Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 Airplanes; and Model ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-200 STD, ERJ 190-200 LR, and ERJ 190-200 IGW Airplanes, 7511-7513 [2011-2926]

Download as PDF 7511 Proposed Rules Federal Register Vol. 76, No. 28 Thursday, February 10, 2011 This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The purpose of these notices is to give interested persons an opportunity to participate in the rule making prior to the adoption of the final rules. DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2011–0038; Directorate Identifier 2010–NM–153–AD] RIN 2120–AA64 Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 Airplanes; and Model ERJ 190–100 STD, ERJ 190– 100 LR, ERJ 190–100 IGW, ERJ 190– 200 STD, ERJ 190–200 LR, and ERJ 190–200 IGW Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed 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: SUMMARY: [T]he occurrence of drill marks [has been found] at the lower ring region of the rear pressure bulkhead between [the] circumferential splice joint and rear skin located between stringers 12 and 13. These marks may result in formation of fatigue cracks accelerated by corrosion reducing the structural strength of the rear pressure bulkhead, which may cause a sudden decompression of the passenger cabin. jdjones on DSK8KYBLC1PROD with PROPOSALS-1 * * * * * The proposed AD would require actions that are intended to address the unsafe condition described in the MCAI. DATES: We must receive comments on this proposed AD by March 28, 2011. ADDRESSES: You may send comments by any of the following methods: • Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments. • Fax: (202) 493–2251. VerDate Mar<15>2010 14:39 Feb 09, 2011 Jkt 223001 • Mail: U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue, SE., Washington, DC 20590. • Hand Delivery: U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–40, 1200 New Jersey Avenue, SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this proposed AD, contact Empresa Brasileira de Aeronautica S.A. (EMBRAER), Technical Publications Section (PC 060), Av. Brigadeiro Faria ˜ Lima, 2170—Putim—12227–901 Sao 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 https://www.flyembraer.com. You may review copies of the referenced 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. Examining the AD Docket You may examine the AD docket on the Internet at https:// 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 this proposed AD, 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. FOR FURTHER INFORMATION CONTACT: Cindy Ashforth, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057–3356; telephone 425–227–2768; fax 425–227–1149. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include ‘‘Docket No. FAA–2011–0038; Directorate Identifier 2010–NM–153–AD’’ at the beginning of PO 00000 Frm 00001 Fmt 4702 Sfmt 4702 your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD based on those comments. We will post all comments we receive, without change, to https:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD. Discussion ˆ The Agencia Nacional de Aviacao ¸˜ Civil (ANAC), which is the aviation authority for Brazil, has issued Brazilian Airworthiness Directives 2010–06–01R1 and 2010–06–02R1, both dated August 25, 2010 (referred to after this as ‘‘the MCAI’’), to correct an unsafe condition for the specified products. The MCAI states: [T]he occurrence of drill marks [has been found] at the lower ring region of the rear pressure bulkhead between [the] circumferential splice joint and rear skin located between stringers 12 and 13. These marks may result in formation of fatigue cracks accelerated by corrosion reducing the structural strength of the rear pressure bulkhead, which may cause a sudden decompression of the passenger cabin. The required actions include doing a detailed inspection for signs of drill marks and repairing if necessary. You may obtain further information by examining the MCAI in the AD docket. Relevant Service Information EMBRAER has issued Service Bulletins 170–53–0082 and 190–53– 0042, both Revision 01, both dated April 28, 2010. The actions described in this service information are intended to correct the unsafe condition identified in the MCAI. FAA’s Determination and Requirements of This Proposed AD This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all pertinent information and determined an unsafe E:\FR\FM\10FEP1.SGM 10FEP1 7512 Federal Register / Vol. 76, No. 28 / Thursday, February 10, 2011 / Proposed Rules condition exists and is likely to exist or develop on other products of the same type design. 