AFMS
N'D07
FOR
GARMIN
GFC700
AUTOPILOT
AND
VARIABLE
PITCH
PROPELLER
EQUIPPED
AEROPLANES
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Page APV 2-7
4.
POWERPLANT
LIMITATIONS
Following table reports the operating limitations the installed engine:
ENGINE MANUFACTURER: Lycoming Engines
ENGINE
MODEL:
10-360-MIA
MAXIMUM
POWER:
Max Power
(hp)
Max.
T.O.
180
Max.
Cont
173
.3
Max rpm.
Prop. rpm
2700
2600
Temperatures:
Max CHT
..............
...
...........................
500° F (260° C)
Max Oil ...
..........
.....
.
...
......
.......
..
.........
245° F (118° C)
Oil Pressure:
Minimum Idling ...
..................
.................
25 psi
(I.
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:
Approved
-
Al
Inlet
to
fuel
m1ector
:
Minimum
...
..........................
..
...............................
14
psi (0.96 Bar).
Maximum ..............................
...
............................ 35 psi (2.41 Bar)
Section
2 -
Limitations
Powerplant
limitations
Ed
2,
Rev. 0