GE CF-700 18kN turbofan engine maintenance manual and illustrated parts catalogue

[m13katyusa2020]

GE CF-700 18kN turbofan engine maintenance manual and illustrated parts catalogue on public websites, whose thrust was capable for Learjet 35 jet.

General Characteristics:
Length: 75.5 in (1,918 mm)
Diameter: 33 in (838 mm)
Dry weight: 735 lb (333.4 kg) with optional thrust reverser
Compressor: 8 stage high pressure compressor + 1 stage fan directly driven by the free LP turbine
Turbine: 2 stage high pressure turbine, 1 stage low pressure turbine
Fuel type: Aviation kerosene
Maximum thrust: 4,200 lbf (18.68 kN)
Bypass ratio: 2.0:1 Air mass flow: 84 lb (38 kg)/s through the fan
Specific fuel consumption: 0.67 lb/lbf·hr (68.3·kg/kN·h) at maximum cruising speed
Thrust-to-weight ratio: 6.6
Addition: CF-700 historical pdf OM thanks to user MikeJohnson96:

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Disclaimer: These items are shared for reference, sharing for non-profitable use only.
This manuals and blueprints are not meant to be used for current update material for certification / repair, but make an excellent reference for the scholar, collector, modeler or aircraft buffs .... For proprietary reasons we generally only provide civil manuals and blueprints on long-time out-of-production Aircraft / Engines / Helicopter. The information is for reference only and we do not guarantee the accuracy or currency of any manuals.

Reference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.

 

[m13katyusa2020]

GE CF-700 18kN turbofan engine maintenance manual and illustrated parts catalogue on public websites, whose thrust was capable for Learjet 35 jet.
View attachment 669137View attachment 669139
General Characteristics:
Length: 75.5 in (1,918 mm)
Diameter: 33 in (838 mm)
Dry weight: 735 lb (333.4 kg) with optional thrust reverser
Compressor: 8 stage high pressure compressor + 1 stage fan directly driven by the free LP turbine
Turbine: 2 stage high pressure turbine, 1 stage low pressure turbine
Fuel type: Aviation kerosene
Maximum thrust: 4,200 lbf (18.68 kN)
Bypass ratio: 2.0:1 Air mass flow: 84 lb (38 kg)/s through the fan
Specific fuel consumption: 0.67 lb/lbf·hr (68.3·kg/kN·h) at maximum cruising speed
Thrust-to-weight ratio: 6.6
Disclaimer: These items are shared for reference, sharing for non-profitable use only.
This manuals and blueprints are not meant to be used for current update material for certification / repair, but make an excellent reference for the scholar, collector, modeler or aircraft buffs .... For proprietary reasons we generally only provide civil manuals and blueprints on long-time out-of-production Aircraft / Engines / Helicopter. The information is for reference only and we do not guarantee the accuracy or currency of any manuals.

Reference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.

For materials of the engine, refer to Basic Aircraft Materials and treatment:

Basic Aircraft materials chemical composition, treatment and properties books and manuals thread

was written by George_F.Titterton, who was a top-grade engineer of Grumman Company. He was a knowledgable engineer, who was gone in 1998, at an age of 95 years old. Disclaimer: This item is shared for reference, for non-profitable use only. This manuals and blueprints are not meant to be used...

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