AD 92-19-03

final rule
Data completeness: 70%

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

AD Number
92-19-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
92-NM-35-AD
FR Citation
This information is not available.

Applicability

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

Unsafe Condition

Failure of the ram air turbine (RAT) to release properly due to improper operation of the Teleflex flexible control cables (load to move the handle exceeding 5.5 daN).

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

Required Actions

Within 6 months after the effective date, test the RAT Teleflex flexible control cables to ensure load to move the handle is ≤5.5 daN. If discrepancies (load >5.5 daN) are found, perform maintenance tasks before further flight and repeat every 30 months. Modify the control cables per specified service bulletins to terminate repetitive tasks.

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

Compliance Time

Within 6 months after the effective date of this AD, and thereafter at intervals not to exceed 30 months.

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

Affected Aircraft

AIRBUS INDUSTRIE Model A300, A310, and A300-600 series airplanes where Modification 4803 has not been accomplished.

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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