AD 2003-24-12

final rule
Data completeness: 70%

Airworthiness Directives; Pratt & Whitney JT9D-3A, -7, -7A, -7F, -7H, -7AH, and -7J Turbofan Engines

AD Number
2003-24-12
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2003-NE-52-AD
FR Citation
68 FR 67585

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney JT9D-3A Airworthiness Directives; Pratt & Whitney JT9D-3A, -7, -7A, -7F, -7H, -7AH, and -7J Turbofan Engines

Unsafe Condition

Failed gearbox pressure tube or failed No. 4 bearing front pressure manifold, potentially leading to engine fire due to oil leakage and vibration-induced movement.

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

Required Actions

Visually inspect the clamp assemblies (P/Ns ST1594-06, ST1594-08, ST1594-10) for wear, damage, or missing rubber cushions, and replace if necessary. Visually inspect the gearbox pressure tube (P/N 697896) and No. 4 bearing front pressure manifold (P/N 670663) for nicks, dents, corrosion, or oil leaks, and repair or replace if necessary. Ensure all components are correctly positioned.

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

Compliance Time

Within 250 hours-in-service or at the next shop visit, whichever occurs first, after the effective date.

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

Affected Aircraft

Pratt & Whitney JT9D-3A, -7, -7A, -7F, -7H, -7AH, and -7J turbofan engines with gearbox pressure tube (P/N 697896) and No. 4 bearing front pressure manifold (P/N 670663) installed.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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