AD 2007-12-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Embraer | EMB-135 | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 Airplanes and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes |
Unsafe Condition
Metallic tubes enclosing the vent and pilot valve wires in the left- and right-hand wing fuel tanks could create an ignition source inside the fuel tank, igniting fuel vapor and causing a fuel tank explosion and loss of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the metallic tubes enclosing the vent and pilot valve wires in the left- and right-hand wing fuel tanks with new, improved, non-conductive hoses, in accordance with the Accomplishment Instructions of the specified service bulletins.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 5,000 flight hours or 48 months after the effective date of this AD, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
EMBRAER Model EMB-135ER, -135KE, -135KL, -135LR, -145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes, as identified in EMBRAER Service Bulletin 145-28-0023, Revision 07, dated February 7, 2007; and Model EMB-135BJ airplanes, as identified in EMBRAER Service Bulletin 145LEG-28-0018, Revision 01, dated April 20, 2005.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
The FAA is adopting a new airworthiness directive (AD) for certain EMBRAER Model EMB-135 airplanes and Model EMB-145, -145ER, - 145MR, -145LR, -145XR, -145MP, and -145EP airplanes. This AD requires replacing the metallic tubes enclosing the vent and pilot valve wires in the left- and right-hand wing fuel tanks with non-conductive hoses. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent an ignition source inside the fuel tank that could ignite fuel vapor and cause a fuel tank explosion and loss of the airplane.
Document Text
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[Federal Register Volume 72, Number 114 (Thursday, June 14, 2007)]
[Rules and Regulations]
[Pages 32780-32782]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: E7-11204]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-26354; Directorate Identifier 2006-NM-196-AD;
Amendment 39-15095; AD 2007-12-17]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB-135 Airplanes and Model EMB-145, -145ER, -145MR, -
145LR, -145XR, -145MP, and -145EP Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain EMBRAER Model EMB-135 airplanes and Model EMB-145, -145ER, -
145MR, -145LR, -145XR, -145MP, and -145EP airplanes. This AD requires
replacing the metallic tubes enclosing the vent and pilot valve wires
in the left- and right-hand wing fuel tanks with non-conductive hoses.
This AD results from fuel system reviews conducted by the manufacturer.
We are issuing this AD to prevent an ignition source inside the fuel
tank that could ignite fuel vapor and cause a fuel tank explosion and
loss of the airplane.
DATES: This AD becomes effective July 19, 2007.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of July 19, 2007.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a> or in person at the Docket Management Facility, U.S.
Department
[[Page 32781]]
of Transportation, 400 Seventh Street SW., Nassif Building, Room PL-
401, Washington, DC.
Contact Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box
343--CEP 12.225, Sao Jose dos Campos--SP, Brazil, for service
information identified in this AD.
FOR FURTHER INFORMATION CONTACT: Tom Groves, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
227-1503; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the AD docket on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a>
or in person at the Docket Management Facility office between 9 a.m.
and 5 p.m., Monday through Friday, except Federal holidays. The Docket
Management Facility office (telephone (800) 647-5527) is located on the
plaza level of the Nassif Building at the street address stated in the
ADDRESSES section.
Discussion
The FAA issued a supplemental notice of proposed rulemaking (NPRM)
to amend 14 CFR part 39 to include an AD that would apply to certain
EMBRAER Model EMB-135 airplanes and Model EMB-145, -145ER, -145MR, -
145LR, -145XR, -145MP, and -145EP airplanes. That supplemental NPRM was
published in the Federal Register on March 30, 2007 (72 FR 15075). That
supplemental NPRM proposed to require replacing the metallic tubes
enclosing the vent and pilot valve wires in the left- and right-hand
wing fuel tanks with non-conductive hoses. That supplemental NPRM also
proposed to add airplanes to the applicability.
Comments
We provided the public the opportunity to participate in the
development of this AD. No comments have been received on the
supplemental NPRM or on the determination of the cost to the public.
Clarification of Alternative Method of Compliance (AMOC) Paragraph
We have revised this action to clarify the appropriate procedure
for notifying the principal inspector before using any approved AMOC on
any airplane to which the AMOC applies.
Conclusion
We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD with the
change described previously. We have determined that this change will
neither increase the economic burden on any operator nor increase the
scope of the AD.
Costs of Compliance
This AD affects about 623 airplanes of U.S. registry. The required
actions take about 1 work hour per airplane, at an average labor rate
of $80 per work hour. Required parts cost about $1,121 (for each of 30
Model EMB-135BJ airplanes) or $1,788 (for each of 593 remaining
airplanes). The estimated cost of the AD per airplane is $1,201 or
$1,868. Based on these figures, the estimated cost of the AD for U.S.
operators is $1,143,754.
