Service difficulty report · Nut Plate · Piper PA28140

Difficulty date
September 4, 2020
Submitted
September 5, 2020
Operation
General aviation
Aircraft
N5944U
Make and model
Piper PA28140
Aircraft serial
2826837
Aircraft time
5,600 hours
Part
Nut Plate
Condition
Corroded
Location
Rt Wing
Part time
5,600 hours
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

DEFECT DISCOVERED UPON REMOVAL OF RT FUEL TANK. ALL 4 INDEPENDENT FLOATING NUT PLATES MS2106L08 FOUND SEVERELY CORRODED WITH RUST. THE NUT PLATE HOUSING AND THREADED ANCHOR PORTION WERE RUSTED. THE AREA WHERE THE NUT PLATE CONTACTS THE SPAR CREATED PITTING. THIS PITTING SEEMED TO BE A SUB SURFACE OR UNDERCUTTING TYPE THAT HAD MORE UNSEEN CORROSION THAT WAS ADJACENT THE BASE OF THE NUT PLATE, THAN THE ORIGINAL PENCIL TIP SIZED PITTING. ALTHOUGH THE CORROSION REMOVAL SEEMS SUPERFICIAL, IF GONE UNDETECTED THE DAMAGE COULD HAVE BECOME IRREPARABLE. I BELIEVE THE PITTING WAS ACCELERATED BY CONTAMINATION TRAPPED BETWEEN THE DISSIMILAR METAL OF THE NUT PLATE AND SPAR. I RECOMMEND THAT PA28 OWNERS BECOME AWARE OF THIS POTENTIAL PROBLEM AND EVALUATE THESE NUT PLATES ANY TIME THE FUEL TANKS ARE REMOVED. TO MITIGATE FUTURE NUT PLATE CORROSION, I RECOMMEND APPLYING A ZINC CHROMATE AEROSOL PRIMER TO THE NUT PLATES. THIS WOULD CREATE A BARRIER BETWEEN THE DISSIMILAR METALS AND ACTIVELY PREVENT CORROSION. TAKE NOTE NOT TO SPRAY THE THREADS FROM THE PRIMER (QTIPS WORKED FOR ME) AND MAKE SURE THE FLOATING ANCHOR DOESN'T SEIZE FROM THE DRYING PRIMER.ONLY ONE NUT PLATE SPAR AREA HAS BEEN INSPECTED SO FAR AFTER REMOVAL OF NUT PLATES, BUT THE OTHERS HAVE INDICATION OF SURFACE CORROSION. THE DAMAGE SO FAR IS LIMITED TO THE SPAR AREA WHERE ONE OF FOUR NUTPLATES WAS REMOVED DUE TO RUST AND IS THE RH WING/FUEL TANK HOUSING LOWER INBOARD CORNER SPAR AREA.

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