AD 2017-20-09

final rule
Data completeness: 70%

Airworthiness Directives; General Electric Company Turbofan Engines

AD Number
2017-20-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2017-0254
FR Citation
82 FR 46669

Applicability

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

Unsafe Condition

Using a certain repair procedure for the fan outlet guide vane (OGV) frame could alter the strength capability of the fan OGV frame.

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

Required Actions

Replace all fan OGV frames repaired using the specified procedure.

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

Compliance Time

Within the compliance times specified in the AD, unless already done.

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

Affected Aircraft

All General Electric Company (GE) CF34-8E2, CF34-8E2A1, CF34-8E5, CF34-8E5A1, CF34-8E5A2, CF34-8E6, and CF34-8E6A1 model turbofan engines.

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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