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CESSNA
210 K, L, M, N

TOP PROP PERFROMANCE
CONVERSIONS

STC Number SA00773AT

Applicable Aircraft

Engines

210 K, L, M, and N

IO-520-L

 STC Kit Contents

Number

1 3-Bladed Propeller
1 Polished Spinner
1 Spinner Mounting Kit
1 STC Paperwork

PHC-J3YF-1RF / F7691
C4582-P
A2476-9
SA00773AT

Specifications:

Propeller Part Number
Number of Blades
Blade Design
Installed Propeller and Spinner Weight
Maximum Diameter
Minimum Diameter
TBO

PHC-J3YF-1RF / F7691
3
Scimitar
77.3
78 in.
77 in.
2400 hrs/ 6 years
(whichever occurs first)

Placards:

"Do not exceed 20 inch manifold pressure below 2200 RPM."

Replaces

McCauley C73
McCauley D88
McCauley C404

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