# Airworthiness Directives; Bombardier Model DHC-8-400, -401, and -402 Airplanes
> **Rule** · Final rule. · Published 2004-01-30 · Effective 2004-03-05 · 69 FR 4454
## Document
- **Document number:** 04-1910
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 69 FR 4454
- **Publication date:** 2004-01-30
- **Effective date:** 2004-03-05
- **FAA docket:** Docket No. 2002-NM-311-AD
## Abstract

This amendment adopts a new airworthiness directive (AD); applicable to certain Bombardier Model DHC-8-400, -401, and -402 airplanes; that requires replacing certain flight guidance modules with improved modules, and certain flight control electronic control units with improved units. This action is necessary to prevent loss of the autopilot or manual pitch trim, which may increase the workload of the flightcrew and, under certain conditions, could result in reduced controllability of the airplane. This action is intended to address the identified unsafe condition.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2004/01/30/04-1910/airworthiness-directives-bombardier-model-dhc-8-400--401-and--402-airplanes)
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