Airworthiness Directives; EMBRAER Model EMB-135BJ Airplanes, 2797-2799 [E8-470]

Download as PDF Federal Register / Vol. 73, No. 11 / Wednesday, January 16, 2008 / Rules and Regulations in the event of wire damage, could lead to a short circuit and a possible ignition source, which could result in a fire in 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. Restatement of Requirements of AD 2004– 15–16 Modification (f) Within 4,000 flight hours after September 3, 2004 (the effective date of AD 2004–15–16): Modify the routing of wires in the RH wing by installing cable sleeves, per the Accomplishment Instructions of Airbus Service Bulletin A310–28–2148, Revision 01, dated October 29, 2002; or Revision 02, dated March 9, 2007. As of the effective date of this AD, Revision 02 must be used. Actions Accomplished Previously (g) Modification of the routing of wires accomplished before September 3, 2004, per Airbus Service Bulletin A310–28–2148, dated January 23, 2002, is acceptable for compliance with the corresponding requirements of paragraph (f) of this AD. New Requirements of This AD Modification (Additional Work) (h) For airplanes on which the actions specified in Airbus Service Bulletin A310– 28–2148, dated January 23, 2002; or Airbus Service Bulletin A310–28–2148, Revision 01, dated October 29, 2002; have been done before the effective date of this AD: Within 6,000 flight hours or 30 months after the effective date of this AD, whichever occurs first, perform further modification by installing additional protection sleeves in the outer wing area near the cadensicon sensor and segregating wire route 2S in the RH pylon area, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A310–28–2148, Revision 02, dated March 9, 2007. ebenthall on PRODPC61 with RULES Alternative Methods of Compliance (AMOCs) (i)(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) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. 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. Related Information (j) European Aviation Safety Agency airworthiness directive 2007–0230, dated August 15, 2007, also addresses the subject of this AD. Material Incorporated by Reference (k) You must use Airbus Service Bulletin A310–28–2148, Revision 01, dated October VerDate Aug<31>2005 15:01 Jan 15, 2008 Jkt 214001 2797 29, 2002; or Airbus Service Bulletin A310– 28–2148, Revision 02, dated March 9, 2007; as applicable, to perform the actions that are required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of Airbus Service Bulletin A310–28–2148, Revision 02, dated March 9, 2007, in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. (2) On September 3, 2004 (69 FR 45578, July 30, 2004), the Director of the Federal Register approved the incorporation by reference of Airbus Service Bulletin A310– 28–2148, Revision 01, dated October 29, 2002. (3) Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France, for a copy of this service information. You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or 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: https://www.archives.gov/federal-register/ cfr/ibr-locations.html. We are issuing this AD to require actions to correct the unsafe condition on these products. DATES: This AD becomes effective February 20, 2008. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of February 20, 2008. ADDRESSES: You may examine the AD docket on the Internet at https:// 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, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98057–3356; telephone (425) 227–1175; fax (425) 227–1149. SUPPLEMENTARY INFORMATION: Issued in Renton, Washington, on January 3, 2008. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8–370 Filed 1–15–08; 8:45 am] 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 1, 2007 (72 FR 61822). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states: BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2007–0129; Directorate Identifier 2007–NM–099–AD; Amendment 39–15331; AD 2008–02–01] RIN 2120–AA64 Airworthiness Directives; EMBRAER Model EMB–135BJ Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: 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: It has been found that some adhesive tapes used in the interior furnishings do not comply with the applicable flammability requirements. In case of some nearby ignition source, fire may propagate to the aircraft. PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 It has been found that some adhesive tapes used in the interior furnishings do not comply with the applicable flammability requirements. In case of some nearby ignition source, fire may propagate to the aircraft. The corrective actions include an inspection to determine the presence of cotton adhesive tape, and replacement of the tape with new tape if necessary. 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 E:\FR\FM\16JAR1.SGM 16JAR1 2798 Federal Register / Vol. 73, No. 11 / Wednesday, January 16, 2008 / Rules and Regulations 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 about 41 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 $80 per work-hour. Based on these figures, we estimate the cost of this AD to the U.S. operators to be $6,560, or $160 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. ebenthall on PRODPC61 with RULES 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 VerDate Aug<31>2005 15:01 Jan 15, 2008 Jkt 214001 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 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 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: I PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: I Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new AD: I 2008–02–01 Empresa Brasileira De Aeronautica S.A. (EMBRAER): Amendment 39–15331. Docket No. FAA–2007–0129; Directorate Identifier 2007–NM–099–AD. Effective Date (a) This airworthiness directive (AD) becomes effective February 20, 2008. Affected ADs (b) None. Applicability (c) This AD applies to EMBRAER Model EMB–135BJ airplanes, certificated in any category, as identified in EMBRAER Service Bulletin 145LEG–25–0080, dated October 10, 2006. Subject (d) Air Transport Association (ATA) of America Code 25: Equipment/Furnishings. Reason (e) The mandatory continuing airworthiness information (MCAI) states: It has been found that some adhesive tapes used in the interior furnishings do not comply with the applicable flammability PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 requirements. In case of some nearby ignition source, fire may propagate to the aircraft. The corrective actions include an inspection to determine the presence of cotton adhesive tape, and replacement of the tape with new tape if necessary. Actions and Compliance (f) Within 48 months or 5,000 flight hours after the effective date of this AD, whichever occurs first, unless already done: Carry out a general visual inspection (GVI) for presence of cotton adhesive tape, part number (P/N) FMM 1121–5, in the interior of centerpassenger cabin furnishings, in accordance with the Accomplishment Instructions of EMBRAER Service Bulletin 145LEG–25– 0080, dated October 10, 2006. If any cotton tape, P/N FMM 1121–5, is found, before further flight, replace it with new PVF adhesive tape bearing P/N KB42/75, as specified in paragraphs (f)(1) and (f)(2) of this AD. (1) Replace cotton adhesive tapes, P/N FMM 1121–5, located under the centerpassenger cabin carpet, with new PVF adhesive tapes bearing P/N KB42/75, in accordance with the Accomplishment Instructions of the service bulletin. (2) Replace cotton adhesive tapes, P/N FMM 1121–5, applied to electrical cables in the bottom of the forward galley assembly, to electrical cables and inside the left-hand (LH) and right-hand (RH) forward and LH aft side ledges, and to electrical cables, flexible hose of the video monitor, soundproofing blanket, and in the LH and RH forward and RH aft pocket door covers and partitions, with new PVF adhesive tapes bearing P/N KB42/75 with heat-shrinkable sleeve, P/N RNF–100– 1–0, in accordance with the Accomplishment Instructions of the service bulletin. Note 1: For the purpose of this AD, a general visual inspection (GVI) is: ‘‘A visual examination of the interior or exterior area of an installation or assembly to detect obvious damage, failure or irregularity. This level of inspection is made from within touching distance, unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight or drop-light, and may require removal or opening of access panels or doors. Stands, ladders or platforms may be required to gain proximity to the area being checked.’’ FAA AD Differences Note 2: 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, 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, E:\FR\FM\16JAR1.SGM 16JAR1 Federal Register / Vol. 73, No. 11 / Wednesday, January 16, 2008 / Rules and Regulations ANM–116, FAA, Transport Airplane Directorate, 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 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, under the provisions of the Paperwork Reduction Act, 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 Brazilian Airworthiness Directive 2007–03–04, effective April 10, 2007, and EMBRAER Service Bulletin 145LEG–25–0080, dated October 10, 2006, for related information. Material Incorporated by Reference (i) You must use EMBRAER Service Bulletin 145LEG–25–0080, dated October 10, 2006, 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), P.O. Box 343—CEP 12.225, Sao Jose dos Campos—SP, Brazil. (3) You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or 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: https:// www.archives.gov/federal-register/cfr/ibrlocations.html. Issued in Renton, Washington, on January 4, 2008. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8–470 Filed 1–15–08; 8:45 am] ebenthall on PRODPC61 with RULES BILLING CODE 4910–13–P VerDate Aug<31>2005 15:01 Jan 15, 2008 Jkt 214001 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2007–0082; Directorate Identifier 2007–NM–219–AD; Amendment 39–15332; AD 2008–02–02] RIN 2120–AA64 Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: 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: It has been found that the implementation of the Inertial Reference Units (IRU) on the ERJ–170 [and ERJ–190] may lead, in certain degraded modes, to an erroneous Flight Path Angle (FPA) indication on both Primary Flight Displays, with no alert to the flight crew. On the ERJ–170 [and ERJ–190], FPA is considered as important as pitch and bank angle for piloting purposes. The unsafe condition is reduced ability of the flightcrew to control the flight path of the airplane. We are issuing this AD to require actions to correct the unsafe condition on these products. DATES: This AD becomes effective February 20, 2008. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of February 20, 2008. ADDRESSES: You may examine the AD docket on the Internet at https:// 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: Sanjay Ralhan, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057–3356; telephone (425) 227–1405; fax (425) 227–1149. SUPPLEMENTARY INFORMATION: PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 2799 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 25, 2007 (72 FR 60599). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states: It has been found that the implementation of the Inertial Reference Units (IRU) on the ERJ–170 [and ERJ–190] may lead, in certain degraded modes, to an erroneous Flight Path Angle (FPA) indication on both Primary Flight Displays, with no alert to the flight crew. On the ERJ–170 [and ERJ–190], FPA is considered as important as pitch and bank angle for piloting purposes. The unsafe condition is reduced ability of the flightcrew to control the flight path of the airplane. The corrective action is removal of certain wiring connections in the electrical connectors of both IRUs. 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. Revision to Final Rule for New Service Information EMBRAER has issued a revision to a service bulletin identified in the NPRM as an appropriate source of service information for the AD. EMBRAER Service Bulletin 190–34–0009, Revision 01, dated October 9, 2007, incorporates an existing information notice that revises the wiring manual reference, and adds a serial number to the effectivity of the in-production airplanes that have an equivalent modification. We have changed paragraphs (c) and (f) of this AD accordingly, and added a statement in paragraph (f) giving credit for work performed in accordance with the original version of the service bulletin. Conclusion We reviewed the available data and determined that air safety and the public interest require adopting the AD with the changes described previously. We determined that these changes 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 E:\FR\FM\16JAR1.SGM 16JAR1

