acf domain was triggered too early. This is usually an indicator for some code in the plugin or theme running too early. Translations should be loaded at the init action or later. Please see Debugging in WordPress for more information. (This message was added in version 6.7.0.) in /var/www/vhosts/dev.hartzellprop.com/www/wp-includes/functions.php on line 6121
Manufacturer: Cessna
Aircraft Model(s): A185E, A185F
Applicable Engines: IO-520-D
PDF: CESSNA A185 SA04491CH (C3F04930)
| QTY | DESCRIPTION | ITEM # |
| 1 | 3-Bladed Propeller | HC-C3YF-1RF/F8429 |
| 1 | Polished Spinner | C-3575-P |
| 1 | STC Document Set | SA04491CH |
Applicable Models:
A185E, A185F
Specifications:
86 inch diameter 3-bladed, aluminum hub, aluminum bladed propeller
2400 hour / 6 year TBO
77 pounds (propeller and spinner)
Diameter reduction allowable to 84 inches
NO RPM RESTRICTIONS
Replaces:
McCauley C58 – 86 inch diameter 2-bladed prop
Diameter reduction allowable to 84.5 inches
Oil fill requirement per AD 91-15-04
1200-1500 hour / 5 year TBO
McCauley C403 – 80 inch diameter 3-bladed prop
Diameter reduction allowable to 78.5 inches
2000 hour / 6 year TBO
Advantages:
vs. McCauley C58 2-bladed model
Dramatically improved take off and climb performance
Longer TBO/warranty
Current design, Mc threaded design obsolete
vs. McCauley C401 3-bladed model (86”)
Better take-off and climb performance (80 – 100 FPM at Vy)
Longer TBO/warranty
vs. McCauley C403 3-bladed model
Better take-off and climb performance
Longer TBO/warranty
Notes:
* Note: No engine mount change is required per the Hartzell STC paperwork. Changing to the heavier mounts, however, may be needed if vibration is experienced.
**Note: This propeller should be especially effective for aircraft operating on floats, out of short fields, or with heavy loads.
Interested in more information? Fill out the form below and we’ll contact you shortly.