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 DALA2025123009490Dampener · no testNO TEST FOR DAMPER OF PAX DOOR 832. REF AMDS 5210-7089-LA. REPLACED DOOR DAMPER OF PASSENGER CREW DOOR 832 IAW FAM AMM 52-13-14-000-001-A AND AMM 52-13-14-400-001-A.SDR DALA2025122809428Light · damagedEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. LIGHTING PIECE HAS BROKEN OFF FROM SEAT AN IS ON THE FLOOR. REATTACHED LIGHT ASSY & OPS CHECK GOOD. A/C OK FOR SERVICE REF A320AMM 33-51 . (LP: 1372007)SDR DALA2025122809427Dampener · failedDONT PASS TEST DOOR DAMPER ON PASSENGER CREW DOOR 841 (REFFER TO AMDS CARD 5210-7089-RF). REMOVED DOOR DAMPER ON PASSENGER CREW DOOR 841 P/N FE174-0011 S/ N 1526 ON UNSERVICEABLE CONDITION AS PER A320 FAM AMM 52-11-14- 000-001-A JOB IN PROGRESS. REPLACED DAMSDR DALA2025122209274Oxygen Mask · unwanted deployOXYGEN PANEL MASK DEPLOYED. WHILE SITTING DURING TURBULENCE, THE MASKS SUDDENLY DEPLOYED. WAS ABLE TO PUT IT BACK IN BUT IT SHOULD BE CHECKED OUT JUST IN CASE. INSPECTED AND REINSTALLED O2 CONTAINER AT 2L IAW AMM 35-21. OK FOR SERVICE. (LP: 1359790)SDR DALA2025122209272Generator · failedAFTER PUSHBACK AND ENGINE START FA'S IN AFT GALLEY REPORTED A STRONG BURNING ELECTRICAL ODOR FROM THE AFT CENTER LAV AREA. FLIGHT RETURNED TO THE GATE AND DEPLANED. LAVATORY WASTE SYSTEMS VACUUM GENERATOR. C/W MSI PREVENTION PROGRAM STEPS A - G FOUND VACUUM GSDR DALA2025122209271Slide · no testDONT PASS OPERATIONAL TEST SLIDE RAFT PASSENGER CREW DOOR 841 AT FWD G ALLEY AREA (REFER TO AMDS CARD 5210-7089-RF STEP 36.) PERFORMED TROUBLESHOOTING PROCEDURE AS PER 320 FAM TSM 33-51-00- 810-807-A AND PERFORMED CLEANING OF CONNECTOR 2870VC-A AS PERA320 FAMSDR DALA2025122209276Bottle · no testDID NOT PASS TEST DOOR DAMPER OF PASSENGER CREW DOOR 831. REMOVED PASSENGER CREW DOOR DAMPER 831 ON UNSERVICEABLE CONDITION IAW FAM AMM 52-11-14- 000-001-A, STEP 3.B THRU 4.A. REPLACED THE DOOR DAMPER IAW FAM AMM 52-11-14-000-001-A, AND FAM AMM 52-11-14-400SDR DALA2025121709178Oxygen Box · faultedAFT LT LAV O2 MOD DOOR WILL NOT CLOSE LAVATORY OXYGEN MODULE. AFT LAV (LT) O2 MASK DROPPED ON LANDING IN DTW. C/A: FWD TO MCC , MEL 35-21-02 , "M" PROCEDURE CW , DISPATCH APPROVED , PLACARD INSTALLED. REMOVED AND REPLACED 203 LAV O2 CONTAINER ASSY PER AMM 35-SDR DALA2025120808924Filter · dirtyAPPROXIMATELY 30 SECONDS AFTER CLEARING THE RUNWAY, SMOKE AND HAZE ENTERED THE COCKPIT. SMOKE WAS REPORTED BY THE FAS IN THE CABIN (FAS SAY IT WAS MOSTLY REAR CABIN.) PILOTS USED OXYGEN MASKS. SMOKE DISAPETED W/IN 2 MIN. INSPECTED ENGS FOUND EXCESSIVE SAND ANSDR DALA2025120908980Oxygen Mask · no testCAPT O2 MASK DOES NOT TEST PROPERLY ( LEAK TEST FUNCTION). DFR PER MEL 25- 011-06C O2 BOX WILL NOT TEST. PLACARD INSTRALLED CONTACTED