AD 2017-23-06

final rule
Data completeness: 80%

Airworthiness Directives; General Electric Company Turbofan Engines

AD Number
2017-23-06
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2017-1000
FR Citation
82 FR 52830

Applicability

TypeManufacturerModelDetails
engine General Electric Company Airworthiness Directives; General Electric Company Turbofan Engines

Unsafe Condition

Malfunctions related to the operability bleed valve (OBV) have led to significant fuel leaks, some resulting in engine fires.

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

Required Actions

Inspect the bleed air manifold link rod assemblies and the supply, return, and drain fuel fittings on the OBVs.

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

Compliance Time

Before further flight

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

Affected Aircraft

General Electric Company CF34-8C1, CF34-8C5, CF34-8C5A1, and CF34-8C5B1 engines with serial numbers 965101 through 965670, 194101 through 194999, and 195101 through 195653.

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

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