Manufacturer: Glasair Aviation
Aircraft Model(s): Super II RG 180hp
Applicable Engines: IO-360-B1A 180 hp @ 2700 rpm, IO-360-E1A 180 hp @ 2700 rpm, IO-360-F1A 180 hp @ 2700 rpm, O-360-A1A series 180 hp @ 2700 rpm
|Propeller||HC-F2YR-1BF/F7068-2 (extended hub)|
NEW DESIGN PROPELLER TO ENHANCE CRUISE SPEED WHILE REDUCING DIAMETER. HIGH TWIST DISTRIBUTION TO MEET PERFORMANCE GOAL OF GLASAIR II.
Compact Series Propeller
Aluminium Hub/Aluminium Blade Construction
68″ DIAMETER 2-BLADE ALUMINUM PROPELLER
6 YEAR 2400 HOUR TBO
67″ MINIMUM REPAIR DIAMETER
The following restrictions applies to the Glasair II with the Lycoming O-360-A1A, IO-360-B1A Series engine:
“Stabilized operation is prohibited above 25″ manifold pressure between 2300-2550 RPM and below 15″ manifold pressure above 2600 RPM.”
This restriction is not significant during normal operations, nut is a result of the testing envelope used in a vibration survey.