AD 77-01-07

final rule
Data completeness: 60%

PRATT & WHITNEY AIRCRAFT Models JT9D-3A, -7, -7H, -7A, -7AH, -7F and -20 Engines

AD Number
77-01-07
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Division JT9D-20 PRATT & WHITNEY AIRCRAFT Models JT9D-3A, -7, -7H, -7A, -7AH, -7F and -20 Engines
engine Pratt & Whitney Division JT9D-3A PRATT & WHITNEY AIRCRAFT Models JT9D-3A, -7, -7H, -7A, -7AH, -7F and -20 Engines
engine Pratt & Whitney Division JT9D-7 PRATT & WHITNEY AIRCRAFT Models JT9D-3A, -7, -7H, -7A, -7AH, -7F and -20 Engines
engine Pratt & Whitney Division JT9D-7A PRATT & WHITNEY AIRCRAFT Models JT9D-3A, -7, -7H, -7A, -7AH, -7F and -20 Engines
engine Pratt & Whitney Division JT9D-7AH PRATT & WHITNEY AIRCRAFT Models JT9D-3A, -7, -7H, -7A, -7AH, -7F and -20 Engines
engine Pratt & Whitney Division JT9D-7F PRATT & WHITNEY AIRCRAFT Models JT9D-3A, -7, -7H, -7A, -7AH, -7F and -20 Engines
engine Pratt & Whitney Division JT9D-7H PRATT & WHITNEY AIRCRAFT Models JT9D-3A, -7, -7H, -7A, -7AH, -7F and -20 Engines

Unsafe Condition

Cracking and possible failure of fifth stage turbine hubs due to cyclic life limits exceeding approved figures.

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

Required Actions

Remove from service fifth stage turbine hubs prior to reaching the revised life limits (listed by part number) or within the next 25 cycles after the AD's effective date, whichever is later. Operators may request FAA approval to adjust the 25-cycle compliance interval with substantiating data.

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

Compliance Time

within the next 25 cycles in service after the effective date of this AD

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

Affected Aircraft

Pratt & Whitney Aircraft JT9D-3A, -7, -7H, -7A, -7AH, -7F and -20 engines with fifth stage turbine hubs P/N 704705, 714905, 718905, 719205, and 726805.

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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