Airbus A320-212
Service difficulty reports · 8,183
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'A320212' ORDER BY difficulty_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 sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'A320212' ORDER BY difficulty_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 DALA2026052703210Web · damagedA.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 A320-53-1491. INSTRUCTIONS TO LIASON IN EARTH FOLDER "DELTA SDR DALA2026052703209Seat Track · corrodedLEVEL 2 CORROSION, A1R116 2-79 (200-336). AFT PASSENGER CABIN AT FR66 Y-765, SEAT TRACK WITH CORROSION. NOTE: FOUND DURING PROCESS OF ORNRC 200- 277. C/A: REPLACED SEAT TRACK P/N: 14N00031-103 FROM FR64 TO FR66 -Y 765 WET AREA, DUE TO CORRODED OUT-LIMITS I/A/WSDR DALA2026052703208Seat Track · corrodedLEVEL 2 CORROSION, AFT PASENGER CABIN AT FR66 Y-1292, SEAT TRACK WITH CORROSION. NOTE: FOUND DURING PROCESS OF ORNRC 200-278. C/A: REPLACED SEAT TRACK P/N: 14N00031-101, COUPLING P/N: D5347210420200, D5347210220200, D5347210220400 AND D5347210220600 FROM FR 64SDR DALA2026052703207Seat Track · corrodedSHIP 3251 DISC: LEVEL 2 CORROSION, AFT PASSENGER CABIN AT FR 65, Y 1292, SEAT TRACK BEAM WITH CORROSION. C/A: REPLACED SEAT TRACK P/N = 14N00031-115, COUPLING P/N: D5347210420400, D5347210420200, FROM FR64 TO FR66 Y 1292 WET AREA DUE TO CORRODED OUT-LIMITS IAWSDR DALA2026052703206Seat Track · corrodedLEVEL 2 CORROSION, AFT PASSENGER CABIN AT FR 65, Y 765, SEAT TRACK BEAM WITH CORROSION. REPLACED SEAT TRACK P/N= 14N00031-117 FROM FR 64 TO FR 66 Y 765 WET AREA DUE TO CORRODED OUT LIMITS I/A/W A320 SRM 51-72-11-911- 001 REV= 157.00 DATED 15-APR-26 REF: NAT DSDR DALA2026052703205Repair · misinstalledAAI FINDING-DURING INSPECTION OF AMDS 5310-4051 FOUND PREVIOUS ACCOMPL ISHED SRM REPAIR INSTALLED AT FR23 BETWEEN STRINGERS 23L AND 24L.DURING INSPECTION OF INTERIOR OF FUSELAGE FOUND REPAIR FASTENERS IMPROPERLY INSTALLED.REPAIR ASSOCIATED WITH LOG PAGE 296344SDR DALA2026052703204Fitting · damagedBURRED MATERIAL (OVALIZATION) ON LOWER LATERAL FITTING LT SIDE RACK 80VU ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT REFER TO AA CARD 2515-01014-02A AD RELEATED. COMPLIED WITH ER/A 633192-14AD REV. ORIGINAL APPROVED DATE 23- MAY-2SDR DALA2026052703215None · noneER/A 589110-14AD REV 'A' ISSUED FOR REPAIR AT FR16RH & DOOR STOP 1. FOLLOW ON ACTION REQUIRED. PERFORM SECTION IV EVERY 11500FC AFTER SECTION III. THIS SUPERSE DES LOG 1704322. ASSOCIATED ER/A 14-589110 ADDED FOR AC 3251. (LP: 1608765) AIRCRAFT WAS GROUNDEDSDR DALA2026052703213Window Frame · damagedDURING M2 AND WHILE INSPECTION PER EM 5311-01236-02, CRACK FOUND IN THE UPPER JUNCTION FASTENER HOLE OF FR4 LATERAL WINDOW FRAME, RHS, AT THE INTERFACE WITH RHS FRONT WINDSHIELD FRAME. PER SECTION DTE OF 633157-14AD THE REPAIR OF SECTION I IS LIMITED TO 26,60SDR DALA2026052703203Fitting · cracked*DTE* DURING M2 AND WHILE ACCOMPLISHING EM 5311-01246-01, BOTH LH/RH CONTINUITY FTGS FOUND CRACKED AND ALSO FRONT WINDSHIELD FRAME HOLE D1 CRACKED. C/A: *DTE* PER SECTION DTE OF 633213-14AD, THE REPAIR OF SECTION I IS LIMITED TO 60,000 TOTAL FC (FROM A/C FIRSTSDR DALA2026052403141Stringer · corrodedLEVEL 2 CORROSION, LOWER FUSELAGE, FWD CARGO COMPARTMENT, AT FR.32+75MM, STR.40LH WITH CORROSION. REPAIRED STRINGER 40L, SECTION BETWEEN FR 31 +215MM AND FR 32 + 305MM IAW SRM 53-21-13-300-018, PARAG 1, PARAG 2A, FIGURE 001. THIS TASK IS CATEGORY B REPAIR ANDSDR DALA2026052703212Percussion Mech · faultedL1 DOOR SLIDE DEPLOYED (PARTIAL DEPLOYMENT). R & R L1 DOOR SLIDE ASSY IAW AMM 52-11. R & R DIAPHRAGM IN PERCUSSION MECHANISM OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER OF THE PASSENGER/CREW DOOR IAW AMM 52-10. ALL RII STEPS ACCOMPLSIHED. (LP: 8881442SDR DALA2026052703211Fitting · damagedDURING M2 AND WHILE ACCOMPLISHING EM 2515-01014-02A, MATERIAL BURR WAS FOUND IN THE LT LWR LATERAL FITTING OF RACK FIN 80VU. PER SECTION II OF ER/A 633192-14AD ACCOMPLISH SECTION II INITIAL INSEPCTION WITHIN 19,500 FC FROM SECTION I (22MAY26). REPEAT SECTION SDR DALA2026053103289None · noneDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D AT FR68RH AND S-22 PER ER/A 634286-14AD. C/A: SECTION I IS LIMITED TO 102900FC FROM SECTION I. ER/A TO BE REVI SED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 14-634286 ADSDR DALA2026053103288None · noneDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D AT FR68RH AND S-22 PER ER/A 634286-14AD. C/A: SECTION I IS LIMITED TO 71500FC FROM SECTION I. ER/A TO BE REVIS ED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE ASSOCIATED ER/A 14-634286 ADDESDR DALA2026053103287None · noneDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR AT FR68R H & S-22 PER ER/A 634286-14AD. ER/A TO BE REVISED PRIOR 32328FC FROM SECTION I (40K FC FROM SB 53-1290 EMBODIMENT) ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 14-634286 ADDED FOR AC 3251. (LP:SDR DALA2026053103286None · noneER/A 634286-14AD ISSUED FOR REPAIR AT FR68RH AT S-22. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II EVERY 16200FC AFTER SECTION I. ASSOCIATED ER/A 14-634286 ADDED FOR AC 3251. (LP: 1605169, AIRCRAFT WAS GROUNDED)SDR DALA2026052703214Window Frame · damagedSHIP 3241 DISC: DTE ERA 633400-14AD REV. ORIGINAL. REPAIR AT FR4 LATERAL WINDOW FRAME REQUIRES DTE FOLLOW UP PRIOR TO 64,502 TFC. C/A: REVISE AND UPDATE ERA 633400-14AD WITH DTE RESULTS PRIOR TO 64,502 TFC. REFERENCE AIRBUS DOSSIER 81769612. ASSOCIATED AA 5311SDR DALA2026052403142Latch · brokenOXYGEN PANEL LATCH BROKEN. OXYGEN PANEL OPENED UP DURING TAKEOFF. C/A: VERIFIED AND SECURED OXYGEN PNL AT L3 DOOR 104 LOC IAW A320 AMM 35-21. (LP: 1602678) AIRCRAFTT WAS GROUNDEDSDR DALA2026052103097Oil System · leakingCREW REPORTS MUSTY HAZE IN CABIN, APU RUNNING PACKS OFF. TURNED ON PACKS, MADE ISSUE WORSE. WOULD NOT DISSAPATE UNTIL PACKS AND APU SHUT DOWN. OPENED APU ACCESS DOORS FOR INSPECTION IAW AMM 52-41. INITIAL