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bulletins listed in Table 1 of this AD are acceptable for compliance with the actions in paragraph (k)
of this AD.
Table 1 – Previous Revisions of Service Bulletin
Bombardier Service Bulletin Revision Level Date
601R-32-093 Original October 17, 2003
601R-32-093 A September 21, 2004
2007-03-19 4
25 BW 2007-04
Alternative Methods of Compliance (AMOCs)
(o)(1) The Manager, New York Aircraft Certification Office (ACO), FAA, has the authority to
approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the
AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate
Holding District Office.
Related Information
(p) Canadian airworthiness directive CF-2003-09R1, dated September 21, 2005, also addresses
the subject of this AD.
Material Incorporated by Reference
(q) You must use the applicable service information in Table 2 of this AD to perform the actions
that are required by this AD, unless the AD specifies otherwise.
Table 2 – All Material Incorporated by Reference
Service Bulletin Revision
Level
Date
Bombardier Alert Service Bulletin A601R-32-088, including
Appendices A, B, and C
Original February 20, 2003
Bombardier Alert Service Bulletin A601R-32-088, including
Appendices A, B, and C, dated February 20, 2003
A June 16, 2005
Bombardier Service Bulletin 601R-32-093 B July 14, 2005
(1) The Director of the Federal Register approved the incorporation by reference of the
documents in Table 3 of this AD, in accordance with 5 U.S.C. 552(a) and 1 CFR part 51.
Table 3 – New Material Incorporated by Reference
Service Bulletin Revision
Level
Date
Bombardier Alert Service Bulletin A601R-32-088,
including Appendices A, B, and C, dated February 20,
2003
A June 16, 2005
Bombardier Service Bulletin 601R-32-093 B July 14, 2005
2007-03-19 5
26 BW 2007-04
(2) On August 13, 2004 (69 FR 41421, July 9, 2004), the Director of the Federal Register
approved the incorporation by reference of Bombardier Alert Service Bulletin A601R-32-088,
including Appendices A, B, and C, dated February 20, 2003.
(3) Contact Bombardier, Inc., Canadair, Aerospace Group, P.O. Box 6087, Station Centre-ville,
Montreal, Quebec H3C 3G9, Canada, for a copy of this service information. You may review copies
at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW.,
Room PL-401, Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov; or at the
National Archives and Records Administration (NARA). For information on the availability of this
material at the NARA, call (202) 741-6030, or go to
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
Issued in Renton, Washington, on January 29, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-1876 Filed 2-7-07; 8:45 am]
27 BW 2007-04
FAA
Aircraft Certification Service
AIRWORTHINESS DIRECTIVE
www.faa.gov/aircraft/safety/alerts/
www.gpoaccess.gov/fr/advanced.html
2007-04-03 Empresa Brasileira de Aeronautica S.A. (EMBRAER): Amendment 39-14934.
Docket No. FAA-2006-25925; Directorate Identifier 2006-NM-167-AD.
Effective Date
(a) This AD becomes effective March 21, 2007.
Affected ADs
(b) This AD supersedes AD 2006-04-02.
Applicability
(c) This AD applies to all EMBRAER Model EMB-135BJ, -135ER, -135KE, -135KL, and -
135LR airplanes; and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP
airplanes; certificated in any category.
Unsafe Condition
(d) This AD results from a report of smoke in the cockpit. We are issuing this AD to prevent
ignition of a windowsill drain hose by an overheated relay, which could cause fire and smoke in the
cockpit.
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.
Inspection and Modification of Relay/Relay Socket, and Corrective Actions
(f) Within 600 flight hours or 180 days after the effective date of this AD, whichever occurs first:
Do a one-time detailed inspection for discrepancies of the pitot static heating relay K0057, relay
socket XK0057, and silicone gasket; modify and re-identify the XK0057 relay socket; and do all
applicable corrective actions; in accordance with the Accomplishment Instructions of EMBRAER
Alert Service Bulletin 145LEG-30-A017, dated May 31, 2006 (for Model EMB-135BJ airplanes); or
　
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