# Proposed AD 98-NM-06-AD: McDonnell Douglas Model DC-9-10, -20, - 30, -40, and -50 Series Airplanes, and C-9 (Military) Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 98-26-09
- Action: Notice of proposed rulemaking (NPRM).
- Published: April 20, 1998, 63 FR 19423
- Comments due: June 4, 1998
- Became: [AD 98-26-09](https://openairdocs.org/ad/98-26-09)
- Docket: 98-NM-06-AD
- FR document: 98-10277
- Official PDF: https://openairdocs.org/files/sha256/a3/92/a392f4c11c1d85c1bba20166e6640db49be95f9384ee045762e87b1378ddad35 (from https://www.govinfo.gov/content/pkg/FR-1998-04-20/pdf/98-10277.pdf)
- Federal Register: https://www.federalregister.gov/documents/1998/04/20/98-10277/airworthiness-directives-mcdonnell-douglas-model-dc-9-10--20---30--40-and--50-series-airplanes-and
- Page: https://openairdocs.org/proposed/98-NM-06-AD

## Summary

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 series airplanes, and C-9 (military) airplanes. This proposal would require a one-time visual inspection to determine if the doorstops and corners of the doorjamb of the forward passenger door have been modified, various follow-on repetitive inspections, and modification, if necessary. This proposal is prompted by reports of fatigue cracks found in the fuselage skin and doubler at the corners and doorstops of the doorjamb of the forward passenger door. The actions specified by the proposed AD are intended to detect and correct such fatigue cracking, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane.

## Notices in this docket

- Apr 20, 1998: Notice of proposed rulemaking (NPRM). (first notice), FR document 98-10277, comments due Jun 4, 1998 (https://www.federalregister.gov/documents/1998/04/20/98-10277/airworthiness-directives-mcdonnell-douglas-model-dc-9-10--20---30--40-and--50-series-airplanes-and)

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