MCC OK FOR SVC. SWAPPED CAPT. O2 MASK WITH OBSERVER SEAT O2 MASK, OK TO CONT. ON DEFERRAL. REINSTALLED OBSVRS O2 MASK TO ORIGSDR DALA2025120408848Light · detachedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED AND INOPERATIVE. HANGING DOWN, WIRE STILL ATTACHED. RESECURED EMERGENCY SEAT MOUNTED LIGHT AS REQUIRED. OK FOR SVC SEAT ROW 30D. (LP: 1333983)SDR DALA2025120408849Unknown · odorWHEN WE GOT TO THE JET, THERE WAS A STRONG SMELL SIMILAR RO AN AUTO BURNING CLUTCH SMELL THROUGHOUT THE COCKPIT AND CABIN, THE BATTERIES WERE OFF, APU OFF, EXTERNAL AIR AND PWR ON. STARTED APU AND APU BLEED ON AND IT DISSIPATED. INFO NOTED AND RECORDED. (LP: SDR DALA2025120208778Filter · odorAIRCRAFT FILLED WITH SMOKE AS REVERSER STOWED AND UPON EXITING RUNWAY. NO BURNING SMELL OBSERVED AND SMOKE DISPLAYED UPON SHUTDOWN. INSPECTED ENGINES. FOUND EXCESSIVE DIRT RESIDUE ON BLOCKER DOORS AND IN INLET. RUNWAYS AND TAXIWAY HAVE HEAVY SAND RESIDUE AND SDR DALA2025121609150Tail Cone · missingON WALK AROUND FOUND APU TAILCONE MISSING. PERFORMED SPLICE REPAIR ON WIRE 3348-7875 FROM 18LV IN THE FORWARD TAILCONE AREA. ALSO ROUTED HARNESS & SECURED GROUNDS, IAW ESPM 2347890-53-02-0201. REMOVED TAILCONE IAW AMM 53-58-11. REMOVED APU IAW AMM 49-11-11. SDR DALA2025113008737Fan · failedAFTER STARTING APU AND TURNING ON PACK, AFTER 3 MINUTES THERE WAS AN ACRID BURNING SMELL THAT EACH CREW MENTIONED OF OWN WITHOUT ASKING. SMELL BETTER AFTER PACKS TURNED OFF. ALSO MENTIONED BY PAX. C/W AMDS 0550-2002. FOUND CABIN RECIR FANS AT FAULT. SMELL BURSDR DALA2025113008734Frame · crackedCRACK INDICATION FOUND ON INNER CAP FR 68 LH SIDE, CRACK LENGHT = 1.0 INCH APPROX. REQUESTING REPAIR DISPOSITION ADITIONAL EGINEERING DOCUME NTATION IS REQUIRED AND REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER F LIGHT REFER TO EM 5311-01244 AND SB A320-531491.SDR DALA2025113008733Frame · crackedCRACK INDICATION FOUND ON INNER CAP FR 68 RH SIDE AREA, CRACK LENGHT: 1.5 INCH, REQUESTING REPAIR DISPOSITION ADITIONAL EGINEERING DOCUMENTA TION IS REQUIRED AND REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIG HT REFER TO EM 5311-01244 AND SB A320-531491. CSDR DALA2025113008739Structure · damagedINSPECTION ERA 630590-14AD REV ORIGINAL. REPAIR PART AND HORIZONTAL FLANGES FILLET RADII REQUIRE FOLLOW ON INSPECTIONS PRIOR TO 60,130 TFC AND EVERY 16,200 FC, THEREAFTER. ACCOMPLISH FOLLOW ON INSPECTIONS PER ERA 630590-14AD SECTION II PRIOR TO 60,130 TFC AND SDR DALA2025113008738Frame · damagedDTE ERA 630590-14AD REV ORIGINAL. REPAIR AT FR68 & STR22R, FRAME WEB HORIZONTAL FLANGE IS TIME LIMITED REQUIRING DTE FOLLOW UP PRIOR TO 76,799 TFC. REVISE AND UPDATE ERA 630590-14AD WITH DTE RESULTS PRIOR TO 76,799 TFC. REFERENCE AIRBUS DOSSIER 81694973. ASSOSDR