DA42AFM
<(tDiamond
AIRCRAFT
Operating Limitations
2.4 POWER-PLANT LIMITATIONS
a) Number
of
engines
b) Engine manufacturer
c) Engine designation
2
Thielert Aircraft Engines
TAE 125-01 Centurion 1.7
or
TAE 125-02-99 (if MAM 42-198
is
carried out)
(PIN see Equipment List
in
Chapter 6)
d) RPM limitations (shawn
as
propeller RPM)
Maximum 2300 RPM
Maximum overspeed
e) Engine power
Max. take-off power
Max. continuous power
f) Fuel temperature:
Minimum
Maximum
: 2500 RPM (max. 20 sec)
99 kW (135 DIN-hp) at 2300 RPM
(100%
load)
99
kW (135 DIN-hp) at 2300 RPM
(100%
load)
TAE 125-01 T AE 125-02-99
(MÂM 42-198 carried out)
-30
oc
-30
oc
+75°C
+75
oc
g)
Oil
pressure (indicated values are corrected for pressure altitude)
Minimum 1.0 bar
Maximum
h)
Oil quantity (per engine)
Minimum
Maximum
Maximum oil consumption
: 6.5 bar
4.5 liter (appr. 4.8 US qts)
6.0 liter (appr. 6.3
US
qts)
0.1 liter/hr (appr.
0.1
US qts/hr)
Doc.
No
. 7.01.05-E Rev. 8
15-Dec-20 17
EASA
approved
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