdf/04-17988.pdf)
- Federal Register: https://www.federalregister.gov/documents/2004/08/06/04-17988/airworthiness-directives-boeing-model-737-100--200--200c--300--400-and--500-series-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C5504134C85D221186256EE80053C54F.0001
- Page: https://openairdocs.org/proposed/FAA-2004-18788

## Summary

The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This proposed AD would require repetitive inspections of the intercostal webs, attachment clips, and stringer splice channels for cracks; and corrective action if necessary. This proposed AD is prompted by reports of fatigue cracks on several Boeing Model 737-200 series airplanes. We are proposing this AD to detect and correct fatigue cracking of the intercostals on the forward and aft sides of the forward entry door, which could result in loss of the forward entry door and rapid decompression of the airplane.

## Notices in this docket

- Aug 6, 2004: Notice of proposed rulemaking (NPRM). (first notice), FR document 04-17988, comments due Sep 20, 2004 (https://www.federalregister.gov/documents/2004/08/06/04-17988/airworthiness-directives-boeing-model-737-100--200--200c--300--400-and--500-series-airplanes)

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