DALA2025112508597Light · faultedEMERGENCY EXIT SIGNS INOPERATIVE, INTERMITTENTLY FLASH ON AND OFF ON BOTH DOORS IN THE AFT OF THE AIRCRAFT. PERFORMED OPS TEST OF EMERGENCY LIGHTS PER A320 AMM 33-51. NO 30 DAY HISTORY. OK FOR SERVICE. (LP: 1317100)SDR DALA2025112508595Light · detachedEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:32D / MYCABIN TEXT: FRC33520132D EMERGENGY LIGHT IS HANGING BY WIRE / INTERIOR. C/A: R&R 32D FLOOR EMERGENCY LIGHT BRACKET PER A320 CMM 25-31-51. OPS CK OK. REMOVED PLACARDS. NO 'M' PROC REQ. (LP: 131SDR DALA2025112508586Fitting · damagedLH UPPER ACTUATOR FITTING HAS TWO FASTENERS PULLED THROUGH FITTING. REPAIRED PER PRI 604353-14AD REV. 0, 1, 2, 3, 4, 5 AND 6 AND COMPLIED WITH ER/A 604353-14AD REV. B SECTION III. (LP: 1316696)SDR DALA2025112508583Drain Mast · missingNR 1 ENG DRAIN MAST MISSING. INSTALLED DRAIN AT AFT END OF DRAIN MAST IAW AMM 71-73, A/C OK FOR SVC. (LP: 8108788)SDR DALA2025112508582Bottle · low pressureL1 DOOR EMERGENCY OPERATING CYLINDER PRESS LOW. SERVICED L1 DOOR EMERGENCY OPERATING CYLINDER PER A320 AMM 52-10. NO LEAKS NOTED. (LP: 7661409)SDR DALA2025112508584Door · bindingECAM LG DOOR NOT LOCKED (NOSE GEAR) DURING LANDING GEAR EXTENSION. GO-AROUND PERFORMED, MSG APPEARED AGAIN 2ND EXTENSION BUT CLEARED AFTER ABOUT 10 SEC. C/A: PFR SHOWS N LG DOORS NOT CLOSED WITH 30GA & 31GA FAULTING. OPERATED DOORS WITH GEAR HANDLE AND NOTED LSDR DALA2025112508585Proximity Sensor · faultedAFTER LOWERING LANDING GEAR - LG DOORS NOT CLOSED ON ECAM. ALL GEAR SHOWED DOWN & LOCKED. NOSE GEAR DOOR AMBER ON WHEEL PAGE. FAULT CLEARED AFTER WE INITIATED GO-AROUND. NO GO ODI PROCEDURES FOLLOWED PER A320 ATA 3234. POST FLT RPT ONLY SHOW POST FLT FAULTS PSDR DALA2025112008497Light · damagedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP. ATTACHED WOTH 2-SIDED TAPE AND NO LONGER MOUNTED TO SEAT. NEEDS TO BE REMOUNTED. SECURED AS REQUIRED. (LP: 1311690)SDR DALA2025112008498Radome · damagedSHIP 3237 DISC: BIRD STRIKE ON LOWER NOSE CONE ON CA SIDE. ABOUT 7500' ON CLIMB OUT FROM DENVER. NO ADVERSE CONDITIONS EXPERIENCED. C/A: INSPECTED A/C PER A320 AMM 05-51-14-200-803. DAMAGE NOTED ON RADOME. NO FURTHER DAMAGE ON A/C (WIP 184199) R&R RADOME PER ASDR DALA2025112008496Anchor · damagedREMOVED 3 NUTS FROM LT MLG RETRACT ACTUATOR MOUNT REMOVED 2 REMAINDER NUTS FROM RETRACT ACTUATOR MOUNT PLATE. REMOVED AND REPLACED LT MLG JACK ANCHORAGE ASSY PER ER/A 630497- 14, REV ORIG PER SECTION I PERMANENT REPAIR INSTRUCTIONS; REFER TO L.P 1309462. (LP:SDR DALA2025112008495Not Reported · damagedWORKING PRI ER/A 630497 REV "O". ACCOMPLISHED ALL REPAIR INSTRUCTIONS PRE PRI ER/A 630497 REV "O" PRI REVISIONS 1-4. FINAL ER/A 630497 REV. ORIGINAL SECTION I: PERMANENT REPAIR INSTRUCTIONS