Airbus A320-211

Service difficulty reports · 5,271

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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 CA050404008Windscreen · cracked(CAN) CAPTAIN WINDSCREEN CRACKED IN FLT 36000 FT EMERGENCY DESCENT CARRIED OUT. CRACK SPARKED ELECTRICALLY WHILE CRACKING TIME OF CRACK IS FULL LENGTH 3 FT. WINDOW REPLACED AS PER AMM 56-11-11, WINDOW CONTROLLER CHANGED AND TESTED AS PER AMM 30-42-34 PB 40.Apr 4, 2005 · Airbus A320211 · Flight Compartment WindowsSDR 0500413218Fitting · brokenAFTER TAKEOFF FROM MEM PRIOR TO FLAP RETRACTION, RECEIVED ECAM CAUTION HYD Y RSVR LO LVL. FOLLOWED COM PROCEDURES, RETURNED TO MEM, AND LANDED UNEVENTFULLY. ENGINE DRIVEN PUMP CAVITATED FOR ABOUT 30 SECONDS. FOUND UNION FITTING BROKEN OFF OF BRAKE DUAL DISTMar 29, 2005 · N318US · Airbus A320211 · Hydraulic System, MainSDR 0500363232Odor · detectedDURING DESCENT INTO MEM, EXPERIENCED BURNING ODOR AND OBSERVED WHITE SMOKE IN COCKPIT. DECLARED AN EMERGENCY AND PROCEEDED TO MEM AND LANDED UNEVENTFULLY. INSPECTED ALL AVIONICS BAYS AND BEHIND CIRCUIT BREAKER PANELS, OVENS, AND COFFEEMAKERS WITH NO PROBLEMSMar 21, 2005 · N332NW · Airbus A320211 · Air Distribution SystemSDR CA050303008Pump · leaking(CAN) FAULT: TOTAL LOSS OF ALL GREEN HYD FLUID. LOST MOST OF THE FLUID ON DEPARTURE AND THE REST ON LANDING. NR1 EDP REPLACED IAW AMM 29-11-51. ENG RUN FUNCTIONAL CHECK CARRIED OUT SERVICEABLE.Mar 3, 2005 · Airbus A320211 · Hydraulic Pump (Electric/Engine), MainSDR CA050222004B-Nut · loose(CAN) LT ENGINE OIL INDICATING 7.5 QTS IN FLT WAS INDICATING 15 QTS ON GROUND 2 HOURS EARLIER. CONTINUED LEAKING AT ABOUT 5 QT/HR. A/C LANDED /DIVERTED FOR MAINTENANCE. FOUND AFT BEARING OIL LINE B-NUT LOOSE. TIGHTENED B-NUT. BRACKET SECURED WITH RED RTU. DFeb 22, 2005 · Airbus A320211 · Turbine Engine Oil SystemSDR CA050222005Reservoir · low(CAN) HYD GREEN RESERVOIR LOW LEVEL QTY ZERO. GREEN RESERVOIR SERVICED IAW AMM 12-12-29-611-001.Feb 22, 2005 · Airbus A320211 · Hydraulic Reservoir, MainSDR CA050222006Sensor · open(CAN) LOWERED THE GEAR HANDLE AND GEAR SHOWED IN TRANSIT, THEN E-CAM FOR GEAR NOT DOWN AND LOCKED. RECYCLED THE HANDLE AND GEAR CAME DOWN, LANDED WITHOUT INCIDENT. POST FLT REPORT FLAGS RT NLG DOOR OPEN SENSOR 38GA. INTERCHANGED WITH C1 CARGO PROX SWITCH. LFeb 22, 2005 · Airbus A320211 · Landing Gear Position and WarningSDR CA050111002Servo · intermittent(CAN) FAULT: JUST PRIOR TAKE-OFF, FLIGHT RECEIVED A FLT CTL SPOILER 1 FAULT. CREW TAXIED ONTO A TAXIWAY AND PERFORMED A SUCCESSFUL RESET. HOWEVER, AT 