Airworthiness Directive

AD 2005-10-08 70 FR 28186

Federal Aviation Administration · 14 CFR part 39

FR document
05-9467
Amendment
39-14085
Published
2005-05-17
Models covered
1
Last live check
2026-08-17
AD

2005-10-08

FR doc 05-9467 · 70 FR 28186

AD 2005-10-08Published 2005-05-17Effective 2005-06-21

Requires operators to install torque tube catchers on the control columns of the flight controls.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This AD requires operators to install torque tube catchers on the control columns of the flight controls. This AD is prompted by the discovery that a single malfunction of the torque tube could result in both flight control columns being supported by only one self-aligning bearing. We are issuing this AD to prevent the torque tube from fouling against the underfloor control cables, which could result in reduced controllability of the airplane.

Applies to 1 model in our index