Airworthiness Directives; Pilatus Aircraft Ltd. Model PC-7 Airplanes
airworthiness · Rule · Final rule; correction. · Published 2004-12-14 · Effective 2004-12-27 · 69 FR 74412
Document
Document number
04-27320
Federal Register citation
69 FR 74412
Type
Rule
Action
Final rule; correction.
Category
airworthiness
Manufacturer
Pilatus
Publication date
2004-12-14
Effective date
2004-12-27
FAA docket
Docket No. FAA-2004-18579
Abstract
This document makes a correction to Airworthiness Directive (AD) 2004-23-01, which was published in the Federal Register on November 9, 2004 (69 FR 64832), and applies to certain Pilatus Aircraft Ltd. (Pilatus) Model PC-7 airplanes with any Lear Romec RR53710B type or Lear Romec RR53710K fuel booster pump (Pilatus part number 968.84.11.401; 968.84.11.403; or 968.84.11.404) installed. We incorrectly referenced the amendment number as Amendment 39-13856. The correct amendment number is Amendment 39-13892. This action corrects the regulatory text.