Sikorsky’s S76 is a popular mid size corporate and oil rig support helicopter.
Sikorsky began development work on the S76 (for a time named Spirit) in the mid 1970s and used technologies and experience gained from the military S70 Black Hawk program. The resulting S-76A was powered by two Allison 250C30S turboshafts and could seat 12. First flight was on March 13 1977 and FAA certification was awarded in November 1978.
Current production is of the S76C+ with 18% more powerful FADEC equipped Arriel 2S1 engines. Certification of the C+ was awarded in mid 1996. Forthcoming improvements include composite blades, a quiet tail rotor with curved blades, an active noise and vibration control system, and an advanced health and usage monitoring system. A three LCD screen integrated instrument display system (IIDS) for engine and rotor information is now standard, supplementing the four screen Honeywell EFIS suite.
Along with the calculations of Weight & Balance we have included a section of the performances more useful when planning a flight.
Click on the next icon to test version of limited use.
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| The program presents in a graphical way all the possible loading stations related to the longitudinal balance. You just have to click the seats or scroll the load bars to the right position. Also with a click you can select the takeoff and landing fuel. | At a glance you can check the status of longitudinal W&B in the most critical situations with a clear color code in a scaled schema. | |
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| This feature calculates the maximum Gross Weight for hover Out of Ground Effect depending on Pressure Altitude and Temperature or you can calculate the best altitude for maximum range. | This database stores the data for each aircraft weight along with the date and registration. | |
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