4.2
LIMBACH L 2400 ET/DT
*)
With crankshaft 241.031.013
**)
With crankshaft 241.031.001
***)
With turbocharger 250.173.100
****)
With turbocharger 250.173.105
Edition: 20.06.2018
L 2400 EF/DF/ET/DT/DX/DS
Dimensions
Bore
Stroke
Displacement per Cyl.
Total Displacement
Compression Ratio
Crankshaft Rotation
Ignition Timing
Firing Order
Equipment
Engine management system
Spark Plugs
Ignition Cable
Ignition Harness
Injectors
Fuel Pump
Alternator
Starter
Oil Pump
Oil Filter
Turbocharger
Propeller Flange
Engine Ratings
Max. Take-Off Power
Max. Continuous Power
Engine Rotational Speeds
Max. permissible speed
Max. speed for cruise
Min. continuous speed
Idle speed
Fuel and Oil
Fuel
Engine Oil
Coolant
Operating Manual
97 mm
82 mm
606 cm³
2424 cm³
8.0 : 1
counterclockwise
variable mapped
1-3-2-4
Weber Alpha PI 38
Weber Alpha PI 48
trijekt bee
NGK DCPR7E
LIMBACH
LIMBACH
IWP 43
PIERBURG
BOSCH 14V-33A
BOSCH 14V-55A
BRISE 14V-55A
MAGNETON 1 kW
Geared Pump
241.083.001
250.173.100
250.173.105
250.031.301*)
250.031.302**)
96 kW / 130 HP at 3000 rpm
40 inHg***)
41 inHg****)
85 kW / 115 HP at 3000 rpm
38 inHg***)
39 inHg****)
3200 rpm
See flight and maintainance manual
of airframe manufacturer.
2400 rpm
800 ±100 rpm
see section 10
see section 10
see section 10
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