Service difficulty report · Frame · Airbus A320232

Difficulty date
July 19, 2024
Submitted
July 23, 2024
Operation
Air carrier
Aircraft
N506JB
Make and model
Airbus A320232
Aircraft serial
01235
Aircraft time
86,078 hours, 32,219 cycles
Part
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 / RHS FR16 DOUBLE JOGGLE AREA HOLE C AND #6 / CRACKS - PERMANENT REPAIR; REFERENCES: AEROMAN EA 53-9015-24 REV. 0 (COVER + PARTS 1-3) AIRBUS SB A320-53-1373 REV. 01 AIRBUS RDAF 81411276/028/2024#A AIRBUS DOSSIER 81411276 AIRBUS REPAIR DRW R531-13041 ISSUE F SRM TASK 53-11-12-300-012 DURING THE CURRENT (07/2024) C9 CHECK, REPORTED WHILE THE ACCOMPLISHMENT OF SB CRACKS WERE FOUND ON THE NOSE FWD FUSELAGE DOUBLE JOGGLE AREA AT FR16 RHS AT HOLES #6 (FRAME LAYER), & HOLE C. AEM REPORTED HOLE #C CRACK FREE CONDITION WAS 0.330 INCHES & COLD WORKING 10-3-N WAS PERFORMED INSTEAD OF 10-1-N AT HOLE #6. AIRBUS WAS CONTACTED AND PROVIDED INSTRUCTIONS VIA DOSSIER. THE REPAIR CONSISTED OF PERFORMING REPAIR. AIRBUS APPROVED THIS REPAIR PER THE RDAF AS PERMANENT REPAIR, WITH POST REPAIR INSPECTION REQUIRED: RH FR 16 HOLE #C (AND ASSOCIATED HOLE #D): A. METHOD: I. AT HOLE #C: ROTOTEST INSPECTION AS PER NTM 51-10-01 & 51-10-18 AFTER FASTENER & BUSH REMOVAL. AT HOLE #D: ROTOTEST INSPECTION AS PER NTM 51-10-01 AFTER FASTENER REMOVAL B. THRESHOLD = INTERVAL = 5,400FC 2. RH FR 16 HOLE #6 (AND ASSOCIATED HOLE #5) A.AT HOLE #6: ROTOTEST INSPECTION AS PER NTM 51-10-01 & 51-10-18 AFTER FASTENER AND BUSH REMOVAL. AT HOLE #5: ROTOTEST INSPECTION AS PER NTM 51-10-01 AFTER FASTENER REMOVAL B. THRESHOLD: 6,800FC C. INTERVAL: 5,300FC. EC A24-857-01 ACCOMPLISHES THE PERMANENT REPAIR PER THE REF /1/ AEROMAN EA AND COMPLIES WITH REF /3/ RDAF. EC A24-857-02 IS ISSUED TO ACCOMPLISH THE POST REPAIR INSPECTION REQUIREMENTS ON HOLES #C & #D PER THE REF /3/ RDAF (THRESHOLD = INTERVAL = 5,400FC, METHOD = ROTOTEST). EC A24-857-03 IS ISSUED TO ACCOMPLISH THE POST REPAIR INSPECTION REQUIREMENTS ON HOLES #6 & #5 PER THE REF /3/ RDAF (THRESHOLD = 6,800FC; INTERVAL = 5,300FC; METHOD = ROTOTEST). NOTE: MOD SB A320-53-1380 IS NO LONGER APPLICABLE AT REPAIRED HOLES #C AND #6 AND ASSOCIATED HOLES #5 AND #D ON FR16 RHS ONLY. SUBSTANTIATION: THIS PERMANENT, CATEGORY B, REPAIR HAS BEEN APPROVED VIA REF /3/ RDAF AND IS CLASSIFIED AS MAJOR. (E/C: A24-857-01)

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