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Stinson 108-2 & 108-3 Airplane Flight Manual Supplement

Stinson Model 108-2 & 108-3				CAA Approved
CAA Identification _______________			Dated July 11, 1957
By:

AIRPLANE FLIGHT MANUAL SUPPLEMENT

SENSENICH CORPORATION			PROPELLER INSTALLATION
This aircraft equipped with Franklin Model 644-165-B3 Engine and Sensenich Model M74DR fixed pitch metal propeller must be operated in compliance with the limitations prescribed herein.
  1. LIMITATIONS SECTION
    1. Same as prescribed in the Stinson 108-2 CAA Approved Flight Manuals dated January 4, 1949, in the Stinson 108-3 landplane (skiplane) CAA Approved Airplane Flight Manual dated December 29, 1948, and in the Stinson 108-3 seaplane CAA Approved Flight Manual dated December 28, 1948, except:
    2. PROPELLER:
      1. Fixed Pitch Metal
        Make: Sensenich
        Model: M74DR
        Diameter: 74 inches max., 72.5 inches mm. Static RPM limits with maximum permissible throttle setting: 2500 max., 2300 mm. For the 108-3 airplane only1 the minimum static RPM shall be 2400.
      NOTE: Avoid continuous operation between 2150 and 2250 RPM.
  2. PROCEDURES SECTION
    Same as prescribed in the applicable CAA Approved Flight Manual as listed under paragraph "A" above.
  3. PERFORMANCE SECTION
    Same as prescribed in the applicable CAA Approved Flight Manual as listed under paragraph "A" above, except:
    1. TAKE-OFF, CLIMB AND LANDING:
      (d) Performance with the Sensenich M74DR is equal to or better than that demonstrated with a fixed pitch wood propeller.
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