Airbus A320-211

Service difficulty reports · 5,271

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 = 'A320211'
  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.

SDR DALA1166693231Frame · damagedFRAME 1 CHORD ANGLE DAMAGED BY BIRD STRIKE. CUT OUT DAMAGED SECTION OF FRAME 1 CHORD MPN D5311085201. CUT NEW SECTION OF CHORD, FABRICATED .080" AND .100" 2024-0 REPAIR ANGLES. INSTALLED NEW CHORD SECTION AND REPAIR.Nov 16, 2011 · N331NW · Airbus A320211 · Fuselage Main, FrameSDR DALA1166743231Post · damagedDURING NON ROUTINE CHECK, VERTICAL POST Y-675 LOWER WEB AT FRAME 1 DAMAGED DUE TO BIRD STRIKE. FABTRICATED LOWER WEB FROM 2024-0,.071" AS PER AIRBUS DWG ASNA 3042-8644. INSTALLED AS PER DWG BOD53110066. SEALED AND PAINTED.Nov 14, 2011 · N331NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1166233231Stiffener · damagedHORIZONTAL STIFFENER AT FRAME 1 AND VERTICAL STATION Z-1159 DAMAGED DUE TO BIRD STRIKE. REPLACED STIFFENER MPN D53113100214 PER MPR D5311310021213 AND DRAWING D53113140.Nov 14, 2011 · N331NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1166223231Stiffener · damagedHORIZONTAL STIFFENER AT FRAME 1 AND VERTICAL STATION Z-1329 DAMAGED DUE TO BIRD STRIKE. REPLACED STIFFENER MPN D53113100214 PER SRM 53-11-16 AND DRAWING D53113140.Nov 14, 2011 · N331NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1166703231Skin · damagedDURING NON ROUTINE CHECK, FWD FUSELAGE LWR SKIN BENT FROM Y-330 TO 22.50 INCHES RT OF CENTER AT FR 1 MARKED IN RED. TRIMMED OUT DAMAGED AREA 3" BY 12". FABRICATED AND INSTALLED.09 0" 2024-T3 DOUBLER PER SRM 53-11-11 FIG 221.Nov 13, 2011 · N331NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA1163773231Bulkhead · crackedON DEPARTURE FROM MSP A/C HAD MULTIPLE BIRD STRIKES IN RADOME AREA. RESULTING IN DAMAGE TO RADOME AND FRAME 1 BULKHEAD WEB. REPAIR IN PROGRESS PER ER/A 497863-14.Nov 10, 2011 · N331NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA1163803231Vertical Support · crackedON DEPARTURE FROM MSP, A/C SUSTAINED DAMAGE IN NOSE AREA BY SEVERAL BIRD STRIKES. FRAME 1 BULKHEAD VERT SUPPORT AT STA Y-675 WAS DEFORMED AND CRACKED. REPAIRS IN PROGRESS PER ER/A497784-14. N/R #44.Nov 10, 2011 · N331NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA1163793231Vertical Support · crackedON DEPARTURE FROM MSP, A/C SUSTAINED DAMAGE TO NOSE AREA FROM SEVERAL BIRD STRIKES. FRAME 1 BULKHEAD VERTICAL SUPPORT AT STA Y-330 DEFORMED AND CRACKED. REPAIR IN PROGRESS PER ER/A 497783-14. N/R #45.Nov 10, 2011 · N331NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA1163783231Angle · damagedON DEPARTURE A/C SUSTAINED SEVERAL BIRD STRIKES IN NOSE AREA. RETURNED TO MSP. DAMAGE TO FRAME 1 BULKHEAD OUTER CHORD ANGLE. REPAIR IN PROGRESS PER ER/A 497824-14 ON N/R CARD #59(L/P 0398836).Nov 10, 2011 · N331NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1161733217Wire · brokenDURING NON ROUTINE CHECK, FOUND THE EMERGENCY EXIT PATH LIGHT AT ROW 1AB WIRE BROKEN UNDER SEAT. MAINTENANCE RECONNECTED