Airbus SB A320-53-1263
Service difficulty reports that cite it · 25
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.
Query with SQL
duckdb -csv -c "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"Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR YENA2026042900440Pressure Panel · Airbus A320232DURING 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/ 80SDR YENA2026042900443Pressure Panel · Airbus A320232DURING 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 81742124/0SDR YENA2026020400114Pressure Deck · Airbus A320232DURING 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 1-8SDR YENA2026012100049Pressure Panel · Airbus A321271NXDURING 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 (COVERSDR YENA2026012100052Pressure Deck · Airbus A321271NXDURING 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 1-8SDR YENA2025123001280Pressure Panel · Airbus A320232DURING 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 (COVERSDR YENA2025123001281Pressure Panel · Airbus A320232DURING 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 (COVERSDR YENA2023112901465Pressure Panel · Airbus A320232DURING 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 YENA2023112901469Unknown · Airbus A320232DURING 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 AEROMSDR YENA2023112901470Unknown · Airbus A320232DURING 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 AEROMSDR YENA2023112901471Unknown · Airbus A320232DURING 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 AEROSDR YENA2023112901472Unknown · Airbus A320232DURING 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 AEROMANSDR YENA2023112901473Unknown · Airbus A320232DURING 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 AEROMANSDR YENA2023112901474Unknown · Airbus A320232DURING 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 ); REFSDR YENA2022070700658None · Airbus A320232DURING 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 20SDR DALA2021020100599Frame · Airbus A320212SHIP 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 5311-01SDR YENA2021010400006Not Reported · Airbus A320232DURING HEAVY MAINTENANCE, CRACKS FOUND DURING INSPECTION SB A320-53-1254. REPAIRED PER SB A320-53-1263 & FLIGHTSTAR EA 20046 & RDAS 80854592/003/2020.SDR DALA2020033102083Pressure Plate · Airbus A320212CRACK 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 DALA2020011700376Pressure Panel · Airbus A320212NR 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 A320-53SDR DALA2019120637118Frame · Airbus A320211CRACK 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 FOUNDSDR DALA2019071504202Pressure Panel · Airbus A320212A 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 579495-14ADSDR DALA2019060423392Plate · Airbus A320211A 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 5311-01171-04ASDR DALA2019042972680Pressure Deck · Airbus A320212CRACK 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 CARDSDR DALA2019042972682Pressure Deck · Airbus A320212CRACK 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 WORSDR DALA2019042972707Pressure Plate · Airbus A320212CRACK 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
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