M20A-G, M20J 2-Blade

Aircraft Model(s): M20J, M20A-G
Applicable Engines: O-360-A1D, -A2D & IO-360-A1A, -A3B6(D), -A1B6D

Propeller Model# HC-C2YR-1BFP/F7497

KIT PART# C2R10703STP M20E, F

KIT PART# C2R10704STP M20A-D,G

Base Kit Includes:

HC-C2YR-1BFP/F7497 Scimitar propeller kit C2R10703STP, C2R10704STP, C2R10705STP

QTY	DESCRIPTION	ITEM #
1	STC Document Set	SA02414CH-D
1	Composite Spinner Assembly	103585(F1)
1	2-Bladed Propeller	HC-C2YR-1BFP/F7497

Options:

KIT PART# FOR M20J C2R10705STP

DESCRIPTION	ITEM #	NOTES
Spinner Assembly	A-2295-5P	used on the M20J model
Spinner mounting kit	A-2476-10	used on the M20J model

Applicable Models:
M20A-G M20J

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
Longer TBO
Current, attractive design