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Airworthiness Directives; Honeywell KC 225 Automatic Flight Control Systems

airworthiness · Rule · Final rule; request for comments. · Published 2001-05-23 · Effective 2001-06-15 · 66 FR 28361

Document

Document number
01-12634
Federal Register citation
66 FR 28361
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2001-05-23
Effective date
2001-06-15
FAA docket
Docket No. 2001-CE-08-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Honeywell KC 225 automatic flight control systems (AFCS) that are installed on airplanes. This AD requires you to inspect the KC 225 AFCS to determine the computer modifications (Mods) that are incorporated, deactivate any units with only Mods 1 and/or 2 incorporated, and fabricate and install an appropriate placard if the unit is deactivated/inoperative. The AD would provide, as an alternative method of compliance, the option of installing a unit that incorporated MOD 3 or higher. This AD is the result of several reports that the AFCS is disconnecting without warning in a gross mistrim configuration. The actions specified by this AD are intended to prevent an undesirable autotrim command that the autopilot cannot detect in the required time. The airplane could then deviate from the selected altitude or the autopilot could disconnect without warning, which could result in heavy loads at the control column. Such loads in the pitch axis could result in loss of control of the airplane.

Source

Authoritative
Federal Register document
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