
[Federal Register: June 17, 2010 (Volume 75, Number 116)]
[Rules and Regulations]               
[Page 34357-34359]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr17jn10-10]                         

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-0170; Directorate Identifier 2009-NM-127-AD; 
Amendment 39-16328; AD 2010-12-07]
RIN 2120-AA64

 
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. 
(EMBRAER) Model EMB-135ER, -135KE, -135KL, and -135LR Airplanes; and 
EMBRAER Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -
145EP Airplanes

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

ACTION: Final rule.

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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:

    Reassessment of the damage tolerance analysis resulted in 
threshold reduction for some Structure Significant Items (SSI) of 
the Maintenance Review Board Report (MRBR) Airworthiness Limitations 
Items (ALI). Failure to inspect these structural components, 
according to the new threshold, could prevent a timely detection of 
fatigue cracking. These cracks, if not properly

[[Page 34358]]

addressed, could adversely affect the structural integrity of the 
airplane.

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

DATES: This AD becomes effective July 22, 2010.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of July 22, 
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: Todd Thompson, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 
227-1175; fax (425) 227-1149.

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 February 25, 2010 
(75 FR 8557). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states:

    Reassessment of the damage tolerance analysis resulted in 
threshold reduction for some Structure Significant Items (SSI) of 
the Maintenance Review Board Report (MRBR) Airworthiness Limitations 
Items (ALI). Failure to inspect these structural components, 
according to the new threshold, could prevent a timely detection of 
fatigue cracking. These cracks, if not properly addressed, could 
adversely affect the structural integrity of the airplane.

* * * * *
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.

Conclusion

    We reviewed the available data and determined that air safety and 
the public interest require adopting the AD as proposed.

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 711 products of U.S. registry. 
We also estimate that it will take about 1 work-hour per product to 
comply with the basic requirements of this AD. The average labor rate 
is $85 per work-hour. Based on these figures, we estimate the cost of 
this AD to the U.S. operators to be $60,435, or $85 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

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

2010-12-07 Empresa Brasileira de Aeronautica S.A. (EMBRAER): 
Amendment 39-16328. Docket No. FAA-2010-0170; Directorate Identifier 
2009-NM-127-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective July 22, 
2010.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to all Empresa Brasileira de Aeronautica 
S.A. (EMBRAER) Model EMB-135ER, -135KE, -135KL, and -135LR 
airplanes; and EMBRAER Model EMB-145, -145ER, -145MR, -145LR, -
145XR, -145MP, and -145EP airplanes; certificated in any category.

[[Page 34359]]

Subject

    (d) Air Transport Association (ATA) of America Code 57: Wings.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:
    Reassessment of the damage tolerance analysis resulted in 
threshold reduction for some Structure Significant Items (SSI) of 
the Maintenance Review Board Report (MRBR) Airworthiness Limitations 
Items (ALI). Failure to inspect these structural components, 
according to the new threshold, could prevent a timely detection of 
fatigue cracking. These cracks, if not properly addressed, could 
adversely affect the structural integrity of the airplane.
* * * * *

Compliance

    (f) You are responsible for having the actions required by this 
AD performed within the compliance times specified, unless the 
actions have already been done.

