Airbus A320-211

Service difficulty reports · 5,271

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  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 CA110103002Slat System · binding(CAN) ON APPROACH, FLIGHT DECLARED AN EMERGENCY WITH THEIR SLATS FAILED AT 0 DEGREES. FLIGHT LANDED WITHOUT ISSUE ON RUNWAY 33R. PASSENGERS WERE NOTIFIED OF THE IRREGULAR CONFIGURATION FOR LANDING AND WERE INFORMED ABOUT THE EMERGENCY VEHICLES. AFTER LANDING Dec 27, 2010 · Airbus A320211 · Leading Edge Slat Control SystemSDR DALA1036053213Floor Panel · delaminatedDURING L-CHECK FOUND FWD CARGO COMPARTMENT, ZONE 130 - FLOOR PANEL 131AF DELAMINATED. REMOVED FLOOR PANEL 131AF IAW AMM 53-22-14-000-001. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209. INSTALLED PANEL IAW AMM 53-22-14-000-001.Dec 17, 2010 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA1036043213Floor Panel · crackedDURING L-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR PANEL 151PF CRACKED. REMOVED FLOOR PANEL IAW AMM 53-42-14-000-001. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209. INSTALLED NEW FLOOR PANEL IAW AMM 53-42-14 -000-0.Dec 17, 2010 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA1036033213Floor Panel · delaminatedDURING L-CHECK, FOUND FWD CARGO COMPARTMENT, ZONE 130 FLOOR PANEL 131EF HAS DELAMINATION. REMOVED FLOOR PANEL 131EF IAW AMM 53-22-14-000-001. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209. INSTALLED PANEL IAW AM, M 53-22-14-000-001.Dec 17, 2010 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA1051523221Battery Pack · faultedDURING BATTERY PACK REPLACEMENT, EPSU (13WL) FAULTED, REPLACED (EPSU) EXTERNAL POWER SUPPLY UNIT 13WL AND TESTS OK.Dec 15, 2010 · N321US · Airbus A320211 · Emergency LightingSDR DALA1051303231Wire · brokenDURING EMERGENCY LIGHT TEST FOUND SEAT ROW 16 AND 25 INOPERATIVE. REPAIRED BROKEN WIRING AND TESTS OK, REF LOG PAGE 6191017.Dec 13, 2010 · N331NW · Airbus A320211 · Light System WiringSDR DALA1035333228Stringer · corrodedDURING LINE CHECK FOUND STR 31 AT FR 65 AND FR 66 RT HAS CORROSION JUST BELOW OUTFLOW VALVE. REMOVED DAMAGED SECTION OF STR REMOVED ENTIRE STR DRILLED UP NEW STRINGER. INSTALLED ENTIRE STR 31RT. COMPLIED WITH RII REQUIREMENTS FOR THE INSTALLATION AND SECURITY Dec 10, 2010 · N328NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR CA101214005Latch · failed(CAN) AFTER DEPARTURE, THE FLIGHT CREW RECEIVED AN ENGINE VIBRATION FOLLOWED BY AN ECAM MESSAGE "THRUST REVERSER UNLOCK". THE NUMBER TWO (2) ENGINE WAS SHUTDOWN AS A PRECAUTION. THE AIRCRAFT RETURNED DEPARTING STATION. THE HCU (HYD CONTROL UNIT) AND THE DOORDec 8, 2010 · Airbus A320211 · Engine Thrust ReverserSDR DALA1050943218Light · inoperativePILOT REPORTED SEAT 24C EMERGENCY PATH LIGHT OUT, REPLACED LIGHT ASSY AND