Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airplanes
airworthiness · Rule · Final rule. · Published 2007-08-21 · Effective 2007-09-25 · 72 FR 46542
Document
Document number
E7-16288
Federal Register citation
72 FR 46542
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Mitsubishi Heavy Industries MU-2B Series
Publication date
2007-08-21
Effective date
2007-09-25
FAA docket
Docket No. FAA-2007-27191
Abstract
We are adopting a new airworthiness directive (AD) to supersede 93-07-11 and AD 94-04-16, which apply to certain Mitsubishi Heavy Industries MU-2B series airplanes. AD 93-07-11 and AD 94-04-16 currently require you to reduce the maximum deflection of the elevator nose-down trim to a 1-degree to 3-degree range. When the above AD actions were issued, there was no associated elevator trim indicator change. Without such change, the trim reaches the maximum nose-down limit and the indicator still shows additional nose-down trim available. In attempting to force additional nose-down trim, pilots have manually jammed the trim system preventing subsequent electric trim changes until the pilot manually freed the trim wheel. Consequently, this AD retains the actions from AD 93-07-11 and AD 94- 04-16 and adds the action of modifying the elevator trim indicator scale dial to be consistent with the reduced elevator trim capability. We are issuing this AD to prevent the above scenarios from occurring with consequent loss of control.