# Airworthiness Directives; PILATUS Aircraft Ltd. Model PC-7 Airplanes
> **Rule** · Final rule. · Published 2002-11-01 · Effective 2002-12-20 · 67 FR 66541
## Document
- **Document number:** 02-27418
- **Category:** airworthiness
- **Manufacturer:** PILATUS
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 67 FR 66541
- **Publication date:** 2002-11-01
- **Effective date:** 2002-12-20
- **FAA docket:** Docket No. 2002-CE-28-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain PILATUS Aircraft Ltd. (Pilatus) Model PC-7 airplanes. This AD requires you to repetitively inspect the main landing gear front attachment brackets for cracks, and, if cracks are found, install improved-design brackets. Installing the improved-design brackets terminates the required inspections. 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 cracks in the main landing gear front attachment brackets, which could result in failure of the brackets. Such failure could lead to the main landing gear leg detaching from the wing main spar.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2002/11/01/02-27418/airworthiness-directives-pilatus-aircraft-ltd-model-pc-7-airplanes)
---
*AI Analytics · CC0 1.0*