N340NW

Service difficulty reports · 216

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 = 'N340NW' 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 DALA2015052103409Skin · damagedEXISTING REPAIR FOUND AT EXTERNAL FUSELAGE SKIN FWD NOSE AREA NEAR THE FWD NOSE JACKING POINT. THE EXISTING REPAIR HAD 1 FASTENER LOCATION ELONGATED THROUGH DOUBLER TRIPLER SKIN, INTERNAL DOUBLER AND FRAME. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN 22" BELOMay 20, 2015 · N340NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015051703307Web · corrodedCORROSION ON WEB STRINGER 38R IN AFT CARGO BAY BETWEEN FRAMES 56 - 57. REPLACED THE WEB IAW PRI 535318-14 REV. 0, 1 AND ER/A 535318-14, REV ORIGINAL.May 16, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2016112209087Channel · corrodedCORROSION ON DRY BAY UPPER CHANNEL BETWEEN RIBS 5 AND 6 ON LT WING. REPLACED THE CHANNEL.May 14, 2015 · N340NW · Airbus A320212 · Wing Miscellaneous StructureSDR DALA2015051503299Skin · dentedDURING INSPECTION, FOUND A DENT ON UPPER SKIN, FRAME 85+18 LT SIDE ON TAIL. PERFORMED PERMANENT REPAIR ON UPPER SKIN IAW PRI 535335-14, REV O,1 AND 2 AND ER/A 535335-14.May 14, 2015 · N340NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2016112209088Stringer · corrodedCORROSION ON STRINGER 43L IN AFT CARGO BAY BETWEEN FRAMES 54 TO 55. REPAIRED THE STRINGER.May 12, 2015 · N340NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015051303218Stringer Splice · corrodedDURING INSPECTION, FOUND CORROSION ON SPLICE AT AFT GALLEY AREA ON STRINGER 27L FRAME 67. REPLACED THE STRINGER SPLICE IAW SRM 51-72-11, DWG D5348002 AND ER/A NR 535322-14, REV 0.May 12, 2015 · N340NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2017071905550Repair · out of limitsEXTERNAL SKIN AT LOWER FUSELAGE FROM FRAME 63 TO FRAME 63+9.5" BETWEEN STRINGER 24L TO STRINGER 28L EXISTING REPAIR OUT OF LIMITS, PERMANENT REPAIR PER ER/A 535338-14 REV 0.May 11, 2015 · N340NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015051103172Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND EPSU 10WL INOPERATIVE AT FWD GALLEY AREA. REPLACED EPSU AND OPS TEST WAS GOOD.May 10, 2015 · N340NW · Airbus A320212 · Emergency LightingSDR DALA2015051103171Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 833 LT LOAD TRANSMITTING PROFILE. REPLACED IAW SRM 51-72-11 AND DWG D52279010.May 10, 2015 · N340NW · Airbus A320212 · Emergency ExitsSDR DALA2015051103170Door Frame · crackedDURING INSPECTION, FOUND A CRACK ON EMERGENCY EXIT DOOR 834 SEGMENT FRAME. REPLACED THE FRAME ON EMERGENCY EXIT DOOR IAW SRM 51-72-11 AND DWG D52279010.May 10, 2015 · N340NW · Airbus A320212 · Emergency ExitsSDR DALA2015050803135Tee Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON EMERGENCY EXIT DOOR 834 ON SECTION-T RT IN PASSENGER CABIN L=0.320", W=0.250", D=0.002". REPLACED SECTION T ON EMERGENCY EXIT DOOR 834 RT IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279010.May 7, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2017071905549Skin Panel · nickedNICK WAS FOUND ON FWD FUSELAGE SKIN PANEL OUTER SURFACE AT FR27+17.5INCH BETWEEN STR 41R AND STR 42R, PERFORMED PERMANENT REPAIR PER ERA 534567-14 REV ORIGINAL.May 6, 2015 · N340NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2016112209092Stringer · corrodedCORROSION ON STRINGER 41R BETWEEN FRAMES 50 TO 51. REPAIRED THE STRINGER IAW ER/A.May 6, 2015 · N340NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2016112209091Stringer · corrodedCORROSION ON STRINGER 40R , FRAMES 51 TO 52. REPAIRED THE STRINGER IAW ER/A.May 6, 2015 · N340NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2016112209090Strap · corrodedCORROSION ON STRAP, STRINGERS 27 - 28L, FRAME 67. REPAIRED THE STRAP IAW ER/A.May 6, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2016112209089Skin · corrodedCORROSION UNDER FWD SCUFF PLATE ON EXTERNAL SKIN AT LOWER FUSELAGE BETWEEN FRAMES 16 TO 17. REPAIRED THE SKIN IAW ER/A.May 6, 2015 · N340NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015050703129Fitting · crackedDURING INSPECTION, FOUND CRACK ON FITTING CORNER AT LEVEL FRAME 28 IN FWD CARGO COMPARTMENT BETWEEN STR 36R TO STR 38R, SSI 532180. REPLACED FITTING CORNER AT LEVEL FR 28 IN FWD CARGO COMPARTMENT BETWEEN STR 36R AND 38R IAW SRM 51-72-11 AND DWG D53231668.May 6, 2015 · N340NW · Airbus A320212 · Fuselage Main, Attach FittingsSDR DALA2015050703128Door Frame · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 834 ON SEGMENT FRAME RT IN PASSENGER CAB IN L=0. 