N345NW

Service difficulty reports · 204

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 = 'N345NW' 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 DALA2015032402370Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM, -Y465, AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 67+10", L=0.300", W=0.150", D=0.002. REPLACED FLOORBEAM, -Y465 AT AFT GALLEY AREA FROM FR 64 TO FR 67+10" AND FASTENERS IAW SRM A320 51-72-11 AND 51-42-11 DWG Mar 23, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032402369Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292, FRAME 36 TO 41 IN PASSENGER CABIN L=4.735", W=0.360", D=0.053". EVALUATED SEAT TRACK AND FOUND OUT LIMITS ON JOB CARD 2500-2031). REPLACED SEAT TRACK -Y1292 LOCATED BETWEEN FRAME 36 TO FRAME 41 IN PASMar 23, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015032402368Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB LOWER SURFACE AT LEVEL STR 38L IN AFT CARGO COMPARTMENT BETWEEN FRAME 62 TO FRAME 63. L=O.500", W=O.300", D=O.003". MEASURES APPROXIMATELY SSI 534107. REPLACED WEB AND FASTENERS LOCATED BETWEEN FRAME 62 TO FRAME 63Mar 23, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032402367Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1292 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66+5", L=2", W=1", D=0.003". REPLACED FLOORBEAM +Y1292 LOCATED BETWEEN FR 64 TO FR 66+5" AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000.Mar 23, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032102292Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162 FROM FRAMES 67+5 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG 53472000.Mar 20, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032102291Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1225 FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG 53472000.Mar 20, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032102290Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK +Y765 FRAMES 35 - 36. EVALUATED CORROSION AND FOUND OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-75-11.Mar 20, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015032102289Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT +Y765 AT FWD GALLEY AREA FROM FRAMES 12 - 24. REPLACED FLOOR SUPPORT IAW SRM 51-42-11 AND DWG D53112812.Mar 20, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032102288Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 68 AT AFT GALLEY AREA AND STRINGER 23L. REPLACED CORNER FITTING LOCATED ON FRAME 68 AT AFT GALLEY AREA AND STRINGER 23L IAW SRM 51-72-11 AND DWG D53480019.Mar 20, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032102287Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT TIE LOCATED INTERNAL AREA IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STRINGER 43L TO STRINGER 43R, L=0.250, W=0.200, D=0, .002 . REPLACED CLEAT TIE LOCATED INTERNAL AREA IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEMar 20, 2015 · N345NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015032102286Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66+5", L=0.800", W=0.400", D=0.002". REPLACED FLOORBEAM -Y765 LOCATED BETWEEN FR 64 TO FR 66+5" AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D5347-2230.Mar 20, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032102285Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT TIE LOCATED INTERNAL AREA IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STRINGER 42L TO STRINGER 43L L=0.300, W=0.200, D=0.002. SSI 532180. REPLACED CLEAT AND FASTENERS IN FWD CARGO COMPARTMENT ON FR 28 BETWEEN STMar 20, 2015 · N345NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015031902260Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1225 AT AFT GALLEY AREA FROM FRAME 66 +5" TO FRAME 67+15", L=0.700", W=0.350", D=0.002". REPLACED FLOORBEAM +Y1225 LOC BETWEEN FR 66+5" TO FR 67+15" AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000.Mar 18, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015031902259Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1162 AT AFT GALLEY AREA FROM FRAME 67+15" TO FRAME 69 L=1" W=0.500", D=0.004". REPLACED FLOORBEAM +Y1162 LOCATED BETWEEN FR 67+15" TO FR 69 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D534-72000.Mar 18, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015031902258Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK +Y765, FRAME 41 TO 47 IN PASSENGER CABIN L=4.242", W=0.385",D=0.071". ( EVALUATED SEAT TRACK AND FOUND OUT LIMITS ON JOB CARD NO 2500-2031). REPLACED SEAT TRACK +Y765 LOCATED FRAME 41 TO 47 IN PASSENGEMar 18, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015031802230Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1292 AT FWD GALLEY AREA BETWEEN FR 12 TO FR 24, L=2", W=0.500", D=0.006". REPLACED FLOORBEAM, SEAT TRACK -Y1292, LOCATED AT FWD GALLEY BETWEEN FR 12 TO FR 24 IAW SRM 51-72-11 AND DWG D53112814.Mar 17, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015031802229Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK +Y1292, FRAME 41 TO 47 IN PASSENGER CABIN L=4.062", W=0.390", D=0.070. EVALUATED SEAT TRACK AND FOUND OUT LIMITS ON JOB CARD NR 2500-2031. REPLACED SEAT TRACK +Y1292 BETWEEN FR 41 TO FR 47 SRM 51-72-11 AND DMar 17, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015031802228Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK +Y1292 FRAME 36 TO 41 IN PASSENGER CABIN L=5 .477", W=0.390", D=0.083". EVALUATED SEAT TRACK AND FOUND OUT OF LIMIT ON. REPLACED FLOORBEAM +Y1292 BETWEEN FR 36 TO FR 41 IAW SRM 51-72-11 AND DWG: D53370500.Mar 17, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015031802227Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK, +Y1292, FRAME 35 TO 36 IN PASSENGER CABIN L= 4.010", W=0.389", D=0.085". EVALUATED SEAT TRACK AND FOUND OUT LIMIT ON JOB CARD 2500-2031. REPLACED SEAT TRACK +Y1292, FR 35 TO FR 36 IN PASSENGER CABIN IAW SRMar 17, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015031802226Frame · corrodedDURING INSPECTION, FOUND CORROSION ON WEB FRAME 20 AT LEVEL STR 23R AT FWD GALLEY AREA L=1", W=0.200", D=0.002". REPLACED WEB AND FASTENERS LOCATION FR 20 TO FR 23 AT LEVEL STR 23R AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG NR D531-127783 AND D531-10900.Mar 17, 2015 · N345NW · Airbus A319112 · Fuselage Main, FrameSDR DALA2015031802225Frame · corrodedDURING INSPECTION, FOUND CORROSION ON WEB FRAME 16 AT LEVEL STR 23R AT FWD GALLEY AREA L=0.550", W=0.200, D=0.003". REPLACED WEB FRAME 16 LEVEL, STR 23R AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53112780.Mar 17, 2015 · N345NW · Airbus A319112 · Fuselage Main, FrameSDR DALA2015031702198Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM, +Y254 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24, L=0.300" ; W=0.100" ; D=0.002". REPLACED FLOORBEAM +Y254 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24 IAW SRM 51-72-11 AND DWG D53112816.Mar 16, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015031502138Crossbeam · crackedDURING INSPECTION, FOUND CRACK ON CROSSBEAM AT FRAME 68 STRINGERS 23L - 25L. REPLACED THE CROSSBEAM IAW SRM 51-72-11 AND DWG D53470150.Mar 14, 2015 