Service difficulty report · Bolt · Piper PA24

Difficulty date
July 7, 2002
Submitted
September 23, 2002
Operation
General aviation
Aircraft
N6841P
Make and model
Piper PA24
Aircraft serial
241974
Engine
Lyc O360*
System (JASC)
1430 · Fasteners
Part
Bolt
Part number
AN175C33A
Condition
Corroded
Location
Stabilator
Part time
5,515 hours
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

DURING ANNUAL INSPECTION STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS (PN AN175C33A) THAT ATTACHES THE STABILATOR HORN ASSEMBLY TO THE TORQUE TUBE WERE SEVERLY CORRODED. HORN ASSEMBLY,BOLTS, TOTAL AIRFRAME APPROXIMATELY 5515.0. NO INDICATION THAT STABILATOR HAD BEEN REMOVED PREVIOUSLY. FILED WITH FAA. (SW15200210929)

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