Williams FJ33

Diameter

466.344 mm

Length

976.122 mm

Dry Weight

136.0777 kg

Thrust To Weight

Specific Fuel Consumption

13.766 g/(kN·s)

Architecture

Fan	Fan Stages —	Fan Blades —	Fan Technology —	Fan Pressure Ratio —
Gearbox	Geared Fan No	Gear —	Reduction Ratio —
LP compressor	Low-Pressure Compressor Stages —	Low-Pressure Compressor Technology —	BP Compressor Pressure Ratio —
IP compressor	Intermediary-Pressure Compressor Stages —	Intermediary-Pressure Compressor Technology —	IP Compressor Pressure Ratio —
HP compressor	High-Pressure Compressor Stages —	High-Pressure Compressor Technology —	HP Compressor Pressure Ratio —
Combustor	Combustion Chamber —
HP turbine	High Pressure Compressor Stages —	High-Pressure Turbine Technology —
IP turbine	Intermediary-Pressure Turbine Stages —	Intermediary-Pressure Turbine Technology —
LP turbine	Low-Pressure Turbine Stages —	Low-Pressure Turbine Technology —
Whole engine	Streams 2	Bypass Ratio —	Overall Pressure Ratio —	Afterburner No

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Name	Aircraft Engine	Number of Engines	Length (m)	Flat Wing Span (m)
ATG Javelin	Williams FJ33	2	11.28	7.65
Cirrus Vision SF50	Williams FJ33	1	9.42	11.8
Flaris LAR01	Williams FJ33	1	8.32	8.68

All data (14 fields)

Name: Williams FJ33
Aircraft Engine Manufacturer: TEM (Turbine Engine Manufacturing)
Aircraft Engine Type: Turbofan
Dry Weight (kg): 136.0777
Diameter (mm): 466.344
Length (mm): 976.122
Wikipedia Article (URL): en.wikipedia.org/wiki/Williams_FJ33
Geared Fan: No
Afterburner: No
Streams: 2
Thrust To Weight: 6
Specific Fuel Consumption (g/(kN·s)): 13.766
Compressor Description: 2 spool, 1-stage fan and 3-stage LP axial, 1 HP centrifugal
Turbine Description: 2 spool, 1 HP and 2 LP