# Proposed AD FAA-2006-24092: Pilatus Aircraft Ltd. Models PC-6, PC- 6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2006-15-02
- Products: Pilatus
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: May 9, 2006, 71 FR 26891
- Comments due: June 9, 2006
- Became: [AD 2006-15-02](https://openairdocs.org/ad/2006-15-02)
- Docket: FAA-2006-24092 (https://www.regulations.gov/docket/FAA-2006-24092, where comments are filed)
- Project: 2006-CE-18-AD
- FR document: E6-7017
- Official PDF: https://openairdocs.org/files/sha256/41/d9/41d9867d385778c1e8da204b72362d4eefc41bd3e08d775978645eb05b629faf (from https://www.govinfo.gov/content/pkg/FR-2006-05-09/pdf/E6-7017.pdf)
- Federal Register: https://www.federalregister.gov/documents/2006/05/09/E6-7017/airworthiness-directives-pilatus-aircraft-ltd-models-pc-6-pc-6-h1-pc-6-h2-pc-6350-pc-6350-h1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6DCED06E9B26456B8625716900687041.0001
- Page: https://openairdocs.org/proposed/FAA-2006-24092

## Summary

We propose to supersede Airworthiness Directive (AD) 2003-09- 01, which applies to Pilatus Aircraft Ltd (Pilatus) Model PC-6 airplanes, all manufacturer serial numbers (MSN) up to and including 939. AD 2003-09-01 currently requires you to inspect and correct, as necessary, the aileron control bellcrank assemblies at the wing and fuselage locations. Since we issued AD 2003-09-01, the FAA determined the action should also apply to all the models of the PC-6 airplanes listed in the type certification data sheet of Type Certificate (TC) No. 7A15 that are produced in the United States through a licensing agreement between Pilatus and Fairchild Republic Company (also identified as Fairchild Industries, Fairchild Heli Porter, or Fairchild-Hiller Corporation). In addition, the intent of the applicability of AD 2003-09-01 was to all the affected serial numbers of the airplane models listed in TC No. 7A15. Consequently, this proposed AD would retain all the actions of AD 2003-09-01, would add those Fairchild Republic Company airplanes to the applicability of this proposed AD, and would list out the individual specific airplane models. We are proposing this AD to detect and correct increased friction in the aileron control bellcrank assemblies, which could result in failure of the aileron flight-control system. Such failure could lead to problems in controlling flight.

## Notices in this docket

- May 9, 2006: Notice of proposed rulemaking (NPRM). (first notice), FR document E6-7017, comments due Jun 9, 2006 (https://www.federalregister.gov/documents/2006/05/09/E6-7017/airworthiness-directives-pilatus-aircraft-ltd-models-pc-6-pc-6-h1-pc-6-h2-pc-6350-pc-6350-h1)

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