Service difficulty report · Scuff Plate · Airbus BD5001A11

Difficulty date
September 20, 2024
Submitted
September 24, 2024
Operation
Air carrier
Aircraft
N3085J
Make and model
Airbus BD5001A11
Aircraft serial
55132
Aircraft time
7,920 hours, 3,024 cycles
Part
Scuff Plate
Condition
Corroded
Location
Zone 200
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 HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / RH FWD SERVICE DOOR SCUFF PLATES / UNDERNEATH LOWER SCUFF PLATE / CORROSION - TEMPORARY REPAIR; REFERENCES: /1/ AIRBUS CANADA REO-500-53-21-927 REV. -- /2/ AIRBUS CANADA REO-500-53-21-914 REV. – /3/ DAMAGE REPORT /4/ AVIANOR NRC A49107-1021 /5/ SB BD500-530010 ISSUE 004. DESCRIPTION: DURING THE CURRENT HEAVY CHECK AT YMX DATED SEPTEMBER 2024, N3085J (MSN 55132), WAS FOUND WITH TOTAL THIRTEEN (QTY 13) CORROSION SPOTS AFFECTING THE FORWARD FUSELAGE RH LOWER SKIN (P/N C02312410-007 REF) UNDERNEATH SERVICE DOOR LOWER SCUFF PLATES. SEE THE REF /3/ DAMAGE RPEORT FOR MORE DETAILS. THE FOLLOWING ARE THE MRT DIMENSIONS AFTER THE BLEND OUT: REWORK #1: 0.113” REWORK #2: 0.112"REWORK #3: 0.120" REWORK #4: 0.112" REWORK #5: 0.119" REWORK #6: 0.112" REWORK #7: 0.116" REWORK #8: 0.117" REWORK #9: 0.113" REWORK #10: 0.114" REWORK #11: 0.113" REWORK #12: 0.063" REWORK #13: 0.119". THE ASRP WAS CONSULTED AND NO ALLOWABLES WERE FOUND FOR THIS DAMAGE. AIRBUS CANADA WAS CONTACTED FOR DISPOSITION AND PROVIDED REF /1/ REO FOR REWORK AREA #1 TO #8 WITH APPROVAL OF THE MENTIONED MRT TO BE ACCEPTABLE AS IS WITH INSPECTIONS PERFORMED, SURFACE REPROTECTION APPLIED AND REPLACING AFFECTED FASTENERS AND FOR REWORKED AREA #9 TO #13 AIRBUS PROVIDED REF /2/ REO TO OPEN UP THE HOLES, INSTALL SOLID RIVETS, INSTALL DOUBLER AND APPLY CIC ON THE AREA. REF /1/ AND REF /2/ REO STATED TO COMPLETED REF /5/ SB BD500-530010 ISSUE 004-PART A (THIS SB EC IS ALREADY ASSIGNED TO THIS CHECK). THESE INSTRUCTIONS ARE APPROVED AS A TEMPORARY REPAIR WITH 10000 FH LIMITATION AND REINSPECTION REQUIREMENT. EC AC24-1200-01 IS ISSUED TO TRACK THE TEMPORARY REPAIR ACCOMPLISHMENT IN ACCORDANCE WITH REF /1/REO AND REF /2/ REO WITHOUT DEVIATIONS. EC AC24-1200-02 IS ISSUED TO TRACK THE POST REPAIR INSPECTIONS IN ACCORDANCE WITH REF /1/ REO AND REF /2/ REO (METHOD: DVI, THRESHOLD & INTERVAL: 1000FH) EC AC24-1200-03 IS ISSUED TO TRACK THE PERMANENT REPAIR WITHIN 10,000FH - PENDING OEM INSTRUCTIONS. SUBSTANTIATION: THIS REPAIR HAS BEEN ACCOMPLISHED IN ACCORDANCE WITH REF /1/ & /2/ REO WITHOUT DEVIATIONS. THIS REPAIR IS CLASSIFIED AS MAJOR (E/C: AC24-1200-01)

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