Service difficulty report · Skin · Airbus A320232

Difficulty date
October 3, 2024
Submitted
October 23, 2024
Operation
Air carrier
Aircraft
N433UA
Make and model
Airbus A320232
Aircraft serial
589
Aircraft time
85,688 hours, 34,023 cycles
Part
Skin
Condition
Damaged
Location
Zone 100
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

REF LP 9356893 LIGHTING STRIKE FOUND ON FRAME 54 BETWEEN STR 36L AND STR 37L LENGHT IS .2 BY WIDE 1.7 IAW SRM 53-21-11-283-004 FIG 1,SPEED TAPED DISCREPANT AREA AS PER SRM 51-75-12-911-022. UNLOCKING ACCOMPLISHED GVI OF REMOVED DAMAGED AREA PER SRM 53-21-11-300-900 PART 2&3. CONFIRMED REPAIR MATERIALS PER SRM 53-21-11-300-900 FIG. 1. REMOVED DAMAGED AREA PER SRM 54-41-11-300-109 PAR 2 PART 7. VERIFY REPAIR DOUBLER AND FILLER MATERIAL AS 2024T3 0.063 PO 4569197 AND 2024T3 0.71 PO 5146296 PER SRM 53-41-11-300-109 FIG 1. QC UPDATE: CORRECTED SRM REFERENCE TO 53-41-11-300-109 FIGURE 1. INSPECTED REPAIR DOUBLER PER SRM 53-41-11-305-109 PRT 12 THRU 31 NO DEFECTS OK TO ALODINE PRIME AND INSTALL FABRICATED REPAIR DOUBLER PER SRM 53-41-11-305-109 PAR 2 PART 12 THRU 31. OK TO ALODINE PRIME AND INSTALL. NO REPAIR WASHERS ARE NEED PER SRM 53-21-11-300-900 PAR 2 PART 26. ALL HOLES STEPPED UP TO A NUMBER 6 FASTENER. INSPECTED PER RII. INSPECTED PER RII AND SRM 53-41-11-305-109 STEP 33 THRU 38. INSPECTED PER RII AND SRM 53-41-11-305-109. INSTALLED REPAIR DOUBLER PER SRM 53-41-11-305-109 PAR 32.SEALED PRIMED AND PAINTED AND APPLIED CORBAN TO INNER SKIN PER SRM 53-41-11-305-109 STEPS 33 THRU 38 QC ACHIEVED FIRST. REPAIR DIP REQUIRED PER SRI 53-41-11-205-031 INSPECTION OF REPAIR 60000 FC OR 120000 FH WHICHEVER VALUE FC OR FH IS OKAY TO CARRY REF SRI 53-41-11-205-031 TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS REVIEW.

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