TESTS OK.Dec 8, 2010 · N318US · Airbus A320211 · Emergency LightingSDR DALA1050743217Power Supply · inoperativeAFTER PUSH BACK THE F/A REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE NOT ILLUMINATED, RETURNED TO GATE AND THE FLIGHT CANCELLED. THE FRONT LT EPSU (10WL) WAS REPLACED AND TESTS OK.Dec 6, 2010 · N317US · Airbus A320211 · Emergency LightingSDR CA101206011Actuator · leakingEN ROUTE AT FL380, THE FLIGHT EXPERIENCED A GREEN HYD FAILURE. THE QRH WAS FOLLOWED AND THE FLIGHT CONTINUED TO DESTINATION AND CARRIED OUT AN UNEVENTFUL LANDING. THE CREW USED DIFFERENTIAL BRAKING TO EXIT TO TAXIWAY. ERS DID RESPOND BUT AN EMERGENCY WAS NDec 3, 2010 · Airbus A320211 · Autopilot Trim ServoSDR DALA1035033218Light · no testDURING EMERGENCY LIGHT TEST, AFT LT SHOWED LOAD FAULT, REPLACED SLIDE 2R AND CHECKED OK. (2010-00905)Dec 3, 2010 · N318US · Airbus A320211 · Emergency LightingSDR DALA1033783211Floor Panel · damagedDURING L CHECK FOUND FORWARD CARGO PIT FLOOR PANEL 131HF DAMAGED. REMOVED FLOOR PNL 131HF IAW AMM 53-22-14-020-050. FLOOR PNL 131HF FABRICATED IAW SRM 53-02-00 FIG 201. INSTALLED FLOOR PNL 131HF IAW AMM 53-22-14-400-001.Nov 26, 2010 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA1033773211Floor Panel · damagedDURING L-CHECK FOUND FORWARD CARGO PIT FLOOR PANEL 131AF DAMAGED. REMOVED FLOOR PNL 131AF IAW AMM 53-42-14-020-050. FABRICATED NEW FLOOR 131AF IAW SRM 53-02-00.Nov 24, 2010 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA1033373211Floor Panel · delaminatedDURING L-CHECK FOUND AFT PIT FLOOR PANEL 151LF IS DELAMINATED, 3 X 3 INCH AREA. REMOVED FLOOR PNL 151LF IAW AMM 53-42-14-020-050. RECEIVED NEW FLOOR PNL 151LF IAW SRM 53-02-00 FIG 201. INSTALLED FLOOR PNL 151LF IAW AMM 53-42-14-14-400-001.Nov 23, 2010 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA1033363211Floor Panel · delaminatedDURING L-CHECK FOUND AFT PIT FLOOR PANEL 151DF IS DELAMINATED, 5" X 3" AREA. REMOVED FLOOR PNL 151DF IAW AMM 53-42-14-020-050. RECEIVED NEW FLOOR PANEL 151DF ON TRAVELER NR T10/860791 MATERIAL NR A402 AB-60X144, BATCH NR 1910500 IAW SRM 53-02-00 FIG 209. INSTNov 23, 2010 · N311US · Airbus A320211 · Fuselage Floor PanelSDR CA101115015Windshield · cracked(CAN) DURING CRUISE, THE FLIGHT CREW ENCOUNTERED A CRACKED OUTER WINDSHIELD. THE FLIGHT CREW DIVERTED THE AIRCRAFT. EMERGENCY VEHICLES WERE CALLED OUT LOCALLY AS A PRECAUTION. THE FLIGHT CREW DID NOT DECLARE AN EMERGENCY.Nov 15, 2010 · Airbus A320211 · Flight Compartment WindowsSDR DALA1031043210Slat · gougedDURING L-CHECK FOUND GOUGE IN NR 2 SLAT INBOARD TRAILING EDGE IN 4 LOCATIONS. REPAIRED PER SRM 51-21-11, SRM 57-43-21 FIGURE 204 SHEET 2.Nov 10, 2010 · N310NW · Airbus A320211 · Leading Edge DevicesSDR DALA1031033210Profile · crackedDURING L CHECK FOUND CRACK IN FORWARD