Tecnam P2010 - Powerplant Limitations

AFMS N°D02 FOR VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page V2-7
4. POWERPLANT LIMITATIONS
Following table reports the operating limitations the installed engine:
ENGINE MANUFACTURER: Lycoming Engines
ENGINE MODEL: IO-360-M1A
MAXIMUM POWER:
Max Power
(hp)
Max rpm.
Prop. rpm
Max. T.O.
180 2700
Max. Cont.
173.3 2600
Temperatures:
Max CHT ……………………………………….. 500° F (260° C)
Max Oil …………………………………………. 245° F (118° C)
Oil Pressure:
Minimum Idling ………………………………… 25 psi (1.7 Bar)
Minimum Normal ………………………………. 55 psi (3.8 Bar)
Maximum Normal ……………………………… 95 psi (6.5 Bar)
Starting, Warm-up, taxi and take-off (Max) …… 115 psi (7.9 Bar)
Fuel pressure:
- At Inlet to fuel injector:
Minimum .............................................................. 14 psi (0.96 Bar)
Maximum ............................................................. 35 psi (2.41 Bar)
Section 9 – Supplements
Powerplant limitations
2
nd
Edition, Rev. 1
Approved