SDR AU980413

Service difficulty report · Flyweight · Bnorm BN2A20

Difficulty date
April 15, 1998
Submitted
March 26, 2000
Operation
General aviation
Make and model
Bnorm BN2A20
Engine
Lyc IO540K1B5
Propeller
Hartzl HCC2YK2
Part
Flyweight
Condition
Failed
Location
Propeller Hub
Stage of operation
NR
Nature of condition
E, R
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

(AUS) ON THE FIRST SHUTDOWN OF THE DAY, THE PROPELLER WOULD NOT LATCH AND WENT INTO FEATHER. LATER IN THE DAY, THE PROPELLER FAILED TO ACHIEVE MAXIMUM RPM. THE PROPELLER WAS REMOVED AND INVESTIGATION AFTER REMOVING THE CYLINDER FOUND SUBSTANTIAL DAMAGE TO THE INTERNAL COMPONENTS. DUE TO THE DAMAGE IT WAS NOT POSSIBLE TO ESTABLISH THE CAUSE BUT IT IS SUSPECTED THAT THE WEIGHTS MAY HAVE FAILED DUE TO UNEVEN LOADING OR AS A RESULT OF IMPACT LOADS.