# Airworthiness Directives; Aircraft Belts, Inc. Model CS, CT, FM, FN, GK, GL, JD, JE, JT, JU, MD, ME, MM, MN, NB, PM, PN, RG, and RH Seat Restraint Systems
> **Rule** · Final rule; request for comments. · Published 1998-12-09 · Effective 1998-12-24 · 63 FR 67775
## Document
- **Document number:** 98-32619
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 63 FR 67775
- **Publication date:** 1998-12-09
- **Effective date:** 1998-12-24
- **FAA docket:** Docket No. 98-SW-33-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to Aircraft Belts, Inc. Model CS, CT, FM, FN, GK, GL, JD, JE, JT, JU, MD, ME, MM, MN, NB, PM, PN, RG, and RH seat restraint systems, installed on, but not limited to, Beech Aircraft Corp., Bell Helicopter Textron, Inc., Cessna Aircraft Co., Dassault Aviation, Eurocopter Deutschland, Eurocopter France, Gulfstream Aerospace, Learjet Corp., Lockheed Aircraft Corp., and Piper Aircraft Corp. aircraft. This action requires an inspection to ensure the locking mechanism is engaging properly, and replacing the buckle-half of the seat restraint system, if necessary. This amendment is prompted by the manufacturer reporting two failures of the seat restraint system in the field. The actions specified in this AD are intended to prevent failure of the seat restraint system due to the buckle assembly locking mechanism not engaging properly, which could result in the seat restraint system failing to properly secure the occupant during turbulence or landing.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/12/09/98-32619/airworthiness-directives-aircraft-belts-inc-model-cs-ct-fm-fn-gk-gl-jd-je-jt-ju-md-me-mm-mn-nb-pm-pn)
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