AD 66-21-01

final rule
Data completeness: 70%

PRATT & WHITNEY Model JT3C-7 and JT3C-12 Engines

AD Number
66-21-01
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Division JT3C-12 PRATT & WHITNEY Model JT3C-7 and JT3C-12 Engines
engine Pratt & Whitney Division JT3C-7 PRATT & WHITNEY Model JT3C-7 and JT3C-12 Engines

Unsafe Condition

The first, fifth, and sixth stage compressor rotor disc spacer assemblies (P/N 359410, 359414, and 359415) may fail due to insufficient strength, leading to engine failure.

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

Required Actions

Replace the first, fifth, and sixth stage compressor rotor disc spacer assemblies with new spacer assemblies P/N 460599, 460604, and 460606 respectively. Compliance must be completed within the next 6,000 hours' time in service after the effective date or at the next compressor disassembly, whichever occurs first.

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

Compliance Time

within the next 6,000 hours' time in service after the effective date of this AD or at the next compressor disassembly, whichever occurs first

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

Affected Aircraft

Pratt & Whitney Model JT3C-7 and JT3C-12 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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