N333NW

Service difficulty reports · 118

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 = 'N333NW' 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 DALA2019092005503Floorbeam · corrodedCORROSION FLOOR STRUCTURE LOCATED AT FR 67+16INCH TO FR 69 AND Y-1292 IN PASSENGER CABIN, REPLACED FLOORBEAM STRUCTURE LOCATED AT FR 67 +16 INCH TO FR 69 AND Y-1292 IN PASSENGER CABIN AREA AS PER SRM 51-72-11 AND DWG# D5347200.Sep 19, 2019 · N333NW · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2019092005502Angle · corrodedCORROSION FRAME 71 ANGLE LOCATED BETWEEN STR 27R AND STR 32R AT LOWER FUSELAGE, REPLACED ANGLE LOC AT FR 71 BTW STR 27R AND STR 32R LOWER FUSELAGE AS PER SRM 51-42-11 AND DWG D53571510.Sep 19, 2019 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019091805411Dummy Rail · corrodedCORROSION FLOOR STRUCTURE RAIL DUMMY LOCATED BTW FR 14 TO FR 16 Y+940 IN PASSENGER CABIN (1EA), REPLACED FLOOR STRUCTURE RAIL DUMMY LOCATED BTW FR14 TO FR16 Y+940 IN PASSENGER CABIN (1E/A) AS PER SRM 51-72-11 AND DWG D53112822.Sep 17, 2019 · N333NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019091805410Beam · corrodedCORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 66+6INCH TO FR 70 Y-765 IN PASSENGER CABIN (1E/A), REPLACED FLOOR STRUCTURE BEAM LOCATED BTW FR66+6" TO FR70 Y-765 IN PASSENGER CABIN (1E/A) AS PER SRM 51-42-11 AND DWG D53-472816.Sep 17, 2019 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019061703585Lamp · inoperativeDURING SERVICE CHECK FOUND ALL 4 OVERWING EXIT DOOR PULL HANDLE LIGHTS INOP, RELAMPED LEFT FORWARD AND AFT AND RIGHT FORWARD PULL HANDLE LIGHTSJun 17, 2019 · N333NW · Airbus A320211 · Emergency LightingSDR DALA2019101895981Frame · not reportedFR50 PARTIAL FRAME PERMANENT REPAIR ERA 563639-14 SECTION 2 ITEM #5 MAJOR REPAIR PER SRM 53-00-12-300-004.Jan 17, 2019 · N333NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2018081085006Switch · malfunctionedEMERGENCY LIGHT ILLUMINATED IN FLIGHT WITHOUT POWER LOSS. REMOVED AND REPLACED THE 4WL EMERGENCY LIGHT SWITCH. OPS CHECKED OK.Aug 7, 2018 · N333NW · Airbus A320211 · Emergency LightingSDR DALA2021072604188Skin · corrodedSHIP 3233 CORROSION IN LH/RH WING BOTTOM SKIN ACC PNL FASTENER HOLES. CORRECTIVE ACTION: PERFORMED POST-REPAIR REPETITIVE INSPECTION-LEFT WING AND RIGHT WING BOTTOM SKIN LOWER SURFACE AS PER ER/A 563122-14AD REV.ORIGINAL, SECTION I AND SECTION II AND ADDITIONANov 10, 2017 · N333NW · Airbus A320211 · Wing, Plate/SkinSDR DALA2017072905772Hinge Fitting · damagedFR43 KEEL BEAM FWD HINGE FITTING, RT MLG DOOR FOUND OUT OF ROUND HOLES AIRCRAFT SIDE COMMON TO RT MLG UPPER ACTUATOR FITTINGS. HOLES MARKED AS 4,5,6,7,9,10,11,12, COMPLIED WITH PRI'S 560120-14AD REV A REV 1 THRU 6. REPAIRED REF ERA 560120-14AD REV A.Jul 28, 2017 · N333NW · Airbus A320211 · Fuselage, Door HingeSDR DALA2017072905771Hinge Fitting · damagedFR43 KEEL BEAM FWD HINGE FITTING, RT MLG DOOR FOUND CRACK INDICATIONS ON AIRCRAFT SIDE COMMON TO RMLG UPPER ACTUATOR FITTINGS. HOLES MARKED AS 7,8,10. COMPLIED WITH PRI'S 560120-14AD REV A REV 1 THRU 6. REPAIRED REF ERA 560120-14AD REV A.Jul 28, 2017 · N333NW · Airbus A320211 · Fuselage, Door HingeSDR DALA2017072905770Hinge Fitting · damagedFR43 KEEL BEAM FWD HINGE FITTING, RT MLG DOOR FOUND RMLG AFT UPPER ACTUATOR FITTING HAS SEVERAL OUT OF ROUND HOLES. COMPLIED WITH PRI'S 560120-14AD REV A REV 1 THRU 6. REPAIRED REF ERA 560120-14AD REV A.Jul 28, 2017 · N333NW · Airbus A320211 · Fuselage, Door HingeSDR DALA2017072905769Hinge Fitting · damagedFR43 KEEL BEAM FWD HINGE FITTING, RT MLG DOOR FOUND CRACK INDICATION NOTED IN TOP LAYER OF MATERIAL AT HOLE NR 9. COMPLIED WITH PRI'S 560120-14AD REV A REV 1 THRU 6. REPAIRED REF ERA 560120-14AD REV A.Jul 28, 2017 · N333NW · Airbus A320211 · Fuselage, Door HingeSDR DALA2017011700423Battery · dischargedEPSU INT LOAD AFT L ON SERVICE CK, R AND R EPSU WITH BATTERY 13WL.Jan 16, 2017 · N333NW · Airbus