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Rolls-Royce AE / Turboprop / Powered flight / Turbocharger / Propulsion / Aviation / Aircraft engines / Gas turbines / Jet engines


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Document Date: 2010-07-09 11:20:37


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City

Indianapolis / /

Company

Overall Length Overall Height (max.) AE / Rolls-Royce Corporation AE / Takeoff (5minutes) Maximum Continuous Transient AE / Grade JP8 Fuel Specifications AE / E.040 Rolls-Royce Corporation AE / P/N 23060202 AE / Unison Industries Inc. / Model AE / Fuel Specifications AE / KW (4152 HP) AE / 2100D2 AE / kPa (55 psig) AE / HP / AE 2100 AE / P/N 23053610 AE / Service Bulletin AE / kPa (52 psig) AE / Turbine 15404 15558 15375 16298 Prop Shaft AE / Goodrich / 2100A AE / Series Engines Variants AE / KW (4637 HP) AE / Manual Engine Operation Manual Engine Maintenance Manual AE / 14th Stage AE / ITT / /

Country

United States / United States of America / /

IndustryTerm

oil conforming / maximum oil pressure / engine control equipment / high energy type exciters / /

Organization

Federal Aviation Administration / Metering Unit / United Nations / AE 2100D2 Engine Assembly / AE 2100A Engine Assembly / European Union / AE 2100D2A Engine Assembly / /

/

Position

General / /

Product

2100D2A 3458 KW / Section 275.8 kPa 275.8 kPa 275.8 kPa 275.8 / T-5624 Grade / E150 / iRiver E30 Portable Audio Device / 2100D2 3458 KW / Series Engines Issue 01 / A-1 / /

ProvinceOrState

Indiana / /

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