N329NW

Service difficulty reports · 218

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 = 'N329NW' 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 DALA2015112107210Seat Track · corrodedUPPER FLANGE IN PASSENGER CABIN CORROSION OUT LIMIT SEAT TRACK +Y1292, FRAME 35 TO 36, MEASURES ARE: FR 35 +8", L: 3.905", W: 0.381", D: 0.042'. REPLACED SEAT TRACK 1292 AND FASTENER LOCATED FRAME 35 TO FRAME 36 IAW SRM 51-72-11 AND DWG D53370124.Nov 20, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015112007113Web · corrodedCORROSION ON WEB BETWEEN FRAME 20 AND FRAME 24 MEASURES APPROXIMATELY L:0.210", W:0.190", D:0.003", RT SIDE AT FWD GALLEY AREA. REPLACED WEB BETWEEN FRAME 20 AND FRAME 24 RT SIDE AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53112783, D53114392. MEASURES OF CNov 19, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015112007112Attach Fitting · damagedWEAR FIXED BUSHING INBD LUG ON AILERON OTBD ATTACHMENT FITTING ACTUATOR ON RT WING, REPLACED BUSHING, 1EA ON INBD LUG ON AILERON OTBD FITTING ACTUATOR RT WING IAW CMM 57-61-21.Nov 19, 2015 · N329NW · Airbus A320211 · Wing, Attach FittingsSDR DALA2015112007111Floor Support · corrodedCORROSION ON FLOORBEAM -Y1162 BETWEEN FRAME 67+15" TO FRAME 69 MEASURES APPROXIMATELY L:0.300", W:0.175", D:0.003" AT AFT GALLEY AREA, REPLACED FLOORBEAM -Y1162 BETWEEN FRAME 67+15" TO FRAME 69 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000. MEASURE ARNov 19, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015112007110Floor Support · corrodedCORROSION ON FLOORBEAM -Y1225 BETWEEN FRAME 66+5" TO FRAME 67+15" MEASURES APPROXIMATELY L:0.400", W0.260", D:0.003", AT AFT GALLEY AREA, REPLACED FLOORBEAM -Y1225 BETWEEN FRAME 66+5" TO FRAME 67+15" AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000. MEANov 19, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015112007102Seat Track · crackedCRACK ON SEAT TRACK -Y765, FRAME 36 TO 41 IN PASSENGER CABIN, REPLACED SEAT TRACK -Y765 LOCATION BETWEEN FRAME 36 TO FRAME 41 IAW SRM 51-72-11 AND DWG D53370500 AND D57130147 MEASURE ARE: CRACK, L=0.980".Nov 19, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015111907116Seat Track · crackedCRACK ON SEAT TRACK -Y1292, FRAME 36 TO 41 IN PASSENGER CABIN, REPLACED SEAT TRACK -Y1292 FR36 TO 41 IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D53370500 MEASURE OF CRACK IS 0.517".Nov 18, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015111807109Skin · not reportedPERFORMED NEW REPAIR ON EXTERNAL SKIN TAIL CONE LT SIDE BETWEEN FRAME 84 TO FRAME 85 ON UPPER FUSELAGE IAW SRM 53-51-11, PARAGRAPH 5.B, FIG 203.Nov 17, 2015 · N329NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015111807108Seat Track · corrodedCORROSION ON FLOORBEAM -Y765 BETWEEN FRAME 12 TO FRAME 24 MEASURES APPROXIMATELY L:0.900", W:0.400", D:0.003" AT FWD GALLEY AREA, REPLACED SEAT TRACK -Y765 LOCATED BETWEEN FRAME 12 TO FRAME 24 IAW SRM 51-72-11 AND DWG D53110920 MEASURES OF CORROSION P1: FR20Nov 17, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015111807107Floor Support · corrodedCORROSION ON FLOORBEAM -Y189 BETWEEN FRAME 20 TO FRAME 23 MEASURES APPROXIMATELY L:1.5", W:1", D:0.002" AT FWD GALLEY AREA, REPLACED FLOORBEAM -Y189 BETWEEN FRAME 20 TO FRAME 23 SRM 51-72-11 AND DWG D53112834 MEASURES OF CORRODED AREA ARE L=2.362", W=1.189", Nov 17, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015111807106Skin · not reportedPERFORMED NEW REPAIR ON EXTERNAL SKIN ON FRAME 23 AND BETWEEN STR 22L TO STR 23L IAW SRM 53-00-11, PARA 4.W, REPAIR 7, FIG 238. RECHECK REQUIRED AT 60,000FC IAW SRI 53-00-11 PARA 32 IIR 53-00-11-2-017-00, TABLE 225, PAGE 289.Nov 17, 2015 · N329NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015111807105Skin · not reportedPERFORMED NEW REPAIR ON EXTERNAL SKIN BETWEEN FRAME 51 TO FRAME 52 AND BETWEEN STR 38R TO STR 39R IAW SRM 53-41-11, PAR 5F, REPAIR 4, FIG 207.Nov 17, 2015 · N329NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015111707104Floor Support · corrodedCORROSION ON FLOORBEAM +Y512 BETWEEN FR 64 TO FR 70 MEASURES APPROXIMATELY L=0.270", W=0.115", D=0.003" AT AFT GALLEY AREA. REPLACED FLOORBEAM Y512 BETWEEN FRAME 64 TO FRAME 70 IAW SRM 51-72-11 AND DWG D53472000 MEASURES OF CORROSION ARE L=1.484", W=0.371", DNov 16, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015111606996Floorbeam · damagedELONGATED HOLE CROSSBEAM SECTION ON FLOOR STRUCTURE AT AFT GALLEY AREA ON FRAME 68 STR 24L. REPLACED CROSSBEAM SECTION ON FLOOR STRUCTURE AT AFT GALLEY AREA ON FRAME 68 BETWEEN. STR 23L AND STR 24L IAW SRM 51-72-11 AND DWG D53470150. MEASURE OF ELONGATED HONov 16, 2015 · N329NW · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2015111606995Seat Track · corrodedCORROSION ON SEAT TRACK +Y1292 FRAME 47 TO 64 EVALUATED AND FOUND OUT OF LIMITS ON JC 2500-2032 IN PASSENGER CABIN. MEASURE OF REWORKED ARE: L=3.955, W=0.356, D=0.051. REPLACED SEAT TRACK +Y1292 LOCATED BETWEEN. FRAME 47 TO FRAME 64 IN PASSENGER CABIN. AS IAWNov 15, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015111606994Seat Track · corrodedCORROSION ON SEAT TRACK -Y1292 BETWEEN FRAME 12 TO FRAME 24 MEASURES APPROXIMATELY L=1", W=0.200", D=0.002" AT FWD GALLEY AREA. REPLACED SEAT TRACK -Y1292 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWGS NR D53112812, D531109Nov 15, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015111606993Seat Track · corrodedCORROSION OUT LIMIT SEAT TRACK +Y765, FRAME 41 TO 47 EVALUATED WITH JC 2500-2031 MEASURE ARE: FR 44+7", L=3.869", W=0.385", D=0.043", UPPER FLANGE IN PASSENGER CABIN. REPLACED SEAT TRACK +Y765 LOCATED BETWEEN FRAME 41 TO FRAME 47 IAW SRM 51-72-11 AND DWGS D53Nov 15, 2015 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015111606992Floor Support · corrodedCORROSION ON FLOORBEAM +Y254 BETWEEN, FRAME 12 TO FRAME 24 MEASURES APPROXIMATELY L=0.105", W=0.100", D=0.003" AT FWD GALLEY AREA, REPLACED FLOORBEAM +Y254 BETWEEN FRAME 12 TO FRAME 24 IAW SRM 51-72-11, MEASURE OF CORROSION ARE L=0.452", W=0.377", D=0.080Nov 15, 2015 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016112209099Stringer · corrodedEVIDENCE OF CORROSION FOUND ON STRINGER 43L BETWEEN FRAMES 56 - 57. CUT OUT THE DAMAGED STRINGER SECTION. FABRICATED NEW STRINGER AND COUPLINGS. ALODINED, PRIMED, PAINTED AND INSTALLED NEW PARTS IAW SRM.Apr 28, 2015 · N329NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016112209098Stringer · corrodedEVIDENCE OF CORROSION FOUND ON STRINGER 42L BETWEEN FRAMES 56 - 57. CUT OUT DAMAGED STRINGER SECTION. FABRICATED NEW STRINGER AND COUPLINGS. TREATED, PRIMED, PAINTED AND INSTALLED NEW PARTS IAW SRM.Apr 28, 2015 · N329NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2015042903008Skin · corrodedCORROSION ON SKIN OTBD