Service difficulty report · Window Frame · Airbus A320232

Difficulty date
February 2, 2026
Submitted
February 4, 2026
Operation
Air carrier
Aircraft
N587JB
Make and model
Airbus A320232
Aircraft serial
02177
Aircraft time
80,243 hours, 29,180 cycles
Part
Window Frame
Condition
Cracked
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 / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CTR POST LOWER NODE AREA VERTICAL FLANGE RHS & CONT. FITTING LHS / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0081-25 (COVER + PARTS 1-5) /2/ AIRBUS DOSSIER 81689336 /3/ AIRBUS RDAF 81689336/003/2025 ISSUE A /4/ AIRBUS RI R53113672 ISSUE C RS4 /5/ AIRBUS RI R53112919 ISSUE K /6/ R531-13426 ISSUE G – FWD LOWER TITANIUM PANEL REMOVAL/INSTALLATION. /7/ R531-13467 ISSUE C – FRONT WINDOW FRAME REPLACEMENT. /8/ R531-12972 ISSUE H – LATERAL PANEL FR1-12 REMOVAL/INSTALLATION. /9/ R531-13355 ISSUE C – CROWN PANELS REMOVAL/INSTALLATION. /10/ R531-13470 ISSUE D – FRONT LATERAL WINDOW FRAME JUNCTION. /11/ R531-13241 ISSUE A – SHIM FRONT WINDSHIELD. /12/ R531-13300 ISSUE A – COVER STRIP. DESCRIPTION: DURING CURRENT H6 CHECK OF AC N587JB (MSN 02177) AT SAL, AEROMAN WHILE PERFORMING SB A320-53-1331, REPORTED CRACK WAS FOUND ON THE WINDSHIELD FRAMING CENTER POST LOWER NODE AREA RHS VERTICAL FLANGE. IN ADDITION, THE CONTINUITY FITTING WAS ALSO FOUND TO BE CRACKED. SEE REF /1/ AEROMAN EA FOR FULL DAMAGE DETAILS. AEROMAN REACHED OUT TO AIRBUS FOR REPAIR DISPOSITION VIA REF /2/ DOSSIER. AIRBUS PROVIDED REPAIR DISPOSITION VIA REF/2/ DOSSIER AND APPROVED BY REF/3/ RDAF AS FOLLOWS: CRACK ASSESSMENT WAS PERFORMED AND MIRROR FITTINGS REPLACED AS PER REF /4/ RI R53113672 ISSUE C RS4, CONTINUITY FITTINGS WERE REPLACED AS PER AIRBUS RI R53112919 010 ISSUE K. ADDITIONALLY REPAIR INSTRUCTIONS REF /6/ - REF /12/ WERE REQUIRED EC A25-1024-01 IS RELEASED TO ACCOMPLISH THE PERMANENT REPAIR OF THE CRACK DAMAGES AS PER REF/1/ AEROMAN EA AND REF /3/ RDAF.EC A25-1024-02 IS RELEASED TO ACCOMPLISH THE POST REPAIR INSPECTIONS (HFEC) OF THE CONTINUITY FITTINGS AS REQUIRED BY REF /3/ RDAF AS FOLLOWS: THRESHOLD = 30,600FC (FH NOT RELEVANT) INTERVAL = 8,800 FC (FH NOT RELEVANT) METHOD: HFEC OF CONTINUITY FITTINGS AS PER NTM 53-11-29. NOTE: AS PER REF/3/ RDAF SB 53-1331 IS NO LONGER APPLICABLE ANYMORE TO THIS A/C. SUBSTANTIATION: THIS CAT B PERMANENT REPAIR IS APPROVED BY REF /3/ RDAF AND IS CLASSIFIED AS MAJOR.(E/C: A26-062-01)

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