Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW535A Turbofan Engines; Correction

---
identifier: "/us/fr/E7-9719"
source: "fr"
legal_status: "authoritative_unofficial"
title: "Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW535A Turbofan Engines; Correction"
title_number: 0
title_name: "Federal Register"
section_number: "E7-9719"
section_name: "Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW535A Turbofan Engines; Correction"
positive_law: false
currency: "2007-05-22"
last_updated: "2007-05-22"
format_version: "1.1.0"
generator: "[email protected]"
agency: "Transportation Department"
document_number: "E7-9719"
document_type: "rule"
publication_date: "2007-05-22"
agencies:
  - "Transportation Department"
  - "Federal Aviation Administration"
cfr_references:
  - "14 CFR Part 39"
rin: "2120-AA64"
fr_citation: "72 FR 28589"
fr_volume: 72
docket_ids:
  - "Docket No. FAA-2006-26112"
  - "Directorate Identifier 2006-NE-35-AD"
  - "Amendment 39-14837"
  - "AD 2006-24-08"
effective_date: "2007-05-22"
fr_action: "Final rule; correction."
---


#  [Corrected]

**AGENCY:**

Federal Aviation Administration (FAA), Department of Transportation (DOT).

**ACTION:**

Final rule; correction.

**SUMMARY:**

The FAA is correcting airworthiness directive (AD) 2006-24-08. That AD applies to Pratt & Whitney Canada (P&WC) PW535A turbofan engines. We published that AD in the *Federal Register* on December 4, 2006 (71 FR 70284). The fuel manifold part number (P/N) 3025267-01 listed in paragraph (c) is incorrect. This document corrects that P/N. In all other respects, the original document remains the same.

**EFFECTIVE DATE:**

Effective May 22, 2007.

**FOR FURTHER INFORMATION CONTACT:**

Ian Dargin, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA, 01803; telephone (781) 238-7178; fax (781) 238-7199.

**SUPPLEMENTARY INFORMATION:**

On December 4, 2006 (71 FR 70284), we published a final rule AD, FR Doc, E6-20204, in the *Federal Register* . That AD applies to P&WC PW535A turbofan engines. We need to make the following correction:

§ 39.13

On page 70286, in the second column, in paragraph (c), in the fourth line, “3025267-01” is corrected to read “3052627-01”.

Issued in Burlington, Massachusetts, on May 14, 2007.

Peter A. White,

Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service.