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2010-04-04 BOMBARDIER, INC.: Amendment 39-16197. Docket No. FAA-2009-1027; Directorate Identifier 2009-NM-143-AD.
EFFECTIVE DATE

(a) This airworthiness directive (AD) becomes effective March 30, 2010.

AFFECTED ADS

(b) None.

APPLICABILITY

(c) This AD applies to  the airplanes identified in paragraphs  (c)(1) and
    (c)(2) of this AD; certificated in any category.

(1) Bombardier, Inc.  Model CL-600-2C10 (Regional  Jet Series 700,  701, &
    702) airplanes, serial numbers 10003 through 10268, inclusive.

(2) Bombardier,  Inc.  Model   CL-600-2D15   (Regional  Jet  Series   705)
    airplanes; and Bombardier, Inc. Model CL-600-2D24 (Regional Jet Series
    900) airplanes; serial numbers 15001 through 15205, inclusive.

SUBJECT

(d) Air    Transport    Association    (ATA)   of    America    Code   25:
    Equipment/Furnishings.

REASON

(e) The mandatory continuing airworthiness information (MCAI) states:

    There have been several in-service cases reported of impact damage  to
    the blowout (decompression) panel protective cage assemblies installed
    in the aft baggage cargo compartment. When damaged, these cages  could
    prevent  proper  operation  of  the  blowout  panels,  with  potential
    degradation of smoke detection and fire extinguishing capabilities  in
    the event of a fire.

    This directive  mandates replacement  of the  existing cages  with new
    cages that have greater damage resistance.

ACTIONS AND COMPLIANCE

(f) Unless  already done,  within 5,000  flight hours  after the effective
    date  of this  AD, replace  the existing  cage assemblies  in the  aft
    baggage  cargo  compartment,  in  accordance  with  Bombardier Service
    Bulletin 670BA-25-071, dated May 15, 2009.

FAA AD DIFFERENCES

NOTE 1: This  AD differs  from  the  MCAI  and/or  service information  as
follows: No differences.

OTHER FAA AD PROVISIONS

(g) The following provisions also apply to this AD:

(1) Alternative  Methods  of  Compliance  (AMOCs): The  Manager,  New York
    Aircraft  Certification Office,  ANE-170, FAA,  has  the  authority to
    approve AMOCs for this AD, if requested using the procedures found  in
    14 CFR 39.19.  Send information to  ATTN: Program Manager,  Continuing
    Operational Safety, FAA, New York Aircraft Certification Office,  1600
    Stewart Avenue, Suite 410,  Westbury, New York 11590;  telephone (516)
    228-7300; fax (516)  794-5531. Before using  any approved AMOC  on any
    airplane to which the AMOC applies, notify your principal  maintenance
    inspector (PMI) or principal avionics inspector (PAI), as appropriate,
    or lacking a principal inspector, your local Flight Standards District
    Office. The AMOC approval letter must specifically reference this AD.

(2) Airworthy Product: For any requirement in this AD to obtain corrective
    actions from a manufacturer or other source, use these actions if they
    are FAA-approved.  Corrective actions  are considered  FAA-approved if
    they are approved by the State of Design Authority (or their delegated
    agent). You are required to assure the product is airworthy before  it
    is returned to service.

(3) Reporting Requirements:  For any  reporting requirement  in  this  AD,
    under the provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et
    seq.), the  Office of  Management and  Budget (OMB)  has approved  the
    information  collection  requirements  and  has  assigned  OMB Control
    Number 2120-0056.

RELATED INFORMATION

(h) Refer to MCAI Canadian Airworthiness Directive CF-2009-30, dated  July
    6, 2009; and Bombardier  Service Bulletin 670BA-25-071,  dated May 15,
    2009; for related information.

MATERIAL INCORPORATED BY REFERENCE

(i) You must use Bombardier  Service Bulletin 670BA-25-071, dated May  15,
    2009, to do the actions required  by this AD, unless the AD  specifies
    otherwise.

(1) The  Director of  the Federal  Register approved  the incorporation by
    reference of this service information under 5 U.S.C. 552(a) and 1  CFR
    part 51.

