N374NW

Service difficulty reports · 159

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 = 'N374NW' 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 DALA2018111206602Cooling Fan · leakingCREW REPORTS ON TAXI IN WITH SINGLE ENGINE RUNNING FLIGHT ATTENDANTS SAW HAZE THROUGHOUT THE CABIN WITH AN ODOR. FOUND APU LEAKING OIL FROM COOLING FAN AREA. PERFORMED DECONTAMINATION OF ECS WITH APU INOP. AFTER COOLING FAN AND TRANSFER TUBE REPLACEMENT, APU SNov 11, 2018 · N374NW · Airbus A320212 · APU Bleed Air SystemSDR DALA2018102906333Epsu · inoperative(LP 0798099) EPSU (12WL) INOPERATIVE IN PASSENGER CABIN. REMOVED AND REPLACED SAME. OPERATIONS CHECKS OKAY.Oct 24, 2018 · N374NW · Airbus A320212 · Emergency LightingSDR DALA2018101906179Fitting · cracked(LP 0787455) CRACK INDICATION ON FRAME 16 IN OPEN INBOARD LOWER HOLE AT DOOR STOP FITTING NR 7 RIGHT HAND SIDE AT FORWARD GALLEY AREA . REPLACED INTERCOSTAL FITTING NR 7 IAW SRM 51-72-11 AND DWG D53112300.Oct 16, 2018 · N374NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2018101906178Fitting · cracked(LP 0787452) CRACK INDICATION ON FRAME 16 IN OPEN INBOARD UPPER HOLE AT DOOR STOP FITTING NR 7 RIGHT HAND SIDE AT FORWARD GALLEY AREA. REPLACED INTERCOSTAL FITTING NR 7 IAW SRM 51-72-11 AND DWG D53112300.Oct 16, 2018 · N374NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2018101406134Stop Fitting · crackedCRACK INDICATION ON FRAME 16 IN OPEN INBOARD UPPER HOLE AT DOOR STOP FITTING NR 7 LEFT HAND SIDE AT FORWARD GALLEY AREA. REPLACED INTERCOSTAL FITTING IAW SRM 5-72-11 AND DWG D53112300.Oct 13, 2018 · N374NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2018101606129Floorbeam · corroded(LP 0783091) CORROSION FLOORBEAM -Y1292 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FORWARD GALLEY AREA. (SSI 531189) REPLACED IAW SRM 51-72-11 AND DWG D53112812.Oct 13, 2018 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018101606128Floorbeam · corroded(LP 0781772) CORROSION FLOORBEAM +Y1292 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FORWARD GALLEY AREA. (SSI 531189) REPLACED IAW SRM DWG D53110984.Oct 12, 2018 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018101606127Floorbeam · corroded(LP 0781408) CORROSION FLOOR BEAM _Y765 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FORWARD GALLEY AREA (SSI 531189) REPLACED IAW SRM 51-72-11 AND DWG D 53110920.Oct 12, 2018 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018101606126Floorbeam · corroded(LP 0781394) CORROSION FLOORBEAM Y81 LOCATED BETWEEN FRAME 12 TO FRAME 16 AT FORWARD GALLEY AREA (SSI 531189) REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53112829.Oct 12, 2018 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018101506072Seat Track · corroded(LP 0779770) CORROSION SEAT TRACK +Y765 FRAME 41 TO 47 IN PASSENGER CABIN. REPLACED SEAT TRACK +Y765 FRAME 41 TO FRAME 47 IAW SRM 51-72-11 AND DWG D53370500.Oct 11, 2018 · N374NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018101506071Seat Track · corroded(LP 0779745) CORROSION SEAT TRACK +Y765 FRAME 36 TO 41 IN PASSENGER CABIN. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Oct 11, 2018 · N374NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018101506070Seat Track · corroded(LP 0779706) CORROSION SEAT TRACK -Y765 FRAME 41 TO 47 IN PASSENGER CABIN. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Oct 11, 2018 · N374NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018101506069Seat Track · corroded(LP 0779681) CORROSION SEAT TRACK -Y765 ON FRAME 36 TO FRAME 41. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D5370500.Oct 11, 2018 · N374NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018101506068Floorbeam · corroded(LP 0779644) CORROSION FLOORBEAM +Y1225 LOCATED FRAME 66 TO FRAMED 68 AT AFT GALLEY AREA (SSI 534147) REPLACED IAW SRM 51-72-11 AND DWG D53472780.Oct 11, 2018 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018101506067Floorbeam · corroded(LP 0779642) CORROSION FLOOR BEAM -Y189 LOCATED BETWEEN FRAME 20 TO FRAME 24 AT FORWARD GALLEY AREA (SSI 531189). REPLACED IAW SRM 51-72-11 AND DWG D 53111406.Oct 11, 2018 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018101506066Structure · corroded(LP 0778953) CORROSION WEB LOCATED BETWEEN FRAME 20 TO FRAME 24 AT LEVEL STRINGER 23L AT FORWARD GALLEY AREA (SSI 534189). REPLACED IAW SRM 51-72-11 AND DWG D53112783.Oct 11, 2018 · N374NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2018101406034Web · corrodedCORROSION WEB LOCATION BETWEEN FRAME 20 TO FRAME 24 AT LEVEL STRINGER 23R AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D53112806.Oct 10, 2018 · N374NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2018101106033Floorbeam · corrodedCORROSION FLOORBEAM +Y503.2 LOCATED BETWEEN FRAME 12 TO FRAME 16 AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND SRM 51-72-11 AND DWG D53112825.Oct 10, 2018 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018101006000Not Reported · corrodedCORROSION WE LOCATED FRAME 69 TO FRAME 70 AT LEVEL STRINGER 23L AT AFT GALLEY AREA. REPLACED IAW SRM 51-2-1 AND DWG D53474180.Oct 9, 2018 · N374NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2018092405733Cooling Fan · leakingODOR IN CABIN WITH APU AND PACKS ON. OIL LIKE SMELL. FOUND APU COOLING FAN LEAKING OIL. REMOVED AND REPLACED COOLING FAN IAW AMM. OPERATION AND LEAK CHECK OK.Sep 21, 2018 · N374NW · Airbus A320212 · APU Bleed Air SystemSDR DALA2018092005675Tube · leakingWHEN POWER CAME BACK AT TOP OF DESCENT A SHARP PUNGENT SMELL FILLED THE FLIGHT DECK AND REMAINED THRU SHUTDOWN. MAINTENANCE INSPECTED APU AND FOUND INTAKE ASSEMBLY WITH OILY RESIDUE. REMOVED RIGHT APU DOOR FOR CLEANING AND FOUND NR 1 ENGINE FORWARD SUMP PRESSUSep 19, 2018 · N374NW · Airbus A320212 · Turbine Engine Oil SystemSDR DALA2017012600679Door Frame · crackedCRACK ON FWD LATERAL SEGMENT FRAME INBD ON EMERGENCY EXIT DOOR 843 IN PASSENGER CABIN. REPLACED FWD LATERAL SEGMENT FRAME IAW SRM 51-72-11 AND DWG D52279010.Jan 25, 2017 · N374NW · Airbus A320212 · Emergency ExitsSDR DALA2017012600678Door Frame · crackedCRACK ON AFT LATERAL SEGMENT FRAME INBD ON EMERGENCY EXIT DOOR 843 IN PASSENGER CABIN, REPLACED AFT LATERAL SEGMENT FRAME IAW SRM 51-72-11 AND DWG D52279010.Jan 25, 2017 · N374NW · Airbus A320212 · Emergency ExitsSDR DALA2015110306664Stringer · corrodedCORROSION FOUND ON STRINGER 43L BETWEEN FRAME 56 AND 57. REPAIRED IAW ER/A 541087-14, REV O AND SRM 53-00-13, FIG 201.Nov 2, 2015 · N374NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA13009443274Skin · damagedDURING INSPECTION, FOUND LIGHTNING STRIKE ON EXTERNAL SKIN FR 21+5" AND 3" ABOVE STR 38R APROX, FWD FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN FR 21+5" AND 3" ABOVE STR 38R APROX, FWD FUSELAGE IAW SRM A320 53-00-11, FIG 232.Feb 27, 2013 · N374NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA13009383274Skin · damagedDURING INSPECTION, FOUND LIGHTNING STRIKE ON FASTENER LOC FR 27+19" AND STR 41R LOWER FUSELAGE. PERFORMED PERMANENT REPAIR LOC. FR 27+19" AND STR 41R LOWER FUSELAGE IAW SRM A320 53-21-11, PARA 5J FIG 2013 (SHEET 2) PAGES 327/328.Feb 