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 DALA2017011600419Pin · out of positionEPSU COMM EMER L SHOWN AFTER TEST OF EMER LIGHTS. INSPECTED TB 7225VT AND FOUND PIN PULLED OUT OF 6G POSITION, RESECURED SAME.Jan 15, 2017 · N330NW · Airbus A320211 · Emergency LightingSDR DALA2017011100269Power Supply · inoperativeDURING EMERGENCY LIGHT SYSTEM TEST, FOUND RIGHT POWER SUPPLY UNIT INOPERATIVE. REPLACED THE BATTERY PACK AND POWER SUPPLY.Jan 10, 2017 · N310NW · Airbus A320211 · Emergency LightingSDR DALA2017010800181Box Beam · crackedLEFT SIDE BOX BEAM UPPER FLANGE CRACKED. REPAIRED IAW AMDS 5310-01450-02.Jan 7, 2017 · N318US · Airbus A320211 · Fuselage Main, StructureSDR DALA2017010800183Light · broken11D EMERGENCY LIGHT ASSY FOUND BROKEN, REPLACED THE EMERGENCY LIGHT .Jan 4, 2017 · N331NW · Airbus A320211 · Emergency LightingSDR DALA2017010300152Skin · dentedDENT ON EXTERNAL SKIN LOC AT FR 79 BTW STR 4L TO STR 5L ON UPPER FUSELAGE, PERFORMED REPAIR ON EXTERNAL SKIN LOCATED AT FR 79 BTW STRINGER 4L TO 5L ON UPPER FUSELAGE AS PER SRM 53-51-11 PARAGRAPH 5B FIGURE 203.Dec 31, 2016 · N314US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016123110192Box Beam · crackedCRACK INDICATION IN AFT HOLE OF SIDE BOX BEAM UPPER FLANGE, ON FRAME 43 LT SIDE. CRACK DIRECTION: FWD ON CENTER WING BOX, REPLACED PRESSURE PLATE LOC ON FR 43 LT SIDE AS PER SRM 51-72-11 AND JOB CARD 5310-014-50-02-DEDec 29, 2016 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016123010173Box Beam · crackedCRACK INDICATION IN CENTER HOLE OF SIDE BOX BEAM UPPER FLANGE, ON FRAME 43. THE BOX BEAM WAS REPAIRED IAW SB A320-53-1251 REV 1.Dec 28, 2016 · N314US · Airbus A320211 · Fuselage Main, StructureSDR DALA2016122910170Box Beam · crackedCRACK INDICATION IN CENTER HOLE OF SIDE BOX BEAM UPPER FLANGE, ON FRAME 43 L/H SIDE. CRACK DIRECTION: AFT. ON CENTER WING BOX, REPAIR PER AMDS 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1Dec 28, 2016 · N314US · Airbus A320211 · Fuselage Main, StructureSDR DALA2019010900148Structure · crackedCRACK INDICATION FOUND AT FR16 RHS AT LEVEL OF DOOR STOP NR 7, IN HOLE NR 6 PERFORMED PERMANENT REPAIR ON FR16 RHS DOCUMENTED ON NRC 2/200 W/O 2018-296/1 AS PER ERA 55158014 AD REV.A.Dec 26, 2016 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016122610070Lamp · inoperativeRT AFT OVERWING HANDLE EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP.Dec 24, 2016 · N310NW · Airbus A320211 · Emergency LightingSDR DALA2016122610069Lamp · inoperativeRT FWD EMERGENCY OVERWING HANDLE EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP.Dec 24, 2016 · N310NW · Airbus A320211 · Emergency LightingSDR DALA2016122110166Skin · damagedSCRATCH ON EXTERNAL SKIN STATIC PORT R/H SIDE BTW FR23 TO FR24 BTW STRG29 TO STRG32 AT LOWER FUSELAGE, PERFORMED PERMANENT REPAIR AT SCRATCHAREA AS PER A320 SRM 53-11-11, PAR 5.A(1)B. SOLUTION 2Dec 20, 2016 · N328NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016122210072Compressor · seizedHAD AN ACRID ELECTRICAL ODOR IN THE COCKPIT. REPLACED THE WATER SYSTEM AIR COMPRESSOR. FOUND SEIZED. AIRCRAFT RETURNED TO SERVICE.Dec 