CFM56- 7B TAKE-OFF ENGINE PERFORMANCE WITH THRUST 26300 LB AND 24200 LB

Joseph Pradana Hutamadi

Abstract

As an one of engine manufacturers, CFM produces CFM56-7B with some thrust rating versions to fulfill market demand. In this case, operator has some considerations in choosing engine which is appropriate with the demand. The engine performance is very important to be considered, especially the engine capabilities when it is being maximally operated in takeoff phase.This research discusses about the CFM56-7B engine takeoff performance comparison between 26300 lbs and 24200 lbs thrust rating configuration. By processing Test Cell Result data using formula in Engine Shop Manual - 003, author did a performance calculation to know how much the difference that happened to both of those thrust rating configuration.

Keywords

Engine; Performance; CFM-567B; Thrust

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References

Desianto Duapadang. 2017. Analisis Perhitungan Engine Performance CFM56-7B Dengan Versi Thrust rating 26300 lbs Pada Take-Off Position. Sekolah Tinggi Teknologi Adisutjipto. Yogyakarta

Mattingly, J.D., 2005, “Elements of Gas Turbine Propulsion”. American Institute of Aeronautics and Astronautics.

Sri Mulyani. 2006. Analisis Performa Engine Turbofan Pesawat Boeing 737-300, Sekolah Tinggi Teknologi Adisutjipto. Yogyakarta

Ackert, Shannon. 2011. “Engine Maintenance Concepts for Financiers”. Aircraft Monitor.

Butterworth-Heinemann, 2014, Civil Jet Aircraft Design.

Boeing. 2017. Boeing 737-600/700/800/900 Aircraft maintenance Manual BoeingCompany. Seattle, USA

CFM. 2017, CFM56-7B Engine Shop Manual – 72-00-00-760-003-0-00-PGK-13-003 NA-0 “Engine Assembly – EngineTest 003 – Engine accepatance Test”. France

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