AD 89-09-01

AD Final Rules - DRS_89-09-01.html
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AD Number:
89-09-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; AIRBUS INDUSTRIE Model A300 A310 and A300-600 Series Airplanes
Subject:
Engine Fire Extinguishers
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/01/1989
Make:
Airbus
Model:
A300 B2-1A | A300 B2-1C | A300 B2-203 | A300 B2K-3C | A300 B4-103 | A300 B4-203 | A300 B4-2C | A300 ...Show more
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Superseded AD: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Superseded By: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: 89-09-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-6192

AD NUMBER:   89-09-01

SUBJECT HEADING:   Airworthiness Directives; AIRBUS INDUSTRIE Model A300 A310 and A300-600 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective on May 1, 1989.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
89-09-01 AIRBUS INDUSTRIE: Amendment 39-6192.

Applicability: Model A300 series airplanes, on which Modification 1988 has been accomplished (Post Service Bulletin A300-54-022), and all Model A310 and A300-600 equipped with Walter Kidde or APCO fire extinguisher bottles, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent the inability to actuate the fire extinguisher bottles, accomplish the following:

A. Within 10 days after the effective date of this AD, inspect the engine fire extinguishers for an electrical bonding defect in accordance with Airbus All Operator Telex (AOT) 26/88/01. If defects are found, repair prior to further flight, in accordance with the AOT.

B. Whenever the fire extinguishers bottles are replaced, perform the inspection required by paragraph A., above.

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, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who may add any comments and then send it 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 for the accomplishment of the inspection/modification required by this AD.

All persons affected by this directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to Airbus Industrie, Airbus Support Division Avenue Didier Daurat, 31700 Blagnac, France. This information may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6192, AD 89-09-01) becomes effective on May 1, 1989.

FOOTER: