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 CA160210005Fire Warning · false activation(CAN) NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING FLIGHT FOR ABOUT 10 SEC. PREVIOUS FLIGHT HAD SAME PROBLEM AND WAS CLEARED BY MAINTENANCE. AFTER CONSULTATION WITH DUTY PILOT FLIGHT CONTINUED. FIRE WARNING LIGHT CAME ON AGAIN AND FLIGHT WAS DIVERTED. Feb 10, 2016 · Airbus A320211 · Fire DetectionSDR DALA2016012900831Power Supply · no testEMERGENCY LIGHT CHECK FAILS, EMERGENCY RT UNIT. REPLACED RT EPSU, W/O BATTERY.Jan 28, 2016 · N330NW · Airbus A320211 · Emergency LightingSDR DALA2016012200731Skin · corrodedCORROSION ON EXTERNAL SKIN AT LOWER FUSELAGE ON FRAME 71 BETWEEN STR 28R TO STR 30R. PERFORMED TIME LIMITED REPAIR ON EXTERNAL SKIN AT LOWER FUSELAGE ON FRAME 71 BETWEEN STR 28R TO STR 30R IAW ER/A 542037-14, REV ORIGINAL.Jan 21, 2016 · N333NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016111808969Stringer · corrodedCORROSION ON STRINGER 44 BETWEEN FRAMES 56 AND 59, REMOVED CORROSION AND INSTALLED REPAIR IAW SRM.Jan 19, 2016 · N318US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016012100723Stringer · corrodedFOUND EVEDENCE OF CORROSION IN MULTIPLE LOCATIONS ON S42R BETWEEN FRAMES 54 & 58, REMOVED AREAS OF CORROSION REPAIR ON S42R BETWEEN FRAMES 54 & 58 IAW SRM 53-00-13 F 202.Jan 19, 2016 · N318US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016111808971Frame · corrodedCORROSION ON FRAME 43L AT FRAME 55. REPAIR THE FRAME.Jan 16, 2016 · N318US · Airbus A320211 · Fuselage Main, FrameSDR DALA2016011900504Stringer · corrodedCORROSION ON STRINGER 42L BETWEEN FRAMES 56 AND 57. REMOVED STR 42L BETWEEN FRAMES 55 AND 58. FABRICATED AND INSTALLED STRINGER SECTION AND COUPLING/SPLICE IAW SRM 53-00-13.Jan 16, 2016 · N318US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016011900483Stringer · corrodedFOUND CORROSION ON STRINGER 43L BETWEEN FRAMES 56 AND 57. REMOVED STR 43L BETWEEN FRAME 55 TO 59. INSTALLED NEW STRINGER SECTION IAW SRM 53-00-13.Jan 16, 2016 · N318US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016011300262Connector · disconnectedSEAT ROW 24 EMERGENCY LIGHT INOPERATIVE. RECONNECTED LIGHT ASSY.Jan 12, 2016 · N316US · Airbus A320211 · Light System WiringSDR DALA2016011200260Stringer Splice · corrodedCORROSION ON STR 43L SPLICE REPAIR COUPLING BETWEEN FRAMES 56 AND 57. REPLACED STR 43L SPLICE IAW SRM 53-00-13, FIG 201.Jan 11, 2016 · N316US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016011200259Stringer · corrodedCORROSION ON STR 42L BETWEEN FRAMES 56 AND 57. REPLACED STR SPLICE 42L IAW SRM 53-00-13, FIG 201.Jan 11, 2016 · N316US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR CA160108009Gcu · failed(CAN) GENERATOR 1 FAILED. APU WONT START. PAN PAN DECLARED WITH ATC DUE SINGLE ELECTRICAL SOURCE. GCU NR 1 REPLACED IAW AMM 24-22-34 PB 401,TEST OK.Jan 8, 2016 · Airbus A320211 · AC RegulatorSDR DALA2016091606675Stringer · damagedPERFORMED PERMANENT REPAIR ON STRINGER 43L BTW FR 55 TO FR56 IN AFT CARGO COMPARTMENT AS PER SRM 53-00-13 FIGURE 201, ER/A 542785-14AD REV. ORIGINAL, AND ER/A 549949-14 REV.A,Jan 7, 2016 · N324US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016010800117Stringer · corrodedFOUND CORROSION ON STRINGERS 43L AND 42L BETWEEN BS 56 AND BS 57, REMOVED CORROSION FROM STRINGERS 42L AND 43L BETWEEN FRAMES 56 AND 57 IAW SRM 51-73-00, 917648. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-13 COMPLIED WITH ERA 542785-14.Jan 7, 2016 · N324US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR CA160107002Accumulator · defective(CAN) AFTER PUSH BACK AND WHILE TAXIING FOR DEPARTURE, FLIGHT EXPERIENCED A BLUE HYDRAULIC SYS LOW PRESSURE. IN CONSULTATION WITH MAINTENANCE CONTROL, THE FLIGHT RETURNED TO THE GATE. RESOLUTION BLUE HYD SYS ACCUMULATOR REPLACED IAW AMM 29-12-42 BP401. FUNCTJan 6, 2016 · Airbus A320211 · Hydraulic Power Accumulator, MainSDR CA160105003Thrust Reverser · malfunctioned(CAN) CREW CALLED DX 1HR AFTER ARRIVAL. PATCHED TO MOC TO DISCUSS ISSUE FLT HAD REVERSER 2 PRESSURIZE BROUGHT ENGINE 2 BACK TO IDLE AND RETURNED TO DEPARTURE AIRPORT DECLARED AN EMERGENCY.Jan 4, 2016 · Airbus A320211 · Engine Thrust ReverserSDR DALA2016010700116Wire · damagedSEAT ROW 24 EMERGENCY LIGHT INOPERATIVE, REPAIRED WIRING UNDER SEAT.Jan 2, 2016 · N328NW · Airbus A320211 · Light System WiringSDR DALA2016010200001Power Supply · failedDURING S/C FOUND FWD EMERGENCY POWER SUPPLY UNIT FAULTING FIN10WL, REPLACED EPSU, W/O BATTERY 10WL.Jan 1, 2016 · N347NW · Airbus A320211 · Emergency LightingSDR DALA2016010500080Connector · damagedSEAT 1B FWD EMEGENCY LIGHT, WHITE, INOPERATIVE. REPLACED PIG TAIL AT SEAT 1B.Dec 31, 2015 · N319US · Airbus A320211 · Light System WiringSDR CA151230004Control Servo · leaking(CAN) ACFT DECLARED AN EMERGENCY DUE TO THE LOSS OF THE GREEN HYD SYS. ACFT DID REQUIRE A TOW OFF THE RUNWAY AS THEY WERE UNABLE TO STEER ACFT. RESOLUTION FOUND GREEN HYD SYS RUDDER SERVO CONTROL LEAKING. REPLACED GREEN SYSTEM RUDDER SERVO CONTROL IAW AMM 2Dec 30, 2015 · Airbus A320211 · Rudder ActuatorSDR DALA2015123007799Wire · brokenPAX SEAT EMERGENCY LIGHT INOP, FOUND BROKEN WIRE ON SEAT BOTTOM HARNESS. REPAIRED WIRE.Dec 30, 2015 · N331NW · Airbus A320211 · Light System WiringSDR CA151229022Compressor · stalled(CAN) AT APPROXIMATELY 10KTS ON THE TAKEOFF ROLL THE CREW REPORTED 3 COMPRESSOR STALLS FROM THE LT ENGINE. A LOW SPEED REJECT WAS CARRIED OUT AND THE ACFT RETURNED TO THE GATE FOR INSPECTION. THE ACFT HAD BEEN DEICED AND SNOW WAS STILL FALLING. RESOLUTION TDec 29, 2015 · Airbus A320211 · Turbine Engine Compressor SectionSDR DALA2015121407619Skin · corrodedCORROSION ON INNER SKIN SURFACE OTBD OF STR S42L BETWEEN FRAMES 56-57, REMOVAL OF CORROSION AND BLEND OUT AT INNER SKIN OTBD OF STR 42L BETWEEN FRAMES 56 AND 57 IAW PRI 542225-14, REV STEP 1 TREATED BARE METAL AREAS AND PRIMERED, REF PRI, ERA 542225-14, REV 2.Dec 13, 2015 · N319US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015121407618Stringer · corrodedCORROSION ON STR 42L BETWEEN FRAMES 56-57, REMOVED STR 42L BETWEEN FRAMES 57 AND 58 FABRICATED NEW STRINGER AND COUPLINGS IAW SRM 53-00-13, FIG 201 J.Dec 13, 2015 · N319US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2015121407617Stringer · corrodedCORROSION ON STR 43L BETWEEN FRAMES 55 TO 58, INSTALLED NEW STRINGER 43L, PN D53479420202.Dec 13, 2015 · N319US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2015121407621Wire · brokenSEAT 26C EMERGENCY LIGHT INOPERATIVE. FOUND A WIRE BROKEN, REPLACED LIGHT SOCKET AND WIRING HARNESS.Dec 10, 2015 · N320US · Airbus A320211 · Light System WiringSDR DALA2015121007615Shear Tie · corrodedCORROSION ON CLEAT FRAME 28 LT BETWEEN STR 40/41 MEASURES APPROXIMATELY, L=0.200, W=0.120, D=0.002 IN FWD CARGO COMPARTMENT, REPLACED CLEAT LOCATED ON FR 28 BETWEEN STR 40L TO STR 41L IAW SRM 51-72-11 AND DWG D53231626. MEASURES OF CORROSION ARE L=0.200", W=Dec 10, 2015 · N329NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2015121007614Floor Support · corrodedCORROSION ON FLOOR SUPPORT, -Y465 BETWEEN FRAMES 64 TO 67+10. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534720000.Dec 10, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015121007613Shear Tie · corrodedCORROSION ON SHEAR TIE FRAME 30, BETWEEN STRINGERS 40-41L. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG D53231626.Dec 9, 2015 · N329NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2015120907502Door Sill · corrodedCORROSION ON LOWER SILL STR 23R AT AFT GALLEY AREA L=0.600", W=0.400", D=0.006", REPLACED LOWER SILL, STR 23R AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480505, D53480076, D53470150 MEASURES OF REWORKED AREA ARE: L=1.335", W=1.198", D=0.098".Dec 8, 2015 · N364NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015120807506Sign · malfunctionedRED EMERGENCY EXIT SIGNS AT THE AFR CABIN AND BY DOORS 2L AND 2R WILL NOT ILLUMINATE WHEN THE LANDING GEAR IS EXTENDED WITH THE, NO SMOKING SWITCH POSITIONED TO AUTO, REPLACED EPSU.Dec 4, 2015 · N319US · Airbus A320211 · Emergency LightingSDR DALA2015120207399Shear Tie · corrodedCORROSION ON CLEAT FRAME 31 LT BETWEEN STR 40 - 41L. REPLACED THE CLEAT IAW SRM 51-72-11 AND DWGS D53231626 AND D53231617.Dec 1, 2015 · N329NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2015120207398Shear Tie · corrodedCORROSION ON CLEAT FRAME 33, LT BETWEEN STR 42-43L. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231626 AND D53231535.Dec 1, 2015 · N329NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2015120207397Hinge Fitting · crackedCRACK AT FORWARD KEELBEAM HINGE FITTING ON RETRACTION ACTUATOR LEVEL ON RT MLG L=1.235", REPLACED FORWARD KEELBEAM HINGE FITTING ON RETRACTION ACTUATOR LEVEL ON RT MLG IAW SRM 51-72-11 AND DWG D53370600.Dec 1, 2015 · N329NW · Airbus A320211 · Fuselage, Door HingeSDR DALA2015120107306Battery Pack · inoperativeEMERGENCY EXIT LIGHTS INOPERATIVE AFT, REPLACED EMERGENCY LIGHT BATTERY ABOVE L2 DOOR.Nov 29, 2015 · N319US · Airbus A320211 · Emergency LightingSDR DALA2015113007304Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK -Y1292, FRAME 47 TO 64 EVALUATED AND FOUND OUT OF LIMITS, MEASURE OF REWORKED AREA ARE: L=5.272", W=0.707", D=0.054". REPLACED SEAT TRACK 1292 LOCATED BETWEEN FRAME 47 TO FRAME 64 IN PASSENGER CABIN IAW SRM 51-72-11 ANDNov 29, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015112907246Floor Support · corrodedCORROSION FWD GALLEY AREA ON FLOOR SUPPORT -Y254 BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND ERA: 541388-14, REV ORIGINAL AND DWGS D53112821200.Nov 28, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015112907245Stringer · corrodedCORROSION LOWER FUSELAGE ON STRINGER 25R BETWEEN FRAME 65 TO FRAME 66. , REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53480505.Nov 28, 2015 · N329NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2015120107305Battery Pack · inoperativeINTERIOR AFT LEFT BATTERY, DURING SERVICE CHECK ON F/A PANEL, REPLACED EPSU 13WL BATTERY.Nov 27, 2015 · N314US · Airbus A320211 · Emergency LightingSDR DALA2015112707244Seat Track · corrodedCORROSION ON SEAT TRACK +Y765, FRAMES 47 TO 64 FOUND OUT OF LIMITS IN PASSENGER CABIN. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Nov 26, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015112707243Fitting · corrodedCORROSION ON CORNER FITTING FRAME 16 AT FWD GALLEY AREA ON STR 23L, REPLACED CORNER FITTING ON FRAME 16 AT FWD GALLEY AREA LEVEL STR 23L IAW SRM 51-72-11 AND DWG D53112109. MEASURES OF CORROSION ARE: L=0.722", W=0.123", D=0.040".Nov 26, 2015 · N329NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2016111708956Floor Panel · corrodedCORROSION ALL PLUGS ON FLOOR PANEL 222CF AT FWD GALLEY AREA. REPLACED THE FLOOR PANEL.Nov 24, 2015 · N329NW · Airbus A320211 · Fuselage Floor PanelSDR DALA2015112507218Floor Support · corrodedAFT GALLEY AREA CORROSION ON LOWER SILL BETWEEN FRAME 66 TO FRAME 68 AT LEVEL STR 23L MEASURES APPROXIMATELY L:0.120", W 0.100", 0.002". REPLACED LOWER SILL LT LOCATED BETWEEN FRAME 66 TO FRAME 68 AT LEVEL STR 23L AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D534Nov 24, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015112307217Floor Support · corrodedAFT GALLEY AREA CORROSION ON FLOORBEAM 1732 BETWEEN FRAME 65 AND FRAME 66 MEASURES APPROXIMATELY L:0.750", W:0.300", D:0.002". REPLACED FLOORBEAM 1732 BETWEEN FRAME 65 AND FRAME 66 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53470150. MEASURES OF CORROSION Nov 22, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015112307216Floor Support · corrodedFWD GALLEY AREA CORROSION ON FLOORBEAM 1292 BETWEEN FRAME 12 TO FRAME 24 MEASURES APPROXIMATELY L:0.860", W:0.480", D:0.003". REPLACED SEAT TRACK 1292 AND FASTENER LOCATED BETWEEN FRAME 12 TO FRAME 24 FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53110984, D5311Nov 22, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015112207215Floor Support · corrodedAFT GALLEY AREA CORROSION ON FLOORBEAM 1162 BETWEEN FRAME 67+15" TO FRAME 69, MEASURES APPROXIMATELY L=0.990", W=0.620", D=0.003". REPLACED FLOORBEAM 1162, LOCATED BETWEEN FRAME 67+15" TO FRAME 69 AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000. MEASURE OFNov 21, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015112207214Floor Support · corrodedAFT GALLEY AREA CORROSION ON FLOORBEAM +Y1225 BETWEEN FRAME 66+5" TO FRAME 67+15" MEASURES APPROX L=0.360", W=0.190", D=0.002". REPLACED FLOORBEAM 1225 LOCATED BETWEEN FRAME 66+5" TO FRAME 67+15" AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000, MEASURENov 21, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015112307219Power Supply · inoperativeEMERGENCY LIGHTS AT SEATS 11 THRU 14, 17, 18, 19, 21 THRU 26 INOPERATIVE. REPLACED EPSU.Nov 20, 2015 · N319US · Airbus A320211 · Emergency LightingSDR DALA2015112107213Seat Track · corrodedPASSENGER CABIN CORROSION ON SEAT TRACK 765, FRAMES 47 TO 64 EVALUATED AND FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Nov 20, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015112107212Seat Track · corrodedUPPER FLAGE IN PASSENGER CABIN CORROSION OUT LIMIT SEAT TRACK 1292, FRAME 36 TO 41 MEASURES ARE: FRAME 4 0+16', L: 5.164", W:0.348', D:0.047". REPLACED SEAT TRACK +Y1292 AND FASTENERS LOCATED FRAME 36 TO FRAME 41 IAW SRM 51-72-11 AND DWG D53370500.Nov 20, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
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