AD 70-11-03

final rule
Data completeness: 70%

PRATT & WHITNEY Model JT8D Series Engines

AD Number
70-11-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Division JT8D-1 PRATT & WHITNEY Model JT8D Series Engines
engine Pratt & Whitney Division JT8D-11 PRATT & WHITNEY Model JT8D Series Engines
engine Pratt & Whitney Division JT8D-15 PRATT & WHITNEY Model JT8D Series Engines
engine Pratt & Whitney Division JT8D-15A PRATT & WHITNEY Model JT8D Series Engines
engine Pratt & Whitney Division JT8D-17 PRATT & WHITNEY Model JT8D Series Engines
engine Pratt & Whitney Division JT8D-17A PRATT & WHITNEY Model JT8D Series Engines
engine Pratt & Whitney Division JT8D-17AR PRATT & WHITNEY Model JT8D Series Engines
engine Pratt & Whitney Division JT8D-17R PRATT & WHITNEY Model JT8D Series Engines
engine Pratt & Whitney Division JT8D-1A PRATT & WHITNEY Model JT8D Series Engines
engine Pratt & Whitney Division JT8D-1B PRATT & WHITNEY Model JT8D Series Engines

Unsafe Condition

Sixth stage compressor rotor disc failures caused by disc rim front face galling from blade retention tangs.

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

Required Actions

Replace the suspect sixth stage compressor disc with a new, used, or approved reworked disc. Compliance time depends on hours in service since a 6th stage blade failure: engines with 1200+ hours must replace within 600 hours after AD effective date; those with 1200- hours must replace before 1800 hours since the blade failure.

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

Compliance Time

Compliance required as indicated in the AD's specific timeframes based on hours in service since a 6th stage blade failure.

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

Affected Aircraft

Pratt & Whitney JT8D series engines with sixth stage compressor discs P/N 586906 (wide rim) that had prior blade failures and weren't reworked per SE:RWJ:9-6-24-1 dated 24 June 1969.

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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