Service difficulty report · Spar · Swrngn SA227*

Difficulty date
March 8, 2018
Submitted
July 16, 2018
Operation
General aviation
Make and model
Swrngn SA227*
System (JASC)
5751 · Ailerons
Part
Spar
Condition
Cracked
Location
Right Wing
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

TWO AILERONS WERE SENT TO OUR FACILITY AS SPARE COMPONENTS TO HAVE UPPER AND LOWER SKINS REPLACED DUE TO EXISTING REPAIRS, DENTS, AND OVERALL POOR CONDITION. AFTER FURTHER INSPECTION, CRACKS WERE FOUND IN THE AILERON SPAR AT TWO OF THE THREE HINGE FITTINGS. THIS CONDITION WAS FOUND ON BOTH AILERONS. THESE CRACKS CAN ONLY BE SEEN IF THE HINGE FITTINGS ARE REMOVED. THE FITTINGS ARE HELD IN PLACE WITH BOLTS AND CASTELLATED NUTS. IT IS PROBABLE THAT THE CRACKS ARE A RESULT OF IMPROPER TORQUEING OF THE CASTELLATED NUTS. IF THE COTTER PIN HOLE DOES NOT ALIGN BEFORE MAX TORQUE IS ACHIEVED, THE NUT IS BACKED OFF TO THE NEXT CASTELLATION FOR COTTER PIN INSTALLATION, RESULTING IN A LOOSE FITTING, THE MOVEMENT OF WHICH CAUSE FATIGUE CRACKS AROUND THE BOLT HOLES IN THE SPAR.