# 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
> **Rule** · Final rule; request for comments, correction. · Published 2003-07-16 · 68 FR 41906
## Document
- **Document number:** 03-17950
- **Category:** airworthiness
- **Manufacturer:** Rolls-Royce Corporation (formerly Allison
- **Type:** Rule
- **Action:** Final rule; request for comments, correction.
- **Citation:** 68 FR 41906
- **Publication date:** 2003-07-16
- **FAA docket:** Docket No. 2003-NE-23-AD
## Abstract

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 July 31, 2003. This document corrects that date. In all other respects, the original document remains the same.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2003/07/16/03-17950/airworthiness-directives-rolls-royce-corporation-formerly-allison-engine-company-allison-gas-turbine)
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