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Manufacturer: Glasair Aviation
Aircraft Model(s): Glasair II, II SRG
Applicable Engines: XP-360 180 hp @ 2700 rpm, IO-360 (180 hp)

Propeller Model and Components:

COMPONENT DESCRIPTION
Propeller HC-C2YR-1BF/F7496 (74
Propeller HC-C2YR-1BF/F7496-2 (72
Spinner CONSULT NEW GLASAIR
Governor CONSULT NEW GLASAIR

 

Features:
SUPERIOR XP-360
NEW HARTZELL “BLENDED AIRFOIL” DESIGN FOR USE WITH SUPERIOR AIR PARTS XP-360 WITH 8.5:1 COMPRESSION PISTONS

LYCOMING (I)O-360
NEW HARTZELL “BLENDED AIRFOIL” DESIGN FOR USE WITH LYCOMING 180 HP ENGINES WITH 8.5:1 COMPRESSION PISTONS INCLUDING ELECTRONIC IGNITION AND FADEC

Compact Series Propeller
Aluminium Hub/Aluminium Blade Construction
Constant-Speed
Non-Feathering

Specifications:
74″ OR 72″ DIAMETER 2-BLADE PROPELLER
6 YEAR 2400 HOUR TBO

Performance Testing:

NOTE: TESTING OF THIS PROPELLER ON THE SUPERIOR AIR PARTS XP-360 ENGINE EQUIPPED WITH ELECTRONIC IGNITION AN/OR FADEC HAS NOT BEEN DONE AT THIS TIME.

Restrictions:
SUPERIOR XP-360 RESTRICTIONS:
Hartzell Propeller Model HC-C2YR-1BF/F7496 is satisfactory vibrationwise mounted on Superior Air Parts model O-360-B1A2 and IO-360-B1A2 engines rated at 180HP at 2700 RPM installed IN similar single engine tractor aircraft with the following operating restrictions.
1) Continuous operation is prohibited above 22″ manifold pressure between 2050 and 2200 RPM
2) Diameter range is 74″ to 71″

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.

Hartzell Propeller Model HC-C2YR-1BF/F7496 is satisfactory vibrationwise mounted on Lycoming model IOF-360- A1A rated at 180HP at 2700 RPM and equipped with Aerosance FADEC engine control installed in similar single engine tractor aircraft with the following operating restrictions.
1) Do not operate above 22″ manifold pressure below 2350 RPM.
2) Maximum engine RPM must be limited to 2650 RPM.
The propeller diameter limits are 74 to 72 inches.

Hartzell Propeller