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Manufacturer: Cessna
Aircraft Model(s): 210F-N & T210F-L
Applicable Engines: IO-520-A,J,L and TSIO-520-C,H
PDF: 210F-N, T210F-L
| QTY | DESCRIPTION | ITEM # |
| 1 | 3-Bladed Propeller | PHC-J3YF-1RF/F7691 |
| 1 | Polished Spinner | C-4582-P |
| 1 | STC Paperwork | SA00773AT |
Applicable Models:
210F-N and T210F-L
Specifications:
78 inch dia 3-bladed, scimitar, aluminum, extended hub prop
2400 hour / 6 year TBO
77.3 pounds (propeller and spinner)
Diameter reduction allowable to 77 inches
Placard – “Do not exceed 20 inch of manifold pressure below 2200 RPM.”
Replaces:
McCauley C70,C73 – 82/83 inch diameter 2-bladed propeller
Diameter reduction allowable to 80 inches
1200-1500 hours/5 year TBO
Oil fill requirement per AD 91-15-04
McCauley C77,C88 – 80 inch diameter 3-bladed propeller
Diameter reduction allowable to 78 inches
1200-1500 hours/5 year TBO
McCauley C404 – 82 inch diameter 3-bladed propeller
Diameter reduction allowable to 78.5 inches
1700 hours/5 year TBO
Advantages:
Better take-off and climb performance
Same or slightly better cruise performance
Longer TBO
Dramatically lower noise
Improved appearance
Less blade tip erosion
Current design
Notes:
The original STC was approved for the 210K,L,M & N models (IO-520-L) only. STC was amended in late 2009 to include the additional models listed.
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