airworthiness · Rule · Final rule. · Published 2006-07-17 · Effective 2006-08-21 · 71 FR 40385
Document
Document number
06-6225
Federal Register citation
71 FR 40385
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Twin Commander
Publication date
2006-07-17
Effective date
2006-08-21
FAA docket
Docket No. FAA-2006-23785
Abstract
We are adopting a new airworthiness directive (AD) for all Twin Commander Aircraft Corporation (Twin Commander) Models 690, 690A, and 690B airplanes. This AD requires you to inspect, visually and using fluorescent dye penetrant, the support structures for the inboard and center aileron hinge fittings on both wings for cracks and replace any cracked support structure. This AD requires you to reinforce the support structures for the inboard and center aileron hinge fittings on both wings. This AD results from reports that cracks were found in the support structures for the inboard and center aileron hinge fittings on both wings. We are issuing this AD to detect and correct cracks in the support structures for the inboard and center aileron hinge fittings on both wings, which could result in aileron failure. This failure could lead to reduced controllability or loss of control of the airplane.