AD 2000-09-10

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A300-600 Series Airplanes

AD Number
2000-09-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 99-NM-362-AD
FR Citation
65 FR 30536

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300-600 Airworthiness Directives; Airbus Model A300-600 Series Airplanes

Unsafe Condition

Erratic operation of the wheel tachometers, which could result in degradation of the braking performance, and possible increased landing roll.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Modify the electrical looms of the nose and main landing gear in accordance with Airbus Service Bulletin A300-32-6069, Revision 01, dated December 29, 1999. Modify the rotor shaft attachment of the nose and main landing gear tachometers in accordance with Airbus Service Bulletin A300-32-6077, Revision 01, dated September 25, 1999.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 18 months after the effective date of this AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Airbus Model A300-600 series airplanes, certificated in any category, except those airplanes on which Airbus Modifications 11661 and 11676 (Airbus Service Bulletin A300-32-6069) and 12095 (Airbus Service Bulletin A300-32-6077) have been installed.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.