AD 92-19-04

final rule
Data completeness: 70%

Airworthiness Directives; AIRBUS INDUSTRIE Model A300-B4-620, A310-221, A310-222, A310-322, A300-B4-622, A300-B4-622R, and A310-324 Series Airplanes

AD Number
92-19-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-NM-252-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus SAS A300 B4-620 Airworthiness Directives; AIRBUS INDUSTRIE Model A300-B4-620, A310-221, A310-222, A310-322, A300-B4-622, A300-B4-622R, and A310-324 Series Airplanes
aircraft Airbus SAS A300 B4-622R Airworthiness Directives; AIRBUS INDUSTRIE Model A300-B4-620, A310-221, A310-222, A310-322, A300-B4-622, A300-B4-622R, and A310-324 Series Airplanes
aircraft Airbus SAS A310-221 Airworthiness Directives; AIRBUS INDUSTRIE Model A300-B4-620, A310-221, A310-222, A310-322, A300-B4-622, A300-B4-622R, and A310-324 Series Airplanes
aircraft Airbus SAS A310-222 Airworthiness Directives; AIRBUS INDUSTRIE Model A300-B4-620, A310-221, A310-222, A310-322, A300-B4-622, A300-B4-622R, and A310-324 Series Airplanes
aircraft Airbus SAS A310-322 Airworthiness Directives; AIRBUS INDUSTRIE Model A300-B4-620, A310-221, A310-222, A310-322, A300-B4-622, A300-B4-622R, and A310-324 Series Airplanes
aircraft Airbus SAS A310-324 Airworthiness Directives; AIRBUS INDUSTRIE Model A300-B4-620, A310-221, A310-222, A310-322, A300-B4-622, A300-B4-622R, and A310-324 Series Airplanes

Unsafe Condition

Cracks or a broken link in the forward engine mount thrust link and cracks or forging laps in the aft engine mount beam assembly could reduce structural integrity of the airplane.

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

Required Actions

Perform visual inspections for cracks or broken links in the forward engine mount thrust link and cracks or forging laps in the aft engine mount beam assembly within 500 hours time-in-service after the AD's effective date. Repeat inspections at intervals not exceeding 1,000 landings until specific etch inspections are completed. Conduct etch inspections (initial etch for forward link, dip etch and fluorescent penetrant for aft beam) within 4,000 hours time-in-service or at next engine removal, whichever comes first. Replace components if cracks or defects are found before further flight. Follow specified service bulletins.

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

Compliance Time

Required as indicated, unless accomplished previously.

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

Affected Aircraft

Airbus Model A300-B4-620, A310-221, A310-222, A310-322, A300-B4-622, A300-B4-622R, and A310-324 series airplanes equipped with Pratt & Whitney JT9D-7R4D1, JT9D-7R4E1, JT9D-7R4H1, PW4152, or PW4158 series engines.

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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