AD 90-19-09

final rule
Data completeness: 70%

GENERAL ELECTRIC COMPANY Models CF6-50/-45 Series Engines

AD Number
90-19-09
Status
final_rule
Effective Date
Product Category
engine
Docket
90-ANE-21-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine General Electric Company CF6-45A GENERAL ELECTRIC COMPANY Models CF6-50/-45 Series Engines
engine General Electric Company CF6-45A2 GENERAL ELECTRIC COMPANY Models CF6-50/-45 Series Engines
engine General Electric Company CF6-50A GENERAL ELECTRIC COMPANY Models CF6-50/-45 Series Engines
engine General Electric Company CF6-50C GENERAL ELECTRIC COMPANY Models CF6-50/-45 Series Engines
engine General Electric Company CF6-50C1 GENERAL ELECTRIC COMPANY Models CF6-50/-45 Series Engines
engine General Electric Company CF6-50C2 GENERAL ELECTRIC COMPANY Models CF6-50/-45 Series Engines
engine General Electric Company CF6-50C2B GENERAL ELECTRIC COMPANY Models CF6-50/-45 Series Engines
engine General Electric Company CF6-50C2D GENERAL ELECTRIC COMPANY Models CF6-50/-45 Series Engines
engine General Electric Company CF6-50CA GENERAL ELECTRIC COMPANY Models CF6-50/-45 Series Engines
engine General Electric Company CF6-50E GENERAL ELECTRIC COMPANY Models CF6-50/-45 Series Engines

Unsafe Condition

High Pressure Turbine Stage One Disks with specified part numbers may fail, leading to uncontained engine failure, emergency takeoff abort, and potentially significant aircraft damage.

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

Required Actions

Remove from service specified high pressure turbine stage one disks (Part Numbers 9264M57P01, 9264M57P02, 1322M88P04, 1322M88P05, 1322M88P07, 9283M31P02, 9283M55P04, 9283M55P05) based on disk cycles since new (CSN) and compliance schedules. Replace with serviceable disks as required.

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

Compliance Time

Compliance required as indicated in the AD, with specific deadlines based on cycles in service (CIS) after the effective date (October 1, 1990) or disk cycles since new (CSN), whichever occurs first.

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

Affected Aircraft

General Electric Company CF6-50/-45 series turbofan engines installed in Airbus A300, Boeing 747, and McDonnell Douglas DC-10-15 and DC-10-30 series aircraft.

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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