MATCH. (LP: 1309501)SDR DALA2025112008494None · noneER/A 543344-14 REV A REQUIRES NEW INSPECTIONS. LOGPAGE 2378650 WILL BE CLOSED AND NO LONGER WILL TRACK THE REPAIR PER ER/A 543344-14 REV ORIGINAL. THIS LOG WILL TRACK THE REQUIREMENTS PER ER/A 543344-14 REV A. NEW INSPECTIONS REQUIRED PER ERA 543344-14 REV A SDR DALA2025112008493Not Reported · noneER/A 543343-14 REV A REQUIRES NEW INSPECTIONS. NEW INSPECTIONS REQUIRED PER ERA 543343-14 REV A STARTING AT 39,000 TFC AND EVERY 1,600 FC THEREAFTER. LOGPAGE 2378641 WILL BE CLOSED AND NO LONGER WILL TRACK THE REPAIR PER ER/A 543343-14 REV ORIGINAL. THIS LOG SDR DALA2025112008492Threshold · noneNEW INSPECTION THRESHOLD REQUIRED PER ER/A 563946-14 REV B. THIS LOG PAGE SUPERSEDES LOG PAGE 0565626 PER ER/A 563946-14 REV B. DTE STAGE 2 AND 3 REQUIRED. ACCOMPLISH INSPECTION PER ER/A 563946-14 REV B PRIOR TO SIXTY-FOUR THOUSAND TWO HUNDRED (64,200 ) TOTALSDR DALA2025111808414Hinge · corrodedFOUND CORROSION ON LT MLG ACTUATING CYLINDER INBOARD HINGE. COMPLIED WITH ER/A 630497- 14. (1309462).SDR DALA2025111908442Outflow Valve · faultedATO - BELOW 80KTS DUE TO A VENT SKIN VALVE FAULT. DEFERRED THE AVIONICS COOLING SKIN AIR OUTLET VALVE PER MEL AND CONTINUED. LATER REPLACED THE SKIN AIR OUTLET VALVE. (LP: 8022576)SDR DALA2025120308812Retainer · corrodedCORROSION ON LOWER TROLLEY RETAINER BLOCKS ON GALLEY G1 AT FWD GALLEY AREA. COMPLIED WITH ERA 630077-14 REV. ORIGINAL APPROVED DATE: 07-NOV- 25 MATCHES WITH ALL STEPS ON ERA 630077-14 REV. ORIGINAL, PRI REV0 AND PRI REV.1, IT HAS BEEN VALIDATED, PERFORMED REPSDR DALA2025111308311Thrust Reverser · faultedATO - BETWEEN 70-75 KTS DUE TO ENG 2 REVERSE UNLOCKED ECAM WARNING. RIGHT THRUST REVERSER PLACED ON MEL. OK TO CONTINUE. R & R ROLLERS ON LOWER AND UPPER BLOCKER DOORS LATCH ASSEMBLY REF AMM 78-32. ROLLER MOVEMENT FREE. THRUST REVERSERS OPS TESTED GOOD IAW ASDR DALA2025111108224Oxygen Mask · unwanted deployOXYGEN MASKS AT 14DEF DEPLOYED, ONE MASK. LANYARD WAS PULLED AND OXYGEN WAS FLOWING. OXYGEN GEN DID NOT ACTIVATE, VERIFIED BY TEMP & ARMING PIN STILL INSTALLED. RESTOWED MASKS AT 14DEF IAW AMM 35-21. OK FOR SVC. (LP: 7997714)SDR DALA2025111108223Radome · delaminatedDURING BIRDSTRIKE INSPECTION FOUD DELAMINATION & BUBBLE ON THE INSIDE OF RADOME NOSE. REMOVED NOSE RADOME IAW AMM 53-15. INSTALLED RADOME IAW AMM 53-15-11. OK FOR SVC. (LP: 7726841)SDR DALA2025111108222Antenna · corrodedSHIP 3272 DISC: DURING BIRD STRIKE INSPECTION, FOUND CORROSION DMG ON WEATHER RADAR ANTENNA. R & R WEATHER RADAR ANTENNA ASSEMBLY PER AMM 34-41. OPS CHKD. PERFORMED SYS TEST PER A320 AMM 34-41-00-730 -001-A. OPS CHECK GOOD. NO FAULTS, ACFT OK FOR SVC. (LP: 77SDR DALA2025111308312Elec Connector · corrodedCORROSION ON ELECTRICAL CONECTOR W311 