Airworthiness Directives; EMBRAER Model EMB-145 Series Airplanes
airworthiness · Rule · Final rule. · Published 2000-05-12 · Effective 2000-06-16 · 65 FR 30539
Document
Document number
00-11547
Federal Register citation
65 FR 30539
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
EMBRAER Model EMB-145 Series
Publication date
2000-05-12
Effective date
2000-06-16
FAA docket
Docket No. 99-NM-305-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD), applicable to certain EMBRAER Model EMB-145 series airplanes, that currently requires revisions to the Airplane Flight Manual (AFM) to provide the flight crew with updated procedures for prohibiting use of the autopilot below 1,500 feet above ground level, emergency procedures for pitch trim runaway, and abnormal procedures for autopilot trim failure and stabilizer out of trim. That AD also requires installation of certain warning placards. This amendment requires replacement of a certain integrated computer with a new integrated computer; installation of an upgraded integrated computers checklist; and removal of certain placards and certain limitations in the AFM. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent failure of the pitch trim system, which could cause undetected autopilot trim runaway, and consequent reduced controllability of the airplane, uncommanded autopilot disconnect, and excessive altitude loss.