26, 2013 · N374NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA13008873274Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL LT SIDE FR 68 AFT PAX CABIN. REPLACED LOWER SILL LOCATED LT SIDE BETWEEN FR 66 TO FR 68 AT LEVEL STR 23L AFT PAX CABIN IAW SRM 51-72-11 AND DWG 53480019.Feb 22, 2013 · N374NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13008853274Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION, BEAM -Y1192 FR 67 AFT PAX CABIN SSI 534147 L=1.644" W=0.950" D=0.028". REPLACED BEAM -Y1192 FR 67 TO FR 68 AFT PAX CABIN IAW SRM A320 51-72-11 AND DWG D53472040.Feb 22, 2013 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA13008793274Structure · corrodedDURING INSPECTION, FOUND CORROSION ON FWD LOWER CORNER FR 66 AT LEVEL OF STR 23R AFT PAX CABIN. REPLACED IAW 51-72-11 AND DWG D53480505.Feb 22, 2013 · N374NW · Airbus A320212 · Fuselage Main, StructureSDR DALA13008813274Hinge · wornDURING BEARING REMOVAL OF RUDDER HINGE NR 7 THE BORE FOUND WITH WEAR. THERE IS NO ALLOWABLE DAMAGE NOT REPAIR ON ANY MANUAL, HINGE NR 7 MUST BE REPLACED. REPLACED HINGE NR 7 AND FASTENERS IAW SRM 51-72-11.Feb 21, 2013 · N374NW · Airbus A320212 · Rudder StructureSDR DALA13008773274Floor Support · corrodedDURING INSPECTIO, FOUND CORROSION ON LOWER SILL RT SIDE FR 66 AFT PAX CABIN. REPLACED LOWER SILL AND LOCK FASTENERS. R2 FR 66 TO FR 68 AFT. PAX CABIN IAW SRM A320 51-72-11 AND DWG D53480019.Feb 21, 2013 · N374NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13008763274Structure · corrodedDURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER FR 68 AT LEVEL OF STR 23R AFT PAX CABIN. REPLACED AFT LOWER CORNER LOC. ON FR 68 AT LEVEL OF STR 23R AFT PAX CABIN SRM A320 51-72-11 AND DWG 53480505.Feb 21, 2013 · N374NW · Airbus A320212 · Fuselage Main, StructureSDR DALA13008753274Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM FR 66 -Y464 AFT PAX CABIN. REPLACED FLOORBEAM IAW SRM 51-42-11 AND SRM 51-72-11, DWG D53472816.Feb 21, 2013 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA13008743274Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON BEAM -Y1292 FR 66 AFT PAX CABIN SSI 534147, L=0.438", W=0.118", D=0.028". REPLACED BEAM -Y1292, FR 64 TO FR 66 AFT PAX CABIN IAW SRM 51-72-11 AND DWG D53472000.Feb 21, 2013 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA13008733274Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON BEAM -Y1160 FR 68 AFT PAX CABIN SSI 534147, L=1.205", W=0.752", D=0.033". REPLACED BEAM IAW SRM 51-72-11 AND DWG D53472780.Feb 21, 2013 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA13008033274Web · corrodedAFTER REMOVED SHEAR PLATE IAW ROUTINE CARD 5320-01089-01, FOUND CORRODED WEB AT LEVEL, STR 23R AND BETWEEN FR 69 TO FR 70. REPLACED WEB AT LEVEL STR 23R AND BETWEEN FR 69 TO FR 70 IAW SRM 51-72-11.Feb 18, 2013 · N374NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13009193274Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING OF LT LOWER SILL FR 66 AND FR 68 AFT PAX CABIN. REPLACED CENTER FITTING AND FASTENER OF LT LOWER SILL FR 66 AND FR 68 AFT PAX CABIN IAW SRM 51-72-11 AND DWG D53480009.Feb 17, 2013 · N374NW · Airbus A320212 · Fuselage Main, Attach FittingsSDR DALA13008023274Beam · corrodedDURING INSPECTION, FOUND CORROSION ON BEAM FR 67-68 Y765 AFT PAX CABIN. REPLACED BEAM Y765 LOC FR 67 TO FR 70 AND FASTENER IN AFT PAX CABIN IAW SRM A320 51-72-11.Feb 17, 2013 · N374NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13008013274Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING RT LOWER SILL AFT PAX CABIN SSI 