Airworthiness Directive · Amendment 39-12882 · Turbomeca S.A. Makila Models 1A, 1A1, and 1A2 Turboshaft Engines
Turbomeca S.A. Makila Models 1A, 1A1, and 1A2 Turboshaft Engines
This airworthiness directive (AD) is applicable to Turbomeca S.A. Makila models 1A, 1A1, and 1A2 turboshaft engines with exhaust pipes incorporating modification TU 200A installed. These engines are installed on, but not limited to, Aerospatiale AS 332 "Super Puma Mark I" C, C1, L, L1, and "Super Puma Mark II" L2 helicopters.
This amendment adopts a new airworthiness directive (AD) that is applicable to Turbomeca S.A. Makila Models 1A, 1A1, and 1A2 turboshaft engines with exhaust pipes incorporating modification TU 200A installed. This action requires visual inspections of exhaust pipes for cracks and tears, upon completion of the last flight of each day, and replacement of cracked and torn exhaust pipes before further flight. This action also requires removal from service of modification TU 200A exhaust pipes at the next shop visit or no later than a certain date. This amendment is prompted by several reports of modification TU 200A exhaust pipes cracking at several of the ejector attachment tabs. The actions specified in this AD are intended to prevent the ejector from becoming loose from the exhaust pipe, resulting in damage to the main rotor and tail rotor and loss of helicopter control.
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.
