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"

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SDR DALA1224003209Panel · damagedAFT PIT SLOPE PANEL 152EF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL 152EF IAW DWG 3D25-37705. DAMAGE DIM L=1.75" W=1.75". RETAIN FOR RECORDS.Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1223973209Panel · damagedFORWARD PIT SLOPE PANEL 131FF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL 131FF IAW DWG 3D25-37705. DAMAGE DIM: L=2.5 W=3.5. RETAIN FOR RECORDS.Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1223963209Floor Panel · delaminatedAFT PIT FLOOR PANEL 151DF IS DELAMINATED, 25" X25" AREA. FABRICATED FLOOR PANEL 151DF IAW DWG 3D25-37705. DAMAGE DIM L=10.5" W=11.5". RETAIN FOR RECORDS.Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1223943209Floor Panel · delaminatedAFT PIT FLOOR PANEL 151GF IS DELAMINATED, 20" X 20" AREA. FABRICATED FLOOR PANEL 151GF IAW DWG 3D25-37705. DAMAGE DIM L=20" W=20". RETAIN FOR RECORDS.Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1223923209Panel · damagedFORWARD PIT SLOPE PANEL 132FF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL 132FF IAW DWG 3D25-37705.DAMAGE DIM: L=2.4 W=2.4. RETAIN FOR RECORDS.Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1223913209Panel · delaminatedAFT PIT SLOPE PANEL 151EF IS DELAMINATED AND MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL 151EF IAW DWG 3D25-37705. DAMAGE DIM. L=1.75" W=1.75". RETAIN FOR RECORDS.Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1223903209Floor Support · corrodedDURING CHECK, FOUND FWD UTILITY AREA FLOOR SUPPORT AT FR21 -Y189 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW A320 SRM 51-74-00 CHECKED LIMITS L=1.5" W=1.0" D=.050". FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-11-14 101. REMOVED & REPLACED -Y189Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1223483209Panel · damagedDURING CHECK, FOUND AFT PIT SLOPE PANEL 151NF HAS SEVERAL PUNCTURES AND MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL 151NF ON STAM TRAVELER T12/927899 IAWDWG 3D25-37705.Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1222583209Panel · missingDURING CHECK, FOUND FWD PIT SLOPE PANEL 131BF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED NEW SLOPE PANEL 131FF ON STAM TRAVELER T12/927773 IAW DWG 3D25-37705 DAMAGE DIM: L=4.1 W=4.1 AND INSTALLED.Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1222553209Panel · missingDURING CHECK, FOUND FWD PIT SLOPE PANEL 132JF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED NEW ON STAM TRAVELER T12/927775 IAW DWG 3D25-37705. DAMAGE DIM: L=9.5 W=8.5 AND INSTALLED.Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1222513209Floor Support · corrodedDURING CHECK, FOUND FORWARD CABIN FLOOR SUPPORT AT FR 20 Y503.2 UPPER FLANGES HOLES HAS CORROSION. REMOVED CORROSION IAW A320 SRM 51-74-00. FOUND TO BE OUT OF LIMIT IAW A320 SRM 53-11-14 FIG 103. INSTALLED REPAIR PER SRM 51-42-11.Apr 11, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1222153214Light · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT 24C INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AND OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.Apr 10, 2012 · N314US · Airbus A320211 · Emergency LightingSDR DALA1221493213Light · inoperativeDURING NON ROUTINE CHECK, FOUND LT AFT EPSU UNIT FAULT TEST. MAINTENANCE REPLACED EPSU UNIT AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE.Apr 9, 2012 · N313US · Airbus A320211 · Emergency LightingSDR DALA12006943209Sill · corrodedDURING INSPECTIONS, LT AFT PASSENGER DOOR SILL UPPER SURFACE AT AFT FR 68 IS CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FABRICATED ONE REPAIR ANGLE & INSTALLED IAW SRM 53-41-14 FIG 201 AND 51-42-11.Apr 8, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12006933209Floor Support · corrodedDURING INSPECTIONS, AFT UTILITY AREA FLOOR SUPPORT UPPER AND LOWER FLANGE AT FR 64 TO FR 67 -Y465 HARD POINT HOLES CORRODED. REMOVED CORROSION IAW SRM 51-74-00 & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 5Apr 8, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1221273229Terminal · damagedDURING NON ROUTINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHT AT SEAT 14C INOPERATIVE. MAINTENANCE REPAIRED TERMINAL END AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE.Apr 8, 2012 · N329NW · Airbus A320211 · Light System WiringSDR DALA1221113233Light · inoperativeDURING NON ROUTINE CHECK, FOUND SEVERAL FLOOR PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED AFT EPSU AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE.Apr 6, 2012 · N333NW · Airbus A320211 · Emergency LightingSDR DALA1514953229Skin · crackedLEFT ELEVATOR SKIN CRACKED, FOUR INCHES OTBD OF RIB 7, TWO INCHES INBD AND ELEVEN INCHES AFT OF L/E. REPAIRED IAW 450968.Apr 4, 2012 · N329NW · Airbus A320211 · Elevator, Plate/SkinSDR DALA1514943229Skin · damagedRIGHT ELEVATOR DENTED AND CRACKED BETWEEN RIBS 8-9, TWENTY NINE INCHES INBD OF MOST OTBD HINGE, SEVEN INCHES AFT OF THE L/E. REPAIRED IAW 450963.Apr 4, 2012 · N329NW · Airbus A320211 · Elevator, Plate/SkinSDR CA120326002Unknown · odor(CAN) ON TAXI OUT, THE CREW REPORTED A BURNING ODOR IN THE AFT GALLEY. THE FLIGHT RETURNED TO GATE FOR MAINTENANCE INVESTIGATION. AREA CHECKED, NO FAULT FOUND. NO HISTORY. OK TO PROCEED.Mar 20, 2012 · Airbus A320211 · Air Distribution SystemSDR DALA1216193227Wire · brokenDURING NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 16 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT FLOOR CONNECTOR AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Mar 13, 2012 · N327NW · Airbus A320211 · Light System WiringSDR CA120413009Wire · burned(CAN) DURING MAINTENANCE VISIT, FOUND BURNED WIRES IN RACEWAY ALONG AFT SPAR ON LT WING JUST OTBD OF PYLON UNDER NR 3 SPOILER PANEL. THE SNAG "STOBE LIGHTS STAY ON REGARDLESS OF SWITCH POSITION" WAS CAUSING THE CIRCUIT BREAKER TO OPEN.Mar 8, 2012 · Airbus A320211 · Light System WiringSDR