# Service difficulty reports that cite it: Airbus SB A320-53-1263 A list on [Airbus SB A320-53-1263](https://openairdocs.org/service-documents/airbus/a320-53-1263.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 YENA2026042900440](https://openairdocs.org/sdr/YENA2026042900440.md): Pressure Panel · Airbus A320232 · Apr 29, 2026 · N524JB · Revision 05 > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36LH / PRESSURE PANEL ATTACHMENT HOLES / CRACK DAMAGE - PERMANENT REPAIR; REFERENCES: /1/ REO-L25792.IR /2/ AIRBUS TD/ 80 - [SDR YENA2026042900443](https://openairdocs.org/sdr/YENA2026042900443.md): Pressure Panel · Airbus A320232 · Apr 29, 2026 · N524JB · Revision 05 > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36RH / PRESSURE PANEL HOLE #7 / CRACK DAMAGE - PERMANENT REPAIR; REFERENCES: /1/ REO-L25791.IR /2/ AIRBUS RDAF 81742124/0 - [SDR YENA2026020400114](https://openairdocs.org/sdr/YENA2026020400114.md): Pressure Deck · Airbus A320232 · Feb 2, 2026 · N587JB · Revision 05 > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 RHS / ATTACHMENT HOLES / CRACKS – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0085-25 REV. 0 (COVER + PARTS 1-8 - [SDR YENA2026012100049](https://openairdocs.org/sdr/YENA2026012100049.md): Pressure Panel · Airbus A321271NX · Jan 18, 2026 · N2047J · No revision named > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 36 LH & RH SIDES / PRESSURE PANEL / CRACK DAMAGES AT MULTIPLE HOLES – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0071-25 REV. 0 (COVER - [SDR YENA2026012100052](https://openairdocs.org/sdr/YENA2026012100052.md): Pressure Deck · Airbus A321271NX · Jan 18, 2026 · N2047J · Revision 05 > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 RHS / ATTACHMENT HOLES / CRACKS – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0085-25 REV. 0 (COVER + PARTS 1-8 - [SDR YENA2025123001280](https://openairdocs.org/sdr/YENA2025123001280.md): Pressure Panel · Airbus A320232 · Dec 27, 2025 · N583JB · No revision named > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 36 LH & RH SIDES / PRESSURE PANEL / CRACK DAMAGES AT MULTIPLE HOLES – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0071-25 REV. 0 (COVER - [SDR YENA2025123001281](https://openairdocs.org/sdr/YENA2025123001281.md): Pressure Panel · Airbus A320232 · Dec 27, 2025 · N583JB · No revision named > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 36 LH & RH SIDES / PRESSURE PANEL / CRACK DAMAGES AT MULTIPLE HOLES – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0071-25 REV. 0 (COVER - [SDR YENA2023112901465](https://openairdocs.org/sdr/YENA2023112901465.md): Pressure Panel · Airbus A320232 · Nov 26, 2023 · N552JB · No revision named > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36 / LH & RH SIDES / PRESSURE PANEL ATTACHMENT HOLES / SB A320-53-1263 ACCOMPLISHMENT AND CRACK DAMAGE. PERMANENT REPAIR. - [SDR YENA2023112901469](https://openairdocs.org/sdr/YENA2023112901469.md): Unknown · Airbus A320232 · Nov 26, 2023 · N552JB · Revision 05 > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 RH -Y1523 PLUS 7.045 INCHES ON UPPER SURFACE OF THE PRESSURE DECK, DIRECTION O F CRACK IS: 2 O CLOCK); REF AEROM - [SDR YENA2023112901470](https://openairdocs.org/sdr/YENA2023112901470.md): Unknown · Airbus A320232 · Nov 26, 2023 · N552JB · Revision 05 > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 RH -Y1523 PLUS 7.925 INCHES ON UPPER SURFACE OF THE PRESSURE DECK, DIRECTION O F CRACK IS: 6 O CLOCK); REF AEROM - [SDR YENA2023112901471](https://openairdocs.org/sdr/YENA2023112901471.md): Unknown · Airbus A320232 · Nov 26, 2023 · N552JB · Revision 05 > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 RH -Y1523 PLUS 8.880 INCHES ON UPPER SURFACE OF THE PRESSURE DECK, DIRECTION O F CRACK IS: 6 O CLOCK); REF AERO - [SDR YENA2023112901472](https://openairdocs.org/sdr/YENA2023112901472.md): Unknown · Airbus A320232 · Nov 26, 2023 · N552JB · Revision 05 > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 LH Y1523 PLUS 8.883 INCHES ON UPPER SURFACE OF THE PRESSURE DECK, DIRECTION OF CRACK IS: 4 O CLOCK); REF AEROMAN - [SDR YENA2023112901473](https://openairdocs.org/sdr/YENA2023112901473.md): Unknown · Airbus A320232 · Nov 26, 2023 · N552JB · Revision 05 > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 LH Y1523 PLUS 7.044 INCHES ON UPPER SURFACE OF THE PRESSURE DECK, DIRECTION OF CRACK IS: 2 O CLOCK); REF AEROMAN - [SDR YENA2023112901474](https://openairdocs.org/sdr/YENA2023112901474.md): Unknown · Airbus A320232 · Nov 26, 2023 · N552JB · Revision 05 > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 LH, Y1523 PLUS 7.924 INCHES 2 EA ON UPPER SURFACE OF THE PRESSURE DECK CRACK INDICATION IS 7 AND 5 O CLOCK); REF - [SDR YENA2022070700658](https://openairdocs.org/sdr/YENA2022070700658.md): None · Airbus A320232 · Jan 23, 2022 · N505JB · Revision 03 > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 PRESSURE DECK PANEL ON OPEN FASTENER HOLE 2 INCH OUTBOARD Y1292, CRACK DIRECTION IS 6 OCLOCK IN FWD CARGO COMPA RTMENT (1 EA); REF AEROMAN N/R 20 - [SDR DALA2021020100599](https://openairdocs.org/sdr/DALA2021020100599.md): Frame · Airbus A320212 · Jan 31, 2021 · N372NW · No revision named > SHIP 3272 CRACK FRAME 36 THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR 35LT AND FR 36LT. CORRECTIVE ACTION: MODIFIED FRAME PER DELTA WORK CARD 5311-01 - [SDR YENA2021010400006](https://openairdocs.org/sdr/YENA2021010400006.md): Not Reported · Airbus A320232 · Dec 29, 2020 · N503JB · No revision named > DURING HEAVY MAINTENANCE, CRACKS FOUND DURING INSPECTION SB A320-53-1254. REPAIRED PER SB A320-53-1263 & FLIGHTSTAR EA 20046 & RDAS 80854592/003/2020. - [SDR DALA2020033102083](https://openairdocs.org/sdr/DALA2020033102083.md): Pressure Plate · Airbus A320212 · Mar 24, 2020 · N366NW · No revision named > CRACK INDICATION ON OPEN FASTENER HOLE AT Y 1292 AND 0.585 TO INB THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH, REPAIRD CRACK AS PER - [SDR DALA2020011700376](https://openairdocs.org/sdr/DALA2020011700376.md): Pressure Panel · Airbus A320212 · Jan 15, 2020 · N365NW · No revision named > NR 448:FR35-36 RT PRESSURE PANEL- A CRACK THAT DOES NOT EXCEED THE REPAIR AREA WAS FOUND AT HOLE 6. MODIFY IN ACCORDANCE WITH WORK CARD 5311-01171-4B PRIOR TO FURTHER FLIGHT. AA5311- 01171, SB A320-53 - [SDR DALA2019120637118](https://openairdocs.org/sdr/DALA2019120637118.md): Frame · Airbus A320211 · Dec 2, 2019 · N331NW · No revision named > CRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL AREA AND 15.250 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK. (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND - [SDR DALA2019071504202](https://openairdocs.org/sdr/DALA2019071504202.md): Pressure Panel · Airbus A320212 · Jul 13, 2019 · N348NW · No revision named > A CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BETWEEN FR35RH AND FR36RH. HOLE # 4. -M- AA5311-01171 SB A320-53-1263 AD -2018-06-04. REPAIRED PER PRI 579495-14AD - [SDR DALA2019060423392](https://openairdocs.org/sdr/DALA2019060423392.md): Plate · Airbus A320211 · Jun 1, 2019 · N317US · No revision named > A CRACK(S) THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35 LH AND FR36 LH, MODIFICATION WAS ACCOMPLI- SHED IN ACCORDANCE WITH WORK CARD 5311-01171-04A - [SDR DALA2019042972680](https://openairdocs.org/sdr/DALA2019042972680.md): Pressure Deck · Airbus A320212 · Apr 26, 2019 · N342NW · No revision named > CRACK PRESSURE PANEL AND LONGITUDINAL BEAM THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH IN HOLE 7, MODIFY IN ACCORDANCE WITH WORK CARD - [SDR DALA2019042972682](https://openairdocs.org/sdr/DALA2019042972682.md): Pressure Deck · Airbus A320212 · Apr 26, 2019 · N342NW · No revision named > CRACK PRESSURE PANEL AND LONGITUDINAL BEAM CRACK THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH IN HOLE 6, MODIFY IN ACCORDANCE WITH WOR - [SDR DALA2019042972707](https://openairdocs.org/sdr/DALA2019042972707.md): Pressure Plate · Airbus A320212 · Apr 26, 2019 · N340NW · No revision named > CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESS URE PLATE PANEL BETWEEN FR35RH AND FR36RH, REPAIR AREA OF PRESSURE PLATE LOC BETWEEN FR35RH AND FR36RH MODIFICATION WAS ACCOMPLISHE ## 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/a320-53-1263' 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/a320-53-1263/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.