SDR 5APR577Y68

Service difficulty report · Fitting · Pilats PC1245

Difficulty date
May 18, 2011
Submitted
May 19, 2011
Operation
General aviation
Filed by
5APR577Y
Atlas Aircraft Center Inc
Aircraft
N624AF
Make and model
Pilats PC1245
Aircraft serial
624
Aircraft time
4,430 hours, 4,421 cycles
Engine
Pwa PT6A67B
Engine time
4,430 hours, 4,421 cycles
Propeller
Hartzl HCE4A3D
Part
Fitting
Part number
5551012150
Condition
Separated
Location
Horizontal Stab
Part time
4,430 hours, 4,421 cycles
Stage of operation
IN
How discovered
V
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

THE HORIZONTAL STABILIZER ATTACHMENT FITTING, WHERE THE PITCH TRIM ACTUATOR IS SECURED TO THE STABILIZER. EACH SIDE OF THE ATTACHMENT FITTING HAS 2 LUGS. ON THE LT SIDE, THESE 2 LUGS ARE SEPARATING. THE GAP WAS MEASURED WITH A FEELER GUAGE,AND FOUND TO BE .457 MM.THERE IS NO EVIDENCE OF DAMAGE TO THE STABILIZER. THE BRACKET PN IS 555.10.12.150, ANGLE FITTING LEFT. THE ACFT MFG ISSUED A REPAIR MEMO WITH STATEMENT OF APPROVED DESIGN DATA WITH THE FOLLOWING INSTRUCTIONS. CHECK THE LUGGED FACE OF THE PN 555.1.12.150 (ANGLE FITTING) FOR STRAIGHTNESS. IF WITHIN LIMITS, COMPLETE A VISUAL AND NDT INSPECTION (DYE PENETRANT OR EDDY CURRENT) OF THE ANGLE FITTING AND THE BOLTS. IF NO CRACKS OR DEFECTS NOTED, REINSTALL THE FITTING USING SEALANT.