# Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, -314, and -315 Series Airplanes
> **Rule** · Final rule; correction. · Published 2001-08-27 · Effective 2001-08-10 · 66 FR 44958
## Document
- **Document number:** 01-21490
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 66 FR 44958
- **Publication date:** 2001-08-27
- **Effective date:** 2001-08-10
- **FAA docket:** Docket No. 2000-NM-45-AD
## Abstract

This document corrects information in an existing airworthiness directive (AD) that applies to all Bombardier Model DHC- 8-102, -103, -106, -201, -202, -301, -311, -314, and -315 series airplanes. That AD currently requires revising the Bombardier maintenance program to incorporate repetitive inspections to detect fatigue cracking in certain structures; and corrective actions, if necessary. This document corrects certain airplane models specified in Table 1 of the final rule. This correction is necessary to ensure that operators are notified of the correct airplane models, as specified in Canadian airworthiness directive CF-2000-07, dated March 3, 2000, and de Havilland Temporary Revision TR AWL 2-15, dated September 3, 1999.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2001/08/27/01-21490/airworthiness-directives-bombardier-model-dhc-8-102--103--106--201--202--301--311--314-and--315)
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