# Airworthiness Directives; The Cessna Aircraft Company Model 525 Airplanes
> **Rule** · Final rule; request for comments · Published 2003-10-21 · Effective 2003-10-22 · 68 FR 60028
## Document
- **Document number:** 03-26276
- **Category:** airworthiness
- **Manufacturer:** The Cessna
- **Type:** Rule
- **Action:** Final rule; request for comments
- **Citation:** 68 FR 60028
- **Publication date:** 2003-10-21
- **Effective date:** 2003-10-22
- **FAA docket:** Docket No. 2003-CE-46-AD
## Abstract

The FAA is adopting a new airworthiness directive (AD) for certain The Cessna Aircraft Company (Cessna) Model 525 airplanes. This AD requires you to disengage the pitch trim circuit breaker and AP servo circuit breaker and then tie strap each of them to prevent them from being engaged. This AD is the result of analysis that reveals the potential for a single-wire shorting to 28 volts or a failure of a relay in the electric pitch trim system such that the relay contacts remain closed. We are issuing this AD to correct this single-point failure in the electric pitch trim system, which will result in a runaway pitch trim condition where the pilot could not disconnect using the control wheel autopilot/trim disconnect switch. Failure of the electric trim system would result in a large pitch mistrim and would cause excessive control forces that the pilot could not overcome.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2003/10/21/03-26276/airworthiness-directives-the-cessna-aircraft-company-model-525-airplanes)
---
*AI Analytics · CC0 1.0*