534147 L=1.667" W= 0.575, D=0.094". REPLACED CENTER FITTING RT LOWER SILL AND FASTENER IN AFT PAX CABIN IAW SRM 51-72-11.Feb 17, 2013 · N374NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13008003274Beam · corrodedDURING INSPECTION, FOUND CORROSION ON BEAM FR 67-68 -Y765 AFT PAX CABIN. REPLACED BEAM -Y765 LOC FR 67 TO FR 70 AFT PAX CABIN IAW SRM 51-42-11, 51-72-11.Feb 16, 2013 · N374NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13007993274Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK FR 64+5", FR 66 Y765 AFT PAX CABIN. REPLACED SEAT TRACK IAW SRM 51-72-11.Feb 16, 2013 · N374NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA12017093274Battery · faultedDURING SERVICE CHECK FOUND EPSU 13WL FAULT MESSAGE ON PROGRAM TEST AND BATTERY FAULT ON EPSU 13WL. MX REPLACED BATTERY AND OPS CHECK WAS NORMAL.Dec 24, 2012 · N374NW · Airbus A320212 · Emergency LightingSDR DALA13049743274Lug · damagedRT FWD LUG FOR RT MLG DAMAGED DURING BUSHING INSTALATION DAMAGED RT WING. BORED TO REMOVE DAMAGE AND RE-ESTABLISHED CHAMFERS. ACCOMPLISHED IAW PRI ER/A 49778-14, AD 142948 COMPLIED WITH STEP 2 IAW PRI/ER/A 497778-14AD. NO DEFECTS NOTED INSTALLED BUSHINGS. Dec 6, 2011 · N374NW · Airbus A320212 · Wing, Landing Gear Attach FittingsSDR DALA1156613274Connector · looseDURING NON ROUTINE CHECK, FOUND THE EMERGENCY EXIT PATH LIGHT AT ROW 19 INOPERATIVE. MAINTENANCE RECONNECTED LOOSE CONNECTION AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Oct 2, 2011 · N374NW · Airbus A320212 · Light System WiringSDR DALA1137263274Battery Pack · dischargedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT 13WL INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.May 29, 2011 · N374NW · Airbus A320212 · Emergency LightingSDR DALA1135223274Power Supply · malfunctionedDURING A NON ROUTINE CHECK, FOUND THE AFT RIGHT EPSU FAULT MESSAGE ON CIDS PANEL FOR 13W. MAINTENANCE REPLACED THE SLIDE ASSEMBLY AT DOOR 2R AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.May 17, 2011 · N374NW · Airbus A320212 · Emergency LightingSDR DALA1109863274Dummy Rail · corrodedFWD DUMMY RAIL +Y503.2 IS CORRODED AT FRAME. BLENDED OUT CORRODED AREA IAW SRM 51-74-00, L=2.2" W=2.1" MAX DEPTH=0.079", ORIGINAL MATERIAL THICKNESS =0.079", FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 103. R & R DUMMY RAIL IAW SRM 51-42-11. INSTALLED NEFeb 10, 2011 · N374NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1109843274Stringer · corrodedNEED TO REMOVE FLOOR PANEL 221FF TO ACCESS STRINGER REPAIR. REMOVED FLOOR PANEL 221FF IAW AMM 53-12-12. UPON REMOVAL OF FLOOR PANEL 221FF FOUND CORROSION ON BOTTOM OF PANEL. NO ALLOWABLE LIMITS FOR PANEL. INSTALLED NEW FLOOR PANEL IAW AMM 53-12-12.Feb 10, 2011 · N374NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA1109833274Floorbeam · corrodedFWD CABIN FLOORBEAM -254 IS CORRODED AT FR 18. ORIGINALTHICKNESS .079" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. REMOVED FLOORBEAM AND SPLICE IAW SRM 51-42-11. RECEIVED NEW FLOORBEAM AND MACHINED BEAM AFT END TO FIT SPLICE IAW ER/A 489275-14. LOCATED AND DFeb 10, 2011 · N374NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA1109453274Floorbeam · corrodedFWD CABIN FLOORBEAM +Y1292 IS CORRODED AT FR 16 BLENDED OUT CORRODED AREA IAW SRM 51-74-00, L=7.0" W=1.5" D=0.045", ORIGINAL MATERIAL THICKNESS 0.079", FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105. REMOVED FLOORBEAM IAW SRM 51-42-11. INSTALLED NEW FLFeb 8, 2011 · N374NW · Airbus A320212 · Fuselage Main, Floor Beam
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