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2006-25-09: Auxiliary power unit (APU) power feeder wires

FAA order 2006-25-09 is an airworthiness directive in force since December 27, 2006. The FAA's subject line: Auxiliary power unit (APU) power feeder wires. It names Mcdonnell Douglas MD-11: about 104 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
The Boeing Company
Models
MD-11F
On this site
Mcdonnell Douglas MD-11 104 registered

Dates and paperwork

In force since
December 27, 2006
Published
December 12, 2006 (signed November 30, 2006)
Docket
FAA-2006-26527
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model MD-11F airplanes. This AD requires a general visual inspection for installation of conduit and chafing damage on the auxiliary power unit (APU) power feeder wires and the upper surface of the auxiliary fuel tank and repair if necessary. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to detect and correct unprotected APU power feeder wires that come into close proximity to the upper surface of the auxiliary "piggy back'' fuel tank, which could result in a potential ignition source, and in combination with flammable fuel vapors, could cause a fuel tank explosion and consequent loss of the airplane.

The order itself the regulatory text, as published

Show the full text (3,031 characters)
2006-25-09 McDonnell Douglas: Amendment 39-14850. Docket No. FAA- 2006-26527; Directorate Identifier 2006-NM-220-AD. \n\nEffective Date \n\n\t(a) This AD becomes effective December 27, 2006. \n\nAffected ADs \n\n\t(b) None. \n\nApplicability \n\n\t(c) This AD applies to certain McDonnell Douglas Model MD-11F airplanes, identified in Boeing Alert Service Bulletin MD11-24A222, dated August 16, 2006; certificated in any category. \n\nUnsafe Condition \n\n\t(d) This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to detect and correct unprotected auxiliary power unit (APU) power feeder wires that come into close proximity to the upper surface of the auxiliary "piggy back'' fuel tank, which could result in a potential ignition source, and in combination with flammable fuel vapors, could cause a fuel tank explosion and consequent loss of the airplane. \n\nCompliance \n\n\t(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. \n\nGeneral Visual Inspection \n\n\t(f) Within 24 months after the effective date of this AD, perform a general visual inspection for installation of conduit and chafing damage on APU power feeder wires and upper surface of the auxiliary fuel tank, in accordance with Boeing Alert Service Bulletin MD11-24A222, dated August 16, 2006. Before further flight, accomplish any applicable repair or replacement in accordance with the alert service bulletin. \n\nAlternative Methods of Compliance (AMOCs) \n\n\t(g)(1) The Manager, Los Angeles 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. \n\n\t(2) Before using any AMOC approved in accordance with Sec. 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. \n\nMaterial Incorporated by Reference \n\n\t(h) You must use Boeing Alert Service Bulletin MD11-24A222, dated August 16, 2006, 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 Boeing Commercial Airplanes, Long Beach Division, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Data and Service Management, Dept. C1-L5A (D800-0024), 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 .

Related safety bulletins advice on the same designs, not orders

2018-12-17NM-18-33 · Engine Fuel and Control
2014-11-24NM-15-03 · Flight Controls
2008-12-11NM-09-03 · Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations
2007-04-24NM-07-31 · Rigid hydraulic case drain lines
2006-07-27NM-06-57 · Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/2006-25-09.json · aircraft systems.