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Holding District Office.
Related Information
(k) Canadian airworthiness directive CF-2006-06, dated April 4, 2006, also addresses the subject
of this AD.
Material Incorporated by Reference
(l) You must use Bombardier Service Bulletin 84-78-01, Revision `A,' dated September 15,
2005, to perform the actions that are required by this AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the incorporation by reference of this document in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Bombardier, Inc., Bombardier Regional
Aircraft Division, 123 Garratt Boulevard, Downsview, Ontario M3K 1Y5, 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 February 2, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
39 BW 2007-04
FAA
Aircraft Certification Service
AIRWORTHINESS DIRECTIVE
www.faa.gov/aircraft/safety/alerts/
www.gpoaccess.gov/fr/advanced.html
2007-04-09 Empresa Brasileira De Aeronautica S.A. (Embraer): Amendment 39-14941. FAA-
2006-25892; Directorate Identifier 2006-NM-120-AD.
Effective Date
(a) This AD becomes effective March 23, 2007.
Affected ADs
(b) None.
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 reports of smoke on the flight deck caused by damage from poor
electrical contact due to loosening of the attaching hardware of the power cables of certain
windshield temperature controllers. We are issuing this AD to prevent overheating of the power cable
terminals of the windshield temperature controllers, which could result in smoke on the flight deck.
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 of Part Number (P/N) of Controller
(f) Within 5,000 flight hours after the effective date of this AD, inspect to determine the part
number of the left- and right-hand windshield temperature controllers. A review of airplane
maintenance records is acceptable in lieu of this inspection if the part number of the subject controller
can be conclusively determined from that review. If any windshield temperature controller is found to
have a part number other than Goodrich P/N 3801D2( ), no further action is required by this AD for
that controller.
Replacement of Attaching Hardware, Further Inspection, and Corrective Actions
(g) Before further flight after performing the inspection required by paragraph (f) of this AD, for
all windshield temperature controllers having Goodrich P/N 3801D2( ) or any controller for which
2007-04-09 2
40 BW 2007-04
the part number cannot be conclusively determined: Replace the attaching hardware of the power
cable terminals of the controllers with new, improved attaching hardware having new part numbers.
Concurrently, perform a detailed inspection for signs of melting or damage of the plastic crimping
ring, cable insulation, or terminals of the power cables, and, before further flight, perform applicable
corrective actions. Perform all the actions in accordance with the Accomplishment Instructions of
EMBRAER Service Bulletin 145-30-0043, Revision 02, dated May 25, 2006; or EMBRAER Service
Bulletin 145LEG-30-0013, dated June 28, 2005; as applicable.
Credit for Actions Accomplished Using Previous Issue of Service Bulletin
(h) Actions accomplished before the effective date of this AD in accordance with EMBRAER
Service Bulletin 145-30-0043, dated June 28, 2005; or Revision 01, dated April 7, 2006; are
considered acceptable for compliance with the applicable corresponding actions required by this AD.
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 FR 39.19.
(2) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the
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