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 have 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 that 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. See the ADDRESSES
section for a location to examine the regulatory evaluation.
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 Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2007-12-17 Empresa Brasileira de Aeronautica S.A. (EMBRAER):
Amendment 39-15095. Docket No. FAA-2006-26354; Directorate
Identifier 2006-NM-196-AD.
Effective Date
(a) This AD becomes effective July 19, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to the following airplanes, certificated in
any category; as described in paragraphs (c)(1) and (c)(2) of this
AD.
(1) EMBRAER Model EMB-135ER, -135KE, -135KL, and -135LR
airplanes and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP,
and -145EP airplanes; as identified in EMBRAER Service Bulletin 145-
28-0023, Revision 07, dated February 7, 2007.
(2) EMBRAER Model EMB-135BJ airplanes, as identified in EMBRAER
Service Bulletin 145LEG-28-0018, Revision 01, dated April 20, 2005.
Unsafe Condition
(d) This AD results from fuel system reviews conducted by the
manufacturer. We are issuing this AD to prevent an ignition source
inside the fuel tank that could ignite fuel vapor and cause a fuel
tank explosion and loss of 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.
Tube Replacement
(f) Within 5,000 flight hours or 48 months after the effective
date of this AD, whichever occurs first: Replace the metallic tubes
[[Page 32782]]
enclosing the vent and pilot valve wires in the left- and right-hand
wing fuel tanks with new, improved, non-conductive hoses, in
accordance with the Accomplishment Instructions of the service
bulletin specified in paragraph (f)(1) or (f)(2) of this AD, as
applicable.
(1) For Model EMB-135ER, -135KE, -135KL, -135LR, -145, -145ER, -
145MR, -145LR, -145XR, -145MP, and -145EP airplanes: EMBRAER Service
Bulletin 145-28-0023, Revision 07, dated February 7, 2007.
(2) For Model EMB-135BJ airplanes: EMBRAER Service Bulletin
145LEG-28-0018, Revision 01, dated April 20, 2005.
Credit for Actions Done Using Previous Service Information
(g) Actions accomplished before the effective date of this AD in
accordance with the service information specified in Table 1 of this
AD are considered acceptable for compliance with the corresponding
actions specified in this AD.
Table 1.--Acceptable EMBRAER Service Information
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Service bulletin Revision level Date
----------------------------------------------------------------------------------------------------------------
145-28-0023............................. Original....................... April 19, 2004.
145-28-0023............................. 01............................. June 9, 2004.
145-28-0023............................. 02............................. November 8, 2004.
145-28-0023............................. 03............................. April 27, 2005.
145-28-0023............................. 04............................. November 7, 2005.
145-28-0023............................. 05............................. May 15, 2006.
145-28-0023............................. 06............................. October 31, 2006.
145LEG-28-0018.......................... Original....................... April 23, 2004.
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Alternative Methods of Compliance (AMOCs)
(h)(1) The Manager, ANM-116, International Branch, 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
(i) Brazilian airworthiness directive 2006-06-02, effective June
28, 2006, also addresses the subject of this AD.
Material Incorporated by Reference
(j)(1) You must use EMBRAER Service Bulletin 145-28-0023,
Revision 07, dated February 7, 2007; or EMBRAER Service Bulletin
145LEG-28-0018, Revision 01, dated April 20, 2005; as applicable, to
perform the actions that are required by this AD, unless the AD
specifies otherwise.
(2) EMBRAER Service Bulletin 145LEG-28-0018, Revision 01, dated
April 20, 2005, contains the following effective pages:
------------------------------------------------------------------------
Revision level shown
Page number on page Date shown on page
------------------------------------------------------------------------
1, 2........................ 01.................. April 20, 2005.
3-20........................ Original............ April 23, 2004.
------------------------------------------------------------------------
(Page 2 of EMBRAER Service Bulletin 145LEG-28-0018, Revision 01,
dated April 20, 2005, incorrectly shows a revision date of April 20,
2004; that date should be April 20, 2005.)
(3) The Director of the Federal Register approved the
incorporation by reference of these documents in accordance with 5
U.S.C. 552(a) and 1 CFR part 51. Contact Empresa Brasileira de
Aeronautica S.A. (EMBRAER), P.O. Box 343-CEP 12.225, Sao Jose dos
Campos--SP, Brazil, 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: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued in Renton, Washington, on June 1, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-11204 Filed 6-13-07; 8:45 am]
BILLING CODE 4910-13-P
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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