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that are required by this AD, unless the AD specifies otherwise.
2007-04-05 3
34 BW 2007-04
Table 1 – All Material Incorporated by Reference
Airbus Service Bulletin Revision Level Date
A300-22-0117 Original September 7, 2004
A300-22-0117 01 April 20, 2005
A300-22-0117 02 September 14, 2005
A300-22-0118, excluding
Appendix 01
Original May 18, 2005
(1) The Director of the Federal Register approved the incorporation by reference of the
documents identified in Table 2 of this AD in accordance with 5 U.S.C. 552(a) and 1 CFR part 51.
Table 2 – New Material Incorporated by Reference
Airbus Service Bulletin Revision Level Date
A300-22-0117 01 April 20, 2005
A300-22-0117 02 September 14, 2005
A300-22-0118, excluding
Appendix 01
Original May 18, 2005
(2) On August 1, 2005 (70 FR 36833, June 27, 2005), the Director of the Federal Register
approved the incorporation by reference of Airbus Service Bulletin A300-22-0117, dated September
7, 2004.
(3) Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France, 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 5, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-2412 Filed 2-13-07; 8:45 am]
35 BW 2007-04
FAA
Aircraft Certification Service
AIRWORTHINESS DIRECTIVE
www.faa.gov/aircraft/safety/alerts/
www.gpoaccess.gov/fr/advanced.html
2007-04-06 McDonnell Douglas: Amendment 39-14937. Docket No. FAA-2006-26084; Directorate
Identifier 2006-NM-063-AD.
Effective Date
(a) This AD becomes effective March 21, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to McDonnell Douglas Model DC-8-62 and DC-8-63 airplanes and Model
DC-8-62F and DC-8-63F airplanes, certificated in any category; as identified in McDonnell Douglas
DC-8 Service Bulletin 78-95, Revision 2, dated March 10, 1971.
Unsafe Condition
(d) This AD results from the determination that the thrust reverser systems on McDonnell
Douglas Model DC-8-62, DC-8-63, DC-8-62F, and DC-8-63F airplanes do not adequately preclude
inadvertent deployment of the thrust reversers. We are issuing this AD to prevent inadvertent
deployment of the thrust reversers during takeoff or landing, which could result in loss of control 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.
Modification of Engine Thrust Brake Circuitry
(f) Within 27 months after the effective date of this AD, do the applicable action specified in
paragraph (f)(1) or (f)(2) of this AD, by accomplishing all of the applicable actions specified in the
Accomplishment Instructions of McDonnell Douglas DC-8 Service Bulletin 78-95, Revision 2, dated
March 10, 1971; or Revision 1, dated December 29, 1970.
(1) Revise the wiring for the engine thrust brake circuit and indicating circuit, and do all other
specified actions before further flight after revising the wiring.
(2) Reroute the wiring at plug P1-1762A on the electrical power center generator control panel.
2007-04-06 2
36 BW 2007-04
Alternative Methods of Compliance (AMOCs)
(g)(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
(h) You must use McDonnell Douglas DC-8 Service Bulletin 78-95, Revision 2, dated March 10,
1971; or McDonnell Douglas DC-8 Service Bulletin 78-95, Revision 1, dated December 29, 1970; to
perform the actions that are required by this AD, unless the AD specifies otherwise. McDonnell
Douglas DC-8 Service Bulletin 78-95, Revision 2, dated March 10, 1971, contains the following
effective pages:
Page Number Revision Level Shown
on Page
Date Shown on Page
1, 2, 16, 17 2 March 10, 1971
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