N344NW

Service difficulty reports · 198

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N344NW' AND registry_match = 'registration'
  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 DALA2015061203745Floor Support · brokenBROKEN FLOOR SUPPORT +Y254 AT FWD GALLEY AREA FROM FRAMES 24 TO 35. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53110900.Jun 11, 2015 · N344NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015060903645Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1292 AT FWD GALLEY AREA FROM FRAMES 12 - 24. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D531-12812.Jun 8, 2015 · N344NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015060903644Fitting · corrodedCORROSION ON CENTER FITTING AT AFT GALLEY AREA ON FRAME 66 AND STRINGER 23R. REPLACED CENTER FITTING AT AFT AREA GALLEY BETWEEN FRAME 66 TO FRAME 68 AT LEVEL STR 23R LOWER SILL AREA IAW SRM 51-72-11 AND DWG D53480505.Jun 8, 2015 · N344NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015060903643Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y765 AT FWD GALLEY AREA BETWEEN FRAMES 12 TO 24. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112089.Jun 8, 2015 · N344NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015060903642Fitting · corrodedCORROSION ON CORNER FITTING FRAME 20 AT FWD GALLEY AREA TO STR 23R, L=0.150", W=0.100", D=0.002", SSI 531189. REPLACED CORNER FITTING LOCATION ON FRAME 20 AT FWD GALLEY AREA TO STR 23R IAW SRM 51-72-11 AND DWG D53112225.Jun 8, 2015 · N344NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015060803616Fitting · corrodedCORROSION ON CORNER FITTING, FRAME 20 STRINGER 23L. REPLACED CORNER FITTING IAW SRM 51-72-11 AND DWG D53112225.Jun 7, 2015 · N344NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015060803615Fitting · crackedCRACKED FITTING FRAME 68 STRINGERS 24 - 25L AFT GALLEY AREA. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53470150.Jun 7, 2015 · N344NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015060803614Dummy Rail · corrodedCORROSION ON RAIL DUMMY -Y189 AT FWD GALLEY AREA FROM FRAMES 20 TO 23. REPLACED RAIL DUMMY IAW SRM 51-72-11 AND DWG D531-12834.Jun 7, 2015 · N344NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015060803613Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y254 AT FWD GALLEY AREA FROM FRAMES 12 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D531-12816.Jun 7, 2015 · N344NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015060803612Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y765 AT AFT GALLEY AREA FROM FRAMES 66+ 5 - 70. REPLACED THE FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D534 72000.Jun 7, 2015 · N344NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014103105861Stringer · corrodedFOUND STRINGER 42L BETWEEN FRAMES 56 AND 57 CORRODED. CUTOUT DAMAGED SECTION OF STRINGER 42L BETWEEN FRAMES 56 AND 57 IAW SRM 53-00-13, FIG 201. FABRICATED REPAIR IAW SRM 53-00-13, FIG 201.Oct 30, 2014 · N344NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2014103105860Skin · corrodedMAINTENANCE FOUND AREAS OF CORROSION COMMON TO STRINGERS 42 - 43L, AND THE UNDERLYING SKIN NEAR S42L. ALL DAMAGE IS FOUND BETWEEN FRAMES 56-57. THE STRINGERS WERE REMOVED/CUT FOR SUBSEQUENT SPLICE REPAIRS TO REMOVE THE DAMAGE AND TO GAIN ACCESS TO UNDERLYINGOct 30, 2014 · N344NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA1504603244None · noneREFUEL APERTURE/WING ELECTRONIC BOND IDENTIFIED AS A MAJOR IAW AA 5724-01007.Jul 16, 2013 · N344NW · Airbus A320212 · Standard Practices/StructuresSDR DALA1505143244Skin · dentedDENT 0.060 IN DEEP IN, ZONE 2 OF LT INBD T/E FLAP. REPAIRED IAW SRM 57-52-00.May 16, 2013 · N344NW · Airbus A320212 · Trailing Edge FlapsSDR DALA13016893244Light · inoperativeDURING NON ROUTINE CHECK, FOUND ROW 19 FLOOR EMERGENCY ESCAPE PATH MARKING LIGHT INOPERATIVE. MX REPLACED ROW 19 EMERGENCY FLOOR PATH LIGHT AND FUNCTIONAL CHECK WAS NORMAL.Apr 11, 2013 · N344NW · Airbus A320212 · Emergency LightingSDR DALA12010763244Wire · disconnectedDURING NON ROUTINE CHECK, FOUND EMERGENCY FLOOR LIGHTING AT ROW 2AB INOPERATIVE. FOUND BLACK WIRE TO LIGHT SOCKET PULLED OUT. REPLACED AFT LIGHT SOCKET AT SEAT 2B FOR EMERGENCY PATH LIGHTING AND FUNCTIONAL CHECK WAS NORMAL.Oct 22, 2012 · N344NW · Airbus A320212 · Light System WiringSDR DALA1504613244None · noneRIB 5 AFT PINTLE BUSHINGS IDENTIFIED AS MAJOR.Sep 25, 2011 · N344NW · Airbus A320212 · Standard Practices/StructuresSDR DALA1505133244Skin · chafedRT WING NR 2 SLAT INBD T/E LOWER SURFACE IS CHAFED, REPAIRED IAW SRM 51-23-11.Jul 15, 2011 · N344NW · Airbus A320212 · Leading Edge DevicesSDR DALA1143943244Floor Panel · crackedAFT CARGO COMPT, FLOOR PANEL 151GF, HAS CRACKS AND SEVERAL DENTS ON UPPER SKIN. REMOVED AND REPLACED FLOOR PANEL 151LF AT AFT CARGO IAW A320 AMM 53-42-14-000-0001.Jul 15, 2011 · N344NW · Airbus A320212 · Fuselage Floor PanelSDR DALA1143933244Floorboard · damagedFLOORBOARD 231UF SAGGING. REMOVED, FABRICATED AND INSTALLED FLOOR PANEL 231UF IAW A320 AMM 53-22-12-400-001. RETAIN FOR RECORDS.Jul 15, 2011 · N344NW · Airbus A320212 · Fuselage Floor PanelSDR DALA1143923244Floorboard · damagedFLOORBOARD 232WF SAGGING. REMOVED, FABRICATED, AND INSTALLED FLOOR PANEL 232WF IAW A320 AMM 53-22-12-400-001. RETAIN FOR RECORDS.Jul 15, 2011 · N344NW · Airbus A320212 · Fuselage Floor PanelSDR DALA1143913244Floorboard · damagedFLOORBOARD 251RF SAGGING. REMOVED, FABRICATED, AND INSTALLED FLOOR PANEL 251RF IAW A320 AMM 53-22-12-400-001-000.Jul 15, 2011 · N344NW · Airbus A320212 · Fuselage Floor PanelSDR DALA1143623244Floor Panel · delaminatedAFT CARGO COMPT FLOOR PANEL 161AF IS DELAMINATED AND HAS MULTIPLE DENTS ON UPPER SKIN. REMOVED, FABRICATED, AND INSTALLED NEW PNL 161AF IAW A320 AMM 53-42-14-400-001.Jul 14, 2011 · N344NW · Airbus A320212 · Fuselage Floor PanelSDR DALA1505103244Skin · damagedSTATIC DISCHARGE AT FASTENER FRAME 21 AT CENTER LINE, REPAIRED IAW SRM 53-11-11.May 24, 2011 · N344NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA1505093244Skin · damagedSTATIC DISCHARGE AT FASTENER, FRAME 