AD 2006-10-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | A319-111 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A319-112 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A319-113 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A319-114 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A319-115 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A319-131 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A319-132 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A319-133 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A320-111 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A320-211 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A320-212 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A320-214 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A320-231 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A320-232 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
| aircraft | Airbus SAS | A320-233 | Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes; and Model A320-111 Airplanes |
Unsafe Condition
Reports indicate the low-pressure warning for the fuel pumps of the center fuel tank has come on in flight, which could result in the fuel pumps running while dry, creating a potential ignition source inside the center fuel tank. This, in combination with flammable fuel vapors, could lead to a fuel tank explosion and consequent loss of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 20 months after the effective date, modify the wiring to the fuel pump control of the center fuel tank by performing all actions specified in the Accomplishment Instructions of Airbus Service Bulletin A320-28-1059, Revision 06, dated June 29, 2000.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 20 months after the effective date (June 12, 2006)
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; and Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes, certificated in any category, that have received Airbus Modification 20024 in production (installation of a center tank), except airplanes on which Airbus Modification 24373 has been accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A319-100 and A320-200 series airplanes, and Model A320-111 airplanes. This AD requires modifying the wiring to the fuel pump control of the center fuel tank. This AD results from reports that the low-pressure warning for the fuel pumps of the center fuel tank has come on in flight. We are issuing this AD to ensure that the fuel pumps do not run while dry, which could result in a potential ignition source inside the center fuel tank, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 71, Number 88 (Monday, May 8, 2006)]
[Rules and Regulations]
[Pages 26685-26687]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 06-4232]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-23948; Directorate Identifier 2005-NM-246-AD;
Amendment 39-14587; AD 2006-10-03]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A319-100 and A320-200
Series Airplanes; and Model A320-111 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Airbus Model A319-100 and A320-200 series airplanes, and Model
A320-111 airplanes. This AD requires modifying the wiring to the fuel
pump control of the center fuel tank. This AD results from reports that
the low-pressure warning for the fuel pumps of the center fuel tank has
come on in flight. We are issuing this AD to ensure that the fuel pumps
do not run while dry, which could result in a potential ignition source
inside the center fuel tank, which, in combination with flammable fuel
vapors, could result in a fuel tank explosion and consequent loss of
the airplane.
DATES: This AD becomes effective June 12, 2006.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of June 12,
2006.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a> or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street SW., Nassif Building,
Room PL-401, Washington, DC.
Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex,
France, for service information identified in this AD.
FOR FURTHER INFORMATION CONTACT: Tim Dulin, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2141; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the airworthiness directive (AD) docket on the
Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a> 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 street address stated in the ADDRESSES section.
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to include an AD that would apply to certain Airbus Model
A319-100 and A320-200 series airplanes, and Model A320-111 airplanes.
That NPRM was published in the Federal Register on February 22, 2006
(71 FR 9046). That NPRM proposed to require modifying the wiring to the
fuel pump control of the center fuel tank.
Comments
We provided the public the opportunity to participate in the
development of this AD. We have considered the single comment received.
The commenter, Airbus, supports the NPRM.
Change to the NPRM
We have corrected the date for Airbus Service Bulletin A320-28-
1059, Revision 04, in Table 1 of the AD to February 3, 1999 (instead of
February 4, 1999).
Conclusion
We have carefully reviewed the available data, including the
comment received, and determined that air safety and the public
interest require adopting the AD with the change described previously.
We have determined that this change will neither increase the
[[Page 26686]]
economic burden on any operator nor increase the scope of the AD.
Costs of Compliance
This AD will affect about 119 airplanes of U.S. registry. The
required actions will take about 17 work hours per airplane, at an
average labor rate of $65 per work hour. There is no cost for parts.
Based on these figures, the estimated cost of the AD for U.S. operators
is $131,495, or $1,105 per airplane.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, Section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701, ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We have determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the national government and the States, or on the distribution of power
and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866;
(2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket. See the ADDRESSES
section for a location to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2006-10-03 Airbus: Amendment 39-14587. Docket No. FAA-2006-23948;
Directorate Identifier 2005-NM-246-AD.
Effective Date
(a) This AD becomes effective June 12, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Airbus Model A319-111, -112, -113, -114,
-115, -131, -132, and -133 airplanes; and Model A320-111, -211, -
212, -214, -231, -232, and -233 airplanes; certificated in any
category; that have received Airbus Modification 20024 in production
(installation of a center tank), except airplanes on which Airbus
Modification 24373 has been accomplished.
Unsafe Condition
(d) This AD results from reports that the low-pressure warning
for the fuel pumps of the center fuel tank has come on in flight. We
are issuing this AD to ensure that the fuel pumps do not run while
dry, which could result in a potential ignition source inside the
center fuel tank, which, in combination with flammable fuel vapors,
could result in a fuel tank explosion and consequent loss of the
airplane.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Modification
(f) Within 20 months after the effective date of this AD, modify
the wiring to the fuel pump control of the center fuel tank by doing
all actions specified in the Accomplishment Instructions of Airbus
Service Bulletin A320-28-1059, Revision 06, dated June 29, 2000.
Actions Done in Accordance With Previous Revisions of Service Bulletin
(g) Modifications done before the effective date of this AD in
accordance with the service bulletins identified in Table 1 of this
AD are acceptable for compliance with the requirements of paragraph
(f) of this AD.
Table 1.--Previous Revisions of Service Bulletin
------------------------------------------------------------------------
Revision
Airbus Service Bulletin level Date
------------------------------------------------------------------------
A320-28-1059.................. 04 February 3, 1999.
A320-28-1059.................. 05 March 12, 1999.
------------------------------------------------------------------------
Alternative Methods of Compliance (AMOCs)
(h)(1) The Manager, International Branch, ANM-116, Transport
Airplane Directorate, FAA, has the authority to approve AMOCs for
this AD, if requested in accordance with the procedures found in 14
CFR 39.19.
(2) Before using any AMOC approved in accordance with Sec.
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Related Information
(i) French airworthiness directive F-2005-173, dated October 26,
2005, also addresses the subject of this AD.
Material Incorporated by Reference
(j) You must use Airbus Service Bulletin A320-28-1059, Revision
06, dated June 29, 2000, to perform the actions that are required by
this AD, unless the AD specifies otherwise. The Director of the
Federal Register approved the incorporation by reference of this
document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51.
Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex,
France, for a copy of this service information. You may review
copies at the Docket Management Facility, U.S. Department of
Transportation, 400 Seventh Street, SW., Room PL-401, Nassif
Building, Washington, DC; on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a>; or
at the National Archives and Records Administration (NARA). For
information on the availability of this material at the NARA, call
(202) 741-6030, or go to http://www.archives.gov/ federal--register/
[[Page 26687]]
code--of--federal--regulations/ ibr--locations.html.
Issued in Renton, Washington, on April 28, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 06-4232 Filed 5-5-06; 8:45 am]
BILLING CODE 4910-13-P
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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