Service difficulty report · Bolt · Piper PA28181

Difficulty date
April 8, 2003
Submitted
April 8, 2003
Operation
General aviation
Aircraft
N137FC
Make and model
Piper PA28181
Aircraft serial
8290172
Aircraft time
3,890 hours
Engine
Lyc O360*
System (JASC)
1430 · Fasteners
Part
Bolt
Condition
Undertorqued
Location
Vertical Fin
Part time
3,890 hours
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

DURING ANNUAL INSPECTION FOUND VERTICAL FIN LOOSE. UPON CHECKING ATTACHMENT HARDWARE, FOUND THE FOUR BOLTS AT THE REAR SPAR TO BE INSUFFICIENTLY TORQUED. THE SINGLE BOLT AT THE FRONT SPAR WAS TIGHT BUT WOULD NOT PREVENT SIDE TO SIDE MOVEMENT OF THE FIN(APPROX. 1/4 TO 1/2 INCH. THERE WAS NO RECORD OF THE VERTICAL FIN BEING REMOVED FOR MAINTENANCE AND THIS MECHANIC CANNOT OFFER ANY EXPLANATIONS AS TO WHY THESE BOLTS WERE NOT TIGHT. ALL THE ATTACHING BOLTS WERE REMOVED, THE AREAS SURROUNDING THE BOLT HOLES INSPECTED FOR CRACKS, NEW HARDWARE INSTALLED AND RETORQUED.

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