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 proposed 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 proposed AD. Costs of Compliance Based on the service information, we estimate that this proposed AD would affect about 241 products of U.S. registry. We also estimate that it would take about 1 work-hour per product to comply with the basic requirements of this proposed AD. The average labor rate is $85 per work-hour. Based on these figures, we estimate the cost of the proposed AD on U.S. operators to be $20,485, or $85 per product. In addition, we estimate that any necessary follow-on actions would take about 2 work-hours and require parts costing $20, for a cost of $190 per product. We have no way of determining the number of products that may need these actions. jdjones on DSK8KYBLC1PROD with PROPOSALS-1 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. 14:39 Feb 09, 2011 Jkt 223001 We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 proposed regulation: 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 proposed AD and placed it in the AD docket. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 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. Authority for This Rulemaking VerDate Mar<15>2010 Regulatory Findings § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new AD: Empresa Brasileira de Aeronautica S.A. (EMBRAER): Docket No. FAA–2011– 0038; Directorate Identifier 2010–NM– 153–AD. Comments Due Date (a) We must receive comments by March 28, 2011. Affected ADs (b) None. Applicability (c) This AD applies to Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170–100 LR, –100 STD, –100 SE, and –100 SU airplanes; and Model ERJ 170–200 LR, –200 SU, and –200 STD airplanes; certificated in any category; serial numbers 17000002, 17000004 through 17000013 inclusive, 17000015 through 17000212 inclusive, 17000216 through 17000233 PO 00000 Frm 00002 Fmt 4702 Sfmt 4702 inclusive, 17000236, 17000269, 17000281 through 17000291 inclusive, and 17000293; and Model ERJ 190–100 STD, ERJ 190–100 LR, ERJ 190–100 IGW, ERJ 190–200 STD, ERJ 190–200 LR, and ERJ 190–200 IGW airplanes; certificated in any category; serial numbers 19000002, 19000004, 19000006 through 19000108 inclusive, 19000110 through 19000139 inclusive, 19000141 through 19000157 inclusive, 19000160, 19000165, 19000167 through 19000176 inclusive, 19000178 through 19000199 inclusive, 19000273 through 19000276 inclusive, 19000279 through 19000286 inclusive, 19000288 through 19000295 inclusive, 19000297 through 19000304 inclusive, and 19000309. Subject (d) Air Transport Association (ATA) of America Code 53: Fuselage. Reason (e) The mandatory continuing airworthiness information (MCAI) states: [T]he occurrence of drill marks [has been found] at the lower ring region of the rear pressure bulkhead between [the] circumferential splice joint and rear skin located between stringers 12 and 13. These marks may result in formation of fatigue cracks accelerated by corrosion reducing the structural strength of the rear pressure bulkhead, which may cause a sudden decompression of the passenger cabin. * * * * * 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) Before the accumulation of 20,000 flight cycles, do a detailed inspection for signs of drill marks at the left and right lower ring region of the rear pressure bulkhead between the circumferential splice joint and rear skin between stringers 12 and 13, in accordance with EMBRAER Service Bulletin 170–53– 0082 or 190–53–0042, both Revision 01, both dated April 28, 2010, as applicable. If drill marks are found, repair before further flight, in accordance with EMBRAER Service Bulletin 170–53–0082 or 190–53–0042, both Revision 01, both dated April 28, 2010, as applicable. Note 1: For the purposes of this AD, a detailed inspection is: ‘‘An intensive examination of a specific item, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirror, magnifying lenses, etc., may be necessary. Surface cleaning and elaborate procedures may be required.’’ FAA AD Differences Note 2: This AD differs from the MCAI and/or service information as follows: Although EMBRAER Service Bulletins 170– 53–0082 and 190–53–0042, both Revision 01, both dated April 28, 2010, specify doing a E:\FR\FM\10FEP1.SGM 10FEP1 Federal Register / Vol. 76, No. 28 / Thursday, February 10, 2011 / Proposed Rules jdjones on DSK8KYBLC1PROD with PROPOSALS-1 general visual inspection, this AD requires doing a detailed inspection. products listed above. This proposed AD would require a general visual inspection for cracks and holes of the Other FAA AD Provisions main equipment center (MEC) drip (h) The following provisions also apply to shields, and repairs if necessary; this AD: installation of a fiberglass reinforcing (1) Alternative Methods of Compliance overcoat; and, for certain airplanes, (AMOCs): The Manager, International installation of stiffening panels to the Branch, ANM–116, Transport Airplane MEC drip shields. This proposed AD Directorate, FAA, has the authority to was prompted by a report of a loss of approve AMOCs for this AD, if requested bus control unit number 1 and generator using the procedures found in 14 CFR 39.19. Send information to ATTN: Cindy Ashforth, control units numbers 1 and 2 while the Aerospace Engineer, International Branch, airplane was on the ground, and ANM–116, Transport Airplane Directorate, multiple operator reports of cracked FAA, 1601 Lind Avenue, SW., Renton, MEC drip shields. We are proposing this Washington 98057–3356; telephone 