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[Federal Register Volume 76, Number 3 (Wednesday, January 5, 2011)]
[Rules and Regulations]
[Pages 444-446]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-32809]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-1023 Directorate Identifier 2010-CE-055-AD; 
Amendment 39-16557; AD 2011-01-04]
RIN 2120-AA64

Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. 
(EMBRAER) Model EMB-500 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) issued 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:

    It has been detected a short circuit in harness W101 due to its 
interference with the main door mechanism. Further analysis of the 
affected region has also revealed the possibility of chafing between 
the same harness and the oxygen tubing. The chafing of the wiring 
harness against the oxygen tubing could lead to a short circuit of 
the wiring harness and a subsequent fire in the airplane.
    Since this condition may occur in other airplanes of the same 
type and affects flight safety, a corrective action is required. 
Thus, sufficient reason exists to request compliance with this AD in 
the indicated time limit.

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

DATES: This AD becomes effective February 9, 2011.
    On February 9, 2011, the Director of the Federal Register approved 
the incorporation by reference of certain publications listed in this 
AD.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at Document Management Facility, U.S. 
Department of Transportation, Docket Operations, M-30, West Building 
Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 
20590.
    For service information identified in this AD, contact EMBRAER 
Empresa Brasileira de Aeron[aacute]utica S.A., Phenom Maintenance 
Support, Av. Brig. Farina Lima, 2170, Sao Jose dos Campos--SP, CEP: 
12227-901--PO Box: 38/2, BRASIL, telephone: ++55 12 3927-5383; fax: 
++55 12 3927-2610; E-mail: reliability.executive@embraer.com.br; 
Internet: http://www.embraer.com.br. You may review copies of the 
referenced service information at the FAA, Small Airplane Directorate, 
901 Locust, Kansas City, Missouri 64106. For information on the 
availability of this material at the FAA, call 816-329-4148.

FOR FURTHER INFORMATION CONTACT: Jim Rutherford, Aerospace Engineer, 
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4165; fax: (816) 329-4090.

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 October 15, 2010 (75 
FR 63422). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states:

    It has been detected a short circuit in harness W101 due to its 
interference with the main door mechanism. Further analysis of the 
affected region has also revealed the possibility of chafing between 
the same harness and the oxygen tubing. The chafing of the wiring 
harness against the oxygen tubing could lead to a short circuit of 
the wiring harness and a subsequent fire in the airplane.
    Since this condition may occur in other airplanes of the same 
type and affects flight safety, a corrective action is required. 
Thus, sufficient reason exists to request compliance with this AD in 
the indicated time limit.

The MCAI requires installing clamps to the W101 wiring harness.

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

[[Page 445]]

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 FAA policies. Any such differences are 
highlighted in a Note within the AD.

Costs of Compliance

    We estimate that this AD will affect 83 products of U.S. registry. 
We also estimate that it will take about 12 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 $13 per product.
    Based on these figures, we estimate the cost of this AD to the U.S. 
operators to be $85,739 or $1,033 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 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 Management Facility 
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 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:

2011-01-04 Empresa Brasileira de Aeronautica S.A. (EMBRAER): 
Amendment 39-16557; Docket No. FAA-2010-1023; Directorate Identifier 
2010-CE-055-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective February 
9, 2011.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Empresa Brasileira de Aeronautica S.A. 
(EMBRAER) Model EMB-500 airplanes, serial numbers 50000005 thru 
50000105, certificated in any category.

Subject

    (d) Air Transport Association of America (ATA) Code 92: Wiring 
Elements.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:
    It has been detected a short circuit in harness W101 due to its 
interference with the main door mechanism. Further analysis of the 
affected region has also revealed the possibility of chafing between 
the same harness and the oxygen tubing. The chafing of the wiring 
harness against the oxygen tubing could lead to a short circuit of 
the wiring harness and a subsequent fire in the airplane.
    Since this condition may occur in other airplanes of the same 
type and affects flight safety, a corrective action is required. 
Thus, sufficient reason exists to request compliance with this AD in 
the indicated time limit.

The MCAI requires installing clamps to the W101 wiring harness.

Actions and Compliance

    (f) Unless already done, within 600 hours time-in-service (TIS) 
after February 9, 2011 (the effective date of this AD) or within 12 
months after February 9, 2011 (the effective date of this AD), 
whichever comes first, install clamps and protection sleeves to 
harness W101 within the cockpit area and rework structures to 
eliminate the fretting spots of the harness with the main door 
locking mechanism and with the oxygen tube. Do the installation 
following Empresa Brasileira de Aeron[aacute]utica S.A. (EMBRAER) 
Service Bulletin No. SB 500-24-0002, dated March 8, 2010.

FAA AD Differences

    Note: 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, 
Standards Office, 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: Jim Rutherford, Aerospace Engineer, FAA, Small 
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 
64106; telephone: (816) 329-4165; fax: (816) 329-4090. Before using 
any approved AMOC on any airplane to which the AMOC applies, notify 
your appropriate principal inspector (PI) in the FAA Flight 
Standards District Office (FSDO), or lacking a PI, your local FSDO.
    (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, a federal agency may not conduct or sponsor, and a person 
is not required to respond to, nor shall a person be subject to a 
penalty for failure to comply with a collection of information 
subject to the requirements of the Paperwork Reduction Act unless 
that collection of information displays a current valid OMB Control 
Number. The OMB Control Number for this information collection is 
2120-0056. Public reporting for this collection of information is 
estimated to be approximately 5 minutes per response, including the 
time for reviewing instructions,

[[Page 446]]

completing and reviewing the collection of information. All 
responses to this collection of information are mandatory. Comments 
concerning the accuracy of this burden and suggestions for reducing 
the burden should be directed to the FAA at: 800 Independence Ave., 
SW., Washington, DC 20591, Attn: Information Collection Clearance 
Officer, AES-200.

Related Information

    (h) Refer to MCAI AG[Ecirc]NCIA NACIONAL DE 
AVIA[Ccedil][Atilde]O CIVIL--BRAZIL (ANAC), AD No.: 2010-09-02, 
dated October 17, 2010; and Empresa Brasileira de Aeron[aacute]utica 
S.A. (EMBRAER) Service Bulletin No. SB 500-24-0002, dated March 8, 
2010, for related information.

Material Incorporated by Reference

    (i) You must use Empresa Brasileira de Aeron[aacute]utica S.A. 
(EMBRAER) Service Bulletin No. SB 500-24-0002, dated March 8, 2010, 
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 
EMBRAER Empresa Brasileira de Aeron[aacute]utica S.A., Phenom 
Maintenance Support, Av. Brig. Farina Lima, 2170, Sao Jose dos 
Campos--SP, CEP: 12227-901--PO Box: 38/2, BRASIL, telephone: ++55 12 
3927-5383; fax: ++55 12 3927-2610; E-mail: 
reliability.executive@embraer.com.br; Internet: http://www.embraer.com.br.
    (3) You may review copies of the referenced service information 
at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, 
Missouri 64106. For information on the availability of this material 
at the FAA, call 816-329-4148.
    (4) You may also review copies of the service information 
incorporated by reference for this AD 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 Kansas City, Missouri, on December 21, 2010.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2010-32809 Filed 1-4-11; 8:45 am]
BILLING CODE 4910-13-P
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