AD 2006-07-22

[Federal Register Volume 71, Number 69 (Tuesday, April 11, 2006)]
[Rules and Regulations]
[Pages 18199-18201]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 06-3379]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-23840; Directorate Identifier 2005-NM-232-AD; 
Amendment 39-14549; AD 2006-07-22]
RIN 2120-AA64


Airworthiness Directives; BAE Systems (Operations) Limited Model 
BAe 146 and Model Avro 146-RJ Airplanes

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

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
certain BAE Systems (Operations) Limited Model BAe 146 and Model Avro 
146-RJ airplanes. This AD requires modifying the control cable duct on 
the left bulkhead structure at frame 12, and, for certain airplanes, 
the forward toilet bulkhead structure. This AD results from a 
structural analysis by the manufacturer that revealed that rapid 
decompression of the flight compartment with the door closed could 
cause structural deformation of the left bulkhead structure at frame 
12, and of the attached cable duct structure. The duct structure 
protects the cables for the primary flight controls. We are issuing 
this AD to prevent deformation of the cable duct structure in the event 
of a rapid decompression, which could result in restriction of the 
primary flight controls and consequent reduced controllability of the 
airplane.

DATES: This AD becomes effective May 16, 2006.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in the AD as of May 16, 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 British Aerospace Regional Aircraft American Support, 13850 
Mclearen Road, Herndon, Virginia 20171, for service information 
identified in this AD.

[[Page 18200]]


FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-2125; 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 BAE Systems 
(Operations) Limited Model BAe 146 and Model Avro 146-RJ airplanes. 
That NPRM was published in the Federal Register on February 9, 2006 (71 
FR 6681). That NPRM proposed to require modifying the control cable 
duct on the left bulkhead structure at frame 12, and, for certain 
airplanes, the forward toilet bulkhead structure.

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 safety and the public interest require adopting the AD as proposed.

Costs of Compliance

    This AD affects about 19 airplanes of U.S. registry.
    The modification specified in Part 1 of the service bulletin will 
take about 21 work hours per airplane, at an average labor rate of $65 
per work hour. Required parts will be free of charge. Based on these 
figures, the estimated cost of the AD is $1,365 per airplane.
    The modification specified in Part 2 of the service bulletin will 
take about 5 work hours per airplane, at an average labor rate of $65 
per work hour. Required parts will be free of charge. Based on these 
figures, the estimated cost of the AD is $325 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):

2006-07-22 BAE Systems (Operations) Limited (Formerly British 
Aerospace Regional Aircraft): Amendment 39-14549. Docket No. FAA-
2006-23840; Directorate Identifier 2005-NM-232-AD.

Effective Date

    (a) This AD becomes effective May 16, 2006.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to BAE Systems (Operations) Limited Model 
BAe 146-100A, -200A, and -300A series airplanes, and Model Avro 146-
RJ70A, 146-RJ85A, and 146-RJ100A airplanes; certificated in any 
category; as identified in BAE Systems (Operations) Limited 
Modification Service Bulletin SB.25-459-36241A, Revision 1, dated 
March 30, 2005.

Unsafe Condition

    (d) This AD results from a structural analysis by the 
manufacturer which revealed that rapid decompression of the flight 
compartment with the door closed could cause structural deformation 
of the left bulkhead structure at frame 12, and of the attached 
cable duct structure. The duct structure protects the cables for the 
primary flight controls. We are issuing this AD to prevent 
deformation of the cable duct structure in the event of a rapid 
decompression, which could result in restriction of the primary 
flight controls and consequent reduced controllability 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 9 months after the effective date of this AD: Do the 
actions specified in either paragraph (f)(1) or (f)(2) of this AD by 
doing all the applicable actions specified in the Accomplishment 
Instructions of BAE Systems (Operations) Limited Modification 
Service Bulletin SB.25-459-36241A, Revision 1, dated March 30, 2005.
    (1) For airplanes on which BAE Modification HCM50303C has been 
installed, but on which BAE Modification HCM30033E, HCM30033F, 
HCM30033G, or HCM30033N has not been installed: Modify the control 
cable duct on the left bulkhead structure at frame 12 in accordance 
with Part 1 of the Accomplishment Instructions of the service 
bulletin.
    (2) For airplanes on which BAE Modification HCM50303C has been 
installed, and on which BAE Modification HCM30033E, HCM30033F, 
HCM30033G, or

[[Page 18201]]

HCM30033N has also been installed: Modify the control cable duct on 
the left bulkhead structure at frame 12 and the forward toilet 
bulkhead structure in accordance with Parts 1 and 2 of the 
Accomplishment Instructions of the service bulletin.

Modifications Accomplished According to Previous Issue of Service 
Bulletin

    (g) Modifications accomplished before the effective date of this 
AD in accordance with BAE Systems (Operations) Limited Modification 
Service Bulletin SB.25-459-36241A, dated July 22, 2004, are 
considered acceptable for compliance with the corresponding action 
specified in this AD.

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) British airworthiness directive G-2005-0026, dated September 
21, 2005, also addresses the subject of this AD.

Material Incorporated by Reference

    (j) You must use BAE Systems (Operations) Limited Modification 
Service Bulletin SB.25-459-36241A, Revision 1, dated March 30, 2005, 
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 Regional 
Aircraft American Support, 13850 Mclearen Road, Herndon, Virginia 
20171, 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 March 30, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 06-3379 Filed 4-10-06; 8:45 am]
BILLING CODE 4910-13-P