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93-18-02: Nose Landing Gear wheels

FAA order 93-18-02 is an airworthiness directive in force since November 24, 1993. The FAA's subject line: Nose Landing Gear wheels. It names Airbus A320: about 792 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: landing gear.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Airbus
Models
A320-111, A320-211, A320-231
On this site
Airbus A320 792 registered

Dates and paperwork

In force since
November 24, 1993
Docket
93-NM-29-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (2,278 characters)
93-18-02 AIRBUS INDUSTRIE: Amendment 39-8687. Docket 93-NM-29-AD. Applicability: Model A320-111, -211, and -231 series airplanes, as listed in Airbus Industrie Service Bulletin No. A320-32-1061, Revision 3, dated October 19, 1992; certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent reduced directional control due to loss of the nose landing gear wheel during taxiing or landing, accomplish the following: (a) Within 4 months after the effective date of this AD, modify the nose landing gear wheels in accordance with Airbus Industrie Service Bulletin No. A320-32-1061, Revision 3, dated October 19, 1992. (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, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. 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. (c) 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. (d) The modification shall be done in accordance with Airbus Industrie Service Bulletin No. A320-32-1061, Revision 3, dated October 19, 1992, which contains the following list of effective pages: Page Number Revision Level Shown on Page Date Shown on Page 1-4 3 October 19, 1992 5-7 1 June 10, 1991 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 MauriceBellonte, 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. (e) This amendment becomes effective on November 24, 1993.

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2014-11-06NM-15-02 · Cabin Equipment/Furnishings
2014-06-03NM-14-21 · Communications: Honeywell RTA 44D VHF Transceivers
2013-03-21NM-13-24 · Air Conditioning System: Air Distribution Fan
2012-10-23NM-13-03 · Hydraulic Power System: Power Transfer Unit

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/93-18-02.json · aircraft systems.