20, 2016 · N315US · Airbus A320211 · Air Supply (Water Pressure System)SDR DALA2016121809957Skin · dentedDENT ON UPPER SKIN AT FRAME 81+13 BETWEEN STRINGERS 1 AND 2R , PERFORMED A PERMANENT REPAIR IAW SRM 53-51-11 PARAGRAPH 5.B FIGURE 203.Dec 17, 2016 · N328NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016121509959Connector · unsecureEMERGENCY EXIT SIGN R1 DOOR INOPERATIVE, SECURED THE CONNECTOR.Dec 13, 2016 · N326US · Airbus A320211 · Light System WiringSDR DALA2016121209829Skin · damagedEVIDENCE REWORK PASSENGER CREW DOOR 832 EXTERNAL SKIN LOCATED 15" FROM LOWER EDGE AND 30.5" FROM FWD EDGE AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON PASSENGER CREW DOOR 832 EXTERNAL SKIN LOCATED 15" FROM LOWER EDGE AND 30.5 FROM FWD EDGE AT AFT GALLEY ADec 11, 2016 · N310NW · Airbus A320211 · Passenger/Crew DoorsSDR DALA2016120709694Frame · crackedFRAME 16 WAS FOUND CRACKED, PERFORMED TEMPORARY REPAIR IAW ER/A 551555-14AD REVISION ORIGINAL.Dec 6, 2016 · N313US · Airbus A320211 · Fuselage Main, FrameSDR DALA2016120509633Access Panel · corrodedCORROSION ON ACCESS PANEL 640JB ON RT WING. REPLACED ACCESS PANEL 640JB ON RT WINGDec 4, 2016 · N310NW · Airbus A320211 · Wing, Plate/SkinSDR DALA2016120509632Access Panel · corrodedCORROSION ON ACCESS PANEL 540PB FUEL TANK ON LT WING. REPLACED ACCESS PANEL 540PB ON LT WING.Dec 4, 2016 · N310NW · Airbus A320211 · Wing, Plate/SkinSDR DALA2016120509631Stringer · corrodedCORROSION ON STRINGER 31R IN AFT CARGO COMPARTMENT BETWEEN FRAME 65 TO FRAME 66. REPLACED STRINGER 31R IN AFT CARGO COMPARTMENT FROM FRAME 64 TO FRAME 67 AS PER SRM 51-72-11 AND DWG D53480020.Dec 4, 2016 · N313US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016120409628Skin · damagedLIGHTNING STRIKE DAMAGE, FWD INBD MOUNT HOLE FOR FWD WATER DRAIN MAST. REMOVED DAMAGE PER SRM 53-00-11 FIG 231 SHT 3. REPAIR PER ERA 553223-14AD REV ORIG SECT I.Dec 3, 2016 · N327NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016120409627Stringer · corrodedCORROSION ON STRINGER 25R IN AFT CARGO COMPARTMENT BETWEEN FRAME 65 TO FRAME 66. REPLACED STRINGER 25R IN AFT CARGO COMPARTMENT BETWEEN FR 64 TO FR 67 AS PER SRM 51-72-11 AND DRAWING D53480020.Dec 3, 2016 · N313US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016120209624Beam · crackedLT SIDE BOX FR 43, BEAM CRACKED AT AFT AND MIDDLE HOLES. SEE NR FOR ADDITIONAL INFORMATION 002-0001:5310-01450-01/003 00017 REPAIR WAS ACCOMPLISHED PER AMDS 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.Dec 2, 2016 · N326US · Airbus A320211 · Fuselage Main, StructureSDR DALA2016120209623Skin · damagedEXISTING REWORK ON EXTERNAL SKIN AT LOWER FUSELAGE TO FRAME 31+17" BETWEEN STRINGER 42R TO STRINGER 43R, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BTW FR31TO FR32 AND BTW STR41R TO STR 44 AT LOWER FUSELAGE AS PER SRM 53-00-11 PARAGRAPH 4 W AND FIG 238.Dec 2, 2016 · N310NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016120209626Plate · crackedRT SIDE BOX FR 43 PLATE CRACKED AT FWD HOLE. SEE NR FOR ADDITIONAL INFORMATION 002-0001:5310-01450-01 002 REPLACED PLATE ACCOMPLISHED REPAIR PER AMDS 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.Dec 1, 2016 · N326US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016113009408Frame · corrodedCORROSION ON LOWER SILL FRAME 66 LT AT AFT GALLEY AREA, REPAIRED IAW SRM 53-41-14, PARAGRAPH. 