WIRES AND REPLACED JIFFI JUNCTIONS AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Nov 3, 2011 · N317US · Airbus A320211 · Light System WiringSDR CA111103010Unknown · odor(CAN) FROM TOP OF DESCENT DOWN TO APPROX 400ASL, FAINT ODOR OF ELECTRICAL SMOKE IN FLIGHT DECK ONLY NOTHING VISIBLE, NO OTHER INDICATIONS. ALL NORMAL ON APPROACH. CHECKED FLT DECK AERA, ALL E & E BAYS FWD, MID & AFT, CHECKED O2 COMPARTMENT RAN APU & PACKS, CNov 2, 2011 · Airbus A320211 · Air Distribution SystemSDR CA111103008Brake · malfunctioned(CAN) ON APPROACH, DECLARED EMERGENCY DUE TO FLAP LOCK. PERFORMED RESET OF WING TIP BRAKE OF FLAP SYS & INSPECTION AFTER FLAP/SLAT EXT AT MORE THAN THE FLAP/SLAT LIMITING SPEED IAW AMM 27-50-00-869-005 AND 05-51-13-200-001. OPS CKS OF FLAP/SLAT SYS, CKS GOOct 30, 2011 · Airbus A320211 · Drag Control SystemSDR CA111027003Union · cracked(CAN) SHORTLY AFTER TAKEOFF THE CREW REPORTED A GREEN HYD FAILURE AND RETURNED TO DEPARTURE. LANDING WEIGHT WAS APPROX 2500KG OVER MAXIMUM. REPLACED CRACKED UNION OF GEAR SELECTOR MANIFOLD. REPLACED EDP IAW 29-11-51 AND ENG CASE DRAIN FILTER. ENG GROUND RUOct 24, 2011 · Airbus A320211 · Hydraulic System, MainSDR DALA2016021501058Skin · damagedBELOW CARGO DOOR OPENING AND SCRATCHES VISUALLY INSPECT AND NO CRACKS FOUND AFT DENT 1 X 1, .125" DEEP. FWD 1 X .5", .125" DEEP WITHIN LIMITS IAW SRM 53-11-11, PAR 125, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FRAME 25 TO FRAME 27 AND STR 39R TO SOct 19, 2011 · N330NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR CA111021004Limiter · tripped(CAN) SLATS UNABLE TO DEPLOY, ARFF CALLED OUT. ON SHORT FINAL SLATS DEPLOYED NORMALLY, PAN RESCINDED. FOUND RT SLAT NR 2 OTBD TORQUE LIMITER, PN 830A0000-02, SN 03475, TRIPPED. RESET TORQUE LIMITER IAW AMM 27-80-00-866-006. OPERATIONS CHECKED SERV IAW AMM 2Oct 19, 2011 · Airbus A320211 · Leading Edge Slat Control SystemSDR CA111019013Reservoir · leaking(CAN) CREW ADVISED FLIGHT DISPATCH VIA THE VHF THAT THEY HAD DECLARED A PAN-PAN WITH ATC DUE TO A "GREEN HYDRAULIC LOW RESERVOIR" 20 MINUTES FROM LANDING. CREW REPORTED AN UNEVENTFUL LANDING. THE ACFT REQUIRED A TOW TO THE GATE. LOW LEVEL SWITCH OF GREEN HYD Oct 18, 2011 · Airbus A320211 · Hydraulic Indicating SystemSDR DALA1158093215Power Supply · inoperativeDURING A NON ROUTINE CHECK, MAINTENANCE FOUND AFT LEFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Oct 14, 2011 · N315US · Airbus A320211 · Emergency LightingSDR DALA1157383227Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHTS AT ROWS 13-15, 18-20 AND 24-26 INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY UNIT 13WL AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Oct 8, 2011 · N327NW · Airbus A320211 · Emergency LightingSDR DALA1157433278Skin · crackedCATERING REPORTS CRACK IN RT AFT LOWER CORNER OF SERVICE DOOR. CUT OUT DAMAGED SKIN 1" BY 1.625" PER SRM 5210-00 FIG 203, 730014. FABED DOUBLER FROM 2024T3 .125 AND FILLER FROM 2024T3 .100, AND PRIMED PER SRM 