3000 FT/210 KNOTS ON CLIMB, THE FAULT RETURNED AGAIN. FURTHER INTO THE FLIGHT IN CRUISE SLAT SYSTEM. ACTIOJan 11, 2005 · Airbus A320211 · Drag Control SystemSDR CA041229003Computer · malfunctioned(CAN) F/CTL ELAC 1 PITCH FAULT, F/CTL ELAC 2 PITCH FAULT, F/CTL STAB. JAM, APPEARED ON ECAM. ECAM PROCEDURE COMPLETED NORMALLY AND A/C REMAINED IN ALTN LAW. RESET ELAC 1 & 2 VIA PUSH BUTTONS AND SYSTEM RESET ITSELF. ELAC NR 2 REPLACED AND TESTED PER AMM.Dec 29, 2004 · Airbus A320211 · Elevator Control SystemSDR CA041209001Structure · vibration(CAN) VERT SIGNIFICANT RUMBLE/VIBRATION DURING CLIMB AND CRUISE. A/C ROUTED TO HANGAR FOR INVESTIGATION. NOTE: MORE INFO. WILL FOLLOW AS BECOME AVAIL.Dec 9, 2004 · Airbus A320211 · Fuselage Main, StructureSDR 0401363232Power Supply · shortedDURING FLIGHT, FUMES WERE REPORTED IN THE CABIN AND COCKPIT. NO SMOKE OR HEAT SOURCE WAS IDENTIFIED. THE OZONE FILTER WAS REPLACED, THEN ROW 11F EMERGENCY LIGHTS POWER SUPPLY SHORTED. REPLACED THE POWER SUPPLY AND TESTED OK.Aug 18, 2004 · N332NW · Airbus A320211 · Emergency LightingSDR CA040602007Windshield · failed(CAN) WINDSHIELD OUTER PANE SHATTERED ONLY, AIR TURNBACK WINDSHIELD REPLACED WINDSHIELD HAD 21,599 HRS.Jun 19, 2004 · Airbus A320211 · Flight Compartment WindowsSDR CA040615001Control Unit · failed(CAN) FAULT: ON FINAL APPROACH, WHEN FLAP 1 SELECTED, ONLY SLATS CAME OUT. NO FLAPS, RECYCLED TWICE NOJOY. SLATS ONLY LANDING CARRIED OUT. ACFT OUT OF SERVICE FOR INVESTIGATION. COMMENTS: FURTHER INFO WILL FOLLOW.Jun 15, 2004 · Airbus A320211 · Trailing Edge Flap Control SystemSDR CA040609015Landing Gear · failed(CAN) FAULT: THE NOSE GEAR DID NOT RETRACT AFTER DEPARTURE. THE FLT CREW RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. NO ADDITIONAL INFORMATION WAS PROVIDED BY THE FLIGHT CREW. AIRCRAFT OUT OF SERVICE FOR INVEST. NOTE: MORE INFO WILL FOLLOW WHEJun 9, 2004 · Airbus A320211 · Nose/Tail Landing GearSDR CA040513001Unknown · unknown(CAN) DURING A FULL THRUST TAKEOFF AT APPROX 100 KNTS IAS, ACFT SNAPPED TO THE LT REQUIRED ABRUPT RT RUDDER. AGAIN AT APPROX 130 KNTS IAS, ACFT VEERED LT THOUGH LESS ABRUPT. ALL OTHER INDICATIONS NORMAL AND FLIGHT CONTINUED ON TO DESTINATION. AC TO BE REMOMay 13, 2004 · Airbus A320211 · Flight Control SystemSDR CA040412006Engine · bird ingestion(CAN) FAULT: HIT 2 GEESE ON T/O HIGH SPEED REJECTED RETURNED TO GATE. FOUND EVIDENCE OF BIRD INGESTION AT NR 1 ENG. SEVERAL DAMAGED BLADES, A/C ROUTED TO HANGAR FOR ENGINE BOROSCOPE.Apr 12, 2004 · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA040412BBBLine · leaking(CAN) AFTER T/O FROM YYJ NO.1 OIL QUANTITY FELL TO 2.5 QT. REDUCED TO IDLE THRUST,QUANTITY ROSE TO 4.0 AND THEN STARTED TO FELL AGAIN. SHUT ENGINE DOWN AT 10,000 FT ON APP TO YVR. ACTION: FOUND OIL LINE FITTING LOOSE. OIL LINE LOCATED IN BETWEEN GEAR BOX AND RApr 12, 2004 · Airbus A320211 · Turbine Engine Oil SystemSDR 0400483230Priority Valve · leakingJUST PRIOR TO APPROACH, RECEIVED ECAM MESSAGE 'HYD Y RSVR LO LVL'. FOLLOWED COM AND LANDED UNEVENTFULLY. ECAM INDICATED NEAR TOTAL LOSS OF FLUID. FOUND PRIORITY VALVE AT PTU MANIFOLD LEAKING. REPLACED PRIORITY VALVE AND SERVICED YELLOW HYDRAULIC RESERVOIR. LEAMar 23, 2004 · N330NW · Airbus A320211 · Hydraulic System, MainSDR 0400413217Slide · will not testDURING EMERGENCY SYSTEM TEST, RECEIVED EXT LOAD FWD L MESSAGE. REPLACED THE RIGHT SLIDE GIRT BAR AND SLIDE ASSEMBLY, TESTED OK. REINSTALLED SLIDE COVER AND RE-ARMED DOOR ASSIST BOTTLE. AIRCRAFT RETURNED TO SERVICE.Mar 15, 2004 · N317US · Airbus A320211 · Escape SlideSDR CA040225004Engine · stalled(CAN) REPEAT NR 1 ENG STALL. (MORE INFO WILL FOLLOW)Feb 25, 2004 · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA040219002Engine · stalled(CAN) NR 1 ENGINE STALL IN CRUISE. DUE TO HISTORY MTC ADVISED RETURN FOR INVESTIGATION AND FURTHER T/S. DFDR PULLED.Feb 19, 2004 · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA040129001Odor · detected(CAN) STRONG ELECTRICAL ODOR FOR 2 MIN DURING DESCENT. WENT AWAY AFTER SHUTTING THE VTRS OFF. CIRCUIT BREAKER WAS PULLED FOR THE REMAINING OF THE FLIGHT, DUE UNABLE TO REACH ANYBODY TO INVESTIGATE IN FLIGHT.Jan 29, 2004 · Airbus A320211 · Air Distribution SystemSDR CA040126004Uplock · inoperative(CAN) NOSE LDG DOOR WOULD NOT CLOSE AFTER T/O. RECYCLED 3 TIMES (NO SUCCESS) DOOR CLOSED NORMALLY WITH GEAR DOWN. NLG DOOR UPLOCK REPLACED IAW AMM32-31-21-400-001, CONSIDERED SERVICEABLE.Jan 26, 2004 · Airbus A320211 · Landing Gear Door ActuatorSDR CA040116001Warning System · inoperative(CAN) IN CLIMB OUT OF 17T ECAM MSG DOOR AFT CARGO. PRESSURISATION NORMAL. MSG DISAPPEARED IN CRUISE 10 MIN. LATER. (SEE COMMENTS FOR TROUBLESHOOTING. FOR TROUBLESHOOTING, CARRY OUT TSM FAULT ISOLATION TASK NR 32-31-00-810-831 AND 32-31-00-810-833. SENSOR 34WVJan 16, 2004 · Airbus A320211 · Door Warning SystemSDR CA031224001Wire Harness · chafedF/A NOTICED SPARK FROM OXYGEN PNL. A/C REMAINED IN SERV SEVERAL DAYS. UPON INSPECT, WIRE BUNDLE DIRECTLY ABOVE LAV "E" SMOKE DETECT FOUND CHAFFED ON SMOKE DETECT. INSPECT FOUND ROUTING OF WIRE BUNDLE WITH LITTLE CLEARANCE BETWEEN BUNDLE AND DETECTOR AND REPDec 16, 2003 · Airbus A320211 · Fire Protection System WiringSDR 0301933209Outflow Valve · malfunctionedAT CRUISE FL350, LOST CABIN PRESSURE. CABIN PRESSURE CLIMBED TO 11,000 FT DURING EMERGENCY DESCENT. DESCENDED TO 10,000 FT AT 10,000 FT CABIN RE-PRESSURIZED NORMALLY. PACKS FUNCTIONED NORMALLY AND OUTFLOW VALVE WAS CLOSED DURING EMERGENCY DESCENT. FLIGHT COct 15, 2003 · N309US · Airbus A320211 · Cabin Pressure ControllerSDR CA031015005Control Box · smoke(CAN) VIDEO TRANSCOM POWER BOX WAS SMOKING ON GROUND. NO OTHER DAMAGE FOUND. UNIT REPLACED AND ALL CHECKS NORMALOct 10, 2003 · Airbus A320211 · Entertainment SystemSDR CA031021002Wire · damaged(CAN) DURING A MTCE PREP VISIT FOR RETURNING THE A/C BACK TO LESSOR , MTCE IDENTIFIED A PROBLEM WITH NR 2 ENGINE LP VALVE DURING THE OPERATIONAL TEST OF THE VALVE IAW TASK 28-24-00-790-003. FURTHER TROUBLESHOOTING IDENTIFIED WIRE DL-20-AE-FR-F, SPEC MIL-W-250Sep 26, 2003 · Airbus A320211 · Fuel System WiringSDR 0301593217Tru · inoperativeWHILE AT CRUISE (LAX-MSP) RECEIVED TR2 (NR 2 TRANSFORMER RECTIFIER) FAULT MESSAGE AND NOTED ELECTRICAL BURNING ODOR WITH NO SMOKE VISIBLE. DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. PERFORMED OVERWEIGHT LANDING INSPECTION IAW AMM. REPLACED NBR 2 TRANSFORMER Aug 15, 2003 · N317US · Airbus A320211 · DC Rectifier/ConverterSDR 0301583226Line · chafedIN MODERATE TURBULENCE, AUTOPILOT KICKED OUT AND RECEIVED YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL MESSAGE ON ECAM. FOLLOWED COM PROCEDURE AND LANDED AT DTW UNEVENTFULLY. FOUND YELLOW SYSTEM COMPLETELY EMPTY. FOUND SPOILER HYDRAULIC PRESSURE LINE CHAFED ON Aug 15, 2003 · N326US · Airbus A320211 · Hydraulic System, MainSDR CA030826018Turbine Blades · shingled(CAN) ON ROUTINE SERVICE CHECK FOUND NR 2 ENGINE NOZZLE ASSY CRACKED APPROX 3/4 OF THE WAY AROUND. NO NOTICABLE VIBRATIONS. UPON REMOVAL OF NOZZLE ASSY NOTICED SOME TURBINE BLADES SHINGLED. ENGINE HAD BEEN INSTALLED NOV 2002. ENGINE REMOVED FOR SHOP INVESTIGAAug 13, 2003 · Airbus A320211 · Turbine SectionSDR 0301393207Line · leakingTHIRTY MINUTES INTO FLIGHT, LOST ALL HYDRAULIC FLUID IN YELLOW SYSTEM. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED LEAKING PARKING BRAKE LINE IN RIGHT WHEEL WELL. OPERATIONAL CHECK GOOD AND NO EVIDENCE OF LEAKAGE IN YELLJul 28, 2003 · N307US · Airbus A320211 · Hydraulic System, MainSDR CA030806003Rudder · out of adjust(CAN) DURING FLIGHT CONTROL CHECK AT GATE FOUND RUDDER TRAVEL STOPS SHORT OF FULL DEFLECTION TO THE LEFT. ADJUSTED RUDDER