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Gasoline engine / 3-cylinder / liquid-cooled - max. 24.2 kW (32.4 HP), Tier2 | WG972-E2
Model WG972-E2
Emission Regulation Tier2
Type Vertical 4-cycle liquid cooled Gasoline engine
Number of Cylinders 3
Bore mm(in) 74.5(2.93)
Stroke...
Emission Regulation Tier2
Type Vertical 4-cycle liquid cooled Gasoline engine
Number of Cylinders 3
Bore mm(in) 74.5(2.93)
Stroke...
Gasoline engine / 3-cylinder / liquid-cooled - max. 24.2 kW (32.4 HP), Tier2 | WG972-E2
Model WG972-E2
Emission Regulation Tier2
Type Vertical 4-cycle liquid cooled Gasoline engine
Number of Cylinders 3
Bore mm(in) 74.5(2.93)
Stroke mm(in) 73.6(2.90)
Displacement L (cu.in) 0.962(58.7)
Maximum Speed rpm 3600
Output:
Gross Intermittent kW 24.2
hp 32.4
ps 32.9
Direction of Rotation Counterclockwise Viewed on Flywheel
Fuel Unleaded Gasoline
Starter Capacity V-kW 12-1.0
Alternator Capacity V-A 12-480
Length mm (in) 442.6(17.40)
Width mm (in) 402.0(15.80)
Height mm (in) 503.1(19.80)
Dry Weight kg (lb) 72.0(159.0)
Emission Regulation Tier2
Type Vertical 4-cycle liquid cooled Gasoline engine
Number of Cylinders 3
Bore mm(in) 74.5(2.93)
Stroke mm(in) 73.6(2.90)
Displacement L (cu.in) 0.962(58.7)
Maximum Speed rpm 3600
Output:
Gross Intermittent kW 24.2
hp 32.4
ps 32.9
Direction of Rotation Counterclockwise Viewed on Flywheel
Fuel Unleaded Gasoline
Starter Capacity V-kW 12-1.0
Alternator Capacity V-A 12-480
Length mm (in) 442.6(17.40)
Width mm (in) 402.0(15.80)
Height mm (in) 503.1(19.80)
Dry Weight kg (lb) 72.0(159.0)
Gasoline engine / 3-cylinder / liquid-cooled - max. 18.3 kW (24.5 HP), Tier2 | WG752-E2
Model WG752-E2
Emission Regulation Tier2
Type Vertical 4-cycle liquid cooled Gasoline engine
Number of Cylinders 3
Bore mm(in) 68(2.68)
Stroke...
Emission Regulation Tier2
Type Vertical 4-cycle liquid cooled Gasoline engine
Number of Cylinders 3
Bore mm(in) 68(2.68)
Stroke...
Gasoline engine / 3-cylinder / liquid-cooled - max. 18.3 kW (24.5 HP), Tier2 | WG752-E2
Model WG752-E2
Emission Regulation Tier2
Type Vertical 4-cycle liquid cooled Gasoline engine
Number of Cylinders 3
Bore mm(in) 68(2.68)
Stroke mm(in) 68(2.68)
Displacement L (cu.in) 0.740(45.2)
Maximum Speed rpm 3600
Output:
Gross Intermittent kW 18.3
hp 24.5
ps 24.9
Direction of Rotation Counterclockwise Viewed on Flywheel
Fuel Unleaded Gasoline
Starter Capacity V-kW 12-0.7
Alternator Capacity V-W 12-150
Length mm (in) 421.0(16.57)
Width mm (in) 392.0(15.44)
Height mm (in) 540.0(21.26)
Dry Weight kg (lb) 61.7(136.0)
Emission Regulation Tier2
Type Vertical 4-cycle liquid cooled Gasoline engine
Number of Cylinders 3
Bore mm(in) 68(2.68)
Stroke mm(in) 68(2.68)
Displacement L (cu.in) 0.740(45.2)
Maximum Speed rpm 3600
Output:
Gross Intermittent kW 18.3
hp 24.5
ps 24.9
Direction of Rotation Counterclockwise Viewed on Flywheel
Fuel Unleaded Gasoline
Starter Capacity V-kW 12-0.7
Alternator Capacity V-W 12-150
Length mm (in) 421.0(16.57)
Width mm (in) 392.0(15.44)
Height mm (in) 540.0(21.26)
Dry Weight kg (lb) 61.7(136.0)
Gasoline engine - 18.3 - 45.5 kW, 3 600 r/min | WG series
Gross Intermittent Maximum Speed Cylinders
kW...