CA120312028Controller · failed(CAN) PILOTS SIDE CRACKED WINDSHIELD, BEFORE ACTIONING WINDSHIELD HEAT CIRCUIT BREAKER. OUTER LAYER OF WINDSHIELD CRACKED JUST PRIOR TO TOP OF DECENT. REPLACED CAPTAIN`S WINDSHIELD IN ADDITION, DUE TO NATURE OF LT WINDSHEILD CRACKING & ARCING. LT WINDOW HEAT Mar 8, 2012 · Airbus A320211 · Windshield/Door Rain/Ice RemovalSDR CA120306005Carrier Assy · contaminated(CAN) CAPTAIN WAS DOING WALKAROUND AND NOTICED DARK SMOKE COMING FROM 1 OF THE WHEELS. CAPTAIN ALSO STATED THE F/O DID NOT USE THE BRAKE. INSPECTED AND FOUND EXCESSIVE GREASE ON BRAKE. CLEANED GREASE. NO FLUID LEAKS BRAKE WORKS OK. NOTE: WHEN A LUBE JOB IMar 5, 2012 · Airbus A320211 · Landing Gear Brake SystemSDR DALA1213233217Intercostal · crackedDURING NON ROUTINE CHECK, MAINTENANCE FOUND L2 DOOR MID FWD INTERCOSTAL HAS CRACKED APPROXIMATELY .5 INCHES. REMOVED L2 DOOR MID FWD INTERCOSTAL AND INSTALLED NEW PER SRM 51-42-11.Mar 3, 2012 · N317US · Airbus A320211 · Passenger/Crew DoorsSDR DALA1211333221Light · inoperativeDURING A NON ROUTINE CHECK FOUND THE EMERGENCY PATH LIGHT ATROW 5, 15, 19 AND 25 INOPERATIVE. MAINTENANCE REPAIRED AND RELAMPED AS NEEDED. PERFORMED FUNCTIONAL CHECK AND TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Feb 25, 2012 · N321US · Airbus A320211 · Emergency LightingSDR CA120301001Check Valve · failed(CAN) WHILE ENROUTE THE CREW REPORTED A YELLOW SYSTEM HYDRAULICS QUANTITY LOSS, AFTER DISCUSSION WITH MAINTENANCE THE YELLOW SYSTEM WAS SHUTDOWN AND THE FLIGHT CONTINUED NORMALLY TO DESTINATION. MAINTENANCE ALSO SUGGESTED THE CREW SWITCH THE PUMPS BACK ON JUSFeb 24, 2012 · Airbus A320211 · Hydraulic System, MainSDR DALA1208053231Wire · damagedDURING NON ROUTINE CHECK, FOUND FLOOR EMERGENCY PATH LIGHT AT ROW 22ABC INOPERATIVE. MAINTENANCE RE-TERMINATED WIRES AND OPERATIONAL CHECK WAS NORMAL.Feb 11, 2012 · N331NW · Airbus A320211 · Light System WiringSDR DALA1205333217Epsu · inoperativeDURING NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT ROW 9, 10, 11, 12 AND BOTTOM SIDEWELL OF BOTH OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED RT EPSU AT RIGHT OVERWING EXIT 10W. PERFORMED FUNCTIONAL CHECK AND TEST WAS NORMAL. AIRCRAFT RETURNJan 30, 2012 · N317US · Airbus A320211 · Emergency LightingSDR CA120130005Engine · vibration(CAN) 10 MINUTES BEFORE "TOP OF DESCENT" ENGINE VIBRATION FROM THE RT ENGINE AND COMPRESSOR STALL. CREW REDUCED POWER AND CONTINUED DESCENT. AT 3000 FT AND IDLE POWER THEY AGAIN FELT VIBRATION ON RT WHEN THEY TRIED TO INCREASE POWER BY 5 PERCENT. CONTINUED THJan 29, 2012 · Airbus A320211 · Engine (Turbine/Turboprop)SDR DALA1205363210Light · inoperativeDURING NON ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT AT SEAT 19B INOPERATIVE. MAINTENANCE REPAIRED LIGHT ASSEMBLY AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jan 29, 2012 · N310NW · Airbus A320211 · Emergency LightingSDR DALA1204273212Panel · delaminatedDURING NON ROUTINE CHECK, FOUND FORWARD CARGO SLOPING PANEL 131BF DELAMINATED. FABRICATED ON