5A FIGURE 201.Nov 29, 2016 · N375NC · Airbus A320211 · Fuselage Main, FrameSDR DALA2016112909407Frame · crackedCRACK ON LATERAL FWD SEGMENT FRAME ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN, REPLACED LATERAL FWD SEGMENT FRAME IAW SRM 51-72-11 AND DRAWING D52279010Nov 28, 2016 · N313US · Airbus A320211 · Fuselage Main, StructureSDR DALA2016112509242Frame · crackedFR43 LT SIDE CENTER HOLE CRACKED IN CENTER LAYER BEAM. REPAIRED FR43 LT SIDE BEAM PER 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.Nov 23, 2016 · N333NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2016112409240Plate · crackedFR43 LT SIDE AFT HOLE CRACKED IN UPPER LAYER PRESS PLATE AND CENTER LAYER BEAM. REMOVED AND REPLACED LT PRESSURE PLATE AND REPAIRED BEAM. REF; 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.Nov 23, 2016 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016112209237Slide · unserviceableDURING SERVICE CHECK EPSU CHECK -"EXT ESPU AFT L" ON FAP, REPLACED RT SLIDE.Nov 19, 2016 · N320US · Airbus A320211 · Escape SlideSDR DALA2016111508909Wire · out of positionEMERGENCY EXIT SIGNS INOPERATIVE. FOUND WIRES AT AREA LIGHT AND EXIT SIGN SWAPPED, CORRECTED.Nov 14, 2016 · N332NW · Airbus A320211 · Light System WiringSDR DALA2016111408765Light · inoperativeMULTIPLE BULBS INOP IN MOST LARGE EMERGENCY EXIT SIGNS, RE-LAMP.Nov 14, 2016 · N316US · Airbus A320211 · Emergency LightingSDR DALA2016111408770Connector · looseON CLIMBOUT FLT ATT REPORTED A MUSTY SMELL WITH HEAT IN LAST 4 ROWS OF CABIN. SHUT OFF PAX SYS/PED PWR AND SMELL WENT AWAY, FOUND CONNECTOR J40 LOOSE AT RECEPTACLE AT FLOOR TO BULKHEAD. RESECURED.Nov 10, 2016 · N326US · Airbus A320211 · Electrical Power System WiringSDR DALA2016111008531Light · disconnected14L EMERGENCY LIGHT INOPERATIVE, CONNECTED THE LIGHTNov 9, 2016 · N327NW · Airbus A320211 · Emergency LightingSDR DALA2016110108092Box Beam · damagedSIDE BOX BEAM AT FRAME 43 DAMAGED, REPAIRED IAW AMDS WC 5310-01450-02, IAW SB A320-53-1251 REV 1Oct 31, 2016 · N317US · Airbus A320211 · Fuselage Main, StructureSDR DALA2016102807847Wire · brokenBROKEN EMERGENCY LIGHT WIRE, REPAIRED THE WIRE.Oct 28, 2016 · N315US · Airbus A320211 · Light System WiringSDR DALA2016102707849Light · damagedSEAT MOUNTED EMERGENCY LIGHT SEAT 21C DAMAGED, EMERGENCY LIGHT REPAIRED.Oct 26, 2016 · N318US · Airbus A320211 · Emergency LightingSDR DALA2016102507605Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y160 FROM FRAME 68 TO FRAME 70 AT AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Oct 24, 2016 · N331NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016102507604Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y160 FROM FRAMES 68 TO 70 AT AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53474250.Oct 24, 2016 · N331NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016102107445Web · dentedDENT ON WEB