Airworthiness Directives; Turbomeca Turmo IV A and IV C Series Turboshaft Engines; Correction

---
identifier: "/us/fr/03-14275"
source: "fr"
legal_status: "authoritative_unofficial"
title: "Airworthiness Directives; Turbomeca Turmo IV A and IV C Series Turboshaft Engines; Correction"
title_number: 0
title_name: "Federal Register"
section_number: "03-14275"
section_name: "Airworthiness Directives; Turbomeca Turmo IV A and IV C Series Turboshaft Engines; Correction"
positive_law: false
currency: "2003-06-06"
last_updated: "2003-06-06"
format_version: "1.1.0"
generator: "[email protected]"
agency: "Transportation Department"
document_number: "03-14275"
document_type: "rule"
publication_date: "2003-06-06"
agencies:
  - "Transportation Department"
  - "Federal Aviation Administration"
cfr_references:
  - "14 CFR Part 39"
rin: "2120-AA64"
fr_citation: "68 FR 33854"
fr_volume: 68
docket_ids:
  - "Docket No. 99-NE-12-AD"
  - "Amendment 39-13168"
  - "AD 2003-11-09"
fr_action: "Final rule; correction."
---


#  [Corrected]

**AGENCY:**

Federal Aviation Administration, DOT.

**ACTION:**

Final rule; correction.

**SUMMARY:**

This document makes a correction to Airworthiness Directive (AD) 2003-11-09 applicable to Turbomeca Turmo IV A and IV C series turboshaft engines that was published in the *Federal Register* on May 29, 2003 (68 FR 31970). The engine model in the regulatory section, under applicability, is incorrect. This document corrects that model. In all other respects, the original document remains the same.

**EFFECTIVE DATE:**

July 3, 2003.

**FOR FURTHER INFORMATION CONTACT:**

Antonio Cancelliere, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7751; fax (781) 238-7199.

**SUPPLEMENTARY INFORMATION:**

A final rule AD, FR Doc. 03-13115 applicable to Turbomeca Turmo IV A and IV C series turboshaft engines, was published in the *Federal Register* on May 29, 2003 (68 FR 31970). The following correction is needed:

**14 CFR Part 39**

§ 39.13

On page 31970, in the third column, in the regulatory section, under applicability, in the first paragraph, in the fifth line, “FA 330-PUMA” is corrected to read “SA 330-PUMA”.

Issued in Burlington, MA, on June 2, 2003.

Jay J. Pardee,

Manager, Engine and Propeller Directorate, Aircraft Certification Service.