AD 2010-23-20

final rule
Data completeness: 70%

Airworthiness Directives; General Electric Company (GE) CT7-9C and -9C3 Turboprop Engines

AD Number
2010-23-20
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2010-0732
FR Citation
75 FR 70096

Applicability

TypeManufacturerModelDetails
aircraft General Electric Company (GE) CT7-9C and -9C3 Turboprop Airworthiness Directives; General Electric Company (GE) CT7-9C and -9C3 Turboprop Engines

Unsafe Condition

Nonconforming land balance-cuts on gas generator turbine (GGT) shafts, part number 6068T44P02, could result in the shaft failing before its published life limit, leading to an uncontained engine failure and damage to the airplane.

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

Required Actions

Inspect the GGT shafts listed in Table 1 for nonconforming land balance-cuts using GE CT7-TP Alert Service Bulletin 72-A0501, Revision 01. If nonconforming cuts are found, remove the shaft from service.

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

Compliance Time

At the first shop visit after the effective date of this AD, or within 5,000 cycles since-new, whichever occurs first.

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

Affected Aircraft

General Electric Company CT7-9C and -9C3 turboprop engines with gas generator turbine (GGT) shafts, part number 6068T44P02, and serial numbers listed in Table 1 of the AD. These engines are installed on, but not limited to, EADS CASA CN-235 series airplanes.

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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