# Airworthiness Directives; Eurocopter France Model SA 330F, G, and J Helicopters
> **Rule** · Final rule. · Published 1998-06-09 · Effective 1998-07-14 · 63 FR 31348
## Document
- **Document number:** 98-15199
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 31348
- **Publication date:** 1998-06-09
- **Effective date:** 1998-07-14
- **FAA docket:** Docket No. 97-SW-07-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to Eurocopter France Model SA 330F, G, and J helicopters that requires visually inspecting the intermediate gearbox (IGB) fairing safety stop (safety stop) for cracks, crazing, or edge wear, and if a crack, crazing, or edge wear exceeds the established limits, replacing the safety stop; and, inspecting to ensure that the inclined drive shaft fairing hinge pin is properly locked. A terminating action is provided in the AD by installing an additional safety stop on the IGB fairing. This amendment is prompted by one report of an accident involving the loss of the inclined drive shaft fairing. The actions specified by this AD are intended to prevent loss of the inclined drive shaft fairing, impact with the tail rotor, and subsequent loss of control of the helicopter.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/06/09/98-15199/airworthiness-directives-eurocopter-france-model-sa-330f-g-and-j-helicopters)
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