kW...
Gasoline engine - 18.3 - 45.5 kW, 3 600 r/min | WG series
Gross Intermittent Maximum Speed Cylinders
kW / HP rpm
WG752-G-E3 18.3 / 24.5 3600 3
WG972-G-E3 24.2 / 32.5 3600 3
WG1605-G-E3 42.5 / 57.0 3600 4
kW / HP rpm
WG752-G-E3 18.3 / 24.5 3600 3
WG972-G-E3 24.2 / 32.5 3600 3
WG1605-G-E3 42.5 / 57.0 3600 4
Gasoline engine / 3-cylinder / liquid-cooled - 17.6 kW, 3 600 r/min | DG972-E2
Gross Intermittent (*) Maximum...
Gasoline engine / 3-cylinder / liquid-cooled - 17.6 kW, 3 600 r/min | DG972-E2
Gross Intermittent (*) Maximum Speed Cylinders
kW / HP rpm
DG972-E2 17.6/23.6 3600 3
kW / HP rpm
DG972-E2 17.6/23.6 3600 3
Airplane engine - 4 152 - 6 100 shp | AE 2100
AE 2100 shares a common core with other AE engines and sets new standards in performance, efficiency and economy in modern turboprop engines
AE 2100A - in the 4,000 shp range powers the SAAB 2000 in civil application
The engine's success and versatility is highlighted by its selection for key military transport applications the C130J Hercules and C-27J Spartan
The AE 2100...
AE 2100A - in the 4,000 shp range powers the SAAB 2000 in civil application
The engine's success and versatility is highlighted by its selection for key military transport applications the C130J Hercules and C-27J Spartan
The AE 2100...
Airplane engine - 4 152 - 6 100 shp | AE 2100
AE 2100 shares a common core with other AE engines and sets new standards in performance, efficiency and economy in modern turboprop engines
AE 2100A - in the 4,000 shp range powers the SAAB 2000 in civil application
The engine's success and versatility is highlighted by its selection for key military transport applications the C130J Hercules and C-27J Spartan
The AE 2100 is a turboprop derivative of the T406 turboshaft engine. It has been developed to power the new generation of high-speed regional aircraft in the 50 to 70 seat category, military transports and long-range maritime patrol aircraft.
The engine is coupled to a new technology six-bladed Dowty propeller for use on the 50-seat Saab 2000 and the Lockheed C-130J Hercules military transport.
Lockheed Martin Alenia Tactical Transport Systems (LMATTS) is using the AE 2100D2 to power its new C-27J Spartan medium airlifter, which is an upgrade of the G.222 aircraft, and the ShinMaywa US-1A amphibious search and rescue aircraft using an AE 2100J.
The first AE 2100 prototype ran in 1988 and successful flight tests were undertaken in 1990 on a P-3 Orion test bed. The AE 2100A, AE 2100C and AE 2100D3 are all FAA certified.
The AE 2100 turboprop is a two-shaft design with a 14-stage compressor driven by a two-stage HP turbine
The two-stage IP turbine drives a compound planetary reduction gearbox.
The engine is the first to use dual FADECs (full authority digital engine control) to control both engine and propeller
AE 2100A - in the 4,000 shp range powers the SAAB 2000 in civil application
The engine's success and versatility is highlighted by its selection for key military transport applications the C130J Hercules and C-27J Spartan
The AE 2100 is a turboprop derivative of the T406 turboshaft engine. It has been developed to power the new generation of high-speed regional aircraft in the 50 to 70 seat category, military transports and long-range maritime patrol aircraft.
