SECTION 2 CESSNA
OPERATING LIMITATIONS MODEL T182T NAV III
GFC 700 AFCS
U.S.
FAA APPROVED
POWERPLANT LIMITATIONS
Engine Manufacturer: Textron Lycoming
Engine Model Number: TIO-540-AK1A
Engine Operating Limits for Takeoff and Continuous Operations:
Maximum Continuous Power: . . . . . . . . . . . . . . . . . . 235 rated BHP
at 32 in.hg. and 2400 RPM
Maximum Cylinder Head Temperature: . . . . . . . . . . . 500°F (260°C)
Maximum Oil Temperature: . . . . . . . . . . . . . . . . . . . . .245°F (118°C)
Oil Pressure, Minimum: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .20 PSI
Oil Pressure, Maximum: . . . . . . . . . . . . . . . . . . . . . . . . . . . .115 PSI
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-22851 or SAE J1899 Ashless Dispersant Oil. Oil must comply
with the latest revision and/or supplement for Textron Lycoming
Service Instruction No. 1014 and must be used.
Propeller Manufacturer: McCauley Propeller Systems
Propeller Model Number: B3D36C442-C/80VSB-1
Propeller Diameter:
Maximum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 79.0 INCHES
Minimum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 77.5 INCHES
T182TPHBUS-01
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