Airworthiness Directive · Amendment 39-12885 · Bell Helicopter Textron, Inc. Model 212 Helicopters
Bell Helicopter Textron, Inc. Model 212 Helicopters
Model 212 helicopters, with a vertical fin spar cap, part number (P/N) 212-030-125-001, with retrofit kit, P/N 212- 704-087, installed; vertical fin left-hand spar cap (spar cap), P/N 212-030-125-001, without the retrofit kit installed; or spar cap, P/ N 212-030-447-001 or P/N 212-030-447-101, installed, certificated in any category.
This amendment supersedes an existing airworthiness directive (AD) for Bell Helicopter Textron, Inc. (BHTI) Model 212 helicopters that currently requires, at specified intervals, inspecting for a cracked tail boom and replacing any cracked tail boom. That AD also requires modifying the tail fin and tail boom within 100 hours time-in- service (TIS). This amendment requires modifying and visually inspecting certain vertical fin left-hand spar caps for cracking, loose fasteners, corrosion, or disbonding. If corrosion or loose fasteners are found, this AD requires repairing the vertical fin left-hand spar cap (spar cap) and if a crack or disbonding is found, replacing any cracked or disbonded part with an airworthy part. This AD also requires replacing certain spar caps within 24 months. This AD is prompted by an accident and four failures of the spar cap involving helicopters of similar type design. The actions specified by this AD are intended to prevent failure of a vertical fin spar, loss of a tail rotor, and subsequent loss of control of the helicopter.
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.
