AD 99-16-14

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes

AD Number
99-16-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
99-NM-189-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2-1A Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B2-1C Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B2-203 Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B2K-3C Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-103 Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-203 Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-2C Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-601 Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-603 Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-605R Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes

Unsafe Condition

Failure of both the main valve and the clutch valve of the autopilot yaw actuator can lead to uncommanded rudder deflections. Crossed electrical connectors between the actuator’s main valves and the flight control computers can cause the autopilot actuator to remain engaged and hydraulically pressurized, providing uncommanded inputs to control surfaces.

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

Required Actions

Perform a one-time inspection of autopilot systems for proper engagement to check main electro valve electrical connectors of yaw, roll, and pitch actuators. If systems cannot be engaged, conduct a visual inspection of connectors and correct any incorrect installations. Actions must follow specified procedures in Airbus AOT documents.

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

Compliance Time

Within 10 days after the effective date of this AD

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

Affected Aircraft

All Airbus Model A300, A310, and A300-600 series airplanes, regardless of modifications

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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