Service difficulty report · Fitting · Pilats PC1247

Difficulty date
September 30, 2011
Submitted
October 5, 2011
Operation
General aviation
Filed by
5APR577Y
Atlas Aircraft Center Inc
Aircraft
N959AF
Make and model
Pilats PC1247
Aircraft serial
1059
Aircraft time
1,373 hours, 1,409 cycles
Engine
Pwa PT6A67
Engine time
1,373 hours, 1,409 cycles
Propeller
Hartzl HCE4A3D
Part
Fitting
Part number
5551012150
Condition
Out Of Alignment
Location
Horizontal Stab
Part time
1,373 hours, 1,409 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 GAUGE, AND FOUND TO BE .406MM. THERE IS NO EVIDENCE OF DAMAGE TO THE STABILIZER. THE BRACKET PN IS 555.10.12.150, ANGLE FITTING LT. RESOLUTION: THE ACFT MFG ISSUED A REPAIR MEMO WITH STATEMENT OF APPROVED DESIGN DATA (ECC-12-RM-11-220) WITH THE FOLLOWING INSTRUCTIONS. CHECK THE LUGGED FACE OF THE LT BRACKET PN 555.10.12.150 (ANGLE FITTING LT ) 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 AND HARDWARE USING SEALANT.