Tecnam P2010 - Powerplant Limitations; Maximum Power

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV 2-7
Ed 1, Rev. 1
Section 2 – Limitations -
Powerplant limitations
Approved
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)