Back to AD

AD 91-06-15 ACTIVE

Hydraulic Shut-Off Valves
Key Information
AD Number 91-06-15 Status Active
Effective Date April 22, 1991 Issue Date Not specified
Docket Number 90-NM-229-AD Amendment 39-6941
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

91-06-15 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.