MECHANICAL CONTROL IAW AMM. TESTED ARTIFICIAL FEEL AND RTL. IAW AMM AND ALL CHECKED SERVICABLE.Jul 20, 2003 · Airbus A320211 · Rudder Control SystemSDR CA030624002Bearing · failed(CAN) AT H 02 CHECK ,FOUND RT SLAT TORQUE TUBE STEADY BEARING FIN 6081CM WITH NO BALL BEARINGS LEFT IN BEARING ASSEMBLY THIS STEADY BEARING IS LOCATED INBOARD OF RIB 13 INBOARD SIDE OF TELESCOPING PNEUMATIC DUCT BRACKET ON RT WING LEADING EDGE REMOVE AND REPLJun 20, 2003 · Airbus A320211 · Leading Edge DevicesSDR CA030526005Actuator · malfunctioned(CAN) HOLDING AT FL200 200KTS ELAC2 PITCH FAULT FOLLOWED BY A/P OFF, ALTN LAW AND ELAC 1PITCH FAULT. ECAM SHOWED STAB JAM BUT MAN. PITCH TRIM OK. DIR LAW ON MLG DOWN PITCH TRIM IN MAN STILL AVAIL. A/C HANDLING QUALITY WAS GOOD. NO FAULT LTS ON ELAC2/1 ON O/HEAMay 22, 2003 · Airbus A320211 · Stabilizer ActuatorSDR CA030523003Windshield · broken(CAN) CAPTAINS WINDSHIELD SHATTERED AT 11000 FT. REPLACED THE WINDSHIELD AND HEAT CONTROLLER. HEAT CONTROLLER TOTAL OF WINDSHIELD 8477 HRS TIME SINCE INST 203 HRS.May 17, 2003 · Airbus A320211 · Flight Compartment WindowsSDR AUS20030477Seat Track · corroded(AUS) CABIN FLOOR STRUCTURE CONTAINED LEVEL 2 CORROSION IN THEFOLLOWING AREAS:- 1. DOOR CUTOUT REAR RADIUS AT L1 DOOR2. CENTRE ATTACHMENT ANGLE (LOCATED BETWEEN FORWARD AND REAR RADIUS OF L1 DOOR GUSSETS 3. LT REAR PASSENGER DOOR SILL. RT OUTBOARD SEAT TRACK AApr 30, 2003 · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR 0300653226Fan · burned outDURING CRUISE EXPERIENCED RUMBLING/VIBRATION SEEMING TO COME FROM AVIONICS COMPARTMENT. ALSO EXPERIENCED ELECTRICAL BURING ODOR (NO SMOKE). DIVERTED TO BHM AND LANDED UNEVENTFULLY. VERIFIED AVIONICS BLOWER FAN FAULTY AND APPLIED MEL PROVISIONS. RAN PACK AND VEMar 31, 2003 · N326US · Airbus A320211 · Air Distribution FanSDR 0300643221O-Ring · leakingRECEIVED YELLOW SYSTEM HYDRAULIC RESERVOIR LOW LEVEL WARNING. ECAM INDICATED ZERO QUANTITY IN YELLOW SYSTEM RESERVOIR. DEACTIVATED YELLOW HYDRAULIC SYSTEM PER COM AND LANDED UNEVENTFULLY. REPLACED O-RING AT THE PTU MANIFOLD AND LEAK CHECKED OK. SERVICED YELLOWMar 30, 2003 · N321US · Airbus A320211 · Hydraulic System, MainSDR CA030327002Servo · failed(CAN) ON CLIMB AT 15,000 SIGNIFICANT CYCLIC VIBRATION FELT AT 315 KTS.PROBLEM REDUCED AT SLOWER SPEED AND WORSE WHEN TURNING. RT AILERON SERVO ACTUATOR REPLACED AS PER AMM.Mar 24, 2003 · Airbus A320211 · Aileron Control SystemSDR AUS20030336Frame · corroded(AUS) FORWARD PRESSURE BULKHEAD FRAME 1 CONTAINED LEVEL 2 CORROSION INAREA AROUND UPPER RIGHT HAND