N359NW

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 = 'N359NW' 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 DALA2021062403426Indicator · inoperativeSHIP 3259 AFT RIGHT CABIN DOOR CLOSED IND INOP. CORRECTIVE ACTION: REMOVED AND REPLACED 2R DOOR SLIDE ARMED LIGHT ASSY (3WN2) PER IAW A320 AMM 52-73. OPS TEST GOOD. (7837000)Jun 23, 2021 · N359NW · Airbus A320212 · Door Warning SystemSDR DALA2021070203684Stop Fitting · crackedSHIP 3259 REF AA CARD: 5311-01229-01, L1 DOOR STOP #1 AT FR 16, HAS CRACK INDICATION IN THE FRAME AT #3 HOLE. CORRECTIVE ACTION: REPAIRED PER 5311-01229-01. (1753226)Mar 12, 2021 · N359NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021070203683Stop Fitting · crackedSHIP 3259 REF AA CARD : 5311-01229, R1 DOOR STOP #7 AT FR 16, HAS CRACK INDICATION IN THE INTERCOSTAL AT #1 HOLE. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD AMDS 5311-01229. (1753067)Mar 12, 2021 · N359NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021070203682Stop Fitting · crackedSHIP 3259 REF AA CARD : 5311-01229-01, R1 DOOR STOP #7 AT FR 16, HAS CRACK INDICATION IN THE INTERCOSTAL AT #3 HOLE. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD 5311-01229-01. (1753063)Mar 12, 2021 · N359NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021020900752Door · no testSHIP 3259 DURING TEST SEAT 21ABC PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPS CK GOOD. (7583873)Feb 8, 2021 · N359NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2021020900751Door · no testSHIP 3259 DURING TEST SEAT 3DEF PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPS CK GOOD. (7583872)Feb 8, 2021 · N359NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2020122804319Proximity Sensor · malfunctionedATB-DUE TO LGCIU 1 FAULT WITH AMBER GEAR INDICATION WITH GEAR UP. CORRECTIVE ACTION: REPLACED 14GA PROXIMITY SENSOR AND CONNECTOR.Dec 27, 2020 · N359NW · Airbus A320212 · Landing Gear Position and WarningSDR DALA2020032302008Electrical Box · defectiveDURING PUSHBACK RECEIVED REPORT FROM FLT LEADER OF SMOKE+ ELECTRICAL BURNING SMELL COMING FROM IFE @ 3A+3B; MAINTENANCE WAS UNABLE TO DETERMINE IF OUTLET, CORD OR DEVICE PLUGGED IN WAS AT FAULT, REPLACED SEB AT 3A P/N: RD-FA3124-02Mar 16, 2020 · N359NW · Airbus A320212 · AC Power Distribution SystemSDR DALA2019091505359Frame · crackedCRACK INDICATED AND VERIFIED AT FR16 RH HOLE H3, MODIFIED FRAME PER ERA 580171-14AD REV ORIG SECT 1 AND ERA 581196-14AD REV ORIG SEC 1. COMPLIED WITH PRI 580171-14 REV A PRI REV 0 AND REV 1 AND PRI 581196-14AD PRI REV 0 AND REV 1.Sep 14, 2019 · N359NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2019091505358Frame · crackedCRACK INDICATED AND VERIFIED AT FR16 RH HOLE H2, MODIFIED FRAME PER ERA 580171-14AD REV ORIG SECT 1 AND ERA 581196-14AD REV ORIG SEC 1. COMPLIED WITH PRI 580171-14 REV A PRI REV 0 AND REV 1 AND PRI 581196-14AD PRI REV 0 AND REV 1.Sep 14, 2019 · N359NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2019091405357Frame · damagedFRAME #20, HOLE #36 DAMAGED AND OUT OF ROUND UNABLE TO COMPLETE REQUIRED HFEC INSPECTION. DIA OF HOLE IS .159, MODIFIED FRAME PER ERA 580171-14AD REV ORIG SECT 1 AND ERA 581191-14AD REV ORIG SEC 1. COMPLIED WITH PRI 580171-14 REV A PRI REV 0 AND REV 1 AND PRI Sep 14, 2019 · N359NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2019091405356Frame · damagedFRAME #20, HOLE #28 DAMAGED AND OUT OF ROUND UNABLE TO COMPLETE REQUIRED HFEC INSPECTION. DIA OF HOLE IS .159, MODIFIED FRAME PER ERA 580171-14AD REV ORIG SECT 1 AND ERA 581191-14AD REV ORIG SEC 1. COMPLIED WITH