Actions

    (g) Within 90 days after the effective date of this AD, do the 
following actions, as applicable.
    (1) For EMBRAER Model EMB-135ER, -135KE, -135KL, and -135LR 
airplanes, and Model EMB-145, -145EP, -145ER, -145LR, -145MP, and -
145MR airplanes: Revise the Airworthiness Limitations (ALS) of the 
Instructions for Continued Airworthiness (ICA) to incorporate Tasks 
54-50-00-230-802-A00 and 54-50-00-220-808-A01 specified in Appendix 
2, Airworthiness Limitation Requirements, of EMBRAER EMB135/EMB145 
Maintenance Review Board Report MRB-145/1150, Revision 12, dated 
September 19, 2008 (the ``MRBR''). The initial compliance times for 
the tasks start from the applicable threshold specified in Appendix 
2 of the MRBR, or within 500 flight cycles after the effective date 
of this AD, whichever occurs later.
    (2) For EMBRAER Model EMB-145EP, -145ER, -145LR, -145MR, and -
145MP airplanes: Revise the ALS of the ICA to incorporate Tasks 57-
26-00-250-815-A00, 57-26-00-250-815-A01, 57-26-00-250-813-A00, and 
57-26-00-250-813-A02, specified in Appendix 2, Airworthiness 
Limitation Requirements, of EMBRAER EMB135/EMB145 Maintenance Review 
Board Report MRB-145/1150, Revision 12, dated September 19, 2008 
(``the MRBR''). The initial compliance times for the tasks start 
from the later of the times specified in paragraph (g)(2)(i) or 
(g)(2)(ii) of this AD.
    (i) At the later of the applicable thresholds specified in 
Appendix 2 of the MRBR or within 500 flight cycles after the 
effective date of this AD, whichever occurs later.
    (ii) At the applicable time specified in Section A2.3.2.3.1, 
``Fatigue Threshold Reduced,'' of Appendix 2, Airworthiness 
Limitation Requirements, of the MRBR.
    (3) For all airplanes: Revise the ALS of the ICA to incorporate 
Tasks 57-10-00-250-801-A00 and 57-10-00-250-801-A01 specified in 
EMBRAER Temporary Revision 12-1, dated November 27, 2008, to the 
EMBRAER EMB135/EMB145 Maintenance Review Board Report MRB-145/1150, 
Revision 12, dated September 19, 2008. The initial compliance times 
for the tasks start at the times specified in paragraphs (g)(3)(i) 
and (g)(3)(ii) of this AD, as applicable.
    (i) For Task 57-10-00-250-801-A00: Prior to the accumulation of 
23,600 total flight cycles, or within 500 flight cycles after the 
effective date of this AD, whichever occurs later.
    (ii) For Task 57-10-00-250-801-A01: Within 24,000 flight cycles 
after accomplishing EMBRAER Service Bulletin 145-57-0047, dated 
October 18, 2008, or within 500 flight cycles after the effective 
date of this AD, whichever occurs later.
    (h) After accomplishing the actions specified in paragraph (g) 
of this AD, no alternative inspections, inspection intervals, or 
airworthiness limitations may be used unless the inspections, 
inspection intervals, or airworthiness limitations are approved as 
alternative method of compliance in accordance with the procedures 
specified in paragraph (i) of this AD.

FAA AD Differences

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

Other FAA AD Provisions

    (i) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Branch, ANM-116, Transport Airplane Directorate 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: Todd 
Thompson, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, 
Washington 98057-3356; telephone (425) 227-1175; fax (425) 227-1149. 
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

    (j) Refer to MCAI Brazilian Airworthiness Directive 2009-05-02, 
effective June 1, 2009; EMBRAER Temporary Revision 12-1, dated 
November 27, 2008, to the EMBRAER EMB135/EMB145 Maintenance Review 
Board Report MRB-145/1150, Revision 12, dated September 19, 2008; 
and Tasks 54-50-00-230-802-A00, 54-50-00-220-808-A01, 57-26-00-250-
815-A00, 57-26-00-250-815-A01, 57-26-00-250-813-A00, and 57-26-00-
250-813-A02, specified in Appendix 2, Airworthiness Limitation 
Requirements, of EMBRAER EMB135/EMB145 Maintenance Review Board 
Report MRB-145/1150, Revision 12, dated September 19, 2008; for 
related information.

Material Incorporated by Reference

    (k) You must use EMBRAER Temporary Revision 12-1, dated November 
27, 2008, to the EMBRAER EMB135/EMB145 Maintenance Review Board 
Report MRB-145/1150; and the specified tasks in Appendix 2, 
Airworthiness Limitation Requirements, of EMBRAER EMB135/EMB145 
Maintenance Review Board Report MRB-145/1150, Revision 12, dated 
September 19, 2008; 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 
Empresa Brasileira de Aeronautica S.A. (EMBRAER), Technical 
Publications Section (PC 060), Av. Brigadeiro Faria Lima, 2170--
Putim--12227-901 S[atilde]o Jose dos Campos--SP--BRASIL; telephone: 
+55 12 3927-5852 or +55 12 3309-0732; fax: +55 12 3927-7546; e-mail: 
distrib@embraer.com.br; Internet: http://www.flyembraer.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.
    (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/
ibr_locations.html.

    Issued in Renton, Washington, on May 25, 2010.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.

[FR Doc. 2010-13429 Filed 6-16-10; 8:45 am]
BILLING CODE 4910-13-P