LOCATED ON FRAME 25 INTERNAL FLOOR STRUCTURE AT LEVEL OF CENTER LINE IN FWD CARGO COMPARTMENT. REPLACED WEB LOCATED ON FRAME 26 INTERNAL FLOOR STRUCTURE AT LEVEL OF CENTER LINE FWD CARGO COMPARTMENT AS PER SRM 51-72-11 AND DRAWING D53230808.Oct 20, 2016 · N331NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020121404088Skin · dentedON WALK AROUND PREFLIGHT F/O FOUND A DENT ON AIRCRAFT LEFT, AFT OF RADOME. RECTANGULAR IN SHAPE. BARE METAL SHOWING. CORRECTIVE ACTION: C/W TERMINATING ACTION, PER SRM 53-11-11-205-031. OK FOR SERVICE.Oct 16, 2016 · N333NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016101107228Box Beam · crackedACCOMPLISHED SIDE BOX BEAM UPPER FLANGE AT FR 43 BETWEEN STRINGERS 5 AND 7L OPEN HOLE ET IAW AMDS 5310-01450-01 AND NTM 51-10-01. AFT 2 REMOVED FASTENER HOLES HAVE CRACK INDICATIONS. REPAIRED IAW AMDS 5310-01450-02 AND ERA 551398-14AD REV ORIGINAL,Oct 10, 2016 · N312US · Airbus A320211 · Fuselage Main, StructureSDR DALA2016101107227Box Beam · crackedACCOMPLISHED SIDE BOX BEAM UPPER FLANGE AT FRAME 43 BETWEEN STRINGERS 5 AND 7R OPEN HOLE ET IAW AMDS 5310-01450-01 AND NTM 51-10-01. AFT 2 REMOVED FASTENER HOLES HAVE CRACK INDICATIONS, REPAIRED IAW AMDS 5310-01450-02 AND ERA 551398-14AD REV ORIGINAL,Oct 10, 2016 · N312US · Airbus A320211 · Fuselage Main, StructureSDR DALA2016101007225Skin · damagedSCRATCH ON EXTERNAL SKIN OF PASSENGER CREW DOOR FROM BEAM 2 TO BEAM 3 AND BETWEEN XP 820 TO XP 712 AT AFT GALLEY AREA RH SIDE, REPAIRED IAW ER/A 550213-14AD REV. ORIGINAL SECTION I AND PRI REV. 0 AND 1.Oct 9, 2016 · N332NW · Airbus A320211 · Passenger/Crew DoorsSDR DALA2016101007224Stringer · corrodedCORROSION ON STRINGER 43L FR 33+6 " IN FWD CARGO BAY. REPAIRED THE STRINGER IAW PRI 521412-14 REV. 1 AND ER/A 521412-14 REV B SECTION III.Oct 9, 2016 · N332NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016100607112Shear Tie · damagedELONGATED HOLE ON SHEAR TIE IN FWD CARGO COMPARTMENT ON FRAME 24A BETWEEN STRINGER 41R TO STRINGER 42R, REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DRAWING D53231586.Oct 5, 2016 · N332NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2016100507070Power Supply · inoperativeEMERGENCY LIGHT FWD L EPSU UNIT FAULT, REPLACED FWD LEFT EPSU 10WLOct 5, 2016 · N378NW · Airbus A320211 · Emergency LightingSDR DALA2016100207065Structure · corrodedCORROSION ON LOWER SILL BETWEEN FRAMES 67 TO 68. REPLACED LOWER SILL IAW SRM 51-72-11 AND DRAWING D53480020.Sep 30, 2016 · N332NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016092806958Floorbeam · corrodedCORROSION ON FLOORBEAM -Y1225 TO -Y1165 BETWEEN FRAME 66+5" TO FRAME 67+18" AT AFT GALLEY AREA. REPLACED FLOORBEAM -Y1165 BETWEEN FRAME 66+5" TO FRAME 67+18" AT AFT GALLEY AREA AS PER SRM 51-72-11 AND DRAWING D53172000. FLOORBEAM WAS OUT OF LIMITS AS PER SRMSep 27, 2016 · N332NW · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2016092706959Controller · faultyEMER PWR TEST OF LIGHTS FAULTING L2 DOOR. REPLACED EPSU CONTROLLER AT L2 DOOR.Sep 26, 2016 · N338NW · Airbus A320211 · Emergency Lighting
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