# Airworthiness Directives; Raytheon Model DH 125-1A, -3A, and - 400A Series Airplanes
> **Rule** · Final rule. · Published 1997-05-02 · Effective 1997-06-06 · 62 FR 24013
## Document
- **Document number:** 97-11198
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 62 FR 24013
- **Publication date:** 1997-05-02
- **Effective date:** 1997-06-06
- **FAA docket:** Docket No. 96-NM-190-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Raytheon Model DH 125-1A, -3A, and -400A series airplanes, that requires a one-time inspection to detect scoring of the upper fuselage skin around the periphery of the cockpit canopy blister interface, and repair, if necessary. This amendment is prompted by reports indicating that scoring of the upper fuselage skin had been detected in that area. The actions specified by this AD are intended to detect and correct scoring of the upper fuselage skin around the periphery of the cockpit canopy blister interface, which could result in reduced structural integrity of the fuselage, and consequent cabin depressurization.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1997/05/02/97-11198/airworthiness-directives-raytheon-model-dh-125-1a--3a-and---400a-series-airplanes)
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