52-10-00. ACCOMPLISHED REPAIR IAW A320 SRM 52-10Oct 6, 2011 · N378NW · Airbus A320211 · Service DoorsSDR DALA1157353227Epsu · inoperativeDURING NON ROUTINE CHECK, FOUND THREE SECTIONS OF EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. MAINTENANCE REPLACED LEFT AFT EPSU AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED SERVICE.Oct 6, 2011 · N327NW · Airbus A320211 · Emergency LightingSDR CA111005005Oven · odor(CAN) SMOKE EMANATING FROM GALLEY OVEN, CONSULTED MOC. BREAKER PULLED AND SMOKE DISSIPATED. FLIGHT CONTINUING TO DESTINATION.Oct 5, 2011 · Airbus A320211 · Buffet/GalleysSDR CA111005004Control Unit · failed(CAN) FLIGHT CONTROL UNIT (FCU) NAVIGATION EQUIPMENT, (AUTO PILOT, FLIGHT DIRECTOR, AUTO-THRUST, ALTIMETER) FAILURE IN DESCENT. CFR ON STANDBY FOR ARRIVAL. FCU REPLACED IAW AMM 22-81-12 PB401. AFS AND LAND TEST OK.Oct 5, 2011 · Airbus A320211 · Flight ControllerSDR DALA1155803227Epsu · inoperativeDURING LINE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED AFT LEFT ESPU. OPERATIONALCHECK GOOD.Sep 26, 2011 · N327NW · Airbus A320211 · Emergency LightingSDR DALA1155653218Light · inoperativeDURING A LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHT AT 6C INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.Sep 23, 2011 · N318US · Airbus A320211 · Emergency LightingSDR DALA1155113225Skin · gougedFUSELAGE SKIN GOUGE 23.5 INCHES AFT OF 2L DOOR CUTOUT. APPROX STA 3320 STR 17L. REMOVED DAMAGE BY BLENDING PER A320SRM 51-73-00. THE BLENDED AREA IS OUT OF LIMITS INSTALL TEMP REPAIR INSTALLED DOUBLER PER A320 SRM 53-41-11. INSTALL RII COMPLETE. OK TO PAISep 22, 2011 · N325US · Airbus A320211 · Fuselage Main, Plate/SkinSDR CA110922007Windshield · cracked(CAN) CREW ADVISED FLIGHT DISPATCH VIA THE ACARS THAT THEY WERE DIVERTING DUE TO F/O CRACKED WINDSHIELD. F/O`S WINDSHIELD BEGAN TO CRACK, QRH AND ATB391 WERE REFERENCED AND CREW ELECTED TO DIVERT. RESULTING IN AN OVERWEIGHT LANDING. NO EMERGENCY WAS CALLED,Sep 17, 2011 · Airbus A320211 · Flight Compartment WindowsSDR CA110922009Actuator · failed(CAN) ON APPROACH, THE FLIGHT EXPERIENCED A SLAT/FLAP FAILURE WITH SLATS AT POSITION 2 AND THE FLAPS AT ZERO. A GO AROUND WAS CONDUCTED AND THE QRH WAS CARRIED OUT. AN EMERGENCY WAS DECLARED WITH ATC WITH CABIN CREW AND PASSENGERS BEING BRIEFED. A SECOND APSep 16, 2011 · Airbus A320211 · Trailing Edge Flap ActuatorSDR DALA1153993227Epsu · inoperativeFLIGHT CREW REPORTED NUMEROUS EMERGENCY SEAT PATH LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE EPSU (13WL) AND SYSTEM NOW CHECKS OK.Sep 15, 2011 · N327NW · Airbus A320211 · Emergency LightingSDR CA110923009Proximity Sensor · failed(CAN) THE FLAPS BECAME LOCKED DURING APPROACH. THE FLIGHT CREW PERFORMED A GO AROUND BEFORE LANDING ROUTINELY. CFR VEHICLES WERE PRESENT AS A PRECAUTION, HOWEVER THE ACFT WAS ABLE TAXI TO THE GATE WITHOUT ASSISTANCE. FLAP PDU`S INSPECTED IAW 27-54-00-210 NFSep 11, 2011 · Airbus A320211 · Trailing Flap Position Indicating SystemSDR CA110922010Windshield · cracked(CAN) THE ACFT ENCOUNTERED THE FORWARD WINDSHIELD OUTER PANE SHATTERING INFLIGHT. THE FLIGHT CONTINUED TO DESTINATION AND WAS MET BY MX. F/O WINDSHIELD ASSY REPLACED IAW AMM 56-11-11, PB 401.Sep 11, 2011 · Airbus A320211 · Flight Compartment WindowsSDR DALA1151073211Post · damagedTHE VERTICAL STIFFENER POST P/N D53113-5201 ON THE AFT OF THE FRAME FR1 PRESSURE BULKHEAD WEB SUSTAINED DEFORMATION AT Y=675 Z=169 DUE TO A BIRD STRIKE.Sep 3, 2011 · N311US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA110909010Connector · shorted(CAN) FLIGHT CONTROL MALFUNCTION INCIDENT DETAILS: DURING THE ILS APPROACH FOR RUNWAY, SELECTED FLAP AT 3 AND RECEIVED 2 ECAM MESSAGES "F/CTRL FLAPS FAULT" AND "F/CTRL FLAP SENSOR" WITH FLAPS INDICATING AMBER. RECYCLED FLAP LEVER IAW ECAM, NIL FIX. FLAPS LOSep 2, 2011 · Airbus A320211 · Electrical Power System WiringSDR DALA1150483213Light · wrong partDURING EMERGENCY LIGHT TEST ALL 4 EMERGENCY EXIT HANDLE LIGHTS WERE NOT WORKING. REPLACED BULBS NO HELP. FOUND WRONG BULBS INSTALLED, REPLACED BULBS AND TESTS OK.Aug 28, 2011 · N313US · Airbus A320211 · Emergency LightingSDR DALA1152113211Skin · damagedBIRD STRIKE JUST BELOW F/O`S WINDSCREEN. POST REPAIR C/W ON ERA 495670-14 REV ORIG. ALL STEPS MATCH. PERMANENT REPAIRS ACCOMPLISHED. SKIN REPAIR C/W ON ERA 495514-1 4 REV ORIG. ALL STEPS MATCH PRIS.Aug 23, 2011 · N311US · Airbus A320211 · Fuselage Main, Plate/SkinSDR CA110824003Smoke Detector · false indication(CAN) CREW REPORTED AN AFT CARGO SMOKE WARNING ON THE GROUND, WHICH MX INVESTIGATED. ON APPROACH THE CREW AGAIN REPORTED ANOTHER BRIEF AFT CARGO SMOKE WARNING. CARGO FWD BAY SMOKE RED ECAM ALERT CAME ON FOR LESS THAN 2 SECONDS 3 TIMES DURING FLIGHT. DID NOAug 22, 2011 · Airbus A320211 · Smoke DetectionSDR DALA1150363211Panel · crackedNR 1 ENG PYLON TO WING PANEL 471AL HAS A CRACK AT L/E. REPAIRED PANEL PERMANENT PER ERA 495620-14 REV ORIG. PAINTED PER 51-35-00 A-320. IDENTIFIED PART PER ERA 495620-14 ORIG. INSTALLED PANEL 471AL PER A320 AMM 54-52. PERM REPAIR ACCOMPLISHED PER ERA 49562Aug 20, 2011 · N311US · Airbus A320211 · Nacelle/Pylon, Plate/SkinSDR DALA1148693219Wire · damagedDURING EMERGENCY LIGHT TEST FOUND ROW 5C PATH LIGHT INOPERATIVE. MAINTENANCE REPAIRED WIRE AT CONNECTOR AND TESTS OK.Aug 16, 2011 · N319US · Airbus A320211 · Light System WiringSDR DALA1148203215Wire · damagedDURING EMERGENCY LIGHT TEST, MAINTENANCE FOUND ROW 8C PATH LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A WIRE AT THE CONNECTOR AND LIGHT NOW TESTS OK.Aug 15, 2011 · N315US · Airbus A320211 · Light System WiringSDR DALA1150343217Retainer · damagedDOOR IL STRUCK JETWAY WHEN ROLLED BACKWARD. FOUND LOWER AFT CORNER OF DOOR SEAL RETAINER DAMAGED. C/W ERA 495347-14 REV ORIG. REMOVED AND INSTALLED NEW RETINER CHANNEL PER ERA 495347-14 REV. CLOSED LOG AND REMOVED MONITOR INSPECTION PER ALERT 26AUG11 AND LAug 12, 2011 · N317US · Airbus A320211 · Passenger/Crew DoorsSDR CA110810010Controller · failed(CAN) APPROX 