AD 2020-05-28

final rule
Data completeness: 80%

Airworthiness Directives; International Aero Engines LLC Turbofan Engines

AD Number
2020-05-28
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2019-0614
FR Citation
85 FR 15054

Applicability

TypeManufacturerModelDetails
aircraft International Aero Airworthiness Directives; International Aero Engines LLC Turbofan Engines

Unsafe Condition

multiple reports of in-flight engine shutdowns as the result of high-cycle fatigue causing fracture of certain parts of the main gearbox (MGB) assembly

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

Required Actions

Remove the MGB assembly, part number (P/N) 5322505, and install a part eligible for installation. For engines that operate on 180-minute extended operations (ETOPS) flights, before further flight. For engines that do not operate on ETOPS flights, within 50 flight hours after the effective date of this AD. Replace the electronic engine control (EEC) software to incorporate FCS5.0 software. Replace the integrated drive generator oil pump drive gearshaft assembly in the MGB assembly.

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

Compliance Time

Before further flight for ETOPS flights, within 50 flight hours after the effective date of this AD for non-ETOPS flights

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

Affected Aircraft

All International Aero Engines, LLC (IAE) PW1133G-JM, PW1133GA-JM, PW1130G-JM, PW1129G-JM, PW1127G-JM, PW1127GA-JM, PW1127G1-JM, PW1124G-JM, PW1124G1-JM, and PW1122G-JM model turbofan engines

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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