(2) For  service information  identified in  this AD,  contact Bombardier,
    Inc.,  400  Côte-Vertu  Road West,  Dorval,  Québec  H4S 1Y9,  Canada;
    telephone:      514-855-5000;      fax:      514-855-7401;     e-mail:
    thd.crj@aero.bombardier.com; Internet: http://www.bombardier.com.

(3) You may review copies of the service information at the FAA, Transport
    Airplane Directorate, 1601 Lind  Avenue, SW., Renton, Washington.  For
    information on the availability of this material at the FAA, call  425
    -227-1221 or 425-227-1152.

(4) You  may  also  review copies  of  the  service  information  that  is
    incorporated  by  reference  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/i
    br_locations.html.

Issued in Renton, Washington, on February 4, 2010. Stephen P. Boyd, Acting
Manager, Transport Airplane Directorate, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Craig Yates, Aerospace Engineer, Airframe
and  Mechanical   Systems  Branch,   ANE-171,  FAA,   New  York   Aircraft
Certification Office, 1600 Stewart  Avenue, Suite 410, Westbury,  New York
11590; telephone (516) 228-7355; fax (516) 794-5531.
PREAMBLE 

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

ACTION: Final rule.

SUMMARY: We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

There have been several in-service cases reported of impact damage to the blowout (decompression) panel protective cage assemblies installed in the aft baggage cargo compartment. When damaged, these cages could prevent proper operation of the blowout panels, with potential degradation of smoke detection and fire extinguishing capabilities in the event of a fire.

* * * * *
We are issuing this AD to require actions to correct the unsafe condition on these products.

DATES: This AD becomes effective March 30, 2010.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 30, 2010.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at the U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC.

FOR FURTHER INFORMATION CONTACT: Craig Yates, Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New York 11590; telephone (516) 228-7355; fax (516) 794-5531.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an AD that would apply to the specified products. That NPRM was published in the Federal Register on November 5, 2009 (74 FR 57264). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states:

There have been several in-service cases reported of impact damage to the blowout (decompression) panel protective cage assemblies installed in the aft baggage cargo compartment. When damaged, these cages could prevent proper operation of the blowout panels, with potential degradation of smoke detection and fire extinguishing capabilities in the event of a fire.

This directive mandates replacement of the existing cages with new cages that have greater damage resistance.

You may obtain further information by examining the MCAI in the AD docket.

Comments

We gave the public the opportunity to participate in developing this AD. We received no comments on the NPRM or on the determination of the cost to the public.

Explanation of Changes Made to This AD

We have revised this AD to identify the legal name of the manufacturer as published in the most recent type certificate data sheet for the affected airplane models.

Explanation of Change to Costs of Compliance

Since issuance of the NPRM, we have increased the labor rate used in the Costs of Compliance from $80 per work-hour to $85 per work-hour. The Costs of Compliance information, below, reflects this increase in the specified hourly labor rate.

Conclusion

We reviewed the available data, and determined that air safety and the public interest require adopting the AD with the change described previously. We determined that this change will not increase the economic burden on any operator or increase the scope of the AD.

Differences Between This AD and the MCAI or Service Information

We have reviewed the MCAI and related service information and, in general, agree with their substance. But we might have found it necessary to use different words from those in the MCAI to ensure the AD is clear for U.S. operators and is enforceable. In making these changes, we do not intend to differ substantively from the information provided in the MCAI and related service information.

We might also have required different actions in this AD from those in the MCAI in order to follow our FAA policies. Any such differences are highlighted in a Note within the AD.

Costs of Compliance

We estimate that this AD will affect 361 products of U.S. registry. We also estimate that it will take about 2 work-hours per product to comply with the basic requirements of this AD. The average labor rate is $85 per work-hour. Required parts will cost about $1,263 per product. Where the service information lists required parts costs that are covered under warranty, we have assumed that there will be no charge for these parts. As we do not control warranty coverage for affected parties, some parties may incur costs higher than estimated here. Based on these figures, we estimate the cost of this AD to the U.S. operators to be $517,313, or $1,433 per product.

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 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 this AD:

1. Is not a "significant regulatory action" under Executive Order 12866;

2. Is not a "significant rule" under the 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.

Examining the AD Docket

You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains the NPRM, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone (800) 647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.

Adoption of the Amendment

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

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]

2. The FAA amends Sec. 39.13 by adding the following new AD: