# Airworthiness Directives; Pilatus Aircraft LTD Model PC-6 Airplanes
> **Rule** · Final rule. · Published 2001-01-29 · Effective 2001-03-13 · 66 FR 8079
## Document
- **Document number:** 01-2002
- **Category:** airworthiness
- **Manufacturer:** Pilatus
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 66 FR 8079
- **Publication date:** 2001-01-29
- **Effective date:** 2001-03-13
- **FAA docket:** Docket No. 99-CE-77-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Pilatus Aircraft LTD (Pilatus) Model PC-6 airplanes that are equipped with a certain stabilizer trim actuator. This AD requires you to inspect the lower lug of the actuator for cracks, damage, or distortion; verify that the staked bearing is correctly installed in the bore of the lug; and repair any cracked, damaged, or distorted parts and reassemble any incorrectly installed staked bearing, as necessary. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified by this AD are intended to detect and correct damage, distortion, or cracks in the lower lug assembly, which could result in failure of the lower lug. Such failure could lead to loss of the stabilizer trim actuator with consequent loss of control of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2001/01/29/01-2002/airworthiness-directives-pilatus-aircraft-ltd-model-pc-6-airplanes)
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