OF STRINGER 42L BETWEEN FRAMES 56 & 57. BLENDED OUT DAMAGE IAW SRM 53-00-13 C/P WITH ERA 535534-14AD.Apr 28, 2015 · N329NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13062313229Wire · disconnectedDURING NON ROUTINE CHECK, FOUND TWO EMERGENCY LIGHTS AT ROW 9 INOPERATIVE. MAINTENANCE RECONNECTED LOOSE WIRE AND FUNCTIONAL CHECKED NORMAL.Nov 19, 2013 · N329NW · Airbus A320211 · Light System WiringSDR DALA13042753229Compressor · stalledDURING CRUISE, NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AT APPROXIMATELY 50 PERCENT N1. CREW DECLARED EMERGENCY AND FLIGHT WAS DEVERTED. ACFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED NR 1 ENGINE AND FUNCTIONAL CHECK WAS NORMAL.Sep 5, 2013 · N329NW · Airbus A320211 · Turbine Engine Compressor SectionSDR DALA12012493229Battery Pack · faultedDURING NON ROUTINE CHECK, FOUND RT EMERGENCY LIGHT BATTERY PACK 12WL FAULTED. MAINTENANCE REPLACED BATTERY PACK AT 12WL AND FUNCTIONAL CHECK WAS NORMAL.Nov 10, 2012 · N329NW · Airbus A320211 · Emergency LightingSDR DALA12009213229Battery · inoperativeDURING NON ROUTINE CHECK, FOUND EPSU BATTERY ON LEFT FAULT. MX REPLACED LEFT EPSU BATTERY AND FUNCTIONAL CHECK WAS NORMAL.Oct 3, 2012 · N329NW · Airbus A320211 · Emergency LightingSDR DALA12002963229Battery Pack · inoperativeDURING NON ROUTINE CHECK, FOUND EPSU 10 WON'T WORK. MAINTENANCE REPLACED EPSU AND BATTERY PACK. FUNCTIONAL CHECK WAS NORMAL.Jul 10, 2012 · N329NW · Airbus A320211 · Emergency LightingSDR DALA1221273229Terminal · damagedDURING NON ROUTINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHT AT SEAT 14C INOPERATIVE. MAINTENANCE REPAIRED TERMINAL END AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE.Apr 8, 2012 · N329NW · Airbus A320211 · Light System WiringSDR DALA1514953229Skin · crackedLEFT ELEVATOR SKIN CRACKED, FOUR INCHES OTBD OF RIB 7, TWO INCHES INBD AND ELEVEN INCHES AFT OF L/E. REPAIRED IAW 450968.Apr 4, 2012 · N329NW · Airbus A320211 · Elevator, Plate/SkinSDR DALA1514943229Skin · damagedRIGHT ELEVATOR DENTED AND CRACKED BETWEEN RIBS 8-9, TWENTY NINE INCHES INBD OF MOST OTBD HINGE, SEVEN INCHES AFT OF THE L/E. REPAIRED IAW 450963.Apr 4, 2012 · N329NW · Airbus A320211 · Elevator, Plate/SkinSDR DALA1514933229Bushing · corrodedNLG FORESTAY LT HINGE PIN BUSHING HAS CORROSION. REPAIRED AND REPLACED IAW 306875.Jan 17, 2011 · N329NW · Airbus A320211 · Fuselage, Landing Gear Attach FittingsSDR DALA1018343229Connector · damagedEMERGENCY LIGHT TEST FAULTED, REPAIRED EXIT LIGHT AT SEAT 11ABC CONNECTOR AND TESTS OK.Aug 4, 2010 · N329NW · Airbus A320211 · Light System WiringSDR DALA106583229Floor Support · corrodedDURING H-CHECK FOUND FLOOR SUPPORT HAS CORROSION AT Y-1732. REPLACED IAW SRM 51-10-04, 51-10-02, AND 51-21-11.Mar 27, 2010 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA106573229Seat Track · corrodedDURING H-CHECK, FOUND SEAT TRACK -Y1292 AT FR 66 AND 68 CORRODED. INSTALLED NEW SEAT TRACK IAW SRM 51-42-11.Mar 27, 2010 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA106563229Seat Track · corrodedDURING H-CHECK FOUND SEAT TRACK -Y1292 CORRODED AT FR68 AND 69. REPLACED SEAT TRACK IAW SRM 51-74-00, AND 51-42-11.Mar 27, 2010 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA106553229Seat Track · corrodedDURING H-CHECK, FOUND SEAT TRACK -Y1292 CORRODED AT FR64 AND 66. REPLACED SEAT TRACK IAW SRM 51-42-11.Mar 27, 2010 