Manufacturer: Mooney
Aircraft Model(s): M20A-J
Applicable Engines: O-360-A1D, -A2D & IO-360-A1A, -A3B6(D), -A1B6D
PDF: M20A-J 2-Blade
QTY | DESCRIPTION | ITEM # |
1 | 2-Bladed Propeller | HC-C2YR-1BFP/F7497 |
1 | Composite Spinner Assembly | 103585(F1) |
1 | STC Document Set | SA02414CH-D |
QTY | DESCRIPTION | ITEM # |
1 | 2-Bladed Propeller | HC-C2YR-1BFP/F7497 |
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:
74 inch diameter 2-bladed aluminum hub scimitar propeller
2400 hour / 6 year TBO
62-64 pounds (propeller and spinner)
Diameter reduction allowable to 72.5 inches
Placard -” No cont. ops. above 24″ btwn. 2350 and 2550 rpm” (M20E & M20F only)
Replaces:
Hartzell HC-C2YK-1BF/F7666A-2 or 3Q – 74″ or 73″ dia
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
Hartzell HC-C3YR-1RF/F7282 – 74″ dia. 3-bladed prop
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”.
McCauley C53, C212 or C214 – 74″ dia. 2-bladed prop
Diameter reduction allowable to 72.5 or 73 inches
1200-1500 hour / 5 year or 2000 hour / 6 year TBO
52.3 pounds or 54.3 pounds (propeller and spinner)
Placard – “Avoid cont. ops. below 15″ btwn 1500 and 1950 rpm.” (C212 & C214)
Advantages:
Reduced noise
Same or better climb performance
Improved cruise performance efficiency
Longest TBO
Current, attractive design
Notes:
Not eligible on fixed pitch M20D
Slightly longer take-off roll (3% over 7666-2 blade)
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