Airworthiness Directives; British Aerospace Model BAC 1-11 200 and 400 Series Airplanes, 69430-69432 [05-22592]
Download as PDF
69430
Federal Register / Vol. 70, No. 220 / Wednesday, November 16, 2005 / Rules and Regulations
Note 1: For the purposes of this AD, a
general visual inspection is: ‘‘A visual
examination of an interior or exterior area,
installation, or assembly to detect obvious
damage, failure, or irregularity. This level of
inspection is made from within touching
distance unless otherwise specified. A mirror
may be necessary to ensure visual access to
all surfaces in the inspection area. This level
of inspection is made under normally
available lighting conditions such as
daylight, hangar lighting, flashlight, or
droplight and may require removal or
opening of access panels or doors. Stands,
ladders, or platforms may be required to gain
proximity to the area being checked.’’
(1) For airplanes that have accumulated
20,000 total flight hours or more as of the
effective date of this AD: Within 6 months
after the effective date of this AD.
(2) For airplanes that have accumulated
less than 20,000 total flight hours as of the
effective date of this AD: Within 12 months
after the effective date of this AD.
(g) If, during accomplishment of the
corrective actions required by paragraph (f) of
this AD, the service bulletin requires
contacting the manufacturer for instructions
on repairing heat damage to a component,
wiring, or structure: Before further flight,
repair according to a method approved by
either the Manager, International Branch,
ANM–116, FAA, Transport Airplane
Directorate; or the Civil Aviation Authority—
The Netherlands (or its delegated agent).
Modification
(h) Before further flight after accomplishing
the inspection required by paragraph (f) of
this AD: Replace the blanking plugs of the
bleed air supply ducts with clamping
devices, in accordance with Part D of the
Accomplishment Instructions of Fokker
Service Bulletin SBF50–36–006, dated
October 1, 2001.
Alternative Methods of Compliance
(AMOCs)
(i)(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 14 CFR 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
(j) Dutch airworthiness directive 2001–130,
dated October 31, 2001, also addresses the
subject of this AD.
Material Incorporated by Reference
(k) You must use Fokker Service Bulletin
SBF50–36–006, dated October 1, 2001, 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 Fokker Services B.V., P.O.
Box 231, 2150 AE Nieuw-Vennep, the
Netherlands, for a copy of this service
VerDate Aug<31>2005
11:21 Nov 15, 2005
Jkt 208001
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 https://
dms.dot.gov; 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 https://www.archives.gov/
federal_register/code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on
November 7, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 05–22589 Filed 11–15–05; 8:45 am]
BILLING CODE 4910–13–P
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
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
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 https://
PO 00000
Frm 00010
Fmt 4700
Sfmt 4700
dms.dot.gov 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
https://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 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
E:\FR\FM\16NOR1.SGM
16NOR1
Federal Register / Vol. 70, No. 220 / Wednesday, November 16, 2005 / Rules and Regulations
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.
69431
Costs of Compliance
The following table provides the
estimated costs for U.S. operators to
comply with this AD.
ESTIMATED COSTS
Action
Work hours
AFM Revision ...........................................................................................
Maintenance Program Revision ...............................................................
Average
labor rate
per hour
1
1
Authority for This Rulemaking
List of Subjects in 14 CFR Part 39
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.
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
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.
VerDate Aug<31>2005
11:21 Nov 15, 2005
Jkt 208001
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
I
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
PO 00000
Frm 00011
Fmt 4700
Sfmt 4700
$65
65
Cost per
airplane
$65
65
Number of
U.S.registered
airplanes
11
11
Fleet cost
$715
715
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.
E:\FR\FM\16NOR1.SGM
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69432
Federal Register / Vol. 70, No. 220 / Wednesday, November 16, 2005 / Rules and Regulations
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 § 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 OneEleven 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 https://
dms.dot.gov; 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 https://www.archives.gov/
federal_register/code_of_federal_regulations/
ibr_locations.html.
in the Federal Register on October 18,
2005 (70 FR 60424), Airspace Docket
No. 05–ASW–1. In that rule, the
effective date was inadvertently
published as December 22, 2005. This
action changes the effective date to
April 13, 2006.
In the final rule
published October 18, 2005 (70 FR
60424), the effective date is corrected to
read April 13, 2006.
EFFECTIVE DATE:
FOR FURTHER INFORMATION CONTACT:
Steve Rohring, Airspace and Rules,
Office of System Operations Airspace
and AIM, Federal Aviation
Administration, 800 Independence
Avenue, SW., Washington, DC 20591;
telephone: (202) 267–8783.
