AD 2003-13-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | Allison | Engine Company | Airworthiness Directives; Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) Models 250-C30R/3, -C30R/3M, -C47B, and -C47M Turboshaft Engines; Correction |
Unsafe Condition
This document makes a correction to Airworthiness Directive (AD) 2003-13-10, applicable to Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) Models 250-C30R/3, -C30R/3M, -C47B, and -C47M turboshaft engines. AD 2003-13-10 was published in the Federal Register on June 30, 2003 (68 FR 38590). In the compliance section, paragraph (f) incorrectly references a compliance date of July 15, 2003 and should reference a compliance date of...
Required Actions
Review and comply with the corrected compliance date of July 31, 2003 for the existing AD requirements.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight after July 31, 2003.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Rolls-Royce Corporation (formerly Allison Engine Company) Models 250-C30R/3, -C30R/3M, -C47B, and -C47M turboshaft 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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