PRI 580171-14 REV A PRI REV 0 AND REV 1 AND PRI Sep 14, 2019 · N359NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2019091405351Frame · crackedFRAME #20, HOLE #26 HAS CRACK INDICATION, MODIFIED FRAME PER ERA 580171-14AD REV ORIG SECT 1 AND ERA 581191-14AD REV ORIG SEC 1. COMPLIED WITH PRI 580171-14 REV A PRI REV 0 AND REV 1 AND PRI 581191-14AD PRI REV 0 AND REV 1.Sep 14, 2019 · N359NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2019091405350Frame · crackedFRAME #20, HOLE #18 HAS CRACK INDICATION, MODIFIED FRAME PER ERA 580171-14AD REV ORIG SECT 1 AND ERA 581191-14AD REV ORIG SEC 1. COMPLIED WITH PRI 580171-14 REV A PRI REV 0 AND REV 1 AND PRI 581191-14AD PRI REV 0 AND REV 1.Sep 14, 2019 · N359NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2019090605190Damper · inoperativeAFT LEFT PASSENGER DOOR FAILED DAMPER CHECK, SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0168:5210-7089-LA/ 001 00294 RIGGED PER AMM REMOVED AND REPLACED DOOR DAMPER PER AMM 52-13-14 CYLINDER, DOOR.Sep 6, 2019 · N359NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2019062703897Light · damagedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED, REPLACED 19D SEAT EMG LIGHTJun 24, 2019 · N359NW · Airbus A320212 · Emergency LightingSDR DALA2018060903915Cylinder · low pressureR2 AND L2 DOOR DAMPER AND EMERGENCY CYLINDER BOTTLE PRESSURE LOW. SERVICED. OPERATION CHECKS GOOD.Jun 5, 2018 · N359NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2018060903914Cylinder · low pressureL1 AND R1 DOOR DAMPER AND EMERGENCY CYLINDER BOTTLE PRESSURE LOW. SERVICED. OPERATION CHECKS GOOD.Jun 5, 2018 · N359NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2019102506145Skin · damagedFUSELAGE SKIN FR35-FR36 STRG 1L-STRG 1R DRILLED FASTENER HOLE THROUGH CHEM-MILLED STEP ON UPPER FUSELAGE, PERFORMED SECTION I PERMANENT REPAIR AT FUSELAGE SKIN FR35-FR36 STRG 1L STRG 1R. AS PER PRI 562500-14 REV. 0 AND REV. 1 AND ER/A 562500-14. REV. ORIGINAL.Oct 16, 2017 · N359NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2017092507120Pin · corrodedDURING LEFT MAIN LANDING GEAR INSTALLATION, THE AFT PINTLE PIN WAS FOUND TO BE CORRODED, REPLACED THE PINTLE IAW AMDS CARD 3210-9601-LT/002 NR 00011.Sep 22, 2017 · N359NW · Airbus A320212 · Main Landing Gear Strut/Axle/TruckSDR DALA2016102507602Box Beam · crackedRIGHT SIDE BOX BEAM CRACK INDICATION OF BEAM CENTER HOLE FRAME 43. REPAIRED IAW AMDS 5310-01450-02.Oct 24, 2016 · N359NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2016102507601Box Beam · crackedLEFT SIDE BOX BEAM CRACK INDICATION ON UPPER PRESSURE PLATE CENTER LOCATION, REPLACED IAW AMDS 5310-01450-02.Oct 24, 2016 · N359NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2015110206722Frame · corrodedCORROSION ON FRAME 16 AT Z-520, LEVEL RT SIDE AT FWD GALLEY AREA, PERFORMED PERMANENT REPAIR ON FRAME 16 AT Z-520 LEVEL RT SIDE IAW ERA 535752-14, REV "B", SECTION "1".Oct 29, 2015 · N359NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2015102806726Door · crackedDOOR 831 WAS FOUND CRACKED ON FWD UPPER CORNER. REPLACED FWD UPPER CORNER LOCATED ON DOOR 831 LT SIDE IAW SRM 51-72-11 AND DWG D52110475. MEASURE OF CRACK IS L=1.290".Oct 27, 2015 · N359NW · Airbus A320212 · DoorsSDR DALA2015102806725Door · crackedDOOR 831 WAS FOUND CRACK ON AFT UPPER CORNER. REPLACED AFT UPPER CORNER LOC. ON DOOR 831 IAW SRM 51-72-11 AND DWG D52110475. MEASURES OF CRACK IS L=1.442".Oct 27, 2015 · N359NW · Airbus A320212 · DoorsSDR DALA2015102806656Stringer · corrodedCORROSION ON STR 43L IN AFT CARGO COMPARTMENT FROM FRAME 61 TO FRAME 