DV 20 E AFM Operating Limitations
Doc. No. 4.01.25-E Rev. 2 22-Mar-2022
EASA
approved
Page 2 - 5
2.4 POWER-PLANT LIMITATIONS
a) Engine
Manufacturer : BRP-Powertrain GmbH & Co KG
Engine designation : Rotax 912 iSc3 Sport
Max. take-off power : 73.5 kW max. 5 min
Max. continuous power : 72 kW
b) Propeller
Manufacturer : mt-Propeller
Propeller designation : MTV-21-A / 175-05
Propeller diameter : 175 cm
Prop. pitch angle (@ 61 cm) : 14.5° (low pitch)
30° (high pitch)
c) Governor : mt-Propeller P-850-12 hydraulic governor
d) RPM limitations
Maximum take-off : 5800 RPM (max. 5 min)
Maximum continuous : 5500 RPM
Minimum idle : 1400 RPM
e) Oil pressure (absolute)
Minimum : 0.8 bar below 3500 RPM
Maximum : 7.0 bar for a short period at cold start
Normal range : 2.0 bar - 5.0 bar above 3500 RPM