Airworthiness Directive

AD 2006-17-17 71 FR 50331

Federal Aviation Administration · 14 CFR part 39

FR document
E6-13966
Amendment
39-14738
Published
2006-08-25
Models covered
1
Last live check
2026-08-17
AD

2006-17-17

FR doc E6-13966 · 71 FR 50331

AD 2006-17-17Published 2006-08-25Effective 2006-09-29

Requires inspecting the left and right control column torque tube assemblies to determine the type of rivets installed and replacing incorrect or indeterminate type rivets with the correct type rivets.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-100, DHC-8-200, DHC-8-300, and DHC-8-400 series airplanes. This AD requires inspecting the left and right control column torque tube assemblies to determine the type of rivets installed and replacing incorrect or indeterminate type rivets with the correct type rivets. This AD results from a report that incorrect rivets having lower than required strength were installed on the control column torque tube during production. We are issuing this AD to prevent shear failure of control column torque tube rivets, which could cause unexpected decoupling of the elevators and large unwanted deflection of the free elevator, and consequent reduced controllability of the airplane.

Applies to 1 model in our index