3, 8 O'CLOCK, REPAIRED IAW SRM 53-11-11.May 24, 2011 · N344NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA1505083244Skin · damagedSTATIC DISCHARGE AT FASTENER 1" FWD OF FRAME 2, 8 O`CLOCK, REPAIRED IAW SRM 53-11-11.May 24, 2011 · N344NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA1505073244Frame · damagedDAMAGE 9" AFT FRAME 28, STR 43, REPAIRED IAW SRM 53-21-11.May 2, 2011 · N344NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA1505063244Skin · damagedSKIN DAMAGED 5" AFT FRAME 32 .910 FROM STR 43. REPAIRED IAW SRM 53-21-11.May 2, 2011 · N344NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA1505053244Skin · damagedLIGHTNING STRIKE REPAIR, 5" FWD FRAME 29, STR 43, REPAIRED IAW SRM 53-21-11.May 2, 2011 · N344NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA1023393244Wire · damagedDURING A NON ROUTINE CHECK, FOUND THE SEAT ESCAPE PATH EMERGENCY LIGHT AT ROW 22 INOPERATIVE. MX SPLICED A PULLED APART WIRE TOGETHER AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Sep 17, 2010 · N344NW · Airbus A320212 · Light System WiringSDR DALA1016133244Wire · brokenDURING A NON ROUTINE CHECK, FOUND SEAT 23 EMERGENCY PATH LIGHT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jul 10, 2010 · N344NW · Airbus A320212 · Light System WiringSDR DALA107383244Terminal · looseDURING A NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT 23C INOPERATIVE. MX RECONNECTED A LOOSE TERMINAL AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Apr 10, 2010 · N344NW · Airbus A320212 · Light System WiringSDR DALA1143953244Skin · scratchedGROUND CREW FOUND LARGE SCRATCH ON LT AC SIDE BEHIND & BELOW DOOR 1L. INSP AREA FOR SRM 53-11-11. NO CRACKS NOTED. DEFER TO MONITOR UNTIL 3000 F/C IAW SRM PERFORMED GVI PER SRM 53-11-11 NO CRACKS NOTED. BLENDED SCRATCHES IAW SRM 51-73-00. IN LIMITS PER SRJul 26, 2009 · N344NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR 0602213244Slide · malfunctionedDURING EMERGENCY LIGHT TEST, EPSU EXT LOAD FWL ANNUNCIATED. REPLACED LEFT FORWARD EVACUATION SLIDE ASSEMBLY. CHECKS OK.   Oct 2, 2006 · N344NW · Airbus A320212 · Escape SlideSDR 0602203244Battery Pack · warning messageDURING EMERGENCY LIGHT TEST, EPSU BATTERY R ANNUNCIATED. REPLACED BATTERY PACK 12WL. CHECKS OK.   Oct 2, 2006 · N344NW · Airbus A320212 · Emergency LightingSDR 0103783244Slide · leakingDURING SLIDE SHOP TEST, FAILED LEAK CHECK. OVERHAULED AND REPAIRED PER AIR CRUISERS MAINTENANCE MANUAL PA 15609 AND PACKING PUBLICATION 26657.Oct 12, 2001 · N344NW · Airbus A320212 · Escape SlideSDR 9807083244Light · inoperativeDURING LINE CHECK, EMERGENCY LIGHT TEST FAULTS UNIT EMER R. MAINTENANCE REPLACED LIGHT ASSEMBLY AT RIGHT FORWARD OVERWING EXIT. OPERATIONAL CHECK OK.Apr 21, 1998 · N344NW · Airbus A320212 · Emergency LightingSDR 9805843244Power Supply · dischargedTEST OF EMERGENCY LIGHT SYSTEM REVEALED EMERGENCY POWER SUPPLY 13WL INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPERATIONAL CHECK OK.Apr 3, 1998 · N344NW · Airbus A320212 · Emergency LightingSDR 9723583244Connector · dirtyOVERNIGHT TEST OF EMERGENCY LIGHTS INDICATED FAULTS COMM AFT L AND EXT LOADS, AFT L. MAINTENANCE CLEANED DIRTY CANNON PLUG AT AFT LEFT DOOR SLIDE. OPERATIONAL CHECK OK.Dec 11, 1997 · N344NW · Airbus A320212 · Emergency LightingSDR 9723153244Temp Sensor · malfunctionedFOLLOWING APPLICATION OF TAKEOFF POWER, RECEIVED BRAKES HOT MESSAGE AND ABORTED TAKEOFF AT VERY LOW SPEED. RETURNED TO THE GATE WITH NR 3 BRAKE INDICATING HIGH TEMPERATURE. MAINTENANCE REPLACED THE TEMPERATURE SENSOR ON NR 3 BRAKE. OPERATIONAL CHECK OK.Dec 10, 1997 · N344NW · Airbus A320212 · Landing Gear Brake SystemSDR 9720953244Battery · dischargedDURING THRU FLIGHT LINE CHECK, TEST OF EMERGENCY LIGHT SYSTEM FAULTED AFT LEFT BATTERY. MAINTENANCE REPLACED BATTERY AND POWER SUPPLY, OPERATIONAL CHECK OK.Nov 10, 1997 · N344NW · Airbus A320212 · Emergency LightingSDR 9710343244Bulb · failedDURING LINE MAINTENANCE, FOUND ALL FOUR OVERWING EMERGENCY EXIT HANDLE LIGHTS INOPERATIVE. REPLACED LIGHT BULBS, OPERATIONAL CHECK OK.May 23, 1997 · N344NW · Airbus A320212 · Emergency LightingSDR 9702063244Prox Sensor · malfunctionedDURING APPROACH, A LGCIU 1 FAULT MESSAGE APPEARED INDICATING THAT THE NOSE LANDING GEAR WAS NOT DOWN AND LOCKED. EXECUTED A GO-AROUND AND RECYCLED THE LANDING GEAR. NOSE LANDING GEAR INDICATED DOWN AND LOCKED AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED TJan 30, 1997 · N344NW · Airbus A320212 · Landing Gear Position and WarningSDR 9619403244Battery · dischargedDURING LINE MAINTENANCE CHECK OF THE EMERGENCY LIGHTS SYSTEM BATTERY PACK CAPACITY CHECK, FOUR BATTERY PACKS REQUIRED REPLACEMENT. REPLACED BATTERY PACKS, OPERATIONAL CHECK OK.Sep 7, 1996 · N344NW · Airbus A320212 · Emergency LightingSDR 9615013244Idg · inoperativeDURING FLIGHT, RECEIVED AN OVERHEAT INDICATION ON THE NR 1 INTEGRATED DRIVE GENERATOR. DISCONNECTED SAME PER THE COCKPIT OPERATING MANUAL. APU STARTED NORMALLY, HOWEVER AFTER APPROXIMATELY 10 MINUTES AN APU AUTO SHUTDOWN OCCURRED. DIVERTED TO RNO WITHOUT FUJul 11, 1996 · N344NW · Airbus A320211 · AC Generator-AlternatorSDR 9608903244Hmu · malfunctionedDURING CRUISE FLIGHT NR 2 ENGINE FLAME-OUT OCCURRED, ONE UNSUCCESSFUL RELIGHT WAS ATTEMPTED. THE NR 2 ENGINE FIRE BOTTLE DISCHARGED AND NO ABNORMAL ENGINE OPERATING PARAMETERS WERE NOTICED PRIOR TO FLAME-OUT. AIRCRAFT DIVERTED TO SLC AND LANDED WITHOUT FURTHApr 18, 1996 · N344NW · Airbus A320211 · Fuel Controlling SystemSDR 9607543244Power Supply · inoperativeDURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILED 'INT LOADS AFT LEFT'. REPLACED POWER SUPPLY AND OPERATIONAL CHECK OK.Mar 31, 1996 · N344NW · Airbus A320211 · Emergency LightingSDR 9519603244Warning Syst · malfunctionedDURING TAKEOFF ROLL, ECAM MESSAGE FOR ENGINE NR 2 COMPRESSOR VANE ILLUMINATED. ABORTED TAKEOFF AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PERFORMED NR 2 ENGINE FADEC 'A' AND 'B' TEST. ALL INDICATIONS WERE NORMAL, NO FAULT MESSAGES.Dec 2, 1995 · N344NW · Airbus A320211 · Central Warning
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