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2000-22-21: Fuel Pump Electrical Connector

FAA order 2000-22-21 is an airworthiness directive in force since December 5, 2000. The FAA's subject line: Fuel Pump Electrical Connector. It names Douglas DC-10, Mcdonnell Douglas DC-10, Mcdonnell Douglas MD-10, Mcdonnell Douglas MD-11: about 144 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: fuel system.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
The Boeing Company
Models
DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-30F (KC-10A, KDC-10), DC-10-30F (KC-10A, KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, MD-11, MD-11F
On this site
Douglas DC-10 8 registered
Mcdonnell Douglas DC-10 17 registered
Mcdonnell Douglas MD-10 15 registered
Mcdonnell Douglas MD-11 104 registered

Dates and paperwork

In force since
December 5, 2000
Docket
2000-NM-345-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

This amendment adopts a new airworthiness directive (AD) that is applicable to all McDonnell Douglas Model DC-10, Model MD-10, and Model MD-11 series airplanes. This action requires revising the Airplane Flight Manual (AFM) to ensure that the flight crew is advised of appropriate procedures for disabling certain fuel pump electrical circuits following failure of a fuel pump electrical connector. For certain airplanes, this action also requires revising the AFM to prohibit resetting of tripped fuel pump circuit breakers. This action is necessary to prevent continued arcing following a short circuit of the fuel pump electrical connector, which could damage the conduit that protects the power lead inside the fuel tank, and result in the creation of a potential ignition source in the fuel tank. This action is intended to address the identified unsafe condition.\n\n\tThe incorporation by reference of certain publications listed in the regulations is approved by the Director ofthe Federal Register as of December 5, 2000.\n\n\tComments for inclusion in the Rules Docket must be received on or before January 19, 2001.

The order itself the regulatory text, as published

Show the full text (3,454 characters)
2000-22-21 MCDONNELL DOUGLAS: Amendment 39-11969. Docket 2000-NM-345-AD.\n\n\tApplicability: All Model DC-10, Model MD-10, and Model MD-11 series airplanes; certificated in any category. \n\n\tCompliance: Required as indicated, unless accomplished previously. \n\tTo prevent continued arcing following a short circuit of the fuel pump electrical connector, which could damage the conduit that protects the power lead inside the fuel tank, and result in the creation of a potential ignition source in the fuel tank, accomplish the following: \n\nAirplane Flight Manual (AFM) Revision (Procedures Section)\n\t(a) Within 14 days after the effective date of this AD, insert applicable Interim Operating Procedures regarding abnormal operations for fuel pump electrical connector failures into the Procedures Section of the FAA-approved AFM, in accordance with Boeing Flight Operations Bulletin DC-10-00-01A, MD-11-00-03A, and MD-10-00-02A, dated September 20, 2000.\n\nAirplane Flight Manual Revision (Limitations Section)\n\t(b) For Model DC-10 and Model MD-11 series airplanes: Within 14 days after the effective date of this AD, insert the following information into the "Fuel Management" paragraph of the Limitations Section of the FAA-approved AFM (which may be accomplished by inserting a copy of this AD into the AFM): \n\n\t"Do not reset any tripped fuel pump circuit breakers."\n\n\tNote 1: If the information in paragraph (b) of this AD is already in the "Fuel Management" paragraph of the Limitations Section of the AFM, no further action is required by paragraph (b) of this AD.\n\nAlternative Methods of Compliance\n\t(c) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Los Angeles Aircraft Certification Office (ACO), FAA. Operators shall submit their requests through an appropriate FAA Principal Operations Inspector, who may add comments and then send it to the Manager,Los Angeles ACO.\n\n\tNote 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Los Angeles ACO.\n\nSpecial Flight Permits\n\t(d) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. \n\nIncorporation by Reference\n\t(e) Except as provided by paragraph (b) of this AD, the AFM revision shall be done in accordance with Boeing Flight Operations Bulletin DC-10-00-01A, MD-11-00-03A, and MD-10-00-02A, dated September 20, 2000. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Boeing Commercial Aircraft Group, Long Beach Division, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Technical Publications Business Administration, Dept. C1-L51 (2-60). Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; at the FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.\n\nEffective Date\n\t(f) This amendment becomes effective on December 5, 2000.

Related safety bulletins advice on the same designs, not orders

2019-02-19NE-19-03 · Escape Slide Maintenance Tasks and Intervals - JASC 2565
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

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/2000-22-21.json · aircraft systems.