Service difficulty report · Door Frame · Airbus A320232

Difficulty date
November 6, 2024
Submitted
November 12, 2024
Operation
Air carrier
Aircraft
N571JB
Make and model
Airbus A320232
Aircraft serial
02125
Aircraft time
78,938 hours, 28,634 cycles
Part
Door Frame
Condition
Cracked
Location
Fr 20 Rh
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 / FR 20 RH / DOUBLE JOGGLE AREA / DOOR STOP FITTING 7 HOLE 6 / CRACK - PERMANENT REPAIR (FRAME REPLACEMENT); REFERENCES: /1/ AEROMAN EA 53-9051-24 REV. 0 (COVER & PART 1 - 2) /2/ AIRBUS SB A320-53-1374 REV 03 (JETBLUE EC A320-53-1374) /3/ AIRBUS REPAIR INSTRUCTION R53113041 ISSUE F /4/ AIRBUS RDAF 81468101/003/2024#A /5/ AIRBUS REPAIR INSTRUCTION R531 13211 005 /6/ AIRBUS REPAIR INSTRUCTION R531 13630 009. DURING THE CURRENT (10/2024) M2 CHECK FOR A/C N571JB (MSN 02125), AEROMAN REPORTED THE ACCOMPLISHMENT OF THE REF /2/ SB – A CRACK WAS FOUND ON THE DOUBLE JOGGLE AREA AT FR 20 RH AT DOOR STOP FITTING 7 HOLE 6 IN THE FRAME AND UPPER CORNER DOUBLER LAYERS (USING THE REF /3/ DRAWING NOMENCLATURE). REFER TO REF /1/ EA FOR DETAILS. THE DAMAGE WAS REAMED UP 15.95MM DIAMETER TO ELIMINATE CRACK AND WAS FOUND TO BE OUT OF SRM & RI REPAIRABLE LIMIT. THEREFORE, AIRBUS WAS CONTACTED FOR ASSESSMENT AND PROVIDED REPAIR INSTRUCTIONS TO PERFORM BUSHING REPAIR PER PRINCIPLE OF REF /3/ RI, WITH DEVIATIONS OF NOT PERFORMING SAFETY CUT AND COLD WORKING AND TO INSTALL NOMINAL SIZE FASTENERS AT HOLE #5 & #6. AIRBUS APPROVED THIS REPAIR PER THE REF /4/ AIRBUS RDAF AS A TEMPORARY REPAIR, WITH POST REPAIR INSPECTION REQUIREMENTS AT HOLE #6 AND ASSOCIATED HOLE #5 AS FOLLOW, HOLES #5 AND #6 AT FR20 RH – THRESHOLD & INTERVAL: 3000FC (FROM REPAIR) AT HOLE #6: ROTOTEST AS PER NTM 51-10-01 AFTER FASTENER REMOVAL AND NTM 51-10-18 AFTER BUSH REMOVAL. AT HOLE #5: ROTOTEST AS PER NTM 51-10-01 AFTER FASTENER REMOVAL. EC A24-1307-01 IS ISSUED TO ACCOMPLISH THE TEMPORARY REPAIR PER THE REF /4/ RDAF. EC A24-1307-02 IS ISSUED TO TRACK THE POST REPAIR INSPECTION REQUIREMENTS PER THE REF /4/ RDAF. EC A24-1307-03 IS ISSUED TO TRACK PERMANENT REPAIR (FRAME REPLACEMENT PER REF /5/ & /6/ RI INSTRUCTED VIA TRM 81468101/023) DUE AT 5000FC. NOTE: REF /2/ SB ARE SUPERSEDED BY THE REF /4/ RDAF AT HOLES #5 & #6 ON FR 20 RH. REF /2/ SB REMAINS VALID FOR ALL OTHER LOCATIONS SPECIFIED IN THE SB. SUBSTANTIATION: THIS EC ACCOMPLISHES A FRAME REPLACEMENT AS A PERMANENT SOLUTION AND IS CLASSIFIED AS MAJOR. (E/C: A24-1307-03)

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