Diamond DA 42 - 2.4 Power-Plant Limitations

DA 42 AFM Operating Limitations
Doc. No. 7.01.05-E Rev. 8 15-Dec-2017
EASA
approved
Page 2 - 7
2.4 POWER-PLANT LIMITATIONS
a) Number of engines : 2
b) Engine manufacturer : Thielert Aircraft Engines
c) Engine designation : TAE 125-01 Centurion 1.7
or
TAE 125-02-99 (if MÄM 42-198 is carried out)
(P/N see Equipment List in Chapter 6)
d) RPM limitations (shown as propeller RPM)
Maximum : 2300 RPM
Maximum overspeed : 2500 RPM (max. 20 sec)
e) Engine power
Max. take-off power : 99 kW (135 DIN-hp) at 2300 RPM (100 % load)
Max. continuous power : 99 kW (135 DIN-hp) at 2300 RPM (100 % load)
f) Fuel temperature:
TAE 125-01 TAE 125-02-99
(MÄM 42-198 carried out)
Minimum -30
o
C -30
o
C
Maximum +75
o
C +75
o
C
g) Oil pressure (indicated values are corrected for pressure altitude)
Minimum : 1.0 bar
Maximum : 6.5 bar
h) Oil quantity (per engine)
Minimum : 4.5 liter (appr. 4.8 US qts)
Maximum : 6.0 liter (appr. 6.3 US qts)
Maximum oil consumption : 0.1 liter/hr (appr. 0.1 US qts/hr)