LEFT OVERWING EMERGENCY EXIT DOOR RIGHT LOAD TRANSMITTING PROFILE. REPAIRED PER SRM 51-42-11 & SRM 51-44-11.Nov 10, 2010 · N310NW · Airbus A320211 · Emergency ExitsSDR DALA1031023210Profile · crackedDURING L-CHECK FOUND CRACK IN FORWARD RIGHT OVERWING EMERGENCY EXIT DOOR LEFT LOAD TRANSMITTING PROFILE. REPAIRED PER SRM 51-42-11.Nov 10, 2010 · N310NW · Airbus A320211 · Emergency ExitsSDR DALA1031013210Profile · crackedDURING L-CHECK FOUND CRACK IN FORWARD LEFT OVERWING EMERGENCY EXIT DOOR LEFT LOAD TRANSMITTING PROFILE. REPAIRED PER SRM 51-42-11.Nov 10, 2010 · N310NW · Airbus A320211 · Emergency ExitsSDR DALA1030923210Floor Panel · delaminatedDURING L-CHECK FOUND DELAMINATION ON CARGO FLOOR PANEL 151GF. REPAIRED PER SRM 51-42-11, SRM 53-02-00 FIGURE 209 & AMM 53-42-14-420-050.Nov 9, 2010 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1030913210Floor Panel · delaminatedDURING L-CHECK FOUND DELAMINATION IN 3 AREAS ON CARGO FLOOR PANEL 151DF. REPAIRED PER SRM 51-42-11, SRM 53-02-00 FIGURE 209 & AMM 53-42-14-420-050.Nov 9, 2010 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1030903210Floor Panel · damagedDURING L-CHECK FOUND DAMAGE TO CARGO FLOOR PANEL 151LF. REPAIRED PER SRM 51-42-11, SRM 53-02-00 FIGURE 209 & AMM 53-42-14-420-050.Nov 9, 2010 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1030893210Profile · crackedDURING L-CHECK FOUND CRACK IN FORWARD RIGHT OVERWING EMERGENCY EXIT DOOR LOAD TRANSMITTING PROFILE. REPAIRED PER SRM 51-42-11, SRM 51-75-12.Nov 9, 2010 · N310NW · Airbus A320211 · Emergency ExitsSDR DALA1030863210Profile · crackedDURING L-CHECK FOUND CRACK IN AFT LEFT OVERWING EMERGENCY EXIT DOOR LEFT LOAD TRANSMITTING PROFILE. REPAIRED PER SRM 51-44-11, SRM 51-42-1 & SRM 51-75-12.Nov 8, 2010 · N310NW · Airbus A320211 · Emergency ExitsSDR DALA1030853210Profile · crackedDURING L-CHECK FOUND CRACK IN AFT RT OVERWING EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE. REPAIRED IAW SRM 51-44-11, SRM 51-42-1 & SRM 51-75-12.Nov 8, 2010 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1030843210Profile · crackedDURING L-CHECK FOUND CRACK IN AFT RT OVERWING EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE. REPAIRED IAW SRM 51-44-11, SRM 51-42-1 & SRM 51-75-12.Nov 8, 2010 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1030833210Profile · crackedDURING L-CHECK FOUND CRACK IN AFT LEFT OVERWING EMERGENCY EXIT DOOR RIGHT LOAD TRANSMITTING PROFILE. REPAIRED PER SRM 51-44-11, SRM 51-42-1 & SRM 51-75-12.Nov 8, 2010 · N310NW · Airbus A320211 · Emergency ExitsSDR DALA1030533220Slide · defectiveDURING EMERGENCY LIGHT TEST, AFT LEFT SHOWED LOAD FAULT. REPLACED SLIDE 2L AND CHECKED OK. (2010-00839)Nov 3, 2010 · N320US · Airbus A320211 · Escape SlideSDR DALA1030393220Wire · damagedDURING EMERGENCY LIGHT TEST, SEAT 