Power-Plant Limitations - Diamond DA 40 Flight Manual

DA 40 AFM

2.4 POWER-PLANT LIMITATIONS

a) Engine manufacturer
b) Engine designation
c) RPM limitations
Max. take-off RPM
Max. continuous RPM
d) Manifold pressure limitations
Maximum
e) Oil pressure
Minimum (IDLE)
Maximum
Normal operating range
f) Oil quantity
Minimum
Maximum
g) Oil temperature
Maximum
h) Fuel pressure
Minimum
Maximum
i) Cylinder head temperature
Maximum
j) Propeller manufacturer
Doc. # 6.01.01-E
: Textron Lycoming
: IO-360 M1-A
: 2700 RPM
: 2400 RPM
: FULL throttle
: 25 PSI / 1.72 bar
: 98 PSI / 6.76 bar
: 55 to 95 PSI / 3.8 to 6.55 bar
: 4 qts
: 8 qts
: 245 °F (118 °C)
: 14 PSI / 0.97 bar
: 35 PSI / 2.4 bar
: 500 °F (260 °C)
: mt-Propeller
Rev. 8 01-Dec-2010
Operating
Limitations
EASA
Page 2 - 5
approved