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AD 92-02-14 SUPERSEDED

Emergency Escape Slides
WARNING: This AD has been superseded and is no longer active. Replaced by: 92-02-14 R1. Refer to the superseding AD(s) for current requirements.
Key Information
AD Number 92-02-14 Status Superseded
Effective Date March 02, 1992 Issue Date December 30, 1991
Docket Number 91-NM-255-AD Amendment 39-8150
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section --- - _EMPTY_
Citation This information is not available.
Applicability
Manufacturer(s) Airbus
Model(s) A320-111 A320-211 A320-212 A320-214 A320-231 A320-232 A320-233
Related Airworthiness Directives
Superseded By 92-02-14 R1
Regulatory Text

92-02-14 AIRBUS INDUSTRIE: Amendment 39-8150. Docket 91-NM-255-AD.

Applicability: Model A320 series airplanes through manufacturer's serial number 175, inclusive, certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent failure of the overwing emergency escape slides to deploy, accomplish the following:

(a) Within 50 hours time-in-service after the effective date of this AD, perform an inspection of the flexible control cables on the right-hand and left-hand overwing emergency escape slides to ensure that the flexible control assembly on each overwing escape slide is correctly installed, in accordance with Airbus Industrie All Operator Telex (AOT) 25-02, dated May 16, 1991.
(1) If each flexible control assembly is correctly installed, no further action is required.
(2) If a flexible control assembly is incorrectly installed, prior to further flight, reconnect the assembly, in accordance with the AOT.(b) An alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. The request shall be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, 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 inspections and reconnections of the flexible control assemblies and release cable assemblies required by this AD shall be done in accordance with Airbus Industrie All Operator Telex 25-02, dated May 16, 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, Airbus Support Division, Avenue Didier Daurat, 31700 Blagnac, France. Copies may be inspected at the FAA, Transport Airplane Directorate, Standardization Branch, ANM-113, 1601 Lind Avenue S.W., Renton, Washington; or at the Office of the Federal Register, 1100 L Street N.W., Room 8401, Washington, D.C.

(e) This amendment (39-8150, AD 92-02-14) becomes effective on March 2, 1992.

Office of Primary Responsibility
["AIR-720: Operational Safety Branch"]