2AB PATH LIGHTS WERE INOP. REPAIRED WIRING SPLICE AND CHECKED OK. (2010-00836)Nov 2, 2010 · N320US · Airbus A320211 · Emergency LightingSDR CA101102003Computer · malfunctioned(CAN) THE FLIGHT CREW RECEIVED A BLUE AND GREEN HYDRAULIC OVERHEAT MESSAGE, APPROXIMATELY 10 FEET FROM THE GATE IN CUN. THE AIRCRAFT WAS TOWED THE REMAINING DISTANCE TO THE GATE. FOUND SDAC 1 AT FAULT, FAULT CLEARED WITH INTERCHANGING SDACS. CHANGED SDAC 1 Oct 30, 2010 · Airbus A320211 · Central WarningSDR CA101018008Unknown · odorCABIN CREW REPORTED A STRONG ELECTRICAL ODOR IN THE AFT CABIN BETWEEN THE AFT LAVS. WHEN THE GALLEY POWER IN THE OVERHEAD PANEL WAS TURNED OFF THE ODOR WENT AWAY.Oct 17, 2010 · Airbus A320211 · Air Distribution SystemSDR CA101018007Pump · false indicationAPPROX 1 HR BEFORE ARRIVAL THE CREW REPORTED A LOSS OF THE BLUE HYD SYS. IN FLT ECAM MESSAGE HYD B ELEC PUMP LO PR. TURNED ELEC PUMP BACK ON FOR FINAL. APPEARED TO OPERATE NORMALLY BLUE HYD SYS AND QUANTITY CHECK NORMAL. NO FAULT OR LEAK FOUND IAW TASK 29-Oct 17, 2010 · Airbus A320211 · Hydraulic Pump (Electric/Engine), MainSDR DALA1027313222Skin · corrodedDURING L-CHECK FOUND CORROSION ON SKIN BETWEEN FR 20 - FR 21 STRINGER 44. REPAIRED PER ERA 4844923-14.Oct 16, 2010 · N322US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA1124723222Skin · corrodedFUSELAGE LOWER SKIN FR 20/21 STR 44 CORROSION REPAIR PER ERA484923-14 REPAIR PER SECTION I IS TIME LIMITED FOR DAMAGE TOLERANCE ANLYSIS. ASSOCIATED ER/A 13-484923 ADDED FOR AC 3222 ERA 484923-14 HAS BEEN REVISED TO REV A. SECTION II HAS BEEN DELETED. SECTIOOct 14, 2010 · N322US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA1027023217Socket · defectiveDURING A NON ROUTINE CHECK, FOUND ONE OF TWO OF THE 1B EMERGENCY PATH LIGHT INOPERATIVE. MAINT REPLACED SEAT LIGHT SOCKET AND FUNCTIONAL CHECK WAS NORMAL. A/C RETURNED TO SERVICE. (2010-00803)Oct 14, 2010 · N317US · Airbus A320211 · Emergency LightingSDR DALA1026683222Floor Panel · delaminatedDURING L-CHECK FOUND DELAMINATION ON FORWARD CARGO FLOOR PANEL 131AF. REPLACED FLOOR PANEL PER DWG 3D2537705 & AMM 53-22-14-400-001.Oct 13, 2010 · N322US · Airbus A320211 · Fuselage Floor PanelSDR DALA1026673222Floor Panel · delaminatedDURING L-CHECK FOUND DELAMINATION ON FORWARD CARGO FLOOR PANEL 131HF. REPLACED FLOOR PANEL PER DWG 3D2577705 & AMM 53-22-14-400-001.Oct 13, 2010 · N322US · Airbus A320211 · Fuselage Floor PanelSDR DALA1026383222Floor Panel · deformedDURING L-CHECK FOUND FWD CARGO FLOOR PANEL 131EF DEFORMED, PUNCTURED AND PREVIOUS REPAIR. REPLACED FLOOR PANEL IAW AMM 52-22-14-000-001 & DWG 3D25-37705.Oct 13, 2010 · N322US · Airbus A320211 · Fuselage Floor PanelSDR DALA1026373222Floor Panel · damagedDURING L-CHECK FOUND AFT CARGO FLOOR PANEL 151 DF HAD UPPER SURFACE EXPOSED HONEYCOMB. REPLACED FLOOR PANEL IAW DWG 3D25-37705 & AMM 53-42-14-400-001.Oct 13, 2010 · N322US · Airbus A320211 · Fuselage Floor PanelSDR CA101008001Hose · leakingAFTER DEPARTURE, DURING THE INITIAL CLIMB, THE ACFT GREEN HYD SYS FAILED. THE QRH WAS FOLLOWED AND AN EMERGENCY WAS DECLARED WITH ATC. THE FLIGHT RETURNED TO POINT OF DEPARTURE WHERE AN OVERWEIGHT LANDING OF 69.0 KGS WAS CARRIED OUT WITHOUT FURTHER INCIDENT. Oct 7, 2010 · Airbus A320211 · Hydraulic System, MainSDR DALA1025943223Wire Harness · disconnectedDURING A NON-ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 19 INOPERATIVE. MAINT RECONNECTED HARNESS AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Oct 7, 2010 · N323US · Airbus A320211 · Light System WiringSDR DALA1025773217Wire · brokenDURING A NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT ROWS 11C, 16C, 17C AND 22C, INOPERATIVE. MX REPAIRED A BROKEN WIRE IN CONNECTOR PLUG AND PERFORMED FUNCTIONAL CHECK. CHECK WAS NORMAL.Oct 6, 2010 · N317US · Airbus A320211 · Light System WiringSDR CA101004005Control Unit · malfunctionedTHE ACFT WAS UNABLE TO FULLY EXTEND THE FLAPS FOR INITIAL APPROACH ON RUNWAY 28R. THE FLIGHT CREW ADVISED OF A MISSED APPROACH AND SET UP FOR ANOTHER ARRIVAL. ON THE NEXT APPROACH, THE FLAPS EXTENDED TO A POSITION BETWEEN THE 1 AND 2 SETTING. THE FLIGHT LANDOct 2, 2010 · Airbus A320211 · Trailing Edge Flap Control SystemSDR CA101019014Transceiver · failedFLIGHT DEPARTED, APPROX 55 MINUTES INTO FLIGHT, AND CLIMBING FL 300 - 340, SOME VISIBLE SMOKE WAS NOTICED ENTERING THE FLIGHT DECK. THE SMOKE APPEARED TO BE COMING FROM THE VICINITY OF THE F/O RT SIDE KNEE (PEDASTAL PANEL). NO ACFT SYS MALFUNCTIONS WERE NOTICOct 1, 2010 · Airbus A320211 · Weather Radar SystemSDR CA100930001Actuator · leakingAPPROX 45 MINUTES TO DESTINATION THE CREW REPORTED GREEN HYD LOW PRESSURE INDICATION AND DECLARED AN EMERGENCY.Sep 29, 2010 · Airbus A320211 · Hydraulic System, MainSDR CA100928011Engine · overtempPRIOR TO THRUST REDUCTION ALTITUDE, ENG NR 2 EGT EXCEEDED NORMAL LIMITS. EGT HIT 902 DEGREES FOR 2 SECONDS PRIOR TO SETTING CLIMB THRUST.Sep 28, 2010 · Airbus A320211 · Engine (Turbine/Turboprop)SDR DALA1021643222A/C Pack · malfunctionedENROUTE, CREW RECEIVED AN ECAM "AIR PACK 2 FAULT" WITH PACK 1 ALREADY ON MEL, FOLLOWED QRH PROCEDURES DONNED MASK AND DECLARED AN EMERGENCY FOR RAPID DESCENT TO 10,000 FT. DURING DESCENT PACK 2 RECOVERED & CABIN ALTITUDE HAD REACHED 7,000, PASSENGER MASKS DID Sep 4, 2010 · N322US · Airbus A320211 · Cabin Cooling SystemSDR DALA1021033210Floorboard · damagedFOUND FWD CARGO FLOORBOARDS DAMAGED BEYOND SRM LIMITS. R & R CARGO FLOORBOARDS 131AE AND 131EG IAW AMM 53-22-14.Sep 2, 2010 · N310NW · Airbus A320211 · Fuselage Floor Panel
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