AD 93-14-13

final rule
Data completeness: 70%

TEXTRON LYCOMING Models ALF502R and ALF502L Engines

AD Number
93-14-13
Status
final_rule
Effective Date
Product Category
engine
Docket
91-ANE-55
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Honeywell International Inc. ALF502L TEXTRON LYCOMING Models ALF502R and ALF502L Engines
engine Honeywell International Inc. ALF502L-2 TEXTRON LYCOMING Models ALF502R and ALF502L Engines
engine Honeywell International Inc. ALF502L-2A TEXTRON LYCOMING Models ALF502R and ALF502L Engines
engine Honeywell International Inc. ALF502L-2C TEXTRON LYCOMING Models ALF502R and ALF502L Engines
engine Honeywell International Inc. ALF502L-3 TEXTRON LYCOMING Models ALF502R and ALF502L Engines
engine Honeywell International Inc. ALF502R-3 TEXTRON LYCOMING Models ALF502R and ALF502L Engines
engine Honeywell International Inc. ALF502R-3A TEXTRON LYCOMING Models ALF502R and ALF502L Engines
engine Honeywell International Inc. ALF502R-4 TEXTRON LYCOMING Models ALF502R and ALF502L Engines
engine Honeywell International Inc. ALF502R-5 TEXTRON LYCOMING Models ALF502R and ALF502L Engines
engine Honeywell International Inc. ALF502R-6 TEXTRON LYCOMING Models ALF502R and ALF502L Engines

Unsafe Condition

Third stage turbine disk failure, which could result in engine shutdown.

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Required Actions

Rework the third stage turbine disk blade slots and mark the assembly with a new part number per Textron Lycoming Service Bulletin, or replace with a serviceable part. Compliance must be within specified cycles in service (CIS) based on the disk's cycles on the AD effective date.

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Compliance Time

Compliance required within 1,000 CIS after the effective date for disks with 15,000+ CIS; within 1,000 CIS or next shop visit (later) but before 16,000 CIS for 10,000-15,000 CIS; at next blade removal before 13,000 CIS for less than 10,000 CIS.

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Affected Aircraft

Textron Lycoming ALF502R and ALF502L turbofan engines installed on British Aerospace BAe-146 and Canadair Challenger CL600 aircraft, with specific part numbers on third stage turbine rotor shaft assemblies.

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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