N338NW

Service difficulty reports · 192

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 = 'N338NW' 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 DALA2014102005631Seat Track · corrodedSEAT TRACK BETWEEN FRAMES 41 - 47, Y1292 FOUND CORRODED OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Oct 19, 2014 · N338NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014102005630Structure · corrodedDURING INSPECTION, FOUND CORROSION ON FWD LOWER CORNER AT FRAME 16 RT OF FWD PASSENGER/CREW DOOR CUTOUT. REPLACED IAW SRM 51-72-11 AND DWG D53112109.Oct 19, 2014 · N338NW · Airbus A320212 · Fuselage Structure (General)SDR DALA2014101905629Structure · corrodedDURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER , RT OF FWD PASSENGER/CREW DOOR CUTOUT AT FRAME 20. REPLACED IAW SRM 51-72-11 AND DWG D53112109.Oct 18, 2014 · N338NW · Airbus A320212 · Fuselage Structure (General)SDR DALA2014101905628Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1292 BETWEEN FRAMES 64 - 66+5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472229.Oct 18, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101905627Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 66+5 - 70 . REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.Oct 18, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101905626Seat Track · corrodedDURING INSPECTION, THE SEAT TRACK, BETWEEN FRAMES 47 - 64, Y765, FOUND CORRODED OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Oct 18, 2014 · N338NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014101905625Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1732 BETWEEN FRAMES 65 - 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53470150.Oct 18, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101905624Seat Track · corrodedDURING INSPECTION, SEAT TRACK LOCATED BETWEEN FRAMES 36 - 41 Y1292 WERE FOUND CORRODED OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Oct 18, 2014 · N338NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014101905621Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG.Oct 18, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101905620Seat Track · corrodedSEAT TRACK BETWEEN FRAMES 35 - 36, Y1292 FOUND CORROSION OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370000.Oct 18, 2014 · N338NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014101805623Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Oct 17, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101805622Floor Support · crackedDURING INSPECTION, FOUND A CRACK ON UPPER FLANGE OF FLOOR SUPPORT Y254 BETWEEN FRAMES 25 - 26. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 24 - 35 IAW SRM 51-72-11 AND DWG D53210005.Oct 17, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101705604Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED FWD PAX CABIN ENTRY DOOR BETWEEN FRAMES 17 - 19, STR 23L. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53112109.Oct 16, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101705603Access Panel · corrodedDURING INSPECTION, FOUND CORROSION ON COUNTERSINK OF ACCESS PANEL ON LT WING. REWORKED FUEL PANEL IAW SRM 51-74-00 AND WAS FOUND TO BE OUT LIMITS. REPLACED AND MADE A LEAK CHECK ON FUEL ACCESS PANEL IAW AMM 57-27-11-400-002-A.Oct 16, 2014 · N338NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2014101605568Skin · corrodedDURING INSPECTION, FOUND CORROSION ON EXTERNAL FUSELAGE SKIN FRAME 69+12 AND STRINGERS 29 - 30R. REPAIRED IAW SRM 53-41-11, PARA 5.D, FIGURE 205, PAGES 255 TO 260.Oct 15, 2014 · N338NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2014101605565Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y254 BETWEEN FRAMES 17 - 21. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWGOct 15, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101605564Unknown · corrodedDURING INSPECTION, FOUND CORROSION ON SECTION CONNECTOR LOCATED AT LEVEL OF FRAME 67 AND STR 27L. L=1", W=0.500", D= 0.010" APPROXIMATELY, SSI 534144. REPLACED SECTION CONNECTING LOCATED AT LEVEL OF FRAME 67 AND STR 27L IAW SRM 51-72-11 AND DWG, D53480009.Oct 15, 2014 · N338NW · Airbus A320212 · Fuselage Structure (General)SDR DALA2014101605563Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB LOCATED FWD PAX CABIN AT FRAME 20 Y-1732. REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53114392.Oct 15, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101605567Unknown · corrodedDURING INSPECTION, FOUND CORROSION ON SECTION CONNECTION LOCATED AT LEVEL OF FRAME 67 AND STR 31L. L=1.50", W=0.700", D=0.010" APPROXIMATELY, SSI 534144. REPLACED SECTION CONNECTING LOC AT LEVEL OF FRAME 67 AND STR 31L IAW SRM 51-72-11 AND DWG D53480009.Oct 14, 2014 · N338NW · Airbus A320212 · Fuselage Structure (General)SDR DALA2014101605566Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT AT FRAME 16 Y1292. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 - 24 IAW SRM 51-72-11, DWG D53112812, AND D53110920.Oct 14, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101505557Dummy Rail · corrodedDURING INSPECTION, FOUND CORROSION ON DUMMY RAIL AT FRAME 16, Y503.2. REPLACED THE DUMMY RAIL IAW SRM 51-72-11, DWG D53112825, AND DWG D53110984.Oct 14, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101305497Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 18 AND 20, Y-765. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWGS D53122812, AND D53110920.Oct 12, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101205496Dummy Rail · corrodedDURING INSPECTION, FOUND CORROSION ON DUMMY RAIL BETWEEN FRAMES 12 AND 16. REPLACED THE DUMMY RAIL IAW SRM 51-72-11 AND DWG NR D53110984 AND DWG NO D53112828.Oct 11, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014101205493Receptacle · corrodedDURING INSPECTION, FOUND CORROSION ON LT PYLON SPIGOT RECEPTACLE FITTING BORE. REPLACED PYLON SPIGOT RECEPTACLE IAW SRM 54-51-12.Oct 11, 2014 · N338NW · Airbus A320212 · Nacelle/Pylon Miscellaneous StructureSDR DALA13045553238Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 40L BETWEEN FRAMES 56 AND 57. REMOVED FASTENERS AND BLENDED CORROSION IAW SRM 53-00-13. FABRICATED REPAIR PARTS IAW SRM 53-00-13, FIG 202, SH 4 IAW SRM 53-00-13. INSTALLED REPAIR DOUBLER IAW SRM 53-00-13, FIG Sep 13, 2013 · N338NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA13044983238Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 40L BETWEEN FR 56 AND FR 57. MX COMPLETED WORK IAW SRM 53-00-13, FIG 202, SHEET 4 AND ERA 518798-14, REF LOG PAGE 9922198.Sep 13, 2013 · N338NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA13022773238Wire · brokenSEAT ROW 20C, EMERGENCY LIGHT INOPERATIVE. FOUND WIRE BROKEN. REPLACED SPLICE IAW AMM 20-90-03. LIGHT TESTED GOOD.May 16, 2013 · N338NW · Airbus A320212 · Light System WiringSDR DALA12007603238Skin · dentedGROUND CREW REPORTED LOWER FUSELAGE NOSE DENTED. EXTENDS FROM RT SKIN AIR VALVE TO 4 FT FORWARD. TRIMMED OUT DAMAGE, INSPECTED, FABRICATED FILLERS AND INSTALLED .090" DOUBLER IAW ER/A 507020-14 SECT 1 REV ORIGINAL.Sep 11, 2012 · N338NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA1168963238Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND WING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND FOUR LAMPS. OPERATIONAL CHECK WAS NORMAL AND AIRCRAFT RETURNED SERVICE.Dec 11, 2011 · N338NW · Airbus A320212 · Emergency LightingSDR DALA1158863238Pin · not seatedDURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT SEAT 5 INOPERATIVE. MAINTENANCE RESEATED PIN IN SPLICE AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Oct 18, 2011 · N338NW · Airbus A320212 · Light System WiringSDR DALA1023613238Hose · leakingFLIGHT CREW NOTED A SUBSTANTIAL DIFFERENCE IN FUEL FLOW/FUEL USED BETWEEN ENGINE NR 1 AND NR 2. FLIGHT CREW LANDED ACFT AT DESTINATION AND ENGINE NR2 AUTO SHUTDOWN AS ACFT TURNED OFF OF THE RUNWAY. MX FOUND A FUEL LEAK AT THE MAIN FUEL SUPPLY LINE TO FUEL FILSep 21, 2010 · N338NW · Airbus A320212 · Engine Fuel DistributionSDR DALA107183238Power Supply · inoperativeDURING A NON ROUTINE CHECK FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. MX REPLACED THE POWER SUPPLY AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Apr 5, 2010 · N338NW · Airbus A320212 · Emergency LightingSDR NWAA094303238Fan · damagedNEAR DESCENT BEGAN TO SMELL A HOT BURNING ODOR, CREW DECLARED EMERGENCY AND LANDED UNEVENTFUL. FOUND LEFT CABIN RECIRCULATING FAN DAMAGE.Dec 15, 2009 · N338NW · Airbus A320212 · Air Distribution FanSDR 0601583238Power Supply · inoperativeEMERGENCY EXIT LIGHT AIRCRAFT REAR NOT ON. CORRECTED BY REPLACING EMERGENCY POWER SUPPLY, LIGHTS CHECK GOOD.   Jul 10, 2006 · N338NW · Airbus A320212 · Emergency LightingSDR 0600493238Priority Valve · leakingEN ROUTE ECAM HYD Y ENG 2 PUMP TO RR APPEARED. NO YELLOW FLUID REMAINING. FLIGHT CONTINUED TO DESTINATION DELCLARING A YELLOW EMERGENCY WITH AN UNEVENTFUL LANDING. REMOVED AND REPLACED YELLOW SYSTEM LOW AND HIGH PRESSURE FILTERS (NO CONTAMINATION NOTED). FMar 5, 2006 · N338NW · Airbus A320212 · Hydraulic System, MainSDR 0000493238Blade · nr 1 engineTAKEOFF WAS ABORTED AT 120 KNOTS DUE TO MULTIPLE BIRD STRIKES. MAINTENANCE PERFORMED FUSELAGE BIRD STRIKE INSPECTION AND CLEANED AREAS AS NEEDED. NO DAMAGE TO FUSELAGE. BOTH ENGINES WERE BOROSCOPE INSPECTED AND ALL FAN BLADES WERE REPLACED ON THE NR 1 ENGINFeb 21, 2000 · N338NW · Airbus A320212 · Engine (Turbine/Turboprop)SDR 9724783238Longeron · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON STR 42L BETWEEN FRAMES 33 AND 34. REPAIRED PER EA 32-153859.Dec 5, 1997 · N338NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR 9720593238Ecu · malfunctionedDURING FINAL APPROACH, ENG 2 THRUST LEVER FAULT ANUNCIATED. AUTOLAND WOULD NOT BE COMPLETED DUE TO POOR LOC SIGNAL. THE NR 2 ENGINE WAS SHUT DOWN PER COM. MAINTENANCE REPLACED ENGINE CONTROL UNIT.Nov 3, 1997 · N338NW · Airbus A320212 · Fuel Control/Turbine EnginesSDR 9708863238Prox Sensor · inoperativeDURING CRUISE, ECAM DISPLAYED ANTI-ICE STBY PITOT. SHORTLY THERE AFTER L/G LGCIU 1 FAULT ILLUMINATED. CREW DID NOT WANT TO LAND AT SNA WITH 5,700 FEET OF RUNWAY AND NR 1 ENGINE THRUST REVERSER INOPERATIVE. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENTMay 2, 1997 · N338NW · Airbus A320212 · Landing Gear Position and WarningSDR 9625373238Window · delaminatedDURING CLIMBOUT AT 25,500 FEET, THE FIRST OFFICER'S NR 3 WINDOW OUTER PANE DELAMINATED AND SEPARATED FROM THE MIDDLE PANE. AIRCRAFT RETURNED TO BOS AND ACCOMPLISHED AN UNEVENTFUL OVERWEIGHT LANDING. MAINTENANCE REPLACED THE FIRST OFFICER'S NR 3 WINDOW.Nov 26, 1996 · N338NW · Airbus A320212 · Flight Compartment WindowsSDR 9519553238Boost Pumps · failedDURING TAKEOFF ROLL AS N1 REACHED 40 PERCENT, BOTH FUEL PUMPS IN THE RIGHT TANK INDICATED LOW PRESSURE, ACCOMPANIED BY BOTH PUMP FAULT LIGHTS ILLUMINATING AND A MASTER CAUTION. THE TAKEOFF WAS ABORTED. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES.Nov 30, 1995 · N338NW · Airbus A320211 · Fuel Boost PumpSDR 9509803238Engine · malfunctionedDURING ROTATION, AIRCRAFT YAWED TO THE LEFT ACCOMPANIED BY A LOUD AIR NOISE AND VIBRATION FELT IN THE COCKPIT. NO MESSAGES WERE INDICATED ON ECAM OR STATUS PAGE. OPERATING PROCEDURE WAS FOLLOWED AND THE AIRCRAFT RETURNED TO SEA WHERE AN UNEVENTFUL LANDING TOJun 24, 1995 · N338NW · Airbus A320211 · Engine (Turbine/Turboprop)
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