OF VIASAT ANTENNA LOC ON UPPER FUSELAGE. REMOVED VIASAT ANTENNA GM40 P/N: 1196634-004 S/N: 50204- GM4042641 ON UNSERVICEABLE CONDITION AS PER A320 FAM AMM 44-31- 02-000-801C2 STEP 2.C(1)AND STEP 3.A(4)(6)(8) DUE TO CORROSSDR DALA2025111108221Skin · corrodedCORROSION BOTTON SKIN LOWER SURFACE ON PYLON REINFORCING PLATE BTW RIB 7 AND RIB 8 AT STR 6, LT WING. COMPLIED WITH ER/A 630034-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON ER/A 630034-14AD PRI REV.0 AND ER/A 630034-14AD PRI REV .1IT HAS BEEN VALIDATED. PERFOSDR DALA2025110908153Safety Valve · faultedLANDING GEAR FAILED TO EXTEND ON THE FIRST ATTEMPT CYCLED THE GEAR HANDLE PER THE ECAM. IT TOOK 90-120 SECONDS TO START THE EXTENSION. THE PREVIOUS LANDING GEAR EXTENSION IN BDL WAS NORMAL . C/A: T/S PER A320 TSM 32-31-00-810-836-A, NO FAULTS IN EITHER LGCIU 1SDR DALA2025110908150None · noneDTE ERA 630034-14AD REVISION ORIGINAL. REPAIR PER ERA 630034- 14AD SECTION I IS TIME LIMITED REQUIRING DTE FOLLOW UP PRIOR TO 97,447 TFC OR 198,940 TFH, WHICHEVER COMES FIRST. REVISE AND UPDATE ERA 630034-14AD WITH DTE RESULTS PRIOR TO 97,447 TFC OR 198,940 TSDR DALA2025110908152Unknown · odorFLT ATTENDANTS REPORTED A DIRTY SOCK SMELL COMING FROM THE CABIN VENTS WITH APU BLEED ON. ACCOMPLISHED ON LOG #1291912. (LP: 7845300)SDR DALA2025110908151Elec Connector · contaminatedON ARRIVAL WHEN THE LANDING GEAR HANDLE WAS SELECTED DOWN. THE GEAR DID NOT EXTENT. AFTER 20 SECONDS THE GEAR HANDLE WAS CYCLED FROM DOWN TO UP, TO DOWN. AFTER 20 SECONDS THE GEAR EXTENDED NORMALLY. T/S IAW TSM 32-31-00-810-808-A. NO PROX SENSOR FAULTS ON PFR.SDR DALA2025110608081Ecu · faultedUNCOMMAND ENGINE SHUT DOWN, RESET STARTING IAW MC ENG N1 HUNG. REMOVED AND REPLACED NR 1 ENG ECU IAW AMM 73-21, FADEC BITE TEST AND ENG RUN N1 READ 21%, OPS CHECKED GOOD, OK FOR SERVICE. (LP: 7991956)SDR DALA2025110608080Door Frame · damagedDURING B3 CHECK AND WHILE ACCOMPLISHING EM 5311-01246-03B ON FR 16R, ALL EFFECTIVE HOLES FOUND IN FR 16R FOUND WITH DIAMETERS BEYOND STARTING HOLE DIAMETER, DUE TO FR 16R REPLACEMENT PER SECTION I OF 558682-14. DEFERRED LOG.SDR DALA2025110608079Door Frame · damagedOVERSIZE DIAMETER HOLES JOGGLE AREA FR16 RT, AT DOOR STOP FITTING 7. HOLES H1: 0.2641 H2: 0.3305 H3: 0.2663 H4: 0.3263 H5: 0.2662 H 6: 0.3339 H7: 0.2039 H8: 0.2634 HOLE A: 0.2073 HOLE B: 0.2634 HOLE C: 0.2264 HOLE D:0.2636. COMPLIED WITH ER/A 558682-14AD REV.SDR DALA2025110608078Probe · faultedATO - AT APPROXIMATELY 20 KTS DUE TO FUEL L OUTER TK LO TEMP ECAM WARNING. FLIGHT CREW MEL PLACARDED AND CONTINUED. T/S PER TSM A319 28-42-00-810-816-A. PERFORMED POWER ON BITE EQIS. TESTS PASSED. NO FAULTS ON PFR & LAST LEG. PREVIOUS LEG REPORT ON CH 1 AND
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