[Federal Register: July 9, 2004 (Volume 69, Number 131)]
[Rules and Regulations]
[Page 41417-41418]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr09jy04-19]
[[Page 41417]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2004-NM-35-AD; Amendment 39-13713; AD 2004-14-04]
RIN 2120-AA64
Airworthiness Directives; BAE Systems (Operations) Limited Model
BAe 146 Series Airplanes and Model Avro 146-RJ Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
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SUMMARY: This amendment adopts a new airworthiness directive (AD),
applicable to all BAE Systems (Operations) Limited Model BAe 146 series
airplanes and Model Avro 146-RJ series airplanes, that requires
performing a detailed inspection for chafing of the fuel quantity
indication (FQI) system wiring, and any applicable corrective actions.
These actions are necessary to prevent possible failure of the FQI
system, which could cause the flightcrew to act on misleading
information and possibly lead to in-flight fuel exhaustion. This action
is intended to address the identified unsafe condition.
DATES: Effective August 13, 2004.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of August 13, 2004.
ADDRESSES: The service information referenced in this AD may be
obtained from British Aerospace Regional Aircraft American Support,
13850 Mclearen Road, Herndon, Virginia 20171. This information may be
examined at the Federal Aviation Administration (FAA), Transport
Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton,
Washington; or at the National Archives and Records Administration
(NARA). For information on the availability of this material at NARA,
call (202) 741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-1175; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to include an airworthiness
directive (AD) that is applicable to all BAE Systems (Operations)
Limited Model BAe 146 series airplanes and Model Avro 146-RJ series
airplanes was published in the Federal Register on April 26, 2004 (69
FR 22459). That action proposed to require performing a detailed
inspection for chafing of the fuel quantity indication (FQI) system
wiring, and any applicable corrective actions.
Comments
Interested persons have been afforded an opportunity to participate
in the making of this amendment. No comments have been submitted on the
proposed AD or on the determination of the cost to the public.
Conclusion
After careful review of the available data, including the comments
noted above, the FAA has determined that air safety and the public
interest require the adoption of the rule as proposed.
Cost Impact
The FAA estimates that 54 airplanes of U.S. registry will be
affected by this AD, that it will take approximately 2 work hours per
airplane to accomplish the required inspection, and that the average
labor rate is $65 per work hour. Based on these figures, the cost
impact of the AD on U.S. operators is estimated to be $7,020, or $130
per airplane.
The cost impact figure discussed above is based on assumptions that
no operator has yet accomplished any of the requirements of this AD
action, and that no operator would accomplish those actions in the
future if this AD were not adopted. The cost impact figures discussed
in AD rulemaking actions represent only the time necessary to perform
the specific actions actually required by the AD. These figures
typically do not include incidental costs, such as the time required to
gain access and close up, planning time, or time necessitated by other
administrative actions.
Regulatory Impact
The regulations adopted herein 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. Therefore, it
is determined that this final rule does not have federalism
implications under Executive Order 13132.
For the reasons discussed above, I certify that this action (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. A final evaluation has been prepared for this action
and it is contained in the Rules Docket. A copy of it may be obtained
from the Rules Docket at the location provided under the caption
ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends part 39 of
the Federal Aviation Regulations (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. Section 39.13 is amended by adding the following new airworthiness
directive:
2004-14-04 BAE Systems (Operations) Limited (Formerly British
Aerospace Regional Aircraft): Amendment 39-13713. Docket 2004-NM-35-
AD.
Applicability: All Model BAe 146 series airplanes and Model Avro
146-RJ series airplanes, certificated in any category.
Compliance: Required as indicated, unless accomplished
previously.
To prevent possible failure of the fuel quantity indication
(FQI) system, which could cause the flightcrew to act on misleading
information and possibly lead to in-flight fuel exhaustion,
accomplish the following:
Inspection and Corrective Actions
(a) Within 2 months after the effective date of this AD, perform
a detailed inspection of the wiring of the FQI system for chafing,
and do any applicable corrective actions prior to further flight, in
accordance with the Accomplishment Instructions of BAE Systems
(Operations) Limited Inspection Service Bulletin 28-030, dated
February 21, 2003.
Note 1: For the purposes of this AD, a detailed inspection is
defined as: ``An intensive visual examination of a specific
structural area, system, installation, or assembly to detect damage,
failure, or irregularity. Available lighting is normally
supplemented with a direct source of good lighting at intensity
deemed appropriate by
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the inspector. Inspection aids such as mirror, magnifying lenses,
etc., may be used. Surface cleaning and elaborate access procedures
may be required.''
No Reporting Requirement
(b) Although BAE Systems (Operations) Limited Inspection Service
Bulletin 28-030, dated February 21, 2003, describes procedures for
reporting inspection findings to the manufacturer, this AD does not
require that action.
Alternative Methods of Compliance
(c) In accordance with 14 CFR 39.19, the Manager, International
Branch, ANM-116, Transport Airplane Directorate, FAA, is authorized
to approve alternative methods of compliance for this AD.
Incorporation by Reference
(d) The actions shall be done in accordance with BAE Systems
(Operations) Limited Inspection Service Bulletin 28-030, dated
February 21, 2003. This incorporation by reference was approved by
the Director of the Federal Register in accordance with 5 U.S.C.
552(a) and 1 CFR part 51. Copies may be obtained from British
Aerospace Regional Aircraft American Support, 13850 Mclearen Road,
Herndon, Virginia 20171. Copies may be inspected at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington; or at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal
--register/code--of--federal--regulations/ibr--locations.html.
Note 2: The subject of this AD is addressed in British
airworthiness directive 007-02-2003, dated May 2003.
Effective Date
(e) This amendment becomes effective on August 13, 2004.
Issued in Renton, Washington, on June 29, 2004.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 04-15375 Filed 7-8-04; 8:45 am]
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