Tecnam P2010 - Page 514

AFMS N° D08 FOR ALTERNATIVE AVIONICS CONFIGURATION AND
VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page GV 2-7
4. POWERPLANT LIMITATIONS
Following table reports the operating limitations the installed engine:
ENGINE MANUFACTURER: Lycoming Engines
ENGINE MODEL: IO-360-M1A
M
AXIMUM 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 2 – Limitations
POWERPLANT LIMITATIONS
Ed. 1, Rev. 0