This from Hartzell Manual 115N:
AIRWORTHINESS LIMITATIONS
Propeller: HC-C2YR-1BF/F7666A-2Engine: Lycoming O-360-A1A rated at 180hp at 2700 RPM equipped with Lightspeed Plasma II electronic ignition Max. Diameter 74 inches Min. Diameter 72 inches
Operating Restriction: ?Avoid continuous operation between 2000 and 2250 RPM. Operation above 2600 RPM is limited to takeoff. As soon as practical after takoff, the RPM should be reduced to 2600 RPM or less.?
This from
http://hartzellprop.com/pilots/kit-builders/glasair-ii-ii-srg-io-360-180-hp-new-prop-design/ (Listed under Glasair)
LYCOMING (I)O-360-B1A RESTRICTIONS:
Hartzell Propeller Model HC-C2YR-1BF/F7496 is satisfactory vibrationwise mounted on Lycoming model O-360 A1A rated at 180HP at 2700 RPM and equipped with magneto ignition and/or Lightspeed Plasma II or LASAR electronic ignition installed in similar single engine tractor aircraft with the following operating restrictions.
1) Do not operate above 22″ manifold pressure below 2350 RPM.
2) Operation above 2600 RPM is limited to takeoff. As soon as practical after takeoff the RPM should be reduced to 2600 RPM or less.
The propeller diameter limits are 74 to 72 inches.
Cheers, David
KBTF - RV-6A