Textron Cessna Skyhawk SP - Powerplant Limitations

SECTION 2 CESSNA
OPERATING LIMITATIONS MODEL 172S NAV III
GFC 700 AFCS
U.S.
FAA APPROVED
POWERPLANT LIMITATIONS
Engine Manufacturer: Textron Lycoming
Engine Model Number: IO-360-L2A
Maximum Power: 180 BHP Rating
Engine Operating Limits for Takeoff and Continuous Operations:
Maximum Engine Speed:. . . . . . . . . . . . . . . . . . . . . . . . . .2700 RPM
NOTE
The static RPM range at full throttle is 2300 - 2400 RPM.
Maximum Oil Temperature: . . . . . . . . . . . . . . . . . . . . .245°F (118°C)
Oil Pressure, Minimum: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .20 PSI
Oil Pressure, Maximum: . . . . . . . . . . . . . . . . . . . . . . . . . . . .115 PSI
CAUTION
ENGINE OPERATION WITH INDICATED OIL PRESSURE
BELOW THE GREEN BAND RANGE WHILE IN CRUISE
OR CLIMB CONFIGURATION IS CONSIDERED
ABNORMAL. REFER TO SECTION 3, AMPLIFIED
EMERGENCY PROCEDURES, "LOW OIL PRESSURE".
Fuel Grade: Refer to Fuel Limitations
Oil Grade (Specification):
MIL-L-6082 or SAE J1966 Aviation Grade Straight Mineral Oil or
MIL-L-22851 or SAE J1899 Ashless Dispersant Oil. Oil must comply
with the latest revision and/or supplement for Textron Lycoming
Service Instruction No. 1014, must be used.
Propeller Manufacturer: McCauley Propeller Systems
Propeller Model Number: 1A170E/JHA7660
Propeller Diameter:
Maximum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .76 INCHES
Minimum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .75 INCHES
172SPHBUS-01
2-6