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AD 91-16-03 ACTIVE

Escape Slide Girt Bars
Key Information
AD Number 91-16-03 Status Active
Effective Date September 11, 1991 Issue Date Not specified
Docket Number 91-NM-90-AD Amendment 39-7093
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Airbus
Model(s) A300 B2-1A A300 B2-1C A300 B2-203 A300 B2K-3C A300 B4-103 A300 B4-203 A300 B4-2C A300 B4-601 A300 B4-603 A300 B4-605R A300 B4-620 A300 B4-622R A300 F4-605R A300 F4-622R A310-203 A310-221 A310-222 A310-304 A310-322 A310-324 A310-325
Regulatory Text

91-16-03 AIRBUS INDUSTRIE: Amendment 39-7093. Docket No. 91-NM-90-AD.

Applicability: Model A300, A310, and A300-600 series airplanes equipped with escape slides, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent delayed passenger evacuation during an emergency, accomplish the following:

A. Within 30 days after the effective date of this AD, or prior to the accumulation of 300 hours time-in-service after the effective date of this AD, whichever occurs first, perform a close visual inspection of the escape slide girt bars for correct installation, in accordance with paragraph 4 of Airbus Industrie All Operators Telex (AOT) 25-01, dated July 30, 1990. If the girt bars are incorrectly installed, prior to further flight, repair 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 approvedby the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate.

NOTE: The request should 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 airplanes to a base in order to comply with the requirements of this AD.

D. The inspection and repair requirements shall be done in accordance with Airbus Industrie All Operators Telex (AOT) 25-01, dated July 30, 1990. 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, Renton, Washington; or at the Office of the Federal Register, 1100 L Street N.W.,Room 8401, Washington, D.C.

This amendment (39-7093, AD 91-16-03) becomes effective on September 11, 1991.