800". ATTACH FORM 5100-3201, SSI 522102-01-1, REPLACED SEGMENT FRAME ON EMERGENCY EXIT DOOR 834 RT ON PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279010.May 6, 2015 · N340NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2016112209093Skin · corrodedCORROSION ON EXTERNAL SKIN UNDER SCUFF PLATE LT SIDE BETWEEN FRAMES 16 TO 20. REPAIR THE SKIN IAW ER/A.May 5, 2015 · N340NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015050603114Door Frame · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 844 SEGMENT FRAME LT IN PASSENGER CABIN, L=0.780". ATTACH FORM 5100-3201, SSI 522102-01-1. REPLACED SEGMENT FRAME LT ON EMERGENCY EXIT DOOR 844 IAW SRM 51-72-11 AND DWG D52279040, D52279010.May 5, 2015 · N340NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2015050603112Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 834 ON LT LOAD TRANSMITTING PROFILE IN PASSENGER CABIN, L=0.350". ATTACH FORM 5100-3201 AND SSI 522102-01-1. REPLACED TRANSMITTING PROFILE LOCATED ON EMERGENCY EXIT DOOR 834 IN PASSENGER CABIN IAW SRM 51-May 5, 2015 · N340NW · Airbus A320212 · Emergency ExitsSDR DALA2015050603111Door Frame · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 833 ON RT SEGMENT FRAME IN PASSENGER CABIN, L=0.572". ATTACH FORM 5100-3201 AND SSI 522102 -01-1. REPLACED SEGMENT FRAME RT ON EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279040May 5, 2015 · N340NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2015050603110Door Frame · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 844 ON SEGMENT FRAME RT IN PASSENGER CABIN, L=0.200". ATTACH FORM 5100-3201, SSI 522102-01 -1. REPLACED SEGMENT FRAME RT ON EMERGENCY EXIT DOOR 844 IAW SRM 51-72-11 AND DWG D52279040, D52279010.May 5, 2015 · N340NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2015050603109Tee Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON EMERGENCY EXIT DOOR 844 ON LT SECTION-T IN PASSENGER CABIN L=0.225", W=0.100", D=0.002". ATTACH FORM IF CORROSION LEVEL 2 OR GREATER AND SSI 522102-01-1. REPLACED LT SECTION -Y OF EMERGENCY EXIT DOOR 844 IAW SRM 51-72-May 5, 2015 · N340NW · Airbus A320212 · Emergency ExitsSDR DALA2015050603095Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 834 ON RT LOAD TRANSMITTING PROFILE IN PASSENGER CABIN L=0.820". ATTACH FORM 5100-3201, SSI 522102-01-1. REPLACED LOAD TRANSMITTING PROFILE LOCATED ON EXIT DOOR 834 IN PASSENGER CABIN IAW SRM 51-72-11 ANMay 5, 2015 · N340NW · Airbus A320212 · Emergency ExitsSDR DALA2015050503108Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 833 ON RT LOAD TRANSMITTING PROFILE IN PASSENGER CABIN, L=0.279". ATTACH FORM 5100-3201 AND SSI522102-01-1. REPLACED SEGMENT, PROFILE AND FASTENERS LOCATED ON EMERGENCY EXIT DOOR 833 ON RT LOAD TRANSMITTIMay 4, 2015 · N340NW · Airbus A320212 · Emergency ExitsSDR DALA2015050503107Threshold · corrodedDURING INSPECTION, FOUND CORROSION ON THRESHOLD SHEET IN AFT CARGO COMPARTMENT BETWEEN FRAME 52A TO FRAME 56, L=1.300", W=1.131", D=0.002". MEASURES APPROXIMATE, REPLACED THRESHOLD SHEET IN AFT CARGO COMPARTMENT BETWEEN FRAME 52A TO FRAME 56 IAW SRM 51-72-11 May 4, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050403106Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 843 ON RT LOAD TRANSMITTING PROFILE IN PASSENGER CABIN, L=0.430. ATTACH FORM 5100-3201 AND SSI522102-01-1. REPLACED RT LOAD TRANSMITTING PROFILE ON EMERGENCY EXIT DOOR 843 IN PASSENGER CABIN IAW SRM 51-72May 3, 2015 · N340NW · Airbus A320212 · Emergency ExitsSDR DALA2015050403105Door Frame · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 843 ON RT SEGMENT FRAME IN PASSENGER CABIN L=0.790". ATTACH FORM 5100-3201 AND SSI 522102-01-1. REPLACED RT SEGMENT FRAME ON EMERGENCY EXIT DOOR 843 IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279020.May 3, 2015 · N340NW · Airbus A320212 · Emergency ExitsSDR DALA2015050403104Door Frame · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 843 ON LT SEGMENT FRAME IN PASSENGER CABIN, L=0.300". ATTACH FORM 5100-3201 AND SSI 522102-01-1. REPLACED LT SEGMENT FRAME IN PASSENGER EMERGENCY EXIT DOOR IAW SRM 51-72-11 AND DWG D52279020. MEASURE OF CRMay 3, 2015 · N340NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2015050403103Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR 843 ON LT LOAD TRANSMITTING PROFILE IN PASSENGER CABIN L=0.700". ATTACH FORM 5100-3201 AND SSI 522102-01-1. REPLACED LT LOAD TRANSMITTING PROFILE ON EMERGENCY EXIT DOOR 843 IN PASSENGER CABIN IAW SRM 51-May 3, 2015 · N340NW · Airbus A320212 · Emergency