Specifications

SECTION 2 CESSNA
OPERATING LIMITATIONS MODEL 172R NAV III
GFC 700 AFCS
U.S.
FAA APPROVED
POWERPLANT LIMITATIONS
Engine Manufacturer: Textron Lycoming
Engine Model Number: IO-360-L2A
Maximum Power: 160 BHP Rating
Engine Operating Limits for Takeoff and Continuous Operations:
Maximum Engine Speed:. . . . . . . . . . . . . . . . . . . . . . . . . .2400 RPM
NOTE
The static RPM range at full throttle is 2065 - 2165 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 AND SHOULD BE INSPECTED BY
QUALIFIED MAINTENANCE PERSONNEL BEFORE
NEXT FLIGHT.
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: 1C235/LFA7570
Propeller Diameter:
Maximum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .75 INCHES
Minimum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .74 INCHES
172RPHBUS-00
2-6