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 6121Manufacturer: 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
| COMPONENT | DESCRIPTION |
| Propeller | HC-F2YR-1BF/F7068-2 (extended hub) |
| Propeller | HC-C2YR-1BF/F7068-2 |
| Spinner | |
| Governor |
Features:
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
Constant-Speed
Non-Feathering
Specifications:
68″ DIAMETER 2-BLADE ALUMINUM PROPELLER
61.5 LBS.
6 YEAR 2400 HOUR TBO
67″ MINIMUM REPAIR DIAMETER
Restrictions:
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.
Name: Glasair Aviation
Phone: 360-435-8533
Website: https://glasairaviation.com/