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Manufacturer: Piper
Aircraft Model(s): PA-24
Applicable Engines: O-360 engine
PDF: Piper PA24 (180HP) Comanche Scimitar
| QTY | DESCRIPTION | ITEM # |
| 1 | 2-Bladed Propeller | HC-C2YR-1BFP/F7497 |
| 1 | Composite Spinner | 103585(F1) – white OR 103585(F2) – silver |
| 1 | STC Document Set | SA00631CH |
| DESCRIPTION | ITEM # | NOTES |
PA24 (180HP) Comanche Scimitar
Applicable Models:
PA-24
Specifications:
74 inch diameter 2-bladed, aluminum hub “Scimitar” propeller
Diameter reduction allowed to 72.5 inches
2400 hour / 6 year TBO
62 pounds (propeller and spinner)
Replaces:Hartzell 72 inch diameter 2-bladed, aluminum hub propeller
No diameter reduction allowed
2400 hour / 6 year TBO
58 pounds (propeller and spinner)
Placard – “Avoid continuous ops. between 2000 and 2250 RPM.”
McCauley C14 – 74 inch diameter 2-bladed prop
Diameter reduction allowable to 72 inches
1200 hours / 5 year TBO
63 pounds (prop & spinner)
Placard – “Avoid continuous operations while descending between 2250 and 2550 RPM.”
Hartzell HC-92ZK-8D/8447A-12A – 72 inch 2-bladed steel hub prop
66 pounds (prop & spinner)
Diameter reduction allowable to 70.5 inches
500 hour inspection per AD95-11-08
2000 hour / 5 year TBO
Advantages:
Improved cruise performance (1-4 knots)
Eliminates RPM limitations and placards
Longer TBO
Current design
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