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2015031302136Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT +Y765 IN AFT GALLEY AREA FROM FRAMES 64 - 66+5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Mar 12, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015031102117Dummy Rail · corrodedDURING INSPECTION, FOUND CORROSION ON RAIL DUMMY -Y189 AT FWD GALLEY AREA FROM FRAME 20 TO FRAME 23, L=0.300", W=0.200", D=0.002". REPLACED RAIL DUMMY -Y189 AT FWD GALLEY AREA BETWEEN FR 20 TO FR 23 IAW SRM 51-72-11 AND DWG D53112834.Mar 10, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014120806429Power Supply · inoperativeDURING EMERGENCY LIGHT BATTERY REPLACEMENT FOUND POWER SUPPLY NEAR OVERWING EXIT INOPERATIVE. REPLACED POWER SUPPLY EPSU, W/O BATTERY AND FUNCTIONAL CHECK WAS NORMAL.Dec 7, 2014 · N345NW · Airbus A320212 · Emergency LightingSDR DALA13059753245Wire · brokenDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS AT SEAT ROWS 19 AND 25 INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE SPICE. OPS CHECKED NORMAL.Nov 8, 2013 · N345NW · Airbus A320212 · Light System WiringSDR DALA13008953245Wire · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT 25C INOPERATIVE. MX REPAIRED BROKEN WIRE AND PERFORMED FUNCTIONAL CHECK NORMAL.Feb 18, 2013 · N345NW · Airbus A320212 · Light System WiringSDR DALA12005393245Wire · brokenDURING NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND FUNCTIONAL CHECK WAS NORMAL.Aug 16, 2012 · N345NW · Airbus A320212 · Light System WiringSDR DALA1122843245Light · brokenDURING EMERGENCY LIGHT TEST FOUND SEAT ROW 11 INOP. REPLACED BROKEN LIGHT ASSEMBLY AND TESTS OK.Mar 22, 2011 · N345NW · Airbus A320212 · Emergency LightingSDR DALA1025613245Power Supply · inoperativeDURING A NON ROUTINE CHECK, MX FOUND THE EMERGENCY PATH LIGHT AT ROW 1, 2, 3, 6, 7, AND 8 INOPERATIVE. REPLACED POWER SUPPLY UNIT AND OPERATIONAL TEST WAS NORMAL.Oct 3, 2010 · N345NW · Airbus A320212 · Emergency LightingSDR DALA1019813245Battery Pack · inoperativeDURING A NON ROUTINE CHECK, FOUND ROW 3 FIRST CLASS AND ROW 3 COACH CLASS PATH LIGHT INOPERATIVE. MX REPLACED BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Aug 17, 2010 · N345NW · Airbus A320212 · Emergency LightingSDR NWAA094153245Battery Pack · dischargedEMERGENCY EXIT LIGHTS FAILED TEST. REPLACED EPSU AND BATTERY PACK AND TESTED OK.Dec 4, 2009 · N345NW · Airbus A320212 · Emergency LightingSDR NWAA092853245Engine · bird ingestionDURING TAKEOFF FLIGHT CREW HEARD A LOUD BANG. SHORTLY THEREAFTER ENGINE NR 1 EGT BEGAN TO CLIMB OUT OF LIMITS. FLIGHT CREW SHUTDOWN ENGINE NR 1 AND RETURNED TO DEPARTURE AIRPORT. MAINTENANCE FOUND METAL IN THE TAIL PIPE. EVIDENCE OF BIRD STRIKE IN INLET COAug 9, 2009 · N345NW · Airbus A320212 · Engine (Turbine/Turboprop)SDR NWAA09203245Epsu · failedEMERGENCY LIGHT TEST AT CIDS PANEL FAILS, EPSU EXT LOAD EMER L MESSAGE. REPLACED EPSU 11WL, CHECKS GOOD. (K)Jan 26, 2009 · N345NW · Airbus A320212 · Emergency LightingSDR NWAA080193245Line · leakingDURING CRUISE FLIGHT, ENGINE NR 2 FUEL BURN WAS EXCESSIVE. FLIGHT CREW DIVERTED TO MIA PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE FOUND A FUEL LEAK AT NR 2 ENGINE HMU FUEL HEAT RETURN LINE CONNECTION. FUEL HEAT RETURN LINE AND GASKET REPLACED.Jan 16, 2008 · N345NW · Airbus A320212 · Engine Fuel DistributionSDR 0602553245Sign · activatedFORWARD LEFT AND RIGHT CABIN DOOR EMERGENCY EXIT SIGNS DID NOT ILLUMINATE WHEN GEAR SELECTED DOWN, OTHER EXITS SIGNS CHECK NORMAL. CORRECTED BY REPLACING CIDS DIRECTOR NR 2 AND EPSU. CHECKS OK.Nov 30, 2006 · N345NW · Airbus A320212 · Emergency LightingSDR 0601163245Power Supply · dischargedOVERWING EMERGENCY EXIT LIGHTING REPORTED INOP BY FLIGHT ATTENDANT. REPLACED LEFT AND RIGHT SIDE OVERWING EMERGENCY POWER SUPPLIES. OPS CHECK OK.May 31, 2006 · N345NW · Airbus A320212 · Emergency LightingSDR 0600843245Battery Pack · no testDURING A-CHECK THE AFT EMERGENCY POWER SUPPLY UNIT TEST FAILED. REPLACED EPSU 32-3350-9-0010 S/N 01997 AND BATTERY PACK 32-3300-4-0074.May 1, 2006 · N345NW · Airbus A320212 · Emergency LightingSDR 0600793245Connector · inoperativeON APPROACH MIDDLE EXIT LIGHTS ROW 10 AND OVERWING EXIT LIGHTS DID NOT ILLUMINATE. REPLACED PLUG TO EPSU.Apr 23, 2006 · N345NW · Airbus A320212 · Light System WiringSDR 0600783245Power Supply · inoperativeFOUND PRIOR TO FLIGHT MIDDLE CABIN AISLE LIGHTS AND OVERWING EXIT SIGNS INOP. REPLACED EPSU 32-3350-9-0010 S/N 00350.Apr 12, 2006 · N345NW · Airbus A320212 · Emergency LightingSDR 0203553245Duct · damagedON CLIMBOUT, CABIN PRESSURE CLIMBED AT 1000 FT/MIN AT 26,000 FT: CABIN AT 8000 FT AND CLIMBING AT 600 FT/MIN. ACCOMPLISHED EMERGENCY DESCENT TO 10,000 FT. MAXIMUM CABIN PRESSURE REACHED WAS 12,000 FT. THERE WAS A LOUD AIR LEAK SOUND IN CABIN. OXYGEN MASKS Oct 24, 2002 · N345NW · Airbus A320212 · Air Distribution SystemSDR 0104223245Door · out of adjAFTER TAKEOFF, NOSE GEAR DOORS DID NOT CLOSE. GEAR RETRACTED NORMALLY. RECYCLED GEAR WITH NO HELP. FLEW AT 250 IAS PER COM 2.32.9. NOSE GEAR DOORS APPEARED TO BE CLOSED. AIRCRAFT MADE AN UNEVENTFUL LANDING. JACKED AIRCRAFT AND CYCLED GEAR. ADJUSTED RIGHNov 9, 2001 · N345NW · Airbus A320212 · Landing Gear Door Retract SectionSDR 0004503245Uplock, Nlg · inoperativeAFTER TAKEOFF WHEN LANDING GEAR SELECTED UP, RECEIVED "L/G DOORS NOT CLOSED" MESSAGE. THE ECAM LANDING GEAR PAGE INDICATED THE NOSE LANDING GEAR DOORS OPEN. CYCLED GEAR WITH SAME THE RESULTS. SELECTED GEAR DOWN WITH NORMAL INDICATIONS AND RETURNED TO DEPARTUREDec 11, 2000 · N345NW · Airbus A320212 · Landing Gear Door Retract SectionSDR 9723083245Wire · brokenDURING OVERNIGHT MAINTENANCE TEST OF FLOOR PATH EMERGENCY LIGHT SYSTEM, BOTH RED LIGHTS WERE FOUND INOPERATIVE AT SEAT 10L. MAINTENANCE REPAIRED BROKEN WIRE. OPERATIONAL CHECK OK.Dec 5, 1997 · N345NW · Airbus A320212 · Light System WiringSDR 9721513245Battery · dischargedDURING OVERNIGHT MAINTENANCE, FAULT OF THE EMERGENCY LIGHT, LEFT UNIT, DISPLAYED ON CIDS TEST PANEL. REPLACED THE BATTERY PACK ON THE LEFT EMERGENCY POWER SUPPLY UNIT, OPERATIONAL CHECK OK.Nov 16, 1997 · N345NW · Airbus A320212 · Emergency LightingSDR 9609023245Retract Mech · malfunctionedDURING CLIMBOUT, THE LANDING GEAR DID NOT RETRACT ACCOMPANIED BY LANDNG GEAR NOT UPLOCKED MESSAGE. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT.Apr 16, 1996 · N345NW · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR 9608593245Prox Sensor · failedDURING APPROACH AFTER LANDING GEAR EXTENSION, THREE RED LANDING GEAR INDICATION LIGHTS ILLUMINATED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOOR PROXIMITY SENSOApr 13, 1996 · N345NW · Airbus A320211 · Landing Gear Position and WarningSDR 9608223245Prox Sensors · dirtyDURING APPROACH AFTER LANDING GEAR EXTENSION, RECEIVED L/G GEAR NOT DOWNLOCKED MESSAGE. ALL THREE LANDING GEAR INDICATION TRIANGLES WERE ILLUMINATED RED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANApr 10, 1996 · N345NW · Airbus A320211 · Landing Gear Position and WarningSDR 9607863245Retract Mech · malfunctionedDURING APPROACH, THE LANDING GEAR DID NOT EXTEND. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES.Apr 7, 1996 · N345NW · Airbus A320211 · Landing Gear Retraction/Extension System
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