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SOLOY TURBINE PAC
POHS CESSNA T206H/206H
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:
Approved Landing Range:
LANDING GEAR LIMITATIONS
Nose Wheel Size:
Main Wheel Size:
MAXIMUM OPERATING ALTITUDE LIMITS
Maximum Operating Altitude:
F.A.A. Approved
0 to 20
0 to 40
6.00-6
5.00-5
(Limited to 6.00-6 main
wheel size only with 5.00-5
nose wheel)
6.00-6
8.00-6
8.50-6
20,000 feet.
2-13
November 17, 2015
SECTION 2
LIMITATIONS
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