ExitsSDR DALA2015050303099Structure · corrodedDURING INSPECTION, FOUND CORROSION ON COVER SHEET ALONG IN AFT CARGO COMPARMENT BETWEEN FRAME 52A TO FRAME 56, L=1.50", W=1.700", D=0.002". MEASURES APPROXIMATELY SSI 534107. REPLACED COVER SHEET LOCATED IN AFT CARGO COMPARTMENT BETWEEN FRAME 52A TO FRAME 56May 2, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2016112209097Seat Track · corrodedSEAT TRACK CORRODED -Y765, FRAMES 47 TO 64. REPLACED THE SEAT TRACK IAW SRM.Apr 28, 2015 · N340NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016112209096Fitting · corrodedCORROSION ON SPIGOT RECEPTACLE FITTING UPPER SPAR BORE OF THE LT PYLON. REPLACED SPIGOT RECEPTABLE FITTING IAW SRM.Apr 28, 2015 · N340NW · Airbus A320212 · Nacelle/Pylon, Main FrameSDR DALA2016112209095Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 26R, FRAME 67. REPLACED THE STRINGER SPLICE IAW SRM.Apr 28, 2015 · N340NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015042903009Fitting · corrodedCORROSION ON CENTER FITTING. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53480019.Apr 28, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042903006Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1292 FRAMES 64 TO 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Apr 28, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042903003Seat Track · corrodedCORROSION ON SEAT TRACK -Y765, FRAMES 41 TO 47. FOUND OUT OF LIMITS IAW AMDS 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Apr 28, 2015 · N340NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015042903002Fitting · corrodedCORROSION ON CORNER FITTING FRAME 68 STRINGER 23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DRW D534-80019.Apr 28, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042903001Seat Track · corrodedCORROSION ON SEAT TRACK -Y765, FRAMES 36 TO 41. FOUND OUT OF LIMITS IAW AMDS 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Apr 28, 2015 · N340NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015042903000Seat Track · corrodedCORROSION ON SEAT TRACK -Y1292, FRAMES 41 TO 47. FOUND OUT OF LIMITS IAW AMDS 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371112.Apr 28, 2015 · N340NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015042902999Seat Track · corrodedCORROSION ON SEAT TRACK -Y1292, FRAMES 36-41. FOUND OUT OF LIMITS IAW AMDS 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D57130147.Apr 28, 2015 · N340NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015042902998Structure · corrodedCORROSION ON LOWER SILL BETWEEN FRAME 66 TO FRAME 68 AT STR 23R AT AFT GALLEY AREA L=2", W=1", D=0.002. REPLACED LOWER SILL BETWEEN FRAME 66 TO FRAME 68 AT STR 23R AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019. MEASURES OF DAMAGE AREA ARE L=2.886", WApr 28, 2015 · N340NW · Airbus A320212 · Fuselage Structure (General)SDR DALA2015042902997Fitting · corrodedCORROSION ON CORNER FITTING AT FRAME 66 STRINGER 23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D534-80019.Apr 28, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042802996Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1162 AT AFT GALLEY AREA FROM FRAMES 68 TO 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Apr 27, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042802995Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1225 AT AFT GALLEY AREA FROM FRAMES 66 TO 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Apr 27, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042802994Stringer · corrodedCORROSION ON STRINGER 25R AT AFT GALLEY AREA BETWEEN FRAME 64 TO 66. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53480020.Apr 27, 2015 · N340NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015042802993Stringer · corrodedCORROSION ON STRINGER 26R AT AFT GALLEY AREA BETWEEN FRAME 64 TO 66. REPLACED STRINGER 26R IAW SRM 51-72-11 AND DWG D53480020.Apr 27, 2015 · N340NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015042702992Fitting · corrodedCORROSION ON SPIGOT RECEPTACLE FITTING UPPER SPAR ON RT PYLON. REPLACED SPIGOT RECEPTACLE FITTING UPPER SPAR ON RT PYLON IAW SRM 54-51-12.Apr 26, 2015 · N340NW · Airbus A320212 · Nacelle/Pylon Miscellaneous StructureSDR DALA2015042702989Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231MF IN PASSENGER CABIN. FOUND OUT OF LIMITS IAW SRM 53-02-00, TABLE 103 AND WAS REPLACED IAW SRM 53-02-00, PAR 8H, FIG 209.Apr 26, 2015 · N340NW · Airbus A320212 · Fuselage Floor Panel
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