SDR 5APR577Y34

Service difficulty report · Lug · Pilats PC1247

Difficulty date
April 2, 2010
Submitted
April 13, 2010
Operation
General aviation
Aircraft
N421PP
Make and model
Pilats PC1247
Aircraft serial
1010
Aircraft time
425 hours, 353 cycles
Engine
Pwa PT6A67
Engine time
425 hours, 353 cycles
Propeller
Hartzl HCE4A3D
Part
Lug
Part number
5551012150
Condition
Separated
Location
Horizontal Stab
Part time
425 hours, 353 cycles
Component
Horizontal Stab · Pilats
Component part number
5551012037
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

(5APR) THE HORIZONTAL STAB PN 555.10.12.037, SN 815, FWD PITCH TRIM ACTUATOR ATTACHMENT FITTING LT OTBD LUG PN 555.10.12.150, IS SEPARATED FROM THE CTR SECTION OF THE FITTING BY 0.76 MM'S. OTBD ATTACHMENT LUGS ARE NORMALLY ALIGNED WITH THE CTR SECTION OF THE ATTACHMENT FITTING WITH NO GAPS. NOTIFIED ENGINEERING OF THE MECHANICAL IRREGULARITY WITH A MFG DEFECT REPORT; AND RECEIVED TECHNICAL MEMO ECC-12-TM-10-104 IN RESPONSE TO THE DEFECT REPORT. PERFORMED EDDY CURRENT INSP OF THE SUSPECT ATTACHMENT LUG WITH NO DEFECTS NOTED. CHECKED ALIGNMENT AND SYMMETRY OF THE HORIZ STABILIZER UTILIZING FACTORY SPECIFICATIONS FOR THIS ACFT SN WITH NO DEFECTS NOTED. APPLIED PR1422-B2 SEALANT TO THE ATTACHMENT LUG GAP AS AN INTRIM MEASURE, DETERMINED THE ACFT TO BE AIRWORTHY AND RELEASED THE ACFT FOR 50 HOURS OF OPERATION OR UNTIL 4-30-10 IAW THE TECHNICAL MEMO WHILE ENGINEERING DETERMINES A TERMINATING ACTION FOR THE DEFECT. IT APPEARS THAT THE LT ATTACHMENT LUG MAY HAVE BEEN MISALIGNED DURING MFG, OR MAY HAVE SHIFTED DURING OPERATION.