Airworthiness Directives; The Cessna Aircraft Company Model 525 Airplanes
airworthiness · Rule · Final rule; request for comments · Published 2003-10-21 · Effective 2003-10-22 · 68 FR 60028
Document
Document number
03-26276
Federal Register citation
68 FR 60028
Type
Rule
Action
Final rule; request for comments
Category
airworthiness
Manufacturer
The Cessna
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.