# Proposed AD 94-NM-131-AD: British Aerospace Model BAe 146-100A, - 200A, and -300A Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 95-19-13
- Action: Notice of proposed rulemaking (NPRM).
- Published: April 20, 1995, 60 FR 19693
- Comments due: May 31, 1995
- Became: [AD 95-19-13](https://openairdocs.org/ad/95-19-13)
- Docket: 94-NM-131-AD
- FR document: 95-9770
- Official PDF: https://openairdocs.org/files/sha256/11/59/115941c2bd4fa9cb887affd8b4f90778af930b2082b4f11befd071bd5d95ebd9 (from https://www.govinfo.gov/content/pkg/FR-1995-04-20/pdf/95-9770.pdf)
- Federal Register: https://www.federalregister.gov/documents/1995/04/20/95-9770/airworthiness-directives-british-aerospace-model-bae-146-100a---200a-and--300a-airplanes
- Page: https://openairdocs.org/proposed/94-NM-131-AD

## Summary

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to all British Aerospace Model BAe 146-100A, -200A, and -300A airplanes. This proposal would require repetitive inspections for cracking of fuselage frame 29, and repair, if necessary. This proposal is prompted by testing that revealed fatigue cracking in the web and inboard flange of frame 29. The actions specified by the proposed AD are intended to prevent reduced structural integrity of the fuselage, due to fatigue cracking in frame 29.

## Notices in this docket

- Apr 20, 1995: Notice of proposed rulemaking (NPRM). (first notice), FR document 95-9770, comments due May 31, 1995 (https://www.federalregister.gov/documents/1995/04/20/95-9770/airworthiness-directives-british-aerospace-model-bae-146-100a---200a-and--300a-airplanes)

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