Airworthiness directives › 93-24-51
AD 93-24-51 Airworthiness Directives; Airbus Industrie Model A310 and A300- 600 Series Airplanes
Models named: A310, A300-600 series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
All Airbus Model A310 and A300-600 series airplanes, certificated in any category.
Compliance
Required as indicated, unless accomplished previously. To prevent stiff operation of the pitch control and undetected loss of rudder travel limitation function, which may adversely affect controllability of the airplane, accomplish the following: (a) Within 7 days after the effective date of this AD, perform an operational test to verify proper operation of feel and limitation computers (FLC) 1 and 2 in accordance with Airbus Industrie All Operator Telex 27-14, dated November 2, 1993. Thereafter repeat this test at intervals not to exceed 7 days. (b) If any FLC fails the test, prior to further flight, replace with a new or serviceable FLC, or repair the FLC in accordance with a method approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. (c) As of the effective date of this AD, no airplane shall be operated with an inoperative pitch feel system or inoperative pitch feel fault lights. (d) 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, Standardization Branch, ANM-113. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113. Note: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113. (e) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished. (f) The test shall be done in accordance with Airbus Industrie All Operator Telex 27-14, dated November 2, 1993. 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 Airbus Industrie, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (g) This amendment becomes effective on January 20, 1994, to all persons except those persons to whom it was made immediately effective by telegraphic AD T93-24-51, issued December 1, 1993, which contained the requirements of this amendment. Issued in Renton, Washington, on December 28, 1993. Darrell M. Pederson, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 94-21 Filed 1-4-94; 8:45 am] BILLING CODE 4910-13-U
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1