The engine is coupled to a new technology six-bladed Dowty propeller for use on the 50-seat Saab 2000 and the Lockheed C-130J Hercules military transport.
Lockheed Martin Alenia Tactical Transport Systems (LMATTS) is using the AE 2100D2 to power its new C-27J Spartan medium airlifter, which is an upgrade of the G.222 aircraft, and the ShinMaywa US-1A amphibious search and rescue aircraft using an AE 2100J.
The first AE 2100 prototype ran in 1988 and successful flight tests were undertaken in 1990 on a P-3 Orion test bed. The AE 2100A, AE 2100C and AE 2100D3 are all FAA certified.
The AE 2100 turboprop is a two-shaft design with a 14-stage compressor driven by a two-stage HP turbine
The two-stage IP turbine drives a compound planetary reduction gearbox.
The engine is the first to use dual FADECs (full authority digital engine control) to control both engine and propeller
Airplane engine - RR500
More take-off power
More hot and high power
2,000/4,000 hour maintenance intervals
Designed for ease of retrofit
The RR500 turboprop engine is a new and exciting addition to the Rolls-Royce family of engines. The RR500TP is the...
More hot and high power
2,000/4,000 hour maintenance intervals
Designed for ease of retrofit
The RR500 turboprop engine is a new and exciting addition to the Rolls-Royce family of engines. The RR500TP is the...
Airplane engine - RR500
More take-off power
More hot and high power
2,000/4,000 hour maintenance intervals
Designed for ease of retrofit
The RR500 turboprop engine is a new and exciting addition to the Rolls-Royce family of engines. The RR500TP is the premier choice for value conscious operators seeking the multi-fuel benefits and performance of turbine power.
The engine delivers greater speed, improved comfort, increased reliability and unmatched operational capability in a compact design. All of this is available in a power plant offering excellent value and lower lifecycle costs.
Rolls-Royce has unmatched turboprop engine experience that assures the RR500 operator of outstanding performance and global support. Additionally, the RR500TP is well suited for STC conversions of popular general aviation aircraft to turbine power.
Multi-fuel capability - AvGas independence
Excellent power-to-weight ratio
2000 hour shop visit interval
More hot and high power
2,000/4,000 hour maintenance intervals
Designed for ease of retrofit
The RR500 turboprop engine is a new and exciting addition to the Rolls-Royce family of engines. The RR500TP is the premier choice for value conscious operators seeking the multi-fuel benefits and performance of turbine power.
The engine delivers greater speed, improved comfort, increased reliability and unmatched operational capability in a compact design. All of this is available in a power plant offering excellent value and lower lifecycle costs.
Rolls-Royce has unmatched turboprop engine experience that assures the RR500 operator of outstanding performance and global support. Additionally, the RR500TP is well suited for STC conversions of popular general aviation aircraft to turbine power.
Multi-fuel capability - AvGas independence
Excellent power-to-weight ratio
2000 hour shop visit interval
Airplane engine - 300 - 450 shp | M250
One of the industry's most popular 300-450shp turboprop engines
Product details
Excellent power-to-weight ratio
Extremely compact design
62 applications to date, 43 of which were upgrades of piston-engined designs
Over 1,200...
Product details
Excellent power-to-weight ratio
Extremely compact design
62 applications to date, 43 of which were upgrades of piston-engined designs
Over 1,200...
Airplane engine - 300 - 450 shp | M250
One of the industry's most popular 300-450shp turboprop engines
Product details
Excellent power-to-weight ratio
Extremely compact design
62 applications to date, 43 of which were upgrades of piston-engined designs
Over 1,200...
Product details
Excellent power-to-weight ratio
Extremely compact design
62 applications to date, 43 of which were upgrades of piston-engined designs
Over 1,200...