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA106543229Doubler · unknownDURING H-CHECK, REMOVED 4 SPLICES DOUBLER AT FR 66 AT DOOR 2 RT. INSTALLED NEW 4 SPLICE DOUBLER AND CLIPS IAW SRM 51-42-11.Mar 26, 2010 · N329NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA106283229Frame · chafedDURING (H) CHECK FOUND CHAFED AREA ON AFT FUSELAGE FRAME AT FR86. REPAIRED IAW SRM 51-42-11, 51-44-11, 51-75-12.Mar 25, 2010 · N329NW · Airbus A320211 · Fuselage Main, FrameSDR DALA106243229Support · corrodedDURING H-CHECK FOUND CORROSION ON LT SHEAR PLATE SUPPORT FRAME AT FR69-70. REPAIRED PER SRM 51-42-11, 51-74-00.Mar 24, 2010 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA106223229Skin · gougedDURING H-CHECK FOUND GOUGES ON FUSELAGE SKIN AT S43L-S44L BETWEEN FR50-FR51. REPAIRED PER SRM 53-00-11 FIGURE 222 AND 51-42-11.Mar 23, 2010 · N329NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA106203229Sill · corrodedDURING H-CHECK FOUND CORROSION ON DOOR R2 SILL. REPAIRED PER SRM 51-74-00, 51-42-11.Mar 22, 2010 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA106193229Structure · corrodedDURING H-CHECK FOUND CORROSION AT FR28 BETWEEN S41R-S42R. REPAIRED PER SRM 51-42-11.Mar 22, 2010 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA106093209Stringer · corrodedDURING H-CHECK FOUND CORROSION ON RIGHT STRINGER 43 BETWEEN FR 32 AND 33. REPAIRED PER SRM 53-21-13 FIGURE 3.Mar 21, 2010 · N329NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA106083229Floor Panel · damagedDURING H-CHECK FOUND FLOOR PANEL 261AB HAD SEVERAL DAMAGED INSERTS AND DAMAGED EDGES. REPLACED FLOOR PANEL PER DRAWING 3D25-37498.Mar 20, 2010 · N329NW · Airbus A320211 · Fuselage Floor PanelSDR DALA106073229Floor Panel · damagedDURING H-CHECK FOUND FLOOR PANEL 222CF HAD PUNCTURE DAMAGE AND A CRACK ON UPPER AND LOWER SURFACE. FABRICATED REPLACEMENT FLOOR PANEL PER DRAWING 3D25-37498.Mar 20, 2010 · N329NW · Airbus A320211 · Fuselage Floor PanelSDR DALA6063229Seat Track · corrodedDURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1292 BETWEEN FR68 AND FR69. REPAIRED PER SRM 51-42-11.Mar 20, 2010 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA106043229Seat Track · corrodedDURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1292 BETWEEN FR66 AND FR 68. REPAIRED PER SRM 51-42-11.Mar 20, 2010 · N329NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA106053264Floor Support · corrodedDURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT WEB AT -Y1732 FR20. REPAIRED PER SRM 51-42-11.Mar 19, 2010 · N329NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA106033229Structure · corrodedDURING H-CHECK FOUND CORROSION ON RT ENTRY DOOR AT FR 20 FORWARD FACE 1 INCH FROM FLOOR LEVEL AND 4.5 INCHES IN FROM INBOARD EDGE. TEMPORARY REPAIR PER ERA 480337-14 SECTION I. SECTION II REQUIRES REPETITIVE INSPECTION AT EVERY 500 FLIGHT CYCLES AFTER SECTIOMar 19, 2010 · N329NW · Airbus A320211 · Passenger/Crew DoorsSDR DALA105953229Stringer · corrodedDURING H-CHECK FOUND CORROSION ON STRINGER S31R FR 65. REPAIRED PER SRM 51-44-11, 51-42-11.Mar 18, 2010 · N329NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA105623229Sill · corrodedDURING "H" CHECK FOUND CORROSION ON R2 DOOR SILL AT FR66. REPAIRED IAW SRM 51-43-14.Mar 16, 2010 · N329NW · Airbus A320211 · Fuselage Miscellaneous Structure
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