Airworthiness Directives; Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes
airworthiness · Rule · Final rule. · Published 2000-01-11 · Effective 2000-03-03 · 65 FR 1540
Document
Document number
00-537
Federal Register citation
65 FR 1540
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Fairchild
Publication date
2000-01-11
Effective date
2000-03-03
FAA docket
Docket No. 98-CE-84-AD
Abstract
This amendment revises Airworthiness Directive (AD) 98-19-15, which currently requires incorporating information into the Limitations Section of the airplane flight manual (AFM) that imposes a speed restriction and a minimum pilot requirement for Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes equipped with Barber- Colman pitch trim actuators, part number (P/N) 27-19008-001/-004 or P/N 27-19008-002/-005. Since AD 98-19-15 became effective, improved design pitch trim actuators have been developed that, when installed, will eliminate the speed restriction and minimum pilot requirements of the current AD. This AD requires incorporating these installations as a method of complying with the current AD. The actions specified by this AD are intended to lessen the possibility of airplane pitch up caused by mechanical failure of the pitch trim actuator, which could result in a pitch upset and structural failure of the airplane.