AD 2017-12-02

final rule
Data completeness: 80%

Airworthiness Directives; General Electric Company Turbofan Engines

AD Number
2017-12-02
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2017-0016
FR Citation
82 FR 26580

Applicability

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

Unsafe Condition

Fracture of the outer left side signal fuel manifold, part number 2403M46G01, which can lead to in-flight engine shutdown, engine fire, and damage to the airplane.

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

Required Actions

Replace the outer left side signal fuel manifold with a part eligible for installation. Use GE service bulletins, including GEnx-1B SB 73-0053 R00, as guidance for replacement.

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

Compliance Time

Within 12 months of the effective date (July 13, 2017).

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

Affected Aircraft

General Electric Company GEnx-1B64, -1B64/P1, -1B64/P2, -1B67, -1B67/P1, -1B67/P2, -1B70, -1B70/P1, -1B70/P2, -1B70/75/P1, -1B70/75/P2, -1B70C/P1, -1B70C/P2, -1B74/75/P1, -1B74/75/P2, -1B76A/P2 turbofan engines with outer left side signal fuel manifold, part number 2403M46G01, and CAGE code 05813, installed.

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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