Service difficulty report · Insert · Pac CT4B

Difficulty date
September 3, 2003
Submitted
October 15, 2003
Operation
General aviation
Make and model
Pac CT4B
Engine
Cont IO360HB
Propeller
Hartzl BHCC2YF1
Part
Insert
Condition
Wrong Part
Location
Propeller Hub
Part time
127 cycles
Stage of operation
IN
How discovered
9
Nature of condition
O
Precautionary procedure
K

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

What was found

(AUS) ENGINE CRANKSHAFT FLANGE CRACKED AND LEAKING AROUND FACE. CRACK ORIGINATED AT DOWEL HOLE AND PROGRESSED APPROXIMATELY 75 PERCENT OF THE WAY AROUND THE FLANGE. INVESTIGATION FOUND THAT THE PROPELLER HAD BEEN MODIFIED BY THE FITMENT OF A STEEL INSERT IN THE MAIN BORE OF THE HUB. THE INSERT DID NOT HAVE THE REQUIRED INTERNAL CHAMFER FOR CORRECT MATING WITH THE PROPELLER FLANGE SO THAT WHEN THE PROPELLER BOLTS WERE TORQUED THE RESULTING BENDING LOADS CAUSED THE FLANGE TO CRACK. PERSONNEL /MAINTENANCE ERROR. UNAPPROVED PART.