# AD 2000-12-06: Piston Rod Of The Elevator Servo-Controls - Type: Airworthiness directive - Status: Historical - Products: Airbus A330-202, A330-223, A330-301, A330-321, A330-322, A330-323, A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 - Effective: July 20, 2000 - Published: June 15, 2000, 65 FR 37476–37478 - Issued: June 7, 2000 - Issued as: Final rule - Superseded by: [AD 2004-13-25](https://openairdocs.org/ad/2004-13-25) - Product type: Aircraft, Large airplane - Amendment: 39-11784 - Docket: 2000-NM-64-AD - Registered aircraft: 40 may be affected, by airframe or engine model (OpenAirDocs) - Official PDF: https://openairdocs.org/files/sha256/3e/64/3e6462ce2745f7887c1500aaa91eaa392c8a57ea264e113eddc444828e5c11eb (from https://www.govinfo.gov/content/pkg/FR-2000-06-15/pdf/00-14882.pdf) - Federal Register: https://www.federalregister.gov/documents/2000/06/15/00-14882/airworthiness-directives-airbus-model-a330-and-a340-series-airplanes - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0742B554777C297E86256A0F005F01E4.0001 - DRS record last changed: August 7, 2025 - Page: https://openairdocs.org/ad/2000-12-06 ## Summary This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A330 and A340 series airplanes, that requires repetitive inspections to check the play of the eye-end of the piston rod of the elevator servo-controls, and follow-on corrective actions, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to detect and correct excessive play of the eye-end of the piston rod of the elevator servo-controls, which could result in failure of the elevator servo-control. ## The airworthiness directive Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows: 1. The authority citation for part 39 continues to read as follows: ## Rule preamble ### Dates Effective July 20, 2000. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of July 20, 2000. ### Addresses The service information referenced in this AD may be obtained from Airbus Industrie, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France. This information may be examined at the Federal Aviation Administration (FAA), Transport Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. ### For further information contact Norman B. Martenson, Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-2110; fax (425) 227-1149. ### SUPPLEMENTARY INFORMATION A proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an airworthiness directive (AD) that is applicable to certain Airbus Model A330 and A340 series airplanes was published in the Federal Register on April 11, 2000 (65 FR 19348). That action proposed to require repetitive inspections to check the play of the eye-end of the piston rod of the elevator servo-controls, and follow-on corrective actions, if necessary. ### Comments Interested persons have been afforded an opportunity to participate in the making of this amendment. No comments were submitted in response to the proposal or the FAA's determination of the cost to the public. ### Conclusion The FAA has determined that air safety and the public interest require the adoption of the rule as proposed. ### Cost Impact None of the airplanes affected by this action are on the U.S. Register. All airplanes included in the applicability of this rule currently are operated by non-U.S. operators under foreign registry; therefore, they are not directly affected by this AD. However, the FAA considers that this rule is necessary to ensure that the unsafe condition is addressed in the event that any of these subject airplanes are imported and placed on the U.S. Register in the future. Should an affected airplane be imported and placed on the U.S. Register in the future, it would require approximately 2 work hours to accomplish the required actions, at an average labor rate of $60 per work hour. Based on these figures, the cost impact of this AD would be $120 per airplane, per inspection cycle. ### Regulatory Impact The regulations adopted herein will not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government. Therefore, it is determined that this final rule does not have federalism implications under Executive Order 13132. For the reasons discussed above, I certify that this action (1) is not a “significant regulatory action” under Executive Order 12866; (2) is not a “significant rule” under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and (3) will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. A final evaluation has been prepared for this action and it is contained in the Rules Docket. A copy of it may be obtained from the Rules Docket at the location provided under the caption ADDRESSES. ## Affected data sheets (2) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS A43NM](https://openairdocs.org/tcds/A43NM): Airbus SAS; names 6 of 8 models: A340-311, A340-313, A340-211, A340-312, A340-213, A340-212 - [TCDS A46NM](https://openairdocs.org/tcds/A46NM): Airbus SAS; names 6 of 18 models: A330-223, A330-301, A330-321, A330-322, A330-323, A330-202 ## Registered aircraft it may apply to (OpenAirDocs) Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment. - Aircraft: 40 (40 by airframe model, 0 by engine model) - Makers: Airbus 35, Airbus Industrie 5 Models with the most aircraft: - [Airbus A330-323](https://openairdocs.org/model/airbus-a330-323): 21 aircraft (airframe model) - [Airbus A330-223](https://openairdocs.org/model/airbus-a330-223): 11 aircraft (airframe model) - [Airbus A330-202](https://openairdocs.org/model/airbus-a330-202): 2 aircraft (airframe model) - [Airbus Industrie A330-223](https://openairdocs.org/model/airbus-industrie-a330-223): 2 aircraft (airframe model) - [Airbus Industrie A330-323](https://openairdocs.org/model/airbus-industrie-a330-323): 1 aircraft (airframe model) - [Airbus Industrie A340-313](https://openairdocs.org/model/airbus-industrie-a340-313): 1 aircraft (airframe model) - [Airbus Industrie A330-202](https://openairdocs.org/model/airbus-industrie-a330-202): 1 aircraft (airframe model) - [Airbus A340-313](https://openairdocs.org/model/airbus-a340-313): 1 aircraft (airframe model) All 8 models: https://openairdocs.org/ad/2000-12-06/models.md Every aircraft: https://openairdocs.org/ad/2000-12-06/aircraft.md ## Related documents - [AD 2004-13-25](https://openairdocs.org/ad/2004-13-25) (historical): Piston rod of the elevator servo- controls · Airbus A330-201, A330-202, A330-203 and 15 more. Effective Aug 13, 2004. Supersedes this AD - [Proposed rule 2000-NM-64-AD](https://openairdocs.org/proposed/2000-NM-64-AD): Notice of proposed rulemaking (NPRM), published Apr 11, 2000 Its text cites no advisory circulars or STCs. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.