Section I; Limitations; Engines; Fuel - Piper CHEROKEE CRUISER PA-28-140 Information Manual

CHEROKEE CRUISER
SECTION I
LIMITATIONS
The following limitations must be observed in the operation of this airplane:
A. ENGINE
Lycoming 0-320-E2A or 0-320-E3D
ENGINE LIMITS
For all operations 2700 RPM, 150 HP
B. FUEL
AVGAS ONLY
80/87 Octane Aviation Fuel Minimum Grade
C.
PROPELLER
Sensenich M74DM or 74DM6, Maximum diameter 74 inches. minimum diameter 72-112
inches. Static RPM at maximum permissible throttle setting: Not under 2150, not over
2425 for max. allowable weight of 1950 lbs. Not under 2275, not over 2425 for max.
allowable weight of 2150 lbs. No additional tolerance permitted.
D.
POWER INSTRUMENTS
OIL TEMPERATURE
Green Arc (Normal Operating Range)
Red Line (Maximum)
OIL PRESSURE
Green Arc (Normal Operating Range)
Yellow Arc (Caution Range)
Red Line (Minimum)
Red Line (Maximum)
FUEL PRESSURE
Green Arc (Normal Operating Range)
Red Line (Minimum)
Red Line (Maximum)
TACHOMETER
Green Arc (Normal Operating Range)
Red Line (Maximum Continuous Power)
FAA APPROVED MAY 14, 1973
REVISED: JULY 13, 1984
75°F to 245°F
245° F
60 PSI to 90 PSI
25 PSI to 60 PSI
25 PSI
90 PSI
.5 PSI to 8 PSI
.5 PSI
8 PSI
500 to 2700 RPM
2700 RPM
REPORT: VB-557 PAGE 3-1
MODEL: PA-28-140