# SDR YENA2026091000745

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 5, 2026
- Submitted: September 11, 2026
- Operation: Air carrier
- Aircraft: [N784JB](https://openairdocs.org/aircraft/N784JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 04587
- Aircraft time: 56,508 hours, 20,078 cycles
- System (JASC): [5730 · Wing, Plate/Skin](https://openairdocs.org/jasc/5730)
- Part: Access Panel
- Condition: Damaged
- Location: Zone 600
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/YENA2026091000745

## Discrepancy

DURING HEAVY MAINTENANCE, SECONDARY FINDING ELONGATED HOLE CUT OUT FUEL TANK ACCESS PANEL 640KB ON RT WING ; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00042 )  REF AEROMAN PERFORMED PERMANENT REPAIR ON (HOLE #1) LOCATED ON BOTTOM SKIN PANEL #2 BTW RIB 15 TO RIB 16 AT RH WING, THIS REPAIR IS CATEGORY B, INSTALLED BOLTS P/N NAS1790-5R13 ON ACCESS PANEL 640KB IAW SRM A320 SRM 57-21-11-300-002, FOR BUSHING INSTALLED ON HOLE #1 INSPECTION THRESHOLD FROM AIRCRAFT FIRSTFLIGHT AS FOLLOWING 24400FC/48800FH AND SUBSEQUENT INSPECTION AT INTERVALS OF 4800FC/9600FH, METHOD OF INSPECTION GVI IAW SRM A320 57-21-11-205-036 TABLE 3. THE INSPECTION METHOD TO TRACKING ONLY HOLE #2 IS DOCUMENTED IN 2026-355336.  HOLE #1 FUR-A320-57-03412

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