AD 2007-12-17

Historical

Airworthiness directive · Metallic tubes enclosing the vent and pilot valve wires · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more

Effective
July 19, 2007
Published
June 14, 2007 · 72 FR 32780–32782
Issued
June 1, 2007
Superseded by
AD2008-17-05
Models
EMB-135BJ, EMB-135ER, EMB-135KE, EMB-135KL, EMB-135LR, EMB-145 and 6 more
Data sheet
TCDST00011AT
Registered aircraft
431 matched by model
Product
Aircraft · Large airplane
Amendment
39-15095
Docket
FAA-2006-26354
Project
2006-NM-196-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document E7-11204. Only the govinfo PDF is the legal edition. DRS record last changed August 7, 2025.

On this page

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.

The airworthiness directive

2007-12-17 Empresa Brasileira de Aeronautica S.A. (EMBRAER): Amendment 39-15095. Docket No. FAA-2006-26354; Directorate Identifier 2006-NM-196-AD.

(a) Effective Date

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(a) This AD becomes effective July 19, 2007.

(b) Affected ADs

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(b) None.

(c) Applicability

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(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.

(d) Unsafe Condition

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(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.

(e) Compliance

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(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.

(f) Tube Replacement

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(f) Within 5,000 flight hours or 48 months after the effective date of this AD, whichever occurs first: 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 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.

(g) Credit for Actions Done Using Previous Service Information

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(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
Service bulletinRevision levelDate
145-28-0023OriginalApril 19, 2004.
145-28-002301June 9, 2004.
145-28-002302November 8, 2004.
145-28-002303April 27, 2005.
145-28-002304November 7, 2005.
145-28-002305May 15, 2006.
145-28-002306October 31, 2006.
145LEG-28-0018OriginalApril 23, 2004.

(h) Alternative Methods of Compliance (AMOCs)

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(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.

(i) Related Information

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(i) Brazilian airworthiness directive 2006-06-02, effective June 28, 2006, also addresses the subject of this AD.

(j) Material Incorporated by Reference

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(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:

Page numberRevision level shown on pageDate shown on page
1, 201April 20, 2005.
3-20OriginalApril 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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

DatesPage 1

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.

AddressesPage 1

You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility, U.S. Department 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 contactPage 2

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.

Examining the DocketPage 2

You may examine the AD docket on the Internet at http://dms.dot.gov 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.

DiscussionPage 2

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.

CommentsPage 2

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) ParagraphPage 2

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.

ConclusionPage 2

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 CompliancePage 2

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 RulemakingPage 2

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 findingsPage 2

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.

Adoption of the amendmentPage 2

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

1. The authority citation for part 39 continues to read as follows:

2. The Federal Aviation Administration (FAA) amends § 39.13 by adding the following new airworthiness directive (AD):

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 431

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Embraer431 aircraft
By year built
19972017
Registered aircraft by year built: 410 aircraft
19971
199825
199936
200035
200157
200244
200359
200468
200542
200615
20078
20087
20092
20101
20111
20122
20135
20151
20171

21 with no year recorded

By model

Aircraft

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