Airworthiness Directive

AD 2010-24-03 75 FR 71532

Federal Aviation Administration · 14 CFR part 39

FR document
2010-29203
Amendment
39-16521
Published
2010-11-24
Models covered
2
Last live check
2026-08-17
AD

2010-24-03

FR doc 2010-29203 · 75 FR 71532

AD 2010-24-03Published 2010-11-24Effective 2010-12-29

Requires visually inspecting each tail rotor (T/R) control pedal bearing block support (support) for a crack, measuring the thickness of each support, installing support safety tabs on certain supports, and replacing supports of…

Full official abstract

This amendment adopts a new airworthiness directive (AD) for Robinson Model R22, R22 Alpha, R22 Beta, and R22 Mariner helicopters, and Model R44 and R44 II helicopters. This AD requires visually inspecting each tail rotor (T/R) control pedal bearing block support (support) for a crack, measuring the thickness of each support, installing support safety tabs on certain supports, and replacing supports of a certain thickness during the next 2,200 hour overhaul. This amendment is prompted by two reports of Model R22 helicopters experiencing broken supports during flight, which resulted in the T/R control pedals becoming jammed. The actions specified by this AD are intended to prevent the supports from breaking, which can bind the T/R control pedals, resulting in a reduction of yaw control and subsequent loss of control of the helicopter.

Applies to 2 models in our index