Service difficulty report · Splice · Airbus A320232

Difficulty date
September 12, 2019
Submitted
September 16, 2019
Operation
Air carrier
Aircraft
N561JB
Make and model
Airbus A320232
Aircraft serial
1927
Aircraft time
65,831 hours, 23,681 cycles
Part
Splice
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, WHILE ACCOMPLISHING THE REF /3/ SB AS PART OF THE CURRENT HEAVY CHECK THE H2 RT, H3 & H8 LT SIDE HOLES WERE FOUND WITH CRACK AT FR16 RT AND LT CROSSBEAM SPLICING. THE AFFECTED HOLES WERE REAMED UP TO 6.35MM (0.250IN) BUT CRACK PERSISTED ON H2 RT & H3 LT SIDES. MANUFACTURER WAS CONTACTED FOR ASSESSMENT AND PROVIDED A BUSHING REPAIR FOR AFFECTED HOLES H2 RT & H3 LT AND REPAIR DRAWING R531-12926 ISSUE C FOR HOLE H8 LT AND FOR ALL OTHER HOLES WITHOUT CRACK INDICATION AS PER REF /4/ TD. ISSUED THE REF/1/ EA DOCUMENTING THIS REPAIR AS PER THE REF/2/ RDAS. THIS REPAIR REQUIRES A POST REPAIR INSPECTION AT 54000FC, WHERE THE METHOD OF INSPECTION & INTERVAL ARE TBD PER THE REF/2/ RDAS. ALSO PER THE REF/2/ RDAS FOR FR16LT & FR16RT, THE INSPECTIONS REQUIRED PER REF/3/ SB ARE NOW CANCELLED AND SUPERSEDED BY THE MENTIONED INSPECTION OF THIS RDAS. EC A19-640-01 IS ISSUED TO TRACK THIS REPAIR PER THE REF/1/ EA & THE REF/2/ RDAS WITHOUT DEVIATION. IT IS ALSO SET UP TO TERMINATE THE REF/3/ SB. EC A19-640-01 IS ISSUED TO TRACK THE POST REPAIR INSPECTIONS PER THE REF/2/ RDAS WHERE IT IS DUE AT 54000FC FROM REPAIR EMBODIMENT (EMBODIED AT 23681FC / 65831FH ON 08/30/2019). THE METHOD OF INSPECTION AND INTERVAL ARE TBD; THIS REPAIR HAS BEEN APPROVED BY THE REF/2/ RDAS. THIS REPAIR IS CLASSIFIED AS CATEGORY B AND THIS EC IS CLASSIFIED AS “MAJOR”.

More about the Airbus A320-232