AD 2005-26-09

final rule
Data completeness: 80%

Airworthiness Directives; Pratt & Whitney JT9D-7R4 Turbofan Engines

AD Number
2005-26-09
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2005-23072
FR Citation
70 FR 76381

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney JT9D-7R4 Airworthiness Directives; Pratt & Whitney JT9D-7R4 Turbofan Engines

Unsafe Condition

A repair station created their own repair and performed it on 520 1st stage fan blades without approval from Pratt & Whitney. This could result in 1st stage fan blade fracture and uncontained engine failure, leading to possible damage to the airplane.

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

Required Actions

Inspect the blade root thickness of 1st stage fan blades identified by part number and serial number in Table 1 of the AD. Remove fan blades without a circled, letter I marking on the outboard side of the blade platform. Send fan blades to a source-substantiation-approved repair station for inspection. Return to service fan blades that pass inspection after proper marking.

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

Compliance Time

Before installing the listed 1st stage fan blades or at the next fan blade exposure if already installed.

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

Affected Aircraft

Pratt & Whitney JT9D-7R4 turbofan engines installed on, but not limited to, Airbus A300, A310, Boeing 747, and 767 airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.