SUPPLEMENTARY INFORMATION:
History
On October 18, 2005, a final rule was
published in the Federal Register (70
FR 60424), Airspace Docket No. 05–
ASW–1. This rule revised Jet Routes J–
8, J–18, J–19, J–58, J–76, J–104 and J–
244; and VOR Federal Airways V–60,
V–190, V–263 and V–611; Las Vegas,
NM. In that rule, the effective date was
inadvertently published as December
22, 2005. This action changes the
effective date to April 13, 2006.
Delay of Effective Date
BILLING CODE 4910–13–P
Accordingly, pursuant to the
authority delegated to me, the effective
date for Airspace Docket No. 05–ASW–
1, as published in the Federal Register
on October 18, 2005 (70 FR 60424),
Airspace Docket No. 05–ASW–1, is
hereby delayed from December 22, 2005
to April 13, 2006.
DEPARTMENT OF TRANSPORTATION
Authority: 49 U.S.C. 106(g), 40103, 40113,
40120; E.O. 10854, 24 FR 9565, 3 CFR, 1959–
1963 Comp., p. 389.
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]
[Docket No. FAA–2005–22421; Airspace
Docket No. 05–ASW–1]
Issued in Washington, DC, on November 4,
2005.
Edith V. Parish,
Manager, Airspace and Rules.
[FR Doc. 05–22578 Filed 11–15–05; 8:45 am]
RIN 2120–AA66
BILLING CODE 4910–13–P
Federal Aviation Administration
14 CFR Part 71
Revision of Jet Routes J–8, J–18, J–19,
J–58, J–76, J–104 and J–244; and VOR
Federal Airways V–60, V–190, V–263
and V–611; Las Vegas, NM
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; delay of effective
date.
AGENCY:
SUMMARY: This action changes the
effective date of a final rule published
VerDate Aug<31>2005
11:21 Nov 15, 2005
Jkt 208001
PO 00000
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Fmt 4700
Sfmt 4700
DEPARTMENT OF COMMERCE
Bureau of Industry and Security
15 CFR Parts 740, 742, 772 and 774
[Docket No. 051028279–5279–01]
RIN 0694–AD57
Establishment of New License
Exception for the Export or Reexport
to U.S. Persons in Libya of Certain
Items Controlled for Anti-Terrorism
Reasons Only on the Commerce
Control List
Bureau of Industry and
Security, Commerce.
ACTION: Interim rule with request for
comments.
AGENCY:
SUMMARY: In this interim rule, the
Bureau of Industry and Security (BIS)
amends the Export Administration
Regulations (EAR) to implement
changes to export and reexport controls
with respect to Libya. Specifically, in
this rule, BIS establishes a License
Exception authorizing the export or
reexport to U.S. persons in Libya of
certain items listed on the Commerce
Control List and controlled for antiterrorism (AT) reasons only. This rule is
consistent with the President’s decision
to modify United States’ sanctions
against Libya, in response to Libya’s
continuing efforts to dismantle its
weapons of mass destruction (WMD)
and missile programs and its
renunciation of terrorism.
DATES: This rule is effective November
16, 2005. Comments must be received
on or before December 16, 2005.
ADDRESSES: Written comments on this
rule may be sent to the Federal
eRulemaking Portal: https://
www.regulations.gov, or by e-mail to
publiccomments@bis.doc.gov. Include
RIN 0694–AD57 in the subject line of
the message. Comments may be
submitted by mail or hand delivery to
Sheila Quarterman, Office of Exporter
Services, Regulatory Policy Division,
Bureau of Industry and Security,
Department of Commerce, 14th &
Pennsylvania Avenue, NW., Room 2705,
Washington, DC 20230, ATTN: RIN
0694–AD57; or by fax: 202–482–3355.
Send comments regarding the
collection of information to David
Rostker, Office of Management and
Budget (OMB), by e-mail to
David_Rostker@omb.eop.gov, or by fax
to (202) 395–7285.
FOR FURTHER INFORMATION CONTACT: Joan
Roberts, Director, Foreign Policy
Division, Office of Nonproliferation and
Treaty Compliance, Bureau of Industry
and Security, Department of Commerce,
E:\FR\FM\16NOR1.SGM
16NOR1
Agencies
[Federal Register Volume 70, Number 220 (Wednesday, November 16, 2005)]
[Rules and Regulations]
[Pages 69430-69432]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-22592]
-----------------------------------------------------------------------
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 https://
dms.dot.gov 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 https://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 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 https://dms.dot.gov; 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 https://
www.archives.gov/federal_register/code_of_federal_regulations/
ibr_locations.html.
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]
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