A320211 · Emergency LightingSDR 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 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 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 DALA13071513233Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB -Y1732 AT FRAME 16. REPLACED WEB IAW SRM 51-72-11 AND DWG D53112780.Dec 23, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13070983233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT FRAME 18+4" -Y254. REPLACED FLOOR SUPPORT BETWEEN FRAMES 12 TO FR 24 IAW SRM 51-72-11, DWG D53112819, D53112820, D53110984 , D53110900 AND ER/A 520675-14 REV ORIGINAL, REV 0 .Dec 21, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13070173233Skin · crackedDURING INSPECTION, FOUND CRACK ON EXTERNAL SKIN AT FIXED L/E LOWER SURFACE AT LEVEL RIB 15 LT WING. REPAIRED EXTERNAL SKIN AT FIXED L/E LOWER SURFACE AT LEVEL RIB 15 LT WING IAW SRM 57-41-11, FIG 206.Dec 17, 2013 · N333NW · Airbus A320211 · Wing, Plate/SkinSDR DALA13069953233Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL OF LT PASSENGER CREW DOOR AREA BETWEEN FRAMES 66 TO 68. REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG D534 80505.Dec 16, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13069193233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT AT -Y189 FRAME 20+11 IN FWD PAX CABIN. REPLACED FLOOR SUPPORT BETWEEN FRAMES 20 AND 23 IAW SRM 51-72-11 AND DWG D53112834.Dec 15, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13069183233Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON PASSENGER DOOR AFT CORNER FITTING AT FRAME 68 . REPLACED FITTING IAW SRM A320 51-75-11 AND DWG D53480505.Dec 15, 2013 · N333NW · Airbus A320211 · Passenger/Crew DoorsSDR DALA13069173233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 66, Y 254. REPAIRED FLOOR SUPPORT IAW SRM 53-00-14, PARA 4.G, FIG 207, PAGE 250-256.Dec 15, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13070163233Bracket · corrodedDURING INSPECTION, FOUND CORROSION ON TWO BRACKETS, LOCATED EMERGENCY EXIT DOOR 844 THE OF HOOK BRACKET AREA, INTERNAL STRUCTURE. REPLACED BRACKETS, LOCATION ON EMERGENCY EXIT DOOR 844 THE OF HOOK BRACKET AREA INTERNAL STRUCTURE IAW SRM 51-72-11 AND DWG D52Dec 13, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13069143233Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON BORE OF SPIGOT RECEPTACLE FITTING ON LT PYLON. REPLACED RECEPTACLE FITTING IAW SRM 54-51-12.Dec 13, 2013 · N333NW · Airbus A320211 · Nacelle/Pylon, Attach FittingsSDR DALA13071903233Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 - 69 Y-1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.Dec 12, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13070153233Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL OF RT AFT PASSENGER CREW DOOR AREA BETWEEN FRAMES 66 TO 68. . REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG D53480505.Dec 12, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13069133233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 66, Y-1292. REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53472000.Dec 12, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13069123233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 66 TO 68 Y-1292 - Y-1162. REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG NR D53472000.Dec 12, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13069113233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 65 TO 67, Y-308. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472282.Dec 12, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13069103233Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY BETWEEN STRINGERS 40 & 41R FRAME 30. REPLACED CLEAT AND FASTENERS IAW SRM 51-72-11 AND DWG D53231586.Dec 12, 2013 · N333NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13068503233Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY FRAME 31 AND BETWEEN STRINGERS 41-42R. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D5323 1586.Dec 11, 2013 · N333NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13068493233Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY FRAME 31 AND BETWEEN STRINGERS 40-41R. REPLACED CLEAT IAW SRM 51-72-11 AND DWG 53231586.Dec 11, 2013 · N333NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13068483233Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL AREA AT LEVEL FRAME 16+6 AND S23L IN FWD PAX CABIN. REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG NR D53110339.Dec 11, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13068473233Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY LOCATED AT LEVEL FRAME 33 AND BETWEEN STRINGERS 40-41R. REPLACED CLEAT AND FASTENERS IAW SRM A320 51-72-11 AND DWG D53231586.Dec 11, 2013 · N333NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13069093233Bracket · corrodedDURING INSPECTION, FOUND CORROSION ON TWO BRAKETS ON EMERGENCY EXIT DOOR. REPLACED BRACKETS IAW SRM 51-72-11 AND DWG D52279040.Dec 10, 2013 · N333NW · Airbus A320211 · Emergency ExitsSDR DALA13069083233Bracket · corrodedDURING INSPECTION, FOUND CORROSION ON TWO BRACKETS, REPLACED BRACKETS AT EMERGENCY EXIT DOOR, IAW SRM 51-72-11 AND DWG D52279040.Dec 10, 2013 · N333NW · Airbus A320211 · Emergency ExitsSDR DALA13068253233Fitting · corrodedDURING INSPECTION, FOUND CENTER FITTING WITH CORROSION AT STRINGER 23L BETWEEN FRAMES 66 AND 68. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53480019.Dec 10, 2013 · N333NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13068243233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 TO 69 AND Y 1162. REPLACED FLOOR SUPORT IAW SRM 51-72-11 AND DWG D53472000.Dec 10, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13068233233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 66 TO 68 AND BETWEEN Y 1292 AND Y1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Dec 10, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13068223233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 66 AND Y 1292. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472090.Dec 10, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13067263233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 70 AND Y-765. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Dec 8, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13067293233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 70 AND Y512. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG 53472000.Dec 7, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13067253233Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB -Y1732 AT FRAME 20 IN FWD PAX CABIN. REPLACED WEB IAW SRM 51-72-11 AND DWG D53114392.Dec 7, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13067243233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 66 AND Y-765. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472090.Dec 7, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13067273233Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB Y1732 AT FRAME 20 IN FWD PAX CABIN. REPLACED WEB IAW SRM 51-72-11.Dec 6, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13067233233Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM LOCATED ON FRAME 18+5" AND Y254. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53112816.Dec 6, 2013 · N333NW · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13067223233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 AT FRAME 20+10" IN FWD PAX CABIN. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53112812, D53110900.Dec 6, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13066083233Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FR 66 TO FR 70 AND Y-160. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72000.Dec 4, 2013 · N333NW · Airbus A320211 · Fuselage Miscellaneous Structure
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