Service difficulty report · Panel · Airbus A320232

Difficulty date
May 27, 2022
Submitted
May 30, 2022
Operation
Air carrier
Aircraft
N443UA
Make and model
Airbus A320232
Aircraft serial
820
Aircraft time
75,236 hours, 29,837 cycles
Part
Panel
Part number
D5323171320001
Condition
Elongated
Location
Frng Pnl Fr34
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 HMV IN BQN AFTER REMOVAL OF THE BELLY FAIRING PNL AT FR34, FOUND SEVERAL FASTENER HOLES ELONGATED. ORIGINAL HOLE DIA IS 5/32IN. REPAIR OF THE EFFECTED HOLES REQUIRED PER EO-A32F-53-12319-00-WIP COVERED BY ECRA 5321-02074 MM) HILOCK IN HOLES #3,4,5,8,15,16,25,&26. INSTALLED 2ND OVERSIZ FR33/34 AND STGR41LH/RH PER PART 2, STEP 1. OF LATEST REVISION ED 3/16(5.52MM) HILOCK IN HOLES 19,21&29. COMPLETED REPAIR IAW E OF ECRA 5321-02074. O-A32F-53-12319-00-FINAL PER ECRA 5321-02074. CLASSIFIED MINOR R EPAIR CAT-B. NEED DTA DIP FOR REINSPECTION "ON OR BEFORE NOVEMBER 23, 2022, PERFORM INSPECTION OF AIRCRAFT 4643 FUSELAGE STRUCTURE BETWEEN OK TO CARRY INTERIM REPAIR INSPECTIONS TO BE ACCOMPLISHED ON OR TOMC-APPROVAL FROM SC1ELBYC COMMENT BEFORE NOV. 23 2022, ON FR33/34 AND STGR 41LH/RH PER PART 2 STEP 1 OF THE LATEST REV OF ECRA5321-02074 UPON REMOVAL OF BELLY FAIRING PANEL BETWEEN FR33-34 STGR 41L-41R REVIEWED RECORDS UPDATE ELONGATED HOLES WERE FOUND. REAMED HOLES TO REMOVE DMG. ROTOTES T AND DVI WITH NIL FINDINGS. INSTALLED BUSHING AND NOMINAL 3/16( 4.8MM) HILOCK IN HOLES #1 & 22. INSTALLED 1ST OVERSIZE 3/16(5.12 QC REVIEWED T/A: 23NOV22...SN

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