45 MINUTES AFTER T/O, ECAM MESSAGE SHOWING CABIN PRESS EXCESS CABIN ALT. CREW ELECTED TO DESCEND TO 10,000FT AND RETURN WITH OVERWEIGHT LANDING. CPC 2 HAS JUST BEEN REPLACED. CPC, NR2 INSTALLED, HAS A HISTORY OF THIS FAULT FROM PREVIOUS ACFT. Aug 10, 2011 · Airbus A320211 · Cabin Pressure ControllerSDR CA110809001Brake Assy · overheatedBRAKES SMOKING, AS PASSENGERS DEPLANING, ARFF CALLED OUT. NO DEFECTS RAISED.Aug 6, 2011 · Airbus A320211 · BrakeSDR DALA1146873227Epsu · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT ROWS 18, 19, 20, 24, 25, AND 26 WOULD NOT TEST. MAINTENANCE REPLACED EPSU UNIT AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Aug 6, 2011 · N327NW · Airbus A320211 · Emergency LightingSDR CA110809002Flap System · out of rigWHILE ON FINAL, CREW EXPERIENCED FLIGHT CONTROL FLAP/SLAT FAULT. EMERGENCY DECLARED. FLIGHT LANDED, DURING APPROACH- AT 200 KTS, SELECTED FLAPS 1, (NO PROBLEM) AT 185 KTS SELECTED FLAPS 2: ECAM FCTL - FLAPS LOCKED ALIGNMENT FAULT. TSM 27-51-00-810-818 CARRIEAug 5, 2011 · Airbus A320211 · Trailing Edge Flap Control SystemSDR DALA13024003211Skin · damagedRT FUSELAGE SKIN DAMAGED, REPLACE WITH NEW SKIN IAW ER/A 512316-14.Aug 3, 2011 · N311US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA1145693222Epsu · failedDURING NON ROUTINE CHECK, FOUND THE EMERGENCY EPSU AT AFT LEFT FAILED TEST. MAINTENANCE REPLACED EPSU AND UNIT TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jul 30, 2011 · N322US · Airbus A320211 · Emergency LightingSDR CA110728003Flap System · malfunctionedFLIGHT CREW REPORTED FLAP FAIL AT SECOND STAGE ON APPROACH. THE FLIGHT CREW CONDUCTED A GO-AROUND AND AFTER 2 MORE ATTEMPTS THEY WERE ABLE TO EXTEND THE FLAPS FULLY. THE FLIGHT LANDED WITHOUT ISSUE. FLT CONTROL FLAPS FAULT ON APPROACH WHEN FLAP 2 SELECTED FLJul 27, 2011 · Airbus A320211 · Trailing Edge Flap Control SystemSDR DALA1145173213Wire · brokenDURING NON-ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE LIGHT AT 23C INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jul 27, 2011 · N313US · Airbus A320211 · Light System WiringSDR CA111005006Oxygen Mask · failed(CAN) WHILE CARRYING OUT THE OXYGEN MASK INSPECTION IAW REF 1 AND REF 2 ON SUBJECT ACFT AT THE C9 CHECK, SEVERAL MASKS NOT COVERED BY THE INSPECTION PARAMETERS WERE FOUND WITH BROKEN OR CRACKED FLOW INDICATOR VALVES WERE ON MASKS (PN 174080-96, MFR DATES 1-92Jul 26, 2011 · Airbus A320211 · Passenger Oxygen SystemSDR CA110725012Heat Exchanger · failedPACK 1 OVERHEAT ON GROUND ONLY WORKS WELL AIRBOURNE. ALSO FOUND INTERIOR OF EXHAUST PLENUM DISINTEGRATED WHILE TROUBLESHOOTING DEVIATION "PACK 1 INOP".Jul 23, 2011 · Airbus A320211 · Cabin Cooling SystemSDR DALA1144283230Epsu · failedDURING NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT FAILED FAP PANEL TEST AT L1. MAINTENANCE REPLACED THE L1 EPSU AND SYSTEM TEST WAS NORMAL. AIRCRAFT HAS RETURNED TO SERVICE.Jul 23, 2011 · N330NW · Airbus A320211 · Emergency Lighting
Back to Airbus A320-211