SOLOY TURBINE PAC SECTION 2
POHS CESSNA T206H/206H LIMITATIONS
2-13
F.A.A. Approved November 17, 2015
OIL SPECIFICATIONS
The 250 series engines are certified and approved for use with only certain
lubricating oils that comply with MIL-PRF-7808, MIL-PRF-23699, DOD-PRF-
85734, or SAE AS5780 specifications. Refer to the Rolls-Royce M250-C20
Series Operation and Maintenance Manual for current approved oils and
limitations.
OTHER LIMITATIONS
FLIGHT IDLE LIMITS
Flight operations with the power control retarded below FLIGHT IDLE
(14 psi torque minimum) are prohibited.
FLAP LIMITATIONS
Approved Takeoff Range: 0 to 20
Approved Landing Range: 0 to 40
LANDING GEAR LIMITATIONS
Nose Wheel Size: 6.00-6
5.00-5 (Limited to 6.00-6 main
wheel size only with 5.00-5
nose wheel)
Main Wheel Size: 6.00-6
8.00-6
8.50-6
MAXIMUM OPERATING ALTITUDE LIMITS
Maximum Operating Altitude: 20,000 feet.
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