Airworthiness Directive

AD 2007-11-02 Amendment 39-15059

Federal Aviation Administration · 14 CFR part 39

FR document
E7-16770
Amendment
39-15059
Published
2007-08-28
Models covered
1
Last live check
Not yet re-verified
AD

2007-11-02

FR doc E7-16770

AD 2007-11-02Published 2007-08-28Effective 2007-10-02

Requires determining the installation dates for each main rotor push-pull control rod (push-pull rod), inspecting the push-pull rods for corrosion, replacing any push-pull rod which has corrosion that is severe enough to cause…

Full official abstract

This amendment adopts a new airworthiness directive (AD) for Enstrom Helicopter Corporation (Enstrom) Model F-28A, F-28C, F-28F, TH- 28, 280, 280C, 280F, 280FX, 480, and 480B helicopters that requires determining the installation dates for each main rotor push-pull control rod (push-pull rod), inspecting the push-pull rods for corrosion, replacing any push-pull rod which has corrosion that is severe enough to cause pitting, or has visible moisture inside the rod, and repairing each push-pull rod that has corrosion but no pitting. This amendment is prompted by one reported incident in which the helicopter pilot encountered severe in-flight vibration due to the failure of a push-pull rod, requiring an emergency landing. The actions specified by this AD are intended to detect corrosion and prevent failure of a push-pull rod, and subsequent loss of control of the helicopter.

Applies to 1 model in our index