425– AD to prevent water penetration into the 227–2768; fax 425–227–1149. Information MEC, which could result in the loss of may be e-mailed to: 9-ANM-116-AMOCflight critical systems. REQUESTS@faa.gov. Before using any DATES: We must receive comments on approved AMOC, notify your appropriate principal inspector, or lacking a principal this proposed AD by March 28, 2011. inspector, the manager of the local flight ADDRESSES: You may send comments by standards district office/certificate holding any of the following methods: district office. The AMOC approval letter • Federal eRulemaking Portal: Go to must specifically reference this AD. https://www.regulations.gov. Follow the (2) Airworthy Product: For any instructions for submitting comments. requirement in this AD to obtain corrective • Fax: 202–493–2251. actions from a manufacturer or other source, • Mail: U.S. Department of use these actions if they are FAA-approved. Transportation, Docket Operations, Corrective actions are considered FAAM–30, West Building Ground Floor, approved if they are approved by the State Room W12–140, 1200 New Jersey of Design Authority (or their delegated agent). You are required to assure the product Avenue, SE., Washington, DC 20590. is airworthy before it is returned to service. • Hand Delivery: Deliver to Mail address above between 9 a.m. and Related Information 5 p.m., Monday through Friday, except (i) Refer to MCAI Brazilian Airworthiness Federal holidays. Directives 2010–06–01R1 and 2010–06–02R1, For service information identified in both dated August 25, 2010; and EMBRAER this proposed AD, contact Boeing Service Bulletins 170–53–0082 and 190–53– Commercial Airplanes, Attention: Data 0042, both Revision 01, both dated April 28, & Services Management, P.O. Box 3707, 2010; for related information. MC 2H–65, Seattle, Washington 98124– Issued in Renton, Washington, on February 2207; telephone 206–544–5000, 3, 2011. extension 1; fax 206–766–5680; e-mail Ali Bahrami, me.boecom@boeing.com; Internet Manager, Transport Airplane Directorate, https://www.myboeingfleet.com. You Aircraft Certification Service. may review copies of the referenced [FR Doc. 2011–2926 Filed 2–9–11; 8:45 am] service information at the FAA, BILLING CODE 4910–13–P Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of DEPARTMENT OF TRANSPORTATION this material at the FAA, call 425–227– 1221. Federal Aviation Administration Examining the AD Docket 14 CFR Part 39 You may examine the AD docket on the Internet at https:// [Docket No. FAA–2011–0041; Directorate www.regulations.gov; or in person at the Identifier 2010–NM–227–AD] Docket Management Facility between RIN 2120–AA64 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD Airworthiness Directives; The Boeing docket contains this proposed AD, the Company Model 747–400 and –400F regulatory evaluation, any comments Series Airplanes received, and other information. The street address for the Docket Office AGENCY: Federal Aviation (phone: 800–647–5527) is in the Administration (FAA), DOT. ADDRESSES section. Comments will be ACTION: Notice of proposed rulemaking available in the AD docket shortly after (NPRM). receipt. FOR FURTHER INFORMATION CONTACT: SUMMARY: We propose to adopt a new Marcia Smith, Aerospace Engineer, airworthiness directive (AD) for the VerDate Mar<15>2010 14:39 Feb 09, 2011 Jkt 223001 PO 00000 Frm 00003 Fmt 4702 Sfmt 4702 7513 Cabin Safety & Environmental Systems Branch, ANM–150S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue, SW., Renton, Washington 98057–3356; phone: 425–917–6484; fax: 425–917–6590; e-mail: marcia.smith@faa.gov. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under the ADDRESSES section. Include ‘‘Docket No. FAA– 2011–0041; Directorate Identifier 2010– NM–227–AD’’ at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD because of those comments. We will post all comments we receive, without change, to https:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD. Discussion We have received a report of a loss of bus control unit number 1 and generator control units numbers 1 and 2 while the airplane was on the ground, and multiple operators have reported cracked main equipment center (MEC) drip shields. Cracking in the MEC drip shield and exhaust plenum has been identified as part of the water leak path into the MEC. This condition, if not corrected, could result in water penetration into the MEC, which could result in the loss of flight critical systems. Relevant Service Information We reviewed Boeing Alert Service Bulletin 747–25A3588, dated July 19, 2010. The service information describes procedures for performing a general visual inspection of the MEC drip shield for cracks and holes, performing repairs if necessary, and installing a fiberglass reinforcing overcoat to the MEC drip shield. Additionally, for airplanes identified as Groups 1 and 3, the service information describes procedures for installing MEC drip shield panel stiffeners. FAA’s Determination We are proposing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or E:\FR\FM\10FEP1.SGM 10FEP1

Agencies

[Federal Register Volume 76, Number 28 (Thursday, February 10, 2011)]
[Proposed Rules]
[Pages 7511-7513]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2011-2926]


========================================================================
Proposed Rules
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains notices to the public of 
the proposed issuance of rules and regulations. The purpose of these 
notices is to give interested persons an opportunity to participate in 
the rule making prior to the adoption of the final rules.

========================================================================


Federal Register / Vol. 76, No. 28 / Thursday, February 10, 2011 / 
Proposed Rules

[[Page 7511]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-0038; Directorate Identifier 2010-NM-153-AD]
RIN 2120-AA64


Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. 
(EMBRAER) Model ERJ 170 Airplanes; and Model ERJ 190-100 STD, ERJ 190-
100 LR, ERJ 190-100 IGW, ERJ 190-200 STD, ERJ 190-200 LR, and ERJ 190-
200 IGW Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: We propose to adopt a new airworthiness directive (AD) for the 
products listed above. This proposed 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:

    [T]he occurrence of drill marks [has been found] at the lower 
ring region of the rear pressure bulkhead between [the] 
circumferential splice joint and rear skin located between stringers 
12 and 13. These marks may result in formation of fatigue cracks 
accelerated by corrosion reducing the structural strength of the 
rear pressure bulkhead, which may cause a sudden decompression of 
the passenger cabin.
* * * * *
    The proposed AD would require actions that are intended to address 
the unsafe condition described in the MCAI.

DATES: We must receive comments on this proposed AD by March 28, 2011.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: (202) 493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue, SE., Washington, DC 20590.
     Hand Delivery: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-40, 1200 New 
Jersey Avenue, SE., Washington, DC, between 9 a.m. and 5 p.m., Monday 
through Friday, except Federal holidays.
    For service information identified in this proposed 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 https://www.flyembraer.com. You may 
review copies of the referenced 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.

Examining the AD Docket

    You may examine the AD docket on the Internet at https://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 this proposed AD, 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.

FOR FURTHER INFORMATION CONTACT: Cindy Ashforth, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone 425-
227-2768; fax 425-227-1149.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposed AD. Send your comments to an address 
listed under the ADDRESSES section. Include ``Docket No. FAA-2011-0038; 
Directorate Identifier 2010-NM-153-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this proposed AD. We 
will consider all comments received by the closing date and may amend 
this proposed AD based on those comments.
    We will post all comments we receive, without change, to https://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this proposed AD.

Discussion

    The Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC), 
which is the aviation authority for Brazil, has issued Brazilian 
Airworthiness Directives 2010-06-01R1 and 2010-06-02R1, both dated 
August 25, 2010 (referred to after this as ``the MCAI''), to correct an 
unsafe condition for the specified products. The MCAI states:

    [T]he occurrence of drill marks [has been found] at the lower 
ring region of the rear pressure bulkhead between [the] 
circumferential splice joint and rear skin located between stringers 
12 and 13. These marks may result in formation of fatigue cracks 
accelerated by corrosion reducing the structural strength of the 
rear pressure bulkhead, which may cause a sudden decompression of 
the passenger cabin.

    The required actions include doing a detailed inspection for signs 
of drill marks and repairing if necessary. You may obtain further 
information by examining the MCAI in the AD docket.

Relevant Service Information

    EMBRAER has issued Service Bulletins 170-53-0082 and 190-53-0042, 
both Revision 01, both dated April 28, 2010. The actions described in 
this service information are intended to correct the unsafe condition 
identified in the MCAI.

FAA's Determination and Requirements of This Proposed AD

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to our bilateral agreement with the State of Design Authority, we have 
been notified of the unsafe condition described in the MCAI and service 
information referenced above. We are proposing this AD because we 
evaluated all pertinent information and determined an unsafe

[[Page 7512]]

condition exists and is likely to exist or develop on other products of 
the same type design.

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 proposed 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 proposed AD.

