AD 2010-14-19

final rule

Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200, -300, -500 and -600 Series Airplanes

AD Number
2010-14-19
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2009-1215
FR Citation
75 FR 47207

Applicability

TypeManufacturerModelDetails
aircraft Airbus A330-201 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-202 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-203 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-223 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-243 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-301 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-302 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-303 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-321 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-322 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-323 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-341 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-342 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A330-343 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A340-211 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A340-212 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A340-213 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A340-311 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A340-312 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A340-313 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A340-541 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes
aircraft Airbus A340-642 Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-200, -300, -500 and -600 Series Airplanes

Unsafe Condition

Failure of the Halon dual-filter assemblies of the flow metering fire extinguishing system in the forward and bulk cargo compartments could result in inadequate fire suppression.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace or modify the Halon dual-filter assemblies of the flow metering fire extinguishing system in the forward and bulk cargo compartments, as applicable.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Airbus Model A330-200 and -300 series airplanes, and Model A340-200, -300, -500, and -600 series airplanes.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

The FAA is correcting airworthiness directive (AD) 2010-14-19, which published in the Federal Register on July 13, 2010. That AD applies to certain Model A330-200 and -300 series airplanes, and Model A340-200, -300, -500 and -600 series airplanes. A certain service bulletin number in Note 3 of the regulatory section is incorrect. This document corrects that service bulletin number. In all other respects, the original document remains the same.

Document Text

Show stored source text (verify against official source)
[Federal Register Volume 75, Number 150 (Thursday, August 5, 2010)]
[Rules and Regulations]
[Pages 47207-47208]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2010-19151]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2009-1215; Directorate Identifier 2009-NM-126-AD; 
Amendment 39-16364; AD 2010-14-19]
RIN 2120-AA64


Airworthiness Directives; Airbus Model A330-200 and -300 Series 
Airplanes, and Model A340-200, -300, -500 and -600 Series Airplanes

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

ACTION: Final rule; correction.

-----------------------------------------------------------------------

SUMMARY: The FAA is correcting airworthiness directive (AD) 2010-14-19, 
which published in the Federal Register on July 13, 2010. That AD 
applies to certain Model A330-200 and -300 series airplanes, and Model 
A340-200, -300, -500 and -600 series airplanes. A certain service 
bulletin number in Note 3 of the regulatory section is incorrect. This 
document corrects that service bulletin number. In all other respects, 
the original document remains the same.

DATES: This correction is effective August 5, 2010. The effective date 
of AD 2010-14-19 remains August 17, 2010.

ADDRESSES: You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a>; or in person at the Docket Management Facility 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains this AD, the regulatory evaluation, 
any comments received, and other information. The address for the 
Docket Office (telephone 800-647-5527) is the Document Management 
Facility, U.S. Department of Transportation, Docket Operations, M-30, 
West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., 
Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 
227-1138; fax (425) 227-1149.

[[Page 47208]]


SUPPLEMENTARY INFORMATION: On June 29, 2010, the FAA issued AD 2010-14-
19, Amendment 39-16364 (75 FR 39814, July 13, 2010), for certain Airbus 
Model A330-200 and -300 series airplanes, and Model A340-200, -300, -
500 and -600 series airplanes. The AD requires replacing or modifying 
the Halon dual-filter assemblies of the flow metering fire 
extinguishing system in the forward and bulk cargo compartments, as 
applicable.
    As published, Note 3 of the AD specifies in error Airbus Service 
Bulletin A340-26-4038. The correct service bulletin is Airbus Service 
Bulletin A340-26-4030.
    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 August 17, 2010.


Sec.  39.13  [Corrected]

0
In the Federal Register of July 13, 2010, on page 39817, in the second 
and third columns, Note 3 of AD 2010-14-19 is corrected to read as 
follows:
* * * * *

    Note 3:  The Halon dual-filter assembly P/N QA06753 is embodied 
in production through Airbus modification 40041. The Halon dual-
filter assembly P/N QA06753-01 is only embodied in service through 
Airbus Service Bulletin A330-26-3030 or Airbus Service Bulletin 
A340-26-4030. The Halon dual-filter assembly P/N QA06753-02 is 
embodied in production through modification 47197 or 47883 or 50108 
(BCRC) and 51065 or 51329 (LDCC) or in service through Airbus 
Service Bulletin A330-26-3030 or Airbus Service Bulletin A340-26-
4030.

* * * * *

    Issued in Renton, Washington, on July 27, 2010.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2010-19151 Filed 8-4-10; 8:45 am]
BILLING CODE 4910-13-P

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.