Service difficulty report · Shear Plate · Airbus A320232

Difficulty date
July 27, 2019
Submitted
July 31, 2019
Operation
Air carrier
Aircraft
N644JB
Make and model
Airbus A320232
Aircraft serial
2880
Aircraft time
51,854 hours, 18,471 cycles
Part
Shear Plate
Condition
Cracked
Location
Fuselage
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, REPORTED THAT DURING THE ACCOMPLISHMENT OF THE REF /3/ SB FOR INSPECTION OF THE TI- ANGLES BETWEEN THE BELLY FAIRING & KEEL BEAM SIDE PANEL (AS REQUIRED BY THE REF /4/ AD)– THAT ON THE RT SIDE THE TI-ANGLE AT FR 41-42 AND SHEAR PLATE WAS CRACKED. PER THE REF /3/ SB & REF /4/ AD INSTRUCTIONS – THIS CRACKED ANGLE WAS REPLACED, BUT DUE TO THE CRACK IN THE SHEAR PLATE WAS CONTACTED FOR FURTHER INSTRUCTIONS. PROVIDED THE REF /3/ TD – WHICH PROVIDES INSTRUCTIONS TO PERFORM CUTOUT IN THE SHEAR PLATE TO REMOVE THE CRACK DAMAGE, PERFORM NDT INSPECTIONS, MANUFACTURE AND INSTALL DOUBLER/FILLER, AND RESTORE SURFACE PROTECTION. ALL OTHER REQUIREMENTS OF THE REF /3/ SB AND REF /4/ AD REMAIN AND MUST BE COMPLETED. PROVIDED THE REF /2/ RDAS WHICH APPROVES THESE REPAIR INSTRUCTIONS, WITH A 6 MONTH LIMITATION FOR FURTHER DAMAGE TOLERANCE ANALYSIS (DTA) TO BE ACCOMPLISHED. THIS EC ACCOMPLISHES THE PERMANENT REPAIR PER THE REF /1/ EA AND COMPLIES WITH REF /2/ RDAS WITHOUT DEVIATION. THIS EC A19-519-01 PROVIDES THE TIME LIMITED REPAIR INSTRUCTIONS. EC A19-519-02 IS ISSUED TO TRACK THE DTA, DUE WITHIN 6 MONTHS FROM REPAIR ACCOMPLISHMENT; THIS TIME LIMITED REPAIR HAS BEEN APPROVED VIA REF /2/ RDAS, IS VALID FOR 6 MONTHS, AND IS CLASSIFIED AS MAJOR.

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