- Effective
- May 1, 1989
- Models
- A300 B2-1A, A300 B2-1C, A300 B2-203, A300 B2K-3C, A300 B4-103, A300 B4-203 and 18 more
- Data sheet
- TCDSA35EU
- Registered aircraft
- 124 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-6192
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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On this page
The airworthiness directive
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, AD89-09-01) becomes effective on May 1, 1989.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 124
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1983 | 2 |
|---|---|
| 1984 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 3 |
| 1990 | 5 |
| 1991 | 3 |
| 1992 | 7 |
| 1993 | 5 |
| 1994 | 5 |
| 1995 | 8 |
| 1996 | 5 |
| 1997 | 5 |
| 1998 | 6 |
| 1999 | 6 |
| 2000 | 7 |
| 2001 | 11 |
| 2002 | 6 |
| 2003 | 8 |
| 2004 | 7 |
| 2005 | 7 |
| 2006 | 6 |
| 2007 | 6 |
2 with no year recorded