2018-02-01
FR doc 2018-00659 · 83 FR 2366AD 2018-02-01Published 2018-01-17Effective 2018-02-21
Supersedes 2015-08-51
Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.
Requires establishing a life limit and a recurring inspection.
Full official abstract
We are superseding Airworthiness Directive (AD) 2015-08-51 for the Enstrom Helicopter Corporation (Enstrom) Model F-28A, 280, F-28C, F-28C-2, F-28C-2R, 280C, F-28F, F-28F-R, 280F, 280FX, and 480 helicopters. AD 2015-08-51 required an inspection of the main rotor spindle (spindle) and reporting the inspection results to the FAA. This new AD was prompted by additional reports of cracked spindles and requires establishing a life limit and a recurring inspection. The actions of this AD are intended to prevent the unsafe condition on these products.
More directives for Enstrom F-28 / 280 / 480
- AD 2017-26-03 Airworthiness Directives; The Enstrom Helicopter Corporation Helicopters Effective 2018-01-04
- AD 2015-08-51 Airworthiness Directives; The Enstrom Helicopter Corporation Effective 2015-06-02
- AD 2012-11-05 Airworthiness Directives; Enstrom Helicopter Corporation Helicopters Effective 2012-07-03
- AD 2011-26-10 Airworthiness Directives; Enstrom Helicopter Corporation Helicopters Effective 2012-01-23
- AD 2007-11-02 Airworthiness Directives; Enstrom Helicopter Corporation Model F-28A, F-... Effective 2007-10-02
