# Airworthiness Directives; British Aerospace Model BAe 146-100A, - 200A, and -300A Series Airplanes
> **Rule** · Final rule. · Published 1998-10-06 · Effective 1998-11-10 · 63 FR 53550
## Document
- **Document number:** 98-26391
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 53550
- **Publication date:** 1998-10-06
- **Effective date:** 1998-11-10
- **FAA docket:** Docket No. 98-NM-214-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain British Aerospace Model BAe 146-100A, -200A, and -300A series airplanes, that requires either a one-time non-destructive test (NDT) or a visual inspection for cracking of the fuselage skin in the vicinity of frame 29 between stringers 12 and 13, and repair, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to detect and correct fatigue cracking of the fuselage skin in the specified area, which could result in reduced structural integrity of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/10/06/98-26391/airworthiness-directives-british-aerospace-model-bae-146-100a---200a-and--300a-series-airplanes)
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