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FAA orders · airworthiness directive · historical

2002-16-12: AFM - Limitations Section - Spoiler

FAA order 2002-16-12 is an airworthiness directive in force since September 20, 2002. The FAA's subject line: AFM - Limitations Section - Spoiler. It names Airbus A330, Airbus A340: about 163 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Airbus
Models
A330-202, A330-223, A330-243, A330-301, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343, A340-211, A340-212, A340-213, A340-311, A340-312, A340-313
On this site
Airbus A330 153 registered
Airbus A340 10 registered

Dates and paperwork

In force since
September 20, 2002
Published
August 16, 2002 (signed August 7, 2002)
Docket
2001-NM-398-AD
Replaced by
2004-18-14
Status
Historical
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), applicable to certain Airbus Model A330 and A340 series airplanes, that requires revising the Limitations Section of the FAA-approved Airplane Flight Manual to ensure the flightcrew is advised of the proper procedures in the event of uncommanded movement of a spoiler during flight. Such uncommanded movement could result in reduced controllability of the airplane, and consequent significant increased fuel consumption during flight, which could necessitate an in-flight turn-back or diversion to an unscheduled airport destination. This action is intended to address the identified unsafe condition.

The order itself the regulatory text, as published

Show the full text (2,483 characters)
2002-16-12 Airbus: Amendment 39-12851. Docket 2001-NM-398-AD. \n\n\tApplicability: Model A330 and A340 series airplanes, certificated in any category; equipped with any spoiler servo control having part number (P/N)1386A0000-01 or 1386B0000-01, or P/N 1387A0000-01 or 1387B0000-01. \n\n\tCompliance: Required as indicated, unless accomplished previously. \n\n\tTo ensure the flightcrew is advised of the proper procedures in the event of uncommanded movement of a spoiler during flight, which could result in reduced controllability of the airplane and consequent significant increased fuel consumption during flight, and could result in an in-flight turn-back or diversion to an unscheduled airport destination, accomplish the following: \n\nRevision to Airplane Flight Manual (AFM) \n\n\t(a) Within 10 days after the effective date of this AD, revise the Limitations Section of the FAA-approved AFM by including the procedures listed in Figure 1 of this AD. This revision may be done by inserting acopy of the following Figure 1 into the AFM: \n\nBILLING CODE 4910-13-P \n\n\n\n\n\n\tNote 1: When the statement in paragraph (a) of this AD has been incorporated into the FAA-approved general revisions of the AFM, the general revisions may be incorporated into the AFM, provided the statement in this AD and the general revisions is identical. This AD may then be removed from the AFM. \n\nAlternative Methods of Compliance \n\n\t(b) 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 International Branch, ANM-116, FAA. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, International Branch, ANM-116. \n\n\tNote 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the International Branch, ANM-116. \n\nSpecial FlightPermits \n\n\t(c) Special flight permits may be issued in accordance with §§ 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\n\tNote 3: The subject of this AD is addressed in French airworthiness directives 2001-608(B) and 2001-609(B), both dated December 12, 2001. \n\nEffective Date \n\n\t(d) This amendment becomes effective on September 20, 2002.

Related safety bulletins advice on the same designs, not orders

2017-07-19NM-17-20 · Equipment/Furnishings
2009-06-01NM-09-33 · Flight Control Primary Computer (FCPC)
2008-12-11NM-09-03 · Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations
2008-09-03NM-08-43 · Cabin Equipment/Furnishings - Seats
2008-07-02NM-08-31 · Equipment/Furnishings: Non-Textile Floors

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/2002-16-12.json · aircraft systems.