STAM TRAVELER# T12/913531 PER DWG 3D25-37705 FROM FR 24 TO FR 28 STRINGER 34L TO 38L. REPLACED PANEL 131BF IAW A320 AMM 53-22-14.Jan 25, 2012 · N312US · Airbus A320211 · Cargo CompartmentsSDR DALA1204123227Wire · brokenDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 17 ABC INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jan 25, 2012 · N327NW · Airbus A320211 · Light System WiringSDR DALA1204143212Angle · crackedDURING NON ROUTINE CHECK, MAINTENANCE FOUND RT AFT OVERWING EMERGENCY DOOR RT PROFILE CRACKED. REMOVED DAMAGE SEGMENT ANGLE AND INSTALLED FABRICATED SEGMENT ANGLE FROM MATERIAL 2024-0.050C. BATCH 0001942011 PER A320 SRM 52-21-00 & HEAT TREATED BY STAM TRAVELEJan 24, 2012 · N312US · Airbus A320211 · Emergency ExitsSDR DALA1204133212Floor Panel · delaminatedDURING NON ROUTINE CHECK, MAINTENANCE REMOVED AFT CARGO FLOOR PANEL 151PF DUE DELAMINATION. FABRICATED AFT CARGO FLOOR PANEL 151PF ON STAM TRAVELER # T12/913710 IAW DRAWING 3D25-37705 MATERIAL A402AB-60X144 BATCH# 2105510. DAMAGE DIM. L=42" W=21". INSTALLEDJan 24, 2012 · N312US · Airbus A320211 · Fuselage Floor PanelSDR CA120124006Unknown · odor(CAN) THE FLIGHT CREW ENCOUNTERED A BRIEF ELECTRICAL ODOR WHEN THE THROTTLES WERE PULLED BACK AT APPROXIMATELY 11000FT, THIS QUICKLY DISSIPATED.. DURING FINAL APPROACH AND TAXI, THE ELECTRICAL ODOR CAME BACK AND WAS VERY APPARENT IN THE COCKPIT AND THROUGHOUT Jan 23, 2012 · Airbus A320211 · Air Distribution SystemSDR CA120125003Window · cracked(CAN) THE AIRCRAFT ENCOUNTERED A CRACKED (CAPTAIN`S SIDE), FIXED LATERAL WINDOW AFTER DEPARTURE THE FLIGHT CREW RETURNED THE AIRCRAFT. THERE WAS NIL ADVERSE PASSENGER REACTION AND THE AIRCRAFT DID NOT LAND OVERWEIGHT. LT FIXED WINDOW (7DG1) REPLACED IAW AMM 56Jan 22, 2012 · Airbus A320211 · Flight Compartment WindowsSDR DALA1203273212Skin · dentedDURING NON ROUTINE CHECK, FOUND LOWER FWD FUSELAGE EXTERNAL SKIN AT FR 26, BTW STR 42R - 43R DENTED. PERFORMED A DETAILED VISUAL INSP ON EXTERNAL SKIN AND NO CRACKS NOTED. ACCOMPLISHED PERMANENT REPAIR IAW A320 SRM 53-21-11 FIG 216.Jan 20, 2012 · N312US · Airbus A320211 · Fuselage Main, Plate/SkinSDR CA120119006Water Heater · shorted(CAN) PASSENGER SMELLED SMOKE IN LAVATORY E. REPORTED HAVING SEEN SPARKS IN THE AREA BELOW THE SINK. F/A CONFIRMED THE ODOR OF SMOKE AND SWITCHED OFF THE WATER HEATER. SMOKE ODOR DISSIPATED. ON THE GROUND, MAINTENANCE HAD A LOOK AND FOUND SOME EVIDENCE OF AJan 14, 2012 · Airbus A320211 · Wash Water SystemSDR CA120119002Windshield · failed(CAN) ENROUTE IN CRUISE, THE ACFT DEVELOPED A CRACK ON THE CAPTAIN`S FRONT WINDSCREEN. IT CRACKED FROM THE LT PILLAR POST TO THE MIDDLE OF THE WINDSCREEN AND THEN STRAIGHT DOWN TO THE BOTTOM. CAPTAIN`S WINDSCREEN REPLACED IAW AMM 56-11-11, PB401. WINDOW HEAJan 11, 2012 · Airbus A320211 · Flight Compartment WindowsSDR CA120109004Control Valve · failed(CAN) APPROXIMATELY 25 MINUTES AFTER TAKEOFF THE CABIN ALTITUDE BEGAN TO RISE. THE CREW WAS UNABLE TO CONTROL PRESSURIZATION AND PERFORMED AN