62, L=0.550, W=0.400 ; D=0.001. PERMANENT REPAIR IAW SRM 51-42-11, 51-72-11 AND 53-00-13, ITEM 7, FIG 201.Oct 27, 2015 · N359NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015102706526Support Angle · corrodedCORROSION SUPPORT ANGLE ON FRAME 71 BETWEEN STRINGERS 27 - 32R. REPLACED THE SUPPORT ANGLE IAW SRM 51-72-11 AND DWG D53571510.Oct 26, 2015 · N359NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015102606425Trunnion · corrodedWEAR ON TRUNNION INBD FLAP FOUND OUT LIMITS LT WING. REPLACED TRUNNION IAW CMM 57-21-21-400-806-C01.Oct 25, 2015 · N359NW · Airbus A320212 · Wing, Control Surface Attach FittingsSDR DALA2015102606424Trunnion · corrodedWEAR ON TRUNNION INBD FLAP FOUND OUT LIMITS. REPLACED TRUNNION OF INBD. FLAP RT IAW CMM 57-21-21-400-806-C01.Oct 25, 2015 · N359NW · Airbus A320212 · Wing, Control Surface Attach FittingsSDR DALA2015102606411Shear Tie · corrodedCORROSION ON CLEAT FRAME 30 LT IN FWD CARGO COMPARTMENT BETWEEN STR 43L TO STR 44. REPLACED CLEAT LOCATED AT FRAME 30 BETWEEN STR 43L TO STR 44 IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231626.Oct 25, 2015 · N359NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015102506423Floor Support · corrodedCORROSION ON LOWER SILL LT AT AFT GALLEY AREA . REPLACED LOWER SILL LOCATED BETWEEN FRAME 66 TO FRAME 68 AT LEVEL STR 23 LT SIDE AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.Oct 24, 2015 · N359NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015102506422Floor Support · corrodedCORROSION RT ON LOWER SILL AT AFT GALLEY AREA. REPLACED LOWER SILL LOCATED BETWEEN FRAME 66 TO FRAME 68 AT LEVEL STR 23R AFT GALLEY AREA FLOOR STRUCTURE IAW SRM 51-72-11 AND DWG NR D53480019.Oct 24, 2015 · N359NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015102506421Stringer · corrodedCORROSION ON STR 42L IN FWD CARGO COMPARTMENT ON FRAME 32. PERFORMED PERMANENT REPAIR ON STRINGER SECTION 42L IN FWD CARGO COMPARTMENT FROM FRAME 30+16 TO FRAME 32+12" SRM 53-00-13, PARA 4A, FIG 201.Oct 24, 2015 · N359NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015102506420Shear Tie · corrodedCORROSION ON CLEAT FRAME 28 RT IN FWD CARGO COMPARTMENT BETWEEN STR 43R TO STRINGER 44. REPLACED CLEAT FRAME 28, RT IN FWD CARGO COMPARTMENT BETWEEN STR 43R TO STR 44 IAW SRM 51-72-11 AND DWG D53231712, D53231617.Oct 24, 2015 · N359NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015102506419Shear Tie · corrodedCORROSION ON CLEAT FRAME 33 RT IN FWD CARGO COMPARTMENT BETWEEN STR 40R TO STR 41R. REPLACED CLEAT LOCATED AT FR33 BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231586, D53231535.Oct 24, 2015 · N359NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015102506418Shear Tie · corrodedCORROSION ON CLEAT FRAME 28 LT IN FWD CARGO COMPARTMENT BETWEEN STR 41L TO STR 42L. REPLACED CLEAT LOCATED ON FRAME 28 BETWEEN STR 41L TO STR 42L IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231712.Oct 24, 2015 · N359NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015102506417Shear Tie · corrodedCORROSION ON CLEAT FRAME 32 LT IN FWD CARGO COMPARTMENT BETWEEN STR 41L TO STR 42L (SSI 532180). REPLACED CLEAT LOCATED AT FRAME 32 IN FWD CARGO COMPARTMENT BETWEEN STR 41L TO STRINGER 42L IAW SRM 51-72-11 AND DWG D53230385.Oct 24, 2015 · N359NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015102506416Shear Tie · corrodedCORROSION ON CLEAT FRAME 33 LT IN FWD CARGO COMPARTMENT BETWEEN STR 41L TO STR 42L. REPLACED CLEAT FR 33 LT IN FWD CARGO COMPARTMENT BETWEEN STR 41L TO STRINGER 42L AS IAW SRM 51-72-11 AND DWG D53230385.Oct 24, 2015 · N359NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015102506415Shear Tie · corrodedCORROSION ON CLEAT FRAME 28 LT IN FWD CARGO COMPARTMENT BETWEEN STR 40L TO STR 41L SSI 532180. REPLACED CLEAT AND FASTENERS LOCATED ON FRAME 28 LT SIDE IN FWD CARGO COMPARTMENT BETWEEN STR 40L TO STR 41L IAW SRM A320 51-72-11 AND DWG D53231712.Oct 24, 2015 · N359NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2015102506414Shear Tie · corrodedCORROSION ON CLEAT FRAME 26 LT IN FWD CARGO COMPARTMENT BETWEEN STR 42L TO STRINGER 43L. REPLACED CLEAT LOCATED AT FRAME 26 IN FWD CARGO COMPARTMENT BETWEEN STR 42L TO STRINGER 43L IAW SRM 51-72-11 AND DWG D53231712.Oct 24, 2015 · N359NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2015102306406Skin · crackedCRACK ON OTBD FIXED L/E SKIN AT RIB 15 ON LT WING. REPAIRED OTBD FIXED L/E SKIN AT LEVEL RIB 15 ON LT WING IAW SRM 57-41-11, FIG 206.Oct 22, 2015 · N359NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2015102306405Shear Tie · corrodedCORROSION ON CLEAT FRAME 26 LT IN FWD CARGO COMPARTMENT BETWEEN STR 41L TO STR 42L. REPLACED CLEAT ON FRAME 26 IN FWD CARGO COMPARTMENT BETWEEN STR 41L TO STR 42L IAW SRM 51-72-11 AND DWG D53230324.Oct 22, 2015 · N359NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015102306404Seat Track · corrodedCORROSION OUT LIMITS ON SEAT TRACK +Y1292, FRAME 36 - 41. REPLACED SEAT TRACK IAW DWG D53370500.Oct 22, 2015 · N359NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015102206321Shear Tie · corrodedCORROSION ON CLEAT FRAME 30 IN FWD CARGO COMPARTMENT BETWEEN STR 41L TO STR 42L. REPLACED CLEAT LOCATED AT FRAME 30 BETWEEN STR 41L TO STR 42L IAW SRM 51-72-11 AND DWG D53231712; D53230320.Oct 21, 2015 · N359NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015102206320Shear Tie · corrodedCORROSION ON CLEAT FRAME 31 LT IN FWD CARGO COMPARTMENT BETWEEN STR 41L TO STR 42L. REPLACED CLEAT AT FR 31 BETWEEN STR 41L TO STR 42L FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231712.Oct 21, 2015 · N359NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015102206319Seat Track · not reportedOUT OF LIMIT SEAT TRACK +Y1292 FRAMES 41 - 47 EVALUATED WITH JC 2500-2031 MEASURE AFTER REWORK ARE: FRAME 44+6", L=4.825"; W=0.321"; D=0.073" IN PASSENGER CABIN. REPLACED SEAT TRACK Y1292 FRAME 41 TO FRAME 47 IAW SRM 51-72-11.Oct 21, 2015 · N359NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015102206318Profile · crackedCRACK ON LOAD TRANSMITTING PROFILE EMERGENCY EXIT DOOR 833 FWD SIDE IN PASSENGER CABIN. REPLACED LOAD TRANSMITTING PROFILE EMERGENCY EXIT DOOR 833 FWD SIDE IAW SRM 51-72-11 AND DWG D52279036.Oct 21, 2015 · N359NW · Airbus A320212 · Emergency ExitsSDR DALA2015102006309Shear Tie · corrodedCORROSION ON CLEAT FR 29 L/I FWD CARGO COMPARTMENT BETWEEN STR 41L TO STR 42L. REPLACED CLEAT LOCATED AT FR 29 BETWEEN STR 41L TO STR 42L IAW SRM 51-72-11 AND DWG D53231712, D53230324.Oct 19, 2015 · N359NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015101906240Stringer · corrodedCORROSION ON STRINGER 43L IN FWD CARGO BAY FRAME 29. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53231712.Oct 18, 2015 · N359NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015101906239Shear Tie · corrodedCORROSION ON CLEAT FR 26 LT IN FWD CARGO COMPARTMENT BETWEEN STR 40L TO STR 41L. REPLACED CLEAT LOCATED ON FR 26 IN FWD CARGO COMPARTMENT BETWEEN STR 40L TO STR 41L IAW SRM 51-42-11, 51-72-11 AND DWG D53231712.Oct 18, 2015 · N359NW · Airbus A320212 · Fuselage Internal Mounting Structure
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