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Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)

---
identifier: "/us/fr/06-3797"
source: "fr"
legal_status: "authoritative_unofficial"
title: "Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)"
title_number: 0
title_name: "Federal Register"
section_number: "06-3797"
section_name: "Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)"
positive_law: false
currency: "2006-04-21"
last_updated: "2006-04-21"
format_version: "1.1.0"
generator: "[email protected]"
agency: "Transportation Department"
document_number: "06-3797"
document_type: "rule"
publication_date: "2006-04-21"
agencies:
  - "Transportation Department"
  - "Federal Aviation Administration"
cfr_references:
  - "14 CFR Part 39"
rin: "2120-AA64"
fr_citation: "71 FR 20530"
fr_volume: 71
docket_ids:
  - "Docket No. FAA-2006-24364"
  - "Directorate Identifier 2004-NM-272-AD"
  - "Amendment 39-14534"
  - "AD 2006-07-07"
effective_date: "2006-04-17"
fr_action: "Final rule; correction."
---

#  Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)

**AGENCY:**

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

**ACTION:**

Final rule; correction.

**SUMMARY:**

The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the *Federal Register* on March 31, 2006 (71 FR 16206). The error resulted in an incorrect Docket No. This AD applies to certain Airbus Model A300-600 series airplanes. This AD requires modifying nine bolt holes in the vertical flange to prevent cracking before the inspection threshold of AD 98-18-02.

**DATES:**

Effective April 17, 2006.

**ADDRESSES:**

The AD docket contains the proposed AD, comments, and any final disposition. You may examine the AD docket on the Internet at *http://dms.dot.gov,* or in person at the Docket Management Facility office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Management Facility office  (telephone (800) 647-5227) is located on the plaza level of the Nassif Building at the U.S. Department of Transportation, 400 Seventh Street, SW., room PL-401, Washington, DC. This docket number is FAA-2006-24364; the directorate identifier for this docket is 2004-NM-272-AD.

**FOR FURTHER INFORMATION CONTACT:**

Tim Backman, Aerospace Engineer, ANM-116, International Branch, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-2797; fax (425) 227-1149.

**SUPPLEMENTARY INFORMATION:**

On March 15, 2006, the FAA issued AD 2006-07-07, amendment 39-14534 (71 FR 16206, March 31, 2006), for certain Airbus Model A300-600 series airplanes. The AD requires modifying nine bolt holes in the vertical flange to prevent cracking before the inspection threshold of AD 98-18-02.

As published, the AD lists the Docket No. as FAA-2006-24124. The correct Docket No. is FAA-2006-24364.

No other part of the regulatory information has been changed; therefore, the final rule is not republished in the *Federal Register* .

The effective date of this AD remains April 17, 2006.

In the *Federal Register* of March 31, 2006, on page 16206, in the first column; on page 16207, in the third column; and on page 16208 in the second column; the Docket No. of AD 2006-07-07 is corrected to read as follows: FAA-2006-24364.

Issued in Renton, Washington, on April 13, 2006.

Ali Bahrami,

Manager,  Transport Airplane Directorate, Aircraft Certification Service.