Service difficulty report · Stringer · Airbus A320232

Difficulty date
December 23, 2024
Submitted
December 26, 2024
Operation
Air carrier
Aircraft
N517JB
Make and model
Airbus A320232
Aircraft serial
01327
Aircraft time
87,368 hours, 32,570 cycles
Part
Stringer
Condition
Corroded
Location
Zone 500
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: WINGS / LH WING / BOTTOM STRINGER 3 / BOTTOM FLANGE UPPER SURFACE BETWEEN RIB 5 - 6 / CORROSION - TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 57-9074-24 REV. 0 (COVER) /2/ AEROMAN EA 57-9074-24 (PARTS 1-5 & 7-8 FOR REWORK P2) /3/ AEROMAN EA 57-9078-24 REV. 0 (COVER & PART 1-2 FOR LOCAL MANUFACTURING OF CLEAT WITH DEVIATIONS) /4/ AIRBUS RDAF 81467535/055/2024#A /5/ AIRBUS TD/81467535/014/2024#F /6/ AIRBUS DOSSIER 81467535. DESCRIPTION: AT THE CURRENT (12/2024) C9 CHECK FOR N517JB (MSN 1327) AT SAL, WHILE PERFORMING INSPECTIONS PER MPD 572050-02, CORROSION WAS FOUND ON THE LH WING BOTTOM STRINGER 3, BOTTOM FLANGE UPPER SURFACE BETWEEN RIB 5 - 6 – WHICH IS REFERRED TO AS REWORK P2 (STGR 3). SEE FIGURE 1 IN REF /2/ EA PART 1 FOR MORE DETAILS. THE DAMAGES WERE REVIEWED AGAINST SRM 57-21-13 AND FOUND TO BE OUT OF LIMITS SINCE IT EXTENDED TO RIB 5 OUTBOARD FOOT FLANGE. THEREFORE, AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDED INSTRUCTIONS IN THE REF /5/ TD (PAGES 1-8 & 10-15) WHICH PROVIDES INSTRUCTIONS AT REWORKS P2 TO TRIM RIB 5 AND PERFORM BLENDING ON STRINGER 3 AND INSTALL REPAIR ANGLE REINFORCEMENT. AFFECTED FASTENERS HOLES ARE OVERSIZED WITH OVERSIZED FASTENERS INSTALLED. DRY BAY LEAK CHECK AND FUEL TANK SEAL INSPECTION WERE PERFORMED. DURING REPAIR, AN UNDRILLED STRINGER 3 CLEAT (PN D5725090500039) WAS REQUIRED BUT NOT AVAILABLE. AIRBUS APPROVED LOCAL MANUFACTURE OF THE CLEAT WITH DEVIATIONS OF USING ALUMINUM 6061-T6 AND WELDING PER PMS 01-04-20 UNDER REF /6/ MESSAGE 136. THE REPAIR AND CLEAT MANUFACTURING ARE APPROVED BY THE REF /4/ RDAF AS TIME LIMITED REPAIR PENDING DTA DUE IN 6 MONTHS. EC A24-1566-01 ACCOMPLISHES THE REPAIR PER THE REF /1/ & /2/ & /3/ EA AND COMPLIES WITH THE REF /4/ RDAF WITHOUT DEVIATIONS. EC A24-1566-02 PROVIDES A PLACEHOLDER ISSUED TO TRACK THE 6-MONTH LIMITATION FOR THE DTA. NOTE: REPAIRS AT REWORKS P1 (STGR 2) & P3 (STGR 4) ARE ADDRESSED IN EC A24-1565-01/AEROMAN EA 57-9074-24 PART 6. SUBSTANTIATION: THIS TIME LIMITED REPAIR IS APPROVED BY REF /4/ RDAF AND IS CLASSIFIED AS MAJOR. (E/C: A24-1566-01)

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