AD 2005-23-15
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; British Aerospace Model BAC 1-11 200 and 400 Series Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; British Aerospace Model BAC 1-11 200 and 400 Series Airplanes |
Unsafe Condition
Potential ignition sources inside the fuel system, which, in combination with flammable fuel vapors, could result in 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
Revise the airplane flight manual to include applicable amendments advising the flightcrew of procedures to check for proper operation of the fuel system, address tripped circuit breakers, failure of a fuel pump in flight, and operations in a low-fuel situation. Revise the FAA-approved maintenance program to include certain repetitive maintenance tasks intended to improve the safety of the fuel system.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 3 months after the effective date of this AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All British Aerospace Model BAC 1-11 200 and 400 series airplanes, certificated in any category.
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 all British Aerospace Model BAC 1-11 200 and 400 series airplanes. This AD requires revising the airplane flight manual (AFM) to contain applicable AFM amendments, which advise the flightcrew of information pertaining to safely operating the fuel system. The AD also requires revising the FAA-approved maintenance program to include certain repetitive maintenance tasks intended to improve the safety of the fuel system. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent potential ignition sources inside the fuel system, 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 70, Number 220 (Wednesday, November 16, 2005)]
[Rules and Regulations]
[Pages 69430-69432]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 05-22592]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22427; Directorate Identifier 2004-NM-263-AD;
Amendment 39-14373; AD 2005-23-15]
RIN 2120-AA64
Airworthiness Directives; British Aerospace Model BAC 1-11 200
and 400 Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
British Aerospace Model BAC 1-11 200 and 400 series airplanes. This AD
requires revising the airplane flight manual (AFM) to contain
applicable AFM amendments, which advise the flightcrew of information
pertaining to safely operating the fuel system. The AD also requires
revising the FAA-approved maintenance program to include certain
repetitive maintenance tasks intended to improve the safety of the fuel
system. This AD results from fuel system reviews conducted by the
manufacturer. We are issuing this AD to prevent potential ignition
sources inside the fuel system, 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 December 21, 2005.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of December 21,
2005.
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 British Aerospace, Service Support, Airbus Limited, P.O.
Box 77, Bristol BS99 7AR, England, for service information identified
in this AD.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-1175; 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 all British Aerospace
Model BAC 1-11 200 and 400 series airplanes. That NPRM was published in
the Federal Register on September 16, 2005 (70 FR 54671). That NPRM
proposed to require revising the airplane flight manual (AFM) to
contain applicable AFM amendments, which advise the flightcrew of
information pertaining to safely operating the fuel system. The NPRM
also proposed to require revising the FAA-approved maintenance program
to include certain repetitive maintenance tasks intended to improve the
safety of the fuel system.
Clarification of Alternative Method of Compliance (AMOC) Paragraph
We have revised this action to clarify the appropriate procedure
for notifying the principal inspector before using any approved AMOC on
any airplane to which the AMOC applies.
Comments
We provided the public the opportunity to participate in the
development of this AD. We received no comments on the NPRM or on the
determination of the cost to the public.
Conclusion
We have carefully reviewed the available data and determined that
air
[[Page 69431]]
safety and the public interest require adopting the AD with the change
described previously. We have determined that this change will neither
increase the economic burden on any operator nor increase the scope of
the AD.
Costs of Compliance
The following table provides the estimated costs for U.S. operators
to comply with this AD.
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Number of
Average Cost per U.S.-
Action Work hours labor rate airplane registered Fleet cost
per hour airplanes
----------------------------------------------------------------------------------------------------------------
AFM Revision................................... 1 $65 $65 11 $715
Maintenance Program Revision................... 1 65 65 11 715
----------------------------------------------------------------------------------------------------------------
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):
2005-23-15 British Aerospace Airbus Limited: Amendment 39-14373.
Docket No. FAA-2005-22427; Directorate Identifier 2004-NM-263-AD.
Effective Date
(a) This AD becomes effective December 21, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all British Aerospace Model BAC 1-11 200
and 400 series airplanes, certificated in any category.
Unsafe Condition
(d) This AD results from fuel system reviews conducted by the
manufacturer. We are issuing this AD to ensure that the flightcrew
and maintenance personnel are advised of procedures pertaining to
the safety of the fuel system. These procedures are needed to
prevent potential ignition sources inside the fuel system, 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.
Airplane Flight Manual and Maintenance Program Revisions
(f) Within 3 months after the effective date of this AD, do the
actions specified in paragraphs (f)(1) and (f)(2) of this AD to
improve the safety of the fuel system, in accordance with the
Accomplishment Instructions of Airbus UK BAC One-Eleven Alert
Service Bulletin 28-A-PM6057, Issue 1, dated May 10, 2004.
(1) Revise the airplane flight manual to include the applicable
amendments advising the flightcrew of appropriate procedures to
check for proper operation of the fuel system, and to address
tripped circuit breakers, failure of a fuel pump in flight, and
operations in a low-fuel situation, as specified in Table 2 (under
Section 4.11) of the service bulletin.
Note 1: The actions required by paragraph (f)(1) of this AD may
be done by inserting a copy of the applicable advance amendment
bulletins (AABs) specified in Table 2 of Airbus UK BAC One-Eleven
Alert Service Bulletin 28-A-PM6057, Issue 1, dated May 10, 2004,
into the AFM. When information identical to that in the applicable
AABs has been included in the general revisions of the AFM, the AABs
no longer need to be inserted into the AFM.
(2) Revise the FAA-approved maintenance program to include all
repetitive maintenance tasks specified in Table 1 (under Section
4.10.2.) of the service bulletin. Then, thereafter, comply with the
requirements of these maintenance tasks at the interval specified in
Table 1 of the service bulletin; except for airplanes that operate
fewer than a total of 1,250 flight hours per year, accomplish the
requirements of these maintenance tasks at the earlier of the times
specified in columns 2 and 3 of Table 1 of the service bulletin.
Where Table 1 of the service bulletin specifies a repetitive
interval in ``hours,'' for the purposes of this AD, this means
``flight hours.'' Any applicable corrective actions must be done
before further flight.
Note 2: After revising the maintenance program to include the
required periodic maintenance tasks according to paragraph (f)(2) of
this AD, operators do not need to make a maintenance log entry to
show compliance with this AD every time those maintenance tasks are
accomplished thereafter.
[[Page 69432]]
Alternative Methods of Compliance (AMOCs)
(g)(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
(h) British airworthiness directive G-2004-0012, dated June 21,
2004, also addresses the subject of this AD.
Material Incorporated by Reference
(i) You must use Airbus UK BAC One-Eleven Alert Service Bulletin
28-A-PM6057, Issue 1, dated May 10, 2004, 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 British Aerospace, Service Support, Airbus
Limited, P.O. Box 77, Bristol BS99 7AR, England, 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 <a href="http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html">http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html</a>.
Issued in Renton, Washington, on November 7, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-22592 Filed 11-15-05; 8:45 am]
BILLING CODE 4910-13-P
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Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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