VISUAL INSPECTION, FOUND LARGE QTY OF OIL IN APU INLETSDR DALA2026053103309Engine · no discrepancyATO - BIRD STRIKE C/W QRH AND F/COM MAINTENANCE NOTIFIED. NORMAL ENGINE INDICATION DURING ENTIRE EVENT. NO ADVERSE ODORS IN CABIN OR COCKPIT. REMOVED BIRD REMAINS. PERFORMED BIRD STRIKE INSPECTION IAW A320 AMM 05-51. NO DAMAGE NOTED. (LP: 8330410, AIRCRAFT WASDR DALA2026051903077Module · activatedO2 MASKS DROPPED ROW 18 DEF. O2 DEPLOYED WHEN MOVING MASK. PLACED O2 MODULE AT PAX SEAT 18 DEF ON MEL PER 35-21-01A. M PROCEDURE C/W AND SEATS BLOCKED. PLACARD INSTALLED. OK FOR CONTINUED SERVICE. R & R 02 BOTTLE IAW AMM 35-21. M PROCEDURES REVERSED. MEL AND SDR DALA2026051603027Fairing · damagedDIV - DUE TO LOUD POPPING NOISE FROM THE LEFT OVERWING EMERGENCY EXIT DOOR. NO PRESSURIZATION ISSUES REPORTED. UPPER WING TO BODY FAIRING PANEL 191DT WAS FOUND DAMAGED WITH LARGE CHUNKS MISSING, BUT NOT A TOTAL PANEL LOSS. : MAINTENANCE IN PROGRESS. (LP: 86488SDR DALA2026051603024Attach Bracket · corrodedLEVEL 2 CORROSION, LOWER FUSELAGE TOILET SERVICE PANEL SUPPORT ATTACH BRACKETS AND RIVETS CORRODED. REPLACED SUPPORTS P/N: 5348220020000, D5348007321500, D5348027421600, SHIMS (2EA) D5348007320800 AND SPRING (2EA) P/N: D5348007421401 IAW A320 SRM 51-72-11-911SDR DALA2026051603022Floor Support · crackedCRACK (2 E/A) LOCATED ON FLOOR SUPPORT Y254 BTW FR49 TO FR51 IN PASSENGER CABIN. PERFORMED REPAIR INSTRUCTIONS ON FLOOR SUPPORT Y254 BTW FR49 TO FR51 IN PASSENGER CABIN AS PER A320 SRM 53-00-14-300-005 MEASURES OF CRACKS (2 EA) WERE: P1 L= 3.376 IN P2 L= 2.59SDR DALA2026051603026Oxygen Mask · weakCAPTAINS O2 MASK IS VERY WEAK. RESEATED CONNECTOR ON CAPTS O2 MASK. RESTOWED SAME CKS OK. REF A320 AMM 35-13. (LP: 7899412). AIRCRAFT WAS GROUNDEDSDR DALA2026051302980Hydraulic System · lowAT APPX 70KTS "HYD SYS B LO PRESS" ECAM WARN MESSAGE.REJECTTED TAKE OFF. FOUND BLUE SYST ACCUM VERY LOW.SERVICED SAME PER A320 AMM 29-14. PERFORMED OP CHECK OF BLU SYST BUT FOUND THAT ACCUM HAD LEAKED OUT MOST OF ITS PRE CHARGE.DETERMINED ACCUMULATOR BAD.REPLSDR DALA2026051603023Repair · noneINSPECTION ER/A 633568-14 REV ORIGINAL. REPAIR AT REAR FUSELAGE, SKIN AT FR70, BTWN STR31-32RH REQUIRES FOLLOW ON INSPECTIONS PRIOR TO 56,802 TFC AND EVERY 13,000 FC, THEREAFTER. ACCOMPLISH FOLLOW ON INSPECTIONS PER ER/A 633568-14 SECTION II, PRIOR TO 56,802 TSDR DALA2026051102939Stringer · corrodedLEVEL 2 CORRSION, STRINGER 43L BTW FR 56 TO FR 58 IN AFT CARGO COMPARTMENT (SSI 534107). REPLACED STRINGER 43L BTW FR 54 TO FR 60 IN AFT CARGO COMPARTMENT AS PER 320 SRM 51-72-11, A320 SRM 51-42-11 AND DWG D53470345ISSUE: W, RELEASE DATE: 02-NOV-98 AND DWG D5SDR DALA2026051102937Skin · dented: RE-EVALUATE DENT FOR BIRD STRIKE EXTERNAL SKIN LOC. BTW FR1 TO FR 2 AT LEVEL OF -Z339 RH SIDE UPPER FUSELAGE (REFERENCE TO LOG PAGE 8221811). PERFORMED PERMANENT REPAIR AS PER A320 SRM 53-11-11-300-041, LOCATED ON EXTERNAL SKIN BTW FR 1 TO FR 3 AT LEVEL OF SDR DALA2026052403140Aoa · damagedLIGHTENING STRIKE ON ANGLE OF ATTACK (3FP3) BTW FR23 TO FR24 AT STR26L FWD FUSELAGE. REPLACED ANGLE OF ATTACK (3FP3) BTW FR23 TO FR24 AT STR26L FWD FUSELAGE AS PER A320 FAM AMM 34-11-19-000-001-A AND AS PER A320FAM AMM 34-11-19-400-001-A. TEST ARE GOOD. (LP: SDR DALA2026051102938Dampener · failedDOES NOT WORK CORRECTLY DAMPER ON PASSENGER CREW DOOR 832 AT AFT GALLEY AR EA (REFER TO AMDS CARD 5210-7089-LA RII). C/A: REMOVED DAMPER PN: FE174-0031 SN: 29 ON UNSERVICEABLE CONDITION ON PASSENGER CREW DOOR 832 AT AFT GALLEY AREA IAW FAM AMM 52-13-14-000-001SDR DALA2026050802918Brake · stuckHARD VIBRATION ON LANDING AROUND 100 KNOTS AIRCRAFT PULLED TO THE RIGHT ON TAXI IN DID NOT PULL ON TAXI OUT IN ATL. FOUND #3 MAIN BRAKE STICKING. NOT RELEASING PRESSURE. R/R #3 MAIN BRAKE ASSY IAW A320 AMM 32-42. CHECKS GOOD. OK FOR SERVICE. (LP: 8181122). AISDR DALA2026050802917Floor Support · crackedCRACKED INTERCOSTAL FITTING LOCATED INTERNAL STRUCTURE FROM FR11 TO FR1 2 AND Y765 IN COCKPIT. REPLACED INTERCOSTAL FITTING LOCATED INTERNAL STRUCTURE FROM FR11 TO FR12 AND Y765 IN COCKPIT AS PER A320 SRM 51-42-11, SRM 51-72-11 AND DWG D53112787 ISSUE: DOO RELSDR DALA2026050802916Floor Support · crackedCRACKED INTERCOSTAL FITTING LOCATED INTERNAL STRUCTURE FROM FR11 TO FR12 AND Y765 IN COCKPIT. REPLACED INTERCOSTAL FITTING LOCATED INTERNAL STRUCTURE FROM FR11 TO FR12 AND Y765 IN COCKPIT AS PER A320 SRM 51-42-11, SRM51 -72-11 AND DWG D53112787 ISSUE: DOO RELSDR DALA2026050802915Wire · brokenSEAT 21 EMERGENCY LIGHT INOP ROW DEF. DEFERRED MEL 33-50-03A FLOOR PROXIMITY IS INOP. MCC NOTIFIED. NO "M" PROCEDURE REQUIRES. P/N 4NS102-49-42. NIS MSP. FOUND WIRE BROKEN. SPLICED IN NEW WIRE PER ESPM 20-43-11. OPS CHECK GOOD. NO "M" PROCS TO REVERSE. MEL ANSDR DALA2026050802920Pitot Tube · contaminatedF/A AIRSPEED. FOUND BIRD REMAINS IMPAILED ON F/O (#2) PITOT PROBE, REQUIRES BIRD STRIKE INSPECTION. PERFORMED BIRD STRIKE INSPECTION IAW AIRBUS 320 AMM 05-51-14-200 -803-A. NO ADDITIONAL DAMAGES NOTED. PITOT LINE TO ADM IS CLEAN NO REMAINS PAST #2 PITOT. SEE SDR DALA2026050802919Light · brokenSHIP 3267 DISC: CABIN CREW REPORTS THAT FLOOR PROXIMITY EMER. ESCAPE LIGHT IS BROKEN AT SEAT 13DEF. REPLACED HOUSING FOR SEAT 13DEF EMER. ESCAPE LIGHT AS NEEDED, BUT TRIM IS BROKEN UNDER SEAT AT ATTACH POINT. APPLIED TAPE TO HOLD AFT SIDE IN PLACE - LIGHT WORSDR DALA2026050802914Shear Tie · puncturedPUNCTURE SHEAR TIE ON FR 58 AND BTW STR 43R TO STR 44 IN AFT CARGO COMPARTMENT. REPLACED SHEAR TIE ON FR 58 AND BTW STR 43R TO STR 44 IN AFT CARGO COMPARTMENT AS PER A320 SRM 51-72-11, SRM 51-42-11-801, DWG D53470342 ISSUE AE RELEASE DATE 08-JUL-97, DWG D5347SDR DALA2026050502834Floor Support · corrodedCORRODED FLOOR SUPPORT -Y765 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-42-11, DWG D53472816 ISSUE: F AND DWG D53472815, ISSUE: G. MEASURE OF CORROSION WAS L=0.793 IN, W=0.636 IN. D= 0.020 IN. (LP: 1SDR DALA2026050502833Web · crackedCRACKED