# Service difficulty reports that cite it: Airbus SB A320-53-1491 A list on [Airbus SB A320-53-1491](https://openairdocs.org/service-documents/airbus/a320-53-1491.md). Newest first, with the revision each cites, as OpenAirDocs read it from the records’ text. OpenAirDocs read these citations from the records’ text, so one can be misread: check it against the record. A newer revision may exist that no record cites. - [SDR DALA2026053103299](https://openairdocs.org/sdr/DALA2026053103299.md): Stop Fitting · Airbus A320212 · May 29, 2026 · N341NW · No revision named > EXISTING REPAIR FR68, INNER CAP & FR FLANGE, STRG 22 RH AT LEVEL DOOR STOP FITTING 1. CONTACT DELTA LIAISON ENGINEERING FOR ALTERNATE INSPECTION INSTRUCTIONS THAT MAY BE REQUIRED TO COMPLETE WORK CARD - [SDR DALA2026052703210](https://openairdocs.org/sdr/DALA2026052703210.md): Web · Airbus A320212 · May 26, 2026 · N351NW · No revision named > A.A. WORK CARD 5311-01244-02B, REQUESTING REPAIR DISPOSITION. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED, AND REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. REFER TO EM 5311- 01244 AND SB - [SDR DALA2026012800694](https://openairdocs.org/sdr/DALA2026012800694.md): Repair · Airbus A320212 · Jan 24, 2026 · N353NW · No revision named > EXISTING REPAIR DOUBLER ON AREA FR68 RT AT LEVEL DOOR STOP 1, S22R. REFERENCE WORK CARD 5311-01244-02B AND SB A320-53-1491. COMPLIED WITH ER/A 616797-14AD REV B, NOT MATCHES WITH ALL STEPS ON PRI 6167 - [SDR YENA2024100801339](https://openairdocs.org/sdr/YENA2024100801339.md): Door Frame · Airbus A320232 · Oct 5, 2024 · N559JB · Revision 02 > DURING HEAVY MAINTENANCE, REAR FUSELAGESB53-1491 DOOR STOP FITTING NR 1 STR 22L FR 68 HOLE FILLET RADIUS CRACKED PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-9041-24 REV 0 (COVER, PARTS 1-4) /2/ AIRBUS - [SDR DALA2024032503711](https://openairdocs.org/sdr/DALA2024032503711.md): Door Frame · Airbus A320212 · Mar 22, 2024 · N362NW · Revision 01 > SHIP 3262 DISC: AD RELATED: R/H FR.68, STGR. 22, FRAME WEB HORIZONTAL FLANGE LOWER SURFACE RADIUS CRACKED APROX" 1.5 INCH IN LENTHG.REQUESTING REPAIR DISPOSITION.ADITIONAL ENGENIRING DOCUMENTATION IS - [SDR DALA2024022502575](https://openairdocs.org/sdr/DALA2024022502575.md): Frame · Airbus A320212 · Feb 23, 2024 · N367NW · Revision 01 > SHIP 3267 DISC: CRACK INDICATION ON FRAME 68 LH SIDE IN FRAME WEB AFT FACE HORIZONTAL FLANGE AT LEVEN OF STGR 22, CRACK LENGTH IS 0.688 INCH. REQUESTING REP AIR DISPOSITION. ADDITIONAL ENGINEERING DOC - [SDR DALA2024022502576](https://openairdocs.org/sdr/DALA2024022502576.md): Frame · Airbus A320212 · Feb 23, 2024 · N367NW · Revision 01 > SHIP 3267 DISC: CRACK INDICATION ON FRAME 68 RH SIDE IN FRAME WEB AFT FACE HORIZONTAL FLANGE AT LEVEN OF STGR 22, CRACK LENGTH IS 0.214 INCH. REQUESTING REP AIR DISPOSITION. ADDITIONAL ENGINEERING DOC - [SDR CALA2023041001069](https://openairdocs.org/sdr/CALA2023041001069.md): Web · Airbus A320232 · Apr 7, 2023 · N408UA · No revision named > WHILE PERFORMING UAL EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491), CRACK WAS FOUND AT FR 68 RHS STGR 22 LOWER WEB HORIZONTAL FLANGE RADIUS. CRACK LENGTH APPROX.439". RCRAFT N408UA (4108) REACH - [SDR CALA2023040601055](https://openairdocs.org/sdr/CALA2023040601055.md): Web · Airbus A320232 · Apr 6, 2023 · N408UA · No revision named > WHILE PERFORMING UAL EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491), CRACK WAS FOUND AT FR 68 RHS STGR 22 LOWER WEB HORIZONTAL FLANGE RADIUS. CRACK LENGTH APPROX.439". RCRAFT N408UA (4108) REACH - [SDR CALA2023040401024](https://openairdocs.org/sdr/CALA2023040401024.md): Frame · Airbus A320232 · Apr 4, 2023 · N458UA · No revision named > WHILE PERFORMING EA 5341-01231 REV B OP 1 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 LHS STGR 22 WEB HORIZONTAL FLANGE RADIUS AND IN A STOP FITTING HOLE. EMENTS. ACCOMPLISH INITIAL INS - [SDR CALA2023040401025](https://openairdocs.org/sdr/CALA2023040401025.md): Frame · Airbus A320232 · Apr 4, 2023 · N458UA · No revision named > WHILE PERFORMING EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 RH STGR 22 WEB HORIZONTAL FLANGE RADIUS. SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLISH A PERM - [SDR CALA2023040401037](https://openairdocs.org/sdr/CALA2023040401037.md): Flange · Airbus A320232 · Apr 4, 2023 · N458UA · No revision named > WHILE PERFORMING EA 5341-01231 REV B OP 1 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 LHS STGR 22 WEB HORIZONTAL FLANGE RADIUS AND IN A STOP FITTING HOLE. EMENTS. ACCOMPLISH INITIAL INS - [SDR CALA2023040401038](https://openairdocs.org/sdr/CALA2023040401038.md): Flange · Airbus A320232 · Apr 4, 2023 · N458UA · No revision named > WHILE PERFORMING EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 RH STGR 22 WEB HORIZONTAL FLANGE RADIUS. SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLISH A PERM - [SDR CALA2023040401039](https://openairdocs.org/sdr/CALA2023040401039.md): Flange · Airbus A320232 · Apr 4, 2023 · N458UA · No revision named > WHILE PERFORMING EA5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 RH STGR 22 WEB HORIZONTAL FLANGE RADIUS. 22 INNER CAP AND WEB HORIZONTAL FLANGE PER THE LATEST REV - [SDR DALA2023030201559](https://openairdocs.org/sdr/DALA2023030201559.md): None · Airbus A320212 · Mar 2, 2023 · N335NW · No revision named > SHIP 3235 DURING VISUAL INSPECTION PREVIOUS REPAIR WAS FOUND (REPAIR ANGLE) ON OF THE FR 68 LH AND STG 22. W/C 5311-01244-01A, SB A320-53-1491 R0, EASA PAD 21-090". CORRECTIVE ACTION: REPAIRED PER PRI - [SDR DALA2023030201560](https://openairdocs.org/sdr/DALA2023030201560.md): None · Airbus A320212 · Mar 1, 2023 · N335NW · No revision named > SHIP 3235 DURING VISUAL INSPECTION PREVIOUS REPAIR WAS FOUND (REPAIR ANGLE) ON OF THE FR 68 RH AND STG 22. W/C 5311-01244-01B, SB A320-53-1491 R0, EASA PAD 21-090". CORRECTIVE ACTION: REPAIRED PER ERA - [SDR DALA2022111707406](https://openairdocs.org/sdr/DALA2022111707406.md): Repair · Airbus A320211 · Nov 17, 2022 · N332NW · No revision named > SHIP 3232 PREVIOUS REPAIR LOCATED IN INSPECTION AREA FOR WC 5311-01244-01B, SB A320-53-1491 R0, EASA PAD 21-090 (RH SIDE). CORRECTIVE ACTION: COMPLIED WITH ERA 603790-14AD. (2499626) - [SDR DALA2022111807432](https://openairdocs.org/sdr/DALA2022111807432.md): Unknown · Airbus A320211 · Nov 17, 2022 · N332NW · No revision named > SHIP 3232 NEED TO COMPLY WITH INSPECTION AREA FOR WC 5311-01244-01A, SB A320-53-1491 R0, EASA PAD 21-090 (LH SIDE). CORRECTIVE ACTION: COMPLIED WITH. (2500127) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT s.sdr_id, s.difficulty_date, s.aircraft_make, s.aircraft_model, s.part_name, string_agg(DISTINCT c.revision, ', ' ORDER BY c.revision) AS revisions, bool_or(c.incorporated_by_reference) AS incorporated_by_reference, bool_or(c.in_regulatory_text) AS in_regulatory_text FROM 'https://openairdocs.org/data/latest/service_document_citation.parquet' c JOIN 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' s ON s.sdr_id = c.record_id WHERE c.document_id = 'airbus/a320-53-1491' AND c.record_type = 'faa_service_difficulty_report' GROUP BY ALL ORDER BY max(c.record_date) DESC ``` This list as a web page: https://openairdocs.org/service-documents/airbus/a320-53-1491/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.