AD 90-19-07

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AD Number:
90-19-07
Document Type:
AD Final Rules
Docket Number:
90-NM-93-AD
Subject Heading:
Airworthiness Directives; AIRBUS INDUSTRIE Model A310-200 Series Airplanes
Subject:
Wing Inspection
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/23/1990
Make:
Airbus SAS
Model:
A310-203 | A310-221 | A310-222
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 90-19-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-93-AD

AMENDMENT:   39-6731

AD NUMBER:   90-19-07

SUBJECT HEADING:   Airworthiness Directives; AIRBUS INDUSTRIE Model A310-200 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective October 23, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-19-07 AIRBUS INDUSTRIE: Amendment 39-6731. Docket No. 90-NM-93-AD.

Applicability: Model A310-200 series airplanes, up to and including serial number 264, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent reduced structural capability of the wings, accomplish the following:

A. Prior to the accumulation of 12,000 landings, or within 1,500 landings after the effective date of this AD, whichever occurs later, and thereafter at intervals not to exceed 12,000 landings, perform an X-ray inspection of Stringers 6, 7, 8, and 9 run-outs inboard and outboard of Rib 14, in accordance with Airbus Industrie Service Bulletin A310-57-2038, dated November 6, 1989.

B. If cracks are found, repair prior to further flight in accordance with a procedure approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

C. An alternate means 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.

NOTE: The request should be submitted directly to the Manager, Standardization Branch, ANM-113, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Manager, Standardization Branch, ANM-113.

D. 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.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Airbus Industrie, Airbus Support Division, Avenue Didier Daurat, 31700 Blagnac, France. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington.

This amendment (39-6731, AD 90-19-07) becomes effective October 23, 1990.

FOOTER: