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767-28A0077 1 July 8, 2004
767-28A0081 1 July 8, 2004
767-28A0088 Original February 24, 2005
767-28A0089 Original February 24, 2005
Issued in Renton, Washington, on February 5, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-2644 Filed 2-15-07; 8:45 am]
49 BW 2007-04
FAA
Aircraft Certification Service
AIRWORTHINESS DIRECTIVE
www.faa.gov/aircraft/safety/alerts/
www.gpoaccess.gov/fr/advanced.html
2007-04-17 McDonnell Douglas: Amendment 39-14949. Docket No. FAA-2006-26049; Directorate
Identifier 2006-NM-177-AD.
Effective Date
(a) This AD becomes effective March 23, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to McDonnell Douglas airplanes, certificated in any category; as specified in
paragraphs (c)(1), (c)(2), and (c)(3) of this AD.
(1) All Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, and DC-10-30F (KC-10A and
KDC-10) airplanes;
(2) Model DC-10-40 and DC-10-40F airplanes equipped with Pratt & Whitney JT9-20 or JT9-
20J engines; and
(3) All Model MD-10-10F and MD-10-30F airplanes.
Unsafe Condition
(d) This AD results from a report of broken or severed wiring between engine fire detectors and
the fire detection system control module, which caused the fire detection system to become nonfunctional
without flightcrew awareness. We are issuing this AD to prevent unannunciated fire in a
propulsion engine, which could cause injury to flightcrew and passengers or 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.
Control Module Replacement
(f) Within 60 months after the effective date of this AD, replace the control modules of the fire
detection systems of the propulsion engines with new, improved control modules, in accordance with
paragraph 2., ''Main Engine Control Module Replacement Instructions,'' of Meggitt Safety Systems
Service Bulletin 26-34, Revision 2, dated August 15, 2006.
2007-04-17 2
50 BW 2007-04
Credit for Previous Revisions of Service Bulletins
(g) Actions done before the effective date of this AD in accordance with Meggitt Safety Systems
Service Bulletin 26-34, Revision 1, dated July 17, 2006, are acceptable for compliance with the
corresponding actions required by paragraph (f) of this AD.
Alternative Methods of Compliance (AMOCs)
(h)(1) The Manager, Los Angeles Aircraft Certification Office, 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.
Material Incorporated by Reference
(i) You must use Meggitt Safety Systems Service Bulletin 26-34, Revision 2, dated August 15,
2006, to perform the actions that are required by this AD, unless the AD specifies otherwise. Meggitt
Safety Systems Service Bulletin 26-34, Revision 2, dated August 15, 2006, contains the following
effective pages:
Page
number
Revision level
shown on page
Date shown on
page
1–26 2 August 15, 2006.
27–61 1 July 17, 2006.
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 Meggitt Safety Systems, 1915 Voyager
Avenue, Simi Valley, California 93063, 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/ibrlocations.
html.
Issued in Renton, Washington, on February 8, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-2639 Filed 2-15-07; 8:45 am]
51 BW 2007-04
FAA
Aircraft Certification Service
AIRWORTHINESS DIRECTIVE
www.faa.gov/aircraft/safety/alerts/
www.gpoaccess.gov/fr/advanced.html
2007-04-18 Learjet: Amendment 39-14950. Docket No. FAA-2006-25563; Directorate Identifier
2006-NM-083-AD.
Effective Date
(a) This AD becomes effective March 23, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to the Learjet models identified in the applicable Bombardier service bulletin
　
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