Service difficulty report · Floor Panel · Bombdr DHC8402

Difficulty date
January 31, 2016
Submitted
February 3, 2016
Operation
Air carrier
Aircraft
N412QX
Make and model
Bombdr DHC8402
Aircraft serial
4059
Aircraft time
34,337 hours, 35,753 cycles
Part
Floor Panel
Condition
Corroded
Location
Bs 216-234
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

UNDER FLOOR PANEL 133FZ, BETWEEN BS 216 TO BS 234, UNDER THE ISAT BOX BETWEEN STR 31L TO STR 33L, THERE ARE RIVETS WITH EVIDENCE OF POSSIBLE CORROSION, MARKED. REMOVED 23 CORRODED RIVETS FROM INNER LONGITUDINAL STRAP JOINT BETWEEN BS X 216- BS X 234 BETWEEN STR 31L-STR33L, REF SRM 51-42-05. INSTALLED 23 CORRODED RIVETS FROM INNER LONGITUDINAL STRAP JOINT BETWEEN BS X 216- BS X 234 BETWEEN STR 31L-STR 33L REF SRM 51-42-05-02-01 STEP 4D, 3-10. REMOVED CORROSION ON LONGITUDINAL INTERNAL JOINT STRAP BETWEEN X 216-X 234 BETWEEN STR 31L -32L REF SRM 53-00-00 REPAIR-20. LONGITUDINAL INTERNAL STRAP CORRODED 100 PERCENT OF MATERIAL AT APPROXIMATELY 7.25" FWD OF X 234 AND 2.5" INBD OF STR 31L LONGITUDINAL STRAP OUT OF LIMITS. RECEIVED R/D 8/4-53-7262 ISSUE 1. C/W ET INSP UT THICK TEST ON STRAP BETWEEN FS X 216-234 + BETWEEN STR 31P-32P REF NDTM TP1 51-00-06 + 51-00-04. NO DEFECTS NOTED MIN THICK RANGE MEASURED=.000" TO .052". C/W ET INSPECT ON CUTOUT IAW RD 8/4-53-7262, ISSUE 1. FABRICATE REPAIR PACKER AND DOUBLER REF SRM 51-40-07 AND REPAIR RD 8/4-53-7262 MAT 2024T3 .050 TX 0002920,202 + T3.063 TX 00020092. INSTALLED REPAIR PACKER AND DOUBLER REF R/D 8/4-53-7262, ISSUE 1. APPLIED A COAT OF ALUMINIZED POLYURETHANE ENAMEL, F24 TO INNER SURFACE OF REPAIR REF R/D 8/4-53-7262 ISSUE 1. APPLIED MOSITURE DISPLACING COMPOUND TO INNER SURFACE REF R/D 8/4-53-7262 ISSUE 1.