Power Plant Limitations - Piper SEMINOLE 2013 Pilot Operating Handbook

PA-44-180, SEMINOLE
2.5 AIRSPEED INDIcATOR MARkINGS (continued)
MARKING
Red Radial Line
(One Engine Inoperative Air Minimum Control Speed)

2.7 POWER PLANT LIMITATIONS

(a) Number of Engines
(b) Engine Manufacturer
(c) Engine Model No.
Left
Right
(d) Engine Operating Limits
(1) Maximum Horsepower
(2) Maximum Rotation Speed (RPM)
(3) Maximum Manifold Pressure
(4) Maximum Cylinder Head Temperature
(5) Maximum Oil Temperature
(e) Oil Pressure
Minimum
Maximum
(f) Fuel (AVGAS ONLY)
(minimum grade)
(g) Number of Propellers
(h) Propeller Manufacturer
(i) Propeller Hub and Blade Models
Left
Right
(j) Propeller Diameter (inches)
Maximum
Minimum
ISSUED: June 5, 2013
SECTION 2
LIMITATIONS
Lycoming
0-360-A1H6
L0-360-A1H6
Full Throttle
100 or 100LL
Aviation Grade
HC-C2Y(K,R)-2CEUF/
FC7666A-2R
HC-C2Y(K,R)-2CLEUF/
FJC7666A-2R
REPORT: VB-2307
IAS
56 KTS
2
180
2700
500°F
245°F
25 PSI
115 PSI
2
Hartzell
74 IN.
72 IN.
2-3