AD 91-06-15

Airworthiness directive · Hydraulic Shut-Off Valves · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 18 more

Effective
April 22, 1991
Models
A300 B2-1A, A300 B2-1C, A300 B2-203, A300 B2K-3C, A300 B4-103, A300 B4-203 and 15 more
Data sheet
TCDSA35EU
Registered aircraft
122 matched by model
Product
Aircraft · Large airplane
Amendment
39-6941
Docket
90-NM-229-AD

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.

On this page

The airworthiness directive

91-06-15 AIRBUS INDUSTRIE: Amendment 39-6941. Docket No. 90-NM-229-AD.

Applicability: All Model A300, A310, and A300-600 series airplanes, on which Airbus Industrie Modification 8135 has not been accomplished, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent the inability of the hydraulic power fire shut-off valves to close during emergency conditions, accomplish the following:

A. Within 180 days after the effective date of this AD, conduct an inspection of the hydraulic power fire shut-off valves to identify faulty valves, as specified in Airbus Industrie Service Bulletins A300-29-096 (for Model A300 series airplanes), A310-29-2025 (for Model A310 series airplanes), and A300-29-6017 (for Model A300-600 series airplanes), all dated January 29, 1990. Any faulty valve identified must be removed and replaced with a modified valve prior to further flight, in accordance with the appropriate service bulletins.

NOTE: The Airbus Industrie service bulletins reference Lucas Air Equipment Service Bulletin No. B38LC15-29-05, Revision 1, dated February 1990, for additional instructions.

B. 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.

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.

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 (39-6941, AD 91-06-15) becomes effective on April 22, 1991.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 122

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Airbus Industrie74 aircraft
  • Airbus48 aircraft
By year built
19832007
Registered aircraft by year built: 120 aircraft
19832
19841
19851
19881
19892
19905
19913
19927
19935
19945
19958
19965
19975
19986
19996
20007
200111
20026
20038
20047
20057
20066
20076

2 with no year recorded

By model

Aircraft

See all 122 aircraft