Agencies

[Federal Register Volume 73, Number 11 (Wednesday, January 16, 2008)]
[Rules and Regulations]
[Pages 2797-2799]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-470]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-0129; Directorate Identifier 2007-NM-099-AD; 
Amendment 39-15331; AD 2008-02-01]
RIN 2120-AA64


Airworthiness Directives; EMBRAER Model EMB-135BJ Airplanes

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:

    It has been found that some adhesive tapes used in the interior 
furnishings do not comply with the applicable flammability 
requirements. In case of some nearby ignition source, fire may 
propagate to the aircraft.

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

DATES: This AD becomes effective February 20, 2008.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of February 20, 
2008.

ADDRESSES: You may examine the AD docket on the Internet at https://
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, FAA, Transport Airplane Directorate, 
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 November 1, 2007 (72 
FR 61822). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states:

    It has been found that some adhesive tapes used in the interior 
furnishings do not comply with the applicable flammability 
requirements. In case of some nearby ignition source, fire may 
propagate to the aircraft.

The corrective actions include an inspection to determine the presence 
of cotton adhesive tape, and replacement of the tape with new tape if 
necessary. 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

[[Page 2798]]

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 about 41 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 $80 per work-hour. Based on these figures, we estimate 
the cost of this AD to the U.S. operators to be $6,560, or $160 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 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 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:

2008-02-01 Empresa Brasileira De Aeronautica S.A. (EMBRAER): 
Amendment 39-15331. Docket No. FAA-2007-0129; Directorate Identifier 
2007-NM-099-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective February 
20, 2008.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to EMBRAER Model EMB-135BJ airplanes, 
certificated in any category, as identified in EMBRAER Service 
Bulletin 145LEG-25-0080, dated October 10, 2006.

Subject

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

Reason

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

    It has been found that some adhesive tapes used in the interior 
furnishings do not comply with the applicable flammability 
requirements. In case of some nearby ignition source, fire may 
propagate to the aircraft.

The corrective actions include an inspection to determine the 
presence of cotton adhesive tape, and replacement of the tape with 
new tape if necessary.

Actions and Compliance

    (f) Within 48 months or 5,000 flight hours after the effective 
date of this AD, whichever occurs first, unless already done: Carry 
out a general visual inspection (GVI) for presence of cotton 
adhesive tape, part number (P/N) FMM 1121-5, in the interior of 
center-passenger cabin furnishings, in accordance with the 
Accomplishment Instructions of EMBRAER Service Bulletin 145LEG-25-
0080, dated October 10, 2006. If any cotton tape, P/N FMM 1121-5, is 
found, before further flight, replace it with new PVF adhesive tape 
bearing P/N KB42/75, as specified in paragraphs (f)(1) and (f)(2) of 
this AD.
    (1) Replace cotton adhesive tapes, P/N FMM 1121-5, located under 
the center-passenger cabin carpet, with new PVF adhesive tapes 
bearing P/N KB42/75, in accordance with the Accomplishment 
Instructions of the service bulletin.
    (2) Replace cotton adhesive tapes, P/N FMM 1121-5, applied to 
electrical cables in the bottom of the forward galley assembly, to 
electrical cables and inside the left-hand (LH) and right-hand (RH) 
forward and LH aft side ledges, and to electrical cables, flexible 
hose of the video monitor, soundproofing blanket, and in the LH and 
RH forward and RH aft pocket door covers and partitions, with new 
PVF adhesive tapes bearing P/N KB42/75 with heat-shrinkable sleeve, 
P/N RNF-100-1-0, in accordance with the Accomplishment Instructions 
of the service bulletin.

    Note 1: For the purpose of this AD, a general visual inspection 
(GVI) is: ``A visual examination of the interior or exterior area of 
an installation or assembly to detect obvious damage, failure or 
irregularity. This level of inspection is made from within touching 
distance, unless otherwise specified. A mirror may be necessary to 
enhance visual access to all exposed surfaces in the inspection 
area. This level of inspection is made under normally available 
lighting conditions such as daylight, hangar lighting, flashlight or 
drop-light, and may require removal or opening of access panels or 
doors. Stands, ladders or platforms may be required to gain 
proximity to the area being checked.''

FAA AD Differences

    Note 2: 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, 
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,

[[Page 2799]]

ANM-116, FAA, Transport Airplane Directorate, 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 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, under the provisions of the Paperwork Reduction Act, 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 Brazilian Airworthiness Directive 2007-03-04, 
effective April 10, 2007, and EMBRAER Service Bulletin 145LEG-25-
0080, dated October 10, 2006, for related information.

Material Incorporated by Reference

    (i) You must use EMBRAER Service Bulletin 145LEG-25-0080, dated 
October 10, 2006, 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), P.O. Box 343--CEP 
12.225, Sao Jose dos Campos--SP, Brazil.
    (3) You may review copies at the FAA, Transport Airplane 
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or 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: https://www.archives.gov/federal-register/cfr/ibr-
locations.html.

    Issued in Renton, Washington, on January 4, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E8-470 Filed 1-15-08; 8:45 am]
BILLING CODE 4910-13-P
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