Costs of Compliance

    Based on the service information, we estimate that this proposed AD 
would affect about 241 products of U.S. registry. We also estimate that 
it would take about 1 work-hour per product to comply with the basic 
requirements of this proposed AD. The average labor rate is $85 per 
work-hour. Based on these figures, we estimate the cost of the proposed 
AD on U.S. operators to be $20,485, or $85 per product.
    In addition, we estimate that any necessary follow-on actions would 
take about 2 work-hours and require parts costing $20, for a cost of 
$190 per product. We have no way of determining the number of products 
that may need these actions.

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 proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 proposed 
regulation:
    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 proposed AD and placed it in the AD docket.

List of Subjects in 14 CFR Part 39

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

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 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:

Empresa Brasileira de Aeronautica S.A. (EMBRAER): Docket No. FAA-
2011-0038; Directorate Identifier 2010-NM-153-AD.

Comments Due Date

    (a) We must receive comments by March 28, 2011.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Empresa Brasileira de Aeronautica S.A. 
(EMBRAER) Model ERJ 170-100 LR, -100 STD, -100 SE, and -100 SU 
airplanes; and Model ERJ 170-200 LR, -200 SU, and -200 STD 
airplanes; certificated in any category; serial numbers 17000002, 
17000004 through 17000013 inclusive, 17000015 through 17000212 
inclusive, 17000216 through 17000233 inclusive, 17000236, 17000269, 
17000281 through 17000291 inclusive, and 17000293; and Model ERJ 
190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-200 STD, ERJ 
190-200 LR, and ERJ 190-200 IGW airplanes; certificated in any 
category; serial numbers 19000002, 19000004, 19000006 through 
19000108 inclusive, 19000110 through 19000139 inclusive, 19000141 
through 19000157 inclusive, 19000160, 19000165, 19000167 through 
19000176 inclusive, 19000178 through 19000199 inclusive, 19000273 
through 19000276 inclusive, 19000279 through 19000286 inclusive, 
19000288 through 19000295 inclusive, 19000297 through 19000304 
inclusive, and 19000309.

Subject

    (d) Air Transport Association (ATA) of America Code 53: 
Fuselage.

Reason

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

    [T]he occurrence of drill marks [has been found] at the lower 
ring region of the rear pressure bulkhead between [the] 
circumferential splice joint and rear skin located between stringers 
12 and 13. These marks may result in formation of fatigue cracks 
accelerated by corrosion reducing the structural strength of the 
rear pressure bulkhead, which may cause a sudden decompression of 
the passenger cabin.
* * * * *

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) Before the accumulation of 20,000 flight cycles, do a 
detailed inspection for signs of drill marks at the left and right 
lower ring region of the rear pressure bulkhead between the 
circumferential splice joint and rear skin between stringers 12 and 
13, in accordance with EMBRAER Service Bulletin 170-53-0082 or 190-
53-0042, both Revision 01, both dated April 28, 2010, as applicable. 
If drill marks are found, repair before further flight, in 
accordance with EMBRAER Service Bulletin 170-53-0082 or 190-53-0042, 
both Revision 01, both dated April 28, 2010, as applicable.

    Note 1:  For the purposes of this AD, a detailed inspection is: 
``An intensive examination of a specific item, installation, or 
assembly to detect damage, failure, or irregularity. Available 
lighting is normally supplemented with a direct source of good 
lighting at an intensity deemed appropriate. Inspection aids such as 
mirror, magnifying lenses, etc., may be necessary. Surface cleaning 
and elaborate procedures may be required.''

FAA AD Differences

    Note 2:  This AD differs from the MCAI and/or service 
information as follows: Although EMBRAER Service Bulletins 170-53-
0082 and 190-53-0042, both Revision 01, both dated April 28, 2010, 
specify doing a

[[Page 7513]]

general visual inspection, this AD requires doing a detailed 
inspection.

Other FAA AD Provisions

    (h) 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: 
Cindy Ashforth, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, 
Washington 98057-3356; telephone 425-227-2768; fax 425-227-1149. 
Information may be e-mailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. 
Before using any approved AMOC, notify your appropriate principal 
inspector, or lacking a principal inspector, the manager of the 
local flight standards district office/certificate holding 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.

Related Information

    (i) Refer to MCAI Brazilian Airworthiness Directives 2010-06-
01R1 and 2010-06-02R1, both dated August 25, 2010; and EMBRAER 
Service Bulletins 170-53-0082 and 190-53-0042, both Revision 01, 
both dated April 28, 2010; for related information.

    Issued in Renton, Washington, on February 3, 2011.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2011-2926 Filed 2-9-11; 8:45 am]
BILLING CODE 4910-13-P

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