Airworthiness Directive

AD 2007-16-01 Amendment 39-15140

Federal Aviation Administration · 14 CFR part 39

FR document
07-3711
Amendment
39-15140
Published
2007-07-31
Models covered
1
Last live check
Not yet re-verified
AD

2007-16-01

FR doc 07-3711

AD 2007-16-01Published 2007-07-31Effective 2007-08-15

Requires a visual check to determine if a certain serial-numbered main rotor blade retention pin (retention pin) is installed, and removing and replacing any affected retention pin with an airworthy retention pin.

Full official abstract

This amendment adopts a new airworthiness directive (AD) for Enstrom Helicopter Corporation (Enstrom) Model F-28, F-28A, F-28C, F- 28C-2, F-28C-2R, F-28F, F-28F-R, 280, 280C, 280F, 280FX, TH-28, 480, and 480B helicopters. This action requires a visual check to determine if a certain serial-numbered main rotor blade retention pin (retention pin) is installed, and removing and replacing any affected retention pin with an airworthy retention pin. This amendment is prompted by a report from the manufacturer that some retention pins were not manufactured in accordance with specifications cited on the engineering drawing. The actions specified in this AD are intended to prevent failure of a retention pin, separation of a main rotor blade from the helicopter, and subsequent loss of control of the helicopter.

Applies to 1 model in our index