AD 2003-09-14

final rule
Data completeness: 70%

Airworthiness Directives; General Electric CF34-8C1 Turbofan Engines

AD Number
2003-09-14
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2002-NE-23-AD
FR Citation
68 FR 24614

Applicability

TypeManufacturerModelDetails
engine General Electric CF34-8C1 Airworthiness Directives; General Electric CF34-8C1 Turbofan Engines

Unsafe Condition

Rupture of the combustion chamber assembly and possible engine fire due to stress and life analysis conducted by GE.

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

Required Actions

Replace combustion chamber assemblies, part number 4126T87G04, before accumulating a new reduced cyclic life limit.

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

Compliance Time

Before accumulating a new reduced cyclic life limit.

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

Affected Aircraft

General Electric CF34-8C1 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

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

View Official Source ↗ Find More ADs for General Electric CF34-8C1

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