LOCATING CLIP, LEFT HAND LOWER LOCATING CLIP AND RIGHT HAND LOWER LOCATING CLIP.Mar 20, 2003 · Airbus A320211 · Fuselage Main, FrameSDR 0300813224Floorbeam · corrodedDURING M-CHECK, FOUND CORROSION ON FLOOR SUPPORT BEAM AT FRAME 20 LBL 30. REPAIRED PER EA 32-193626.Mar 13, 2003 · N324US · Airbus A320211 · Fuselage Main, Floor BeamSDR 0300363225A/C Pack · odorAPPROXIMATELY 20 MILES FROM TOUCHDOWN EXPERIENCED A STRONG OIL ODOR IN THE COCKPIT AND CABIN. NO SMOKE WS OBSERVED. FOLLOWED COM PROCEDURES AND LANDED UNEVENTFULLY. INSPECTED ELECTRICAL AND HYDRAULIC COMPARTMENTS, LANDING GEAR WELLS AND FOUND NO EVIDENCE OF SOMar 4, 2003 · N325US · Airbus A320211 · Cabin Cooling SystemSDR AUS20030253Sleeve · corroded(AUS) RT PYLON SPIGOT BEARING SLEEVE PITTED AND CORRODED ON INSIDE SURFACE. FOUND DURING INSPECTION IAW J9-IA57-0824(2).Mar 3, 2003 · Airbus A320211 · Nacelle/Pylon, Attach FittingsSDR AUS20030242Stringer · corroded(AUS) STRINGER NR 41L LOCATED BELOW FORWARD CARGO AREA BETWEEN FRAME 30 AND FRAME 31 CONTAINED LEVEL 2 CORROSION. AREA OF CORROSION 127MM (5IN) BY 25.4MM (1IN) AND 0.8636MM (0.034IN) DEEP. FOUND DURING INSPECTION IAW MRBR 53.21.80.Feb 28, 2003 · Airbus A320211 · Fuselage Main, Longeron/StringerSDR AUS20030241Sill · corroded(AUS) BULK CARGO DOOR SILL CONTAINED LEVEL 2 CORROSION. AREA OF CORROSION 52.8MM (2IN) BY 25.4MM (1IN) AND 1.27MM (0.050IN) DEEP. FOUND DURING INSPECTION IAW MRBR 53.41.07.Feb 28, 2003 · Airbus A320211 · Fuselage Miscellaneous StructureSDR AUS20030239Frame · cracked(AUS) RT SIDE DOOR FRAME CRACKED IN HOLE NR 4 FOUND DURING EDDY CURRENT INSPECTION IAW NDT TESTING MANUAL 53-11-53.Feb 28, 2003 · Airbus A320211 · Fuselage Main, FrameSDR CA030304002Engine · stalled(CAN) NR 2 ENGINE STALL IN LEVEL FLT. ECAM MSG NR 2 ENGINE STALL THEN NR 2 ENGINE SHUT DOWN. ECAM ACTIONS CARRIED OUT. CHANGED NR 2 ENGINE IAW AMM.Feb 27, 2003 · Airbus A320211 · Engine (Turbine/Turboprop)SDR 0300243220Service difficultyDuring top of descent engine #1 experienced a compressor stall and flamed out. Flight crew performed an uneventful single engine landing. Maintenance replaced the Hydro Mechanical Unit.Feb 17, 2003 · N320US · Airbus A320211 · Fuel Control/Turbine EnginesSDR CA030410001Rod · damaged(CAN) RUDDER POSITION FEED BACK ROD ASSEMBLY DAMAGED FROM SKYDROL ROD IS MADE FROM A KEVLAR MATERIAL THAT IF A PRE-EXISTING CONDITION ALLOWS SKYDROL TO CONTAMINATE THE STRUCTURE OF THE ROD IT WILL DETERIORATE.Jan 20, 2003 · Airbus A320211 · Rudder Control System
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