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NEW YORK AIRWAYS 6.2 OPERATING LIMITATIONS, V-44 NOTE: The observance of the following as set forth in this section is required by law WEIGHT LIMITATIONS 1. Maximum takeoff and landing weight is 14,350 pounds. NOTE: See section 7.22.1 Flight Preparations for weight and balance and loading data. CENTER OF GRAVITY LIMITS 1. Most forward cg at 14,350 pounds-319 inches aft of the datum reference. 2. Most reward cg at 14,350 pounds -350 inches aft of the datum reference. 3. Most reward cg at 11,500-360.5 inches aft of the datum reference NOTE: Straight Line variation between balance station 360.5 350.0 4. The datum is located 100 inches forward of the centerline of the forward rotor hub. (See section 7.22.1 Flight Preparations, Loading Information). POWER PLANT 1. Wright cyclone models 977C9HD2 (Low Blower) a. Impeller gear ratio, Low Blower- 7.21 to 1. b. Transmission ratio, engine to rotors- 9.7 to 1. c. Fuel, minimum octane--100/130. (115/145 alternate) d. Temperatures: (1) Cylinder head: (a) Takeoff, maximum-260°C (500°F) (b) Maximum continuous, maximum-232°C. (450°F). (2) Oil inlet, maximum-104°C (220°F). (3) Transmission oil, maximum-95°C (203°F). 5 CAA-APPROVED FEBRUARY 26, 1958, V-44
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