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Beaver RX 35 Powered by Rotax 377, Rotax 447 or Rotax 503 twin cylinder aircraft engines.
UltralightNews.com
A problem reported with the use of the above engines on the Beaver has been crankshaft failures. Personal experience indicates that
contributing factors to these failures may be:
1: The use of Rotax engines in a inverted installation.
When the Rotax 337/447/503 are used in an upright installation a gravity feed
system is used to supply oil to the crankshaft main bearings through channels in the
crankcase.
While oil is still supplied to these bearings in an inverted application, it is being
supplied by internal engine pressure, rather than gravity.
When an upright engine, is left in storage oil flows down into the channels in the
case coating the crankshaft bearings.
In an inverted installation this oil flows AWAY from the bearings. This lack of oil on start up can lead to premature
bearing failure. Before starting an engine that has been left in storage it is recommended that the engine be
turned over for several revolutions, with the ignition turned off to bring oil back up into these bearings.
2: The use of long two blade or three blade propellers with too much pitch. This prevents the engine from
developing full RPM which causes the crankshaft to be under load all the time.
Proper RPM for a 277 engine
Proper RPM for a 377/447 Rotax engine
Proper RPM for single carb 503 engine
Proper RPM for a dual carb 503 engine
To much pitch will result in to low an RPM
Beaver, Beaver ultralight aircraft, Beaver RX 35 ultralight
aircraft, Beaver RX 550 ultralight trainer troubleshooting report.
full power
full power
full power
full power
straight and level flight should be 6350 RPM
straight and level flight should be 6600 RPM.
straight and level flight should be 6350 RPM.
straight and level flight should be 6500 RPM.
To little pitch will result in too high an RPM