Service difficulty report · Frame · Airbus A320232

Difficulty date
May 21, 2024
Submitted
May 24, 2024
Operation
Air carrier
Aircraft
N493UA
Make and model
Airbus A320232
Aircraft serial
1821
Aircraft time
65,448 hours, 28,838 cycles
Part
Frame
Part number
D5311275220200
Condition
Cracked
Location
Frm 16
Stage of operation
IN
How discovered
O
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

RH FR 16 UPPER DOUBLE JOGGLE AREA HOLE 4 HAS CRACK INDICATION IN FRAME LAYER 5 OCLOCK DIRECTION (VIEWED FROM OUTSIDE) 100% S.H PER HAECO LCQ NR 9292345 / 26345 IN THE RH FR16 UPPER DOUBLE JOGGLE HOLES NR 5, 6, 7, 8, A & # ORE THE AIRCRAFT REACHES 35,638 TOTAL AIRCRAFT FLIGHT CYCLES. PE CYCLES, THEREAFTER. REMOVAL. C. IF THERE ARE ANY FINDINGS CONTACT ENGINEERING. D. IF TRANSITION FIT. PART 3, PERMANENT REPAIR: THE REPAIR ACCOMPLISH B PER PART 2 OF THE LATEST REVISION OF ECRA 5311-03204 ON OR BEF RFORM REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 6,800 FLIGHT NIL FINDINGS, REINSTALL FASTENERS AS FOLLOWS: ED IN PART 1 IS A CATEGORY B REPAIR REQUIRING REPETITIVE INSPECT ION REQUIREMENTS (RIR) STATED IN PART 2. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5311-03204. , WET INSTALL FASTENER ASNA2657V5 IN TRANSITI THERE IS NO TERMINATING ACTION FOR THESE REPETITIVE QC REQUIREMENTS: 1. FOR RH FR16 DOUBLE JOGGLE HOLES 5, 6, 7, 8, ON FIT. 2. AT HOLE 6, WET INSTALL FASTENER IN TRANSITI REQUIREMENTS.

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