Manufacturer: Mooney
Aircraft Model(s): M20A-J
Applicable Engines: O-360-A1D, -A2D & IO-360-A1A, -A3B6(D), -A1B6D
1 - Composite Spinner Assembly - 103585(F1)
1 - STC Document Set - SA02414CH-D
1 - Spinner Assembly - A-2295-5P
1 - 2-Bladed Propeller - SA02414CH-D
Applicable Models:
M20A-J
*Note: If cowling has been modified, a different spinner assembly may be needed, specific modification changes are required to help ensure a correct fit.
Specifications:
2400 hour / 6 year TBO
62-64 pounds (propeller and spinner)
Placard -” No cont. ops. above 24″ btwn. 2350 and 2550 rpm” (M20E & M20F only)
Replaces:
2-bladed propeller models
Diameter reduction allowable to 72.5 inches or no diameter reduction allowed on q-tip
2000 hour / 5 year TBO
57 or 59 pounds (propeller and spinner)
Placard – “Avoid cont. ops. between 2100 and 2350 rpm.”
Repetitive eddy current inspection per AD2006-18-15
Diameter reduction allowable to 73 inches
2400 hour / 6 year TBO
71 pounds (propeller and spinner)
Placard – “Avoid cont. ops. Below 15″ btwn. 1950 and 2350 rpm”.