WEB -Y765 LOCATED BTW FR 8 TO FR 11 IN COCKPIT. REPLACED WEB -Y765 LOCATED BTW FR 8 TO FR 11 IN COCKPIT AS PER A320 SRM 51-42-11,SRM 51-72-11 ,DWG D53113219 RELEASE ISSUE: BOO DWG D53110285 ISSUE: H00 AND DWG D53113378 ISSUE: B00 MEASURE OF CRACK IS:SDR DALA2026050602894Latch · brokenOXYGEN PANEL LATCH BROKEN. COMPARTMENT PANEL WILL NOT STAY CLOSED. THERE IS TAPE HOLDING IT CLOSED. IT IS THE COMPARTMENT PANEL DIRECTLY ABOVE THE AFT GALLEY SINK. DEFERRED FA OXYGEN GENERATOR AT F104 (ABOVE L2 DOOR) IAW MEL 35-21-01E. O2 GENERATOR DOOR SECURSDR DALA2026050302787Floor Support · corrodedLEVEL 2 CORROSION FLOOR BEAM +Y254 LOCATED BTW FR 16 TO FR 21 FWD GALLEY AREA (SSI 531189). REPLACED FLOOR BEAM Y254 AND FASTENERS LOCATED BTW FR12 TO FR 24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11, A320 SRM 51-42-11 AND DWG D53212367 RELEASE DATE 18-MAY-2SDR DALA2026050302786Web · corrodedLEVEL 2 CORROSION WEB LOCATED AT FR 16 LEVEL STR 23R AT FWD GALLEY AREA. REPLACED WEB LOCATED ON FR12 TO FR16 AT LEVEL STR 23R AT FWD GALLEY AREA IAW SRM 51-72-11; A320 SRM 51-42-11, DWG D53114392 ISSUE B00, RELEASE DATE 01-FEB-19, DWG D53112781 ISSUE E00, RESDR DALA2026050102778Receptacle · corrodedCORROSION ON ELECTRICAL RECEPTACLES (7540 VC) (7542 VC) ON RH WING (REFER TO RII AMDS CARD 2751-9202). REPLACED ELECTRICAL RECEPTACLES (7540 VC) (7542 VC) ON RT WING IAW AIRBUS ESPM 20-56-42 PAGEBLOCK 0301 CONFIG 01, AIRBUS ESPM 20-44-11 PAGEBLOCK 0101 CONFIGSDR DALA2026050102760Floor Support · corrodedCORROSION LEVEL 2 FLOOR BEAM +Y765 HARD POINT BTW FR 69 TO FR 70 AT AFT GALLE Y AREA (SSI 534147). REPLACED FLOOR BEAM Y765 AND FASTENERS LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA. AS PER A320 SRM 51-72-11, A320 SRM 51-42-11. (LP 1569278 - AIRCRAFT WAS GSDR DALA2026050102759Floor Support · corrodedCORROSION LEVEL 2 FLOOR BEAM -Y1162.5 LOCATED BTW FR 68 TO FR 69 AFT GALLEY AREA (SSI 534147). REPLACED BEAM -Y 1162.5 LOC. BTW FR 68 TO FR 69 AT AFT GALLEY AREA AND FASTENERS AS PER A320 SRM 51-42-11, A320 SRM 51-72-11. (LP 1569179 - AIRCRAFT WAS GROUNDED)SDR DALA2026050102758Seat Track · corrodedCORROSION LEVEL 2 SEAT TRACK -Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK -Y1292 AND FASTENERS LOC. FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11. (LP 1569168 - AIRCRAFT WAS GROUNDED)SDR DALA2026050102757Floor Support · corrodedCORROSION LEVEL 2 FLOOR BEAM +Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLE Y AREA (SSI 534147). REPLACED FLOOR BEAM Y1162.5 AND FASTENERS LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11. (LP 1569105 - AIRCRAFT WASSDR DALA2026050102756Floor Support · corrodedCORROSION LEVEL 2 FLOOR BEAM +Y1292 TO Y1162.5 BTW FR 66 TO FR 68 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR BEAM Y1292 AND FASTENERS LOC. BTW FR 66 TO FR 68 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11. (LP 1569095 - AIRCRAFT WAS GROU
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