EMERGENCY DESCENT TO FL180. THE MAXIMUM CABIN ALTITUDE REACHED WAS 10500FT, THE OXYGEN MASKS DID NOT DEPLOY. EMERGENCYJan 7, 2012 · Airbus A320211 · Cabin Cooling SystemSDR CA120103011Controller · failed(CAN) CREW REPORTED OSCILATIONS IN FLIGHT THAT THEY ATTRIBUTED TO FLIGHT CONTROLS AS WELL AS A BANGING SOUND IN FLIGHT. MAINTENANCE TO INVESTIGATED ON ARRIVAL. R & R ACCELEROMETERS 12CE3 + 12CE4 IAW 27-92-16, PB 401+ TSM 27-30-00-810-853. NO FAULT NOTED. 12Jan 1, 2012 · Airbus A320211 · Elevator Control SystemSDR DALA1168643220Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND F/C FLOOR PROXIMITY LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AT 10WL AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Dec 8, 2011 · N320US · Airbus A320211 · Emergency LightingSDR CA111208002Apu · failed(CAN) ABOUT 10-15 MINUTES AFTER ARRIVAL THE RAMP CREW OBSERVED SMOKE OR STEAM COMING FROM THE APU AREA. FIRE DEPARTMENT WAS CALLED AND THEY OPENED THE APU COMPARTMENT TO INVESTIGATE. APU REPLACED, PNDec 7, 2011 · Airbus A320211 · Airborne Auxiliary Power Unit (APU) SystemSDR CA111206003Ballast · overheated(CAN) THE FLIGHT CREW REPORTED A BURNING ODOR IN THE CABIN IN THE AREA OF ROWS 14-17. THE EMERGENCY LIGHTS IN ROWS 14-17 ILLUMINATED BY THEMSELVES AND WERE UNABLE TO BE SHUTOFF, ALSO, OF A CHLORINE ODOR IN THE AFT CABIN. R & R BALLAST IAW AMM 33-21-11, PB 401Dec 5, 2011 · Airbus A320211 · Passenger Compartment LightingSDR CA111206002Check Valve · leaking(CAN) WHILE ENROUTE, THE CREW REPORTED THE YELLOW HYD SYSTEM SHUTDOWN DUE TO LOW PRESSURE DUE TO LOW HYD FLUID LEVEL. THE FLIGHT LANDED NORMALLY AND DID NOT REQUIRE A TOW INTO THE GATE NOR DID THEY DECLARE AN EMERGENCY FOUND CK VALVE LEAKING. ENG CASE DRAINDec 5, 2011 · Airbus A320211 · Hydraulic System, MainSDR DALA1166493210Wire Harness · defectiveDURING NON ROUTINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED EMERGENCY ESCAPE PATH HARNESS AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Nov 29, 2011 · N310NW · Airbus A320211 · Light System WiringSDR CA111123003Actuator · malfunctioned(CAN) FLAP/SLAT JAM ON APPROACH, FLIGHT DIVERTED IN CONSIDERATION OF DESTINED AIRPORT RWY CONDITIONS. FOUND LT NR 6 SLAT TRACK ROTARY ACTUATOR TRIPPED. REPLACED LT NR 6 SLAT TRACK ACTUATOR, 6029CM, IAW AMM 27-84-49. OPERATOR CHECK CARRIED OUT. NO FAULTS. PNov 23, 2011 · Airbus A320211 · Leading Edge Slat ActuatorSDR DALA1165133222Epsu · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT TEST FAILED ON TEST. MAINTENANCE REPLACED EPSU AT 11WL AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Nov 23, 2011 · N322US · Airbus A320211 · Emergency LightingSDR DALA1166723231Bulkhead · damagedDURING NON ROUTINE CHECK, FRAME 1 BULKHEAD WEB DAMAGED BY BIRD STRIKE TRIMMED OUT DAMAGED WEB. HFEC NO CRACKS. FABRICATED .063" WEB SECTION AND .071" 2024-T3 WEB DOUBLER. DRILLED AND INSTALLED PER ER/A 497863-14.Nov 16, 2011 · N331NW · Airbus A320211 · Fuselage Main, Bulkhead
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