N378NW

Service difficulty reports · 178

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 = 'N378NW' 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 DALA2023090807359Unknown · unknownSHIP 3278 A CRACK WAS FOUND IN FR 16 RHS AT HOLE B. CORRECTIVE ACTION: COMPLIED WITH ERA 587478-14AD. (1615327)Sep 16, 2020 · N378NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2020091403065Hinge Fitting · corrodedCORROSION HINGE FITTING LUG NR 2 ELEVATOR ON RT HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED BUSHINGS (2EA) OF HINGE FITTING NR 2 ELEVATOR RT HORIZONTAL STABILIZER, AS PER AIRBUS CMM 55-21-15.Sep 12, 2020 · N378NW · Airbus A320211 · Elevator StructureSDR DALA2020091103044Skin · gougedSHIP 3278, GOUGE EXTERNAL SKIN AT LEVEL OF FR23 AND STRG 23L ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR INSTRUCTIONS ON EXTERNAL SKIN AT LEVEL OF STR.23L FR 23 ON UPPER FUSELAGE, AS PER PRI 587548-14 REV. 0 AND ER/A 587548-14 REV ORIGINASep 11, 2020 · N378NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2020091603097Skin · corrodedCORROSION INLET VALVE AIR SKIN IN FWD AVIONIC COMPARTMENT. CORRECTIVE ACTION: REPLACED INLET VALVE AIR SKIN IN FWD AVIONIC COMPARTMENT, AS PER A320 FAM AMM 21-26.Sep 10, 2020 · N378NW · Airbus A320211 · Pressure Regulator/Outflow ValveSDR DALA2020091103049Web · crackedSHIP 3278, CRACK INDICATION ON WEB AT OPEN FASTENER HOLE COMMON TO AFT LT T ANGLE POSITION, IN MAIN WHEEL WELL. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON SECTION I PERMANENT REPAIR ON FR.42 AT AFT LT SIDE "T" ANGLE POSITION IN MAIN WHEEL WELL, AS PESep 10, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090983012Access Panel · crackedSHIP 3278, CRACK ACCESS PANEL 413DL ON LT PYLON. CORRECTIVE ACTION: REPAIRED BY WELDS ACCESS PANEL 413DL ON LT PYLON, AS PER ER/A NO.540187-14MA REV. ORIGINAL SECTION I.Sep 8, 2020 · N378NW · Airbus A320211 · Nacelle/Pylon, Plate/SkinSDR DALA2020090963011Angle · crackedSHIP 3278, CRACK ANGLE AFT TI ANGLE AT FR 42 RT SIDE IN MAIN WHEEL WELL. CORRECTIVE ACTION: REPLACED TI ANGLE LOC AFT FR 42 RT SIDE IN MAIN WHELL WELL THE REPLACE WAS DOCUMENTED ON AMDS CARD 5353-01006-03.Sep 5, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090953010Web · crackedSHIP 3278, CRACK INDICATION ON WEB AT OPEN FASTENER HOLE COMMON TO AFT UPPER RT TI ANGLE POSITION AT MAIN WHEEL WELL. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON WEB COMMON TO AFT RT TI ANGLE AT MAIN WHEEL WELL, AS PER ER/A N. 587552 14 AD REV ORIGINAL SSep 4, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090953009Web · crackedSHIP 3278, CRACK INDICATION ON WEB AT OPEN FASTENER HOLE COMMON TO AFT LOWER RT TI ANGLE POSITION IN MAIN WHEEL WELL. PERFORMED PERMANENT REPAIR ON WEB COMMON TO AFT RT TI ANGLE AT MAIN WHEEL WELL, AS PER ER/A NO. 587552-14AD REV ORIGINAL SECTION I AND PRI NSep 4, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090943007Shear Tie · corrodedSHIP 3278, CORROSION SHEAR TIE LOCATED AT FR 33 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED AT FR33 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT, AS PER A320 SRM 51-72-11 AND DRAWING D53232647 ISSUSep 4, 2020 · N378NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2020090943006Shear Tie · corrodedSHIP 3278, CORROSION SHEAR TIE LOCATED AT FR30 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED AT FR30 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT, AS PER A320 SRM 51-72-11 AND DRAWING D53232647 ISSUESep 4, 2020 · N378NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2020090232924Support · corrodedCORROSION WEB SUPPORT LOCATED AT LEVEL -Y1732 BTW FR20 TO FR24 AT FWD GALLEY AREA . CORRECTIVE ACTION: REPLACED WEB SUPPORT AT LEVEL -Y1732 BTW FR20 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11-001 AND DWG # D53112783, ISSUE F00 RELEASE DATE:28-MAY-98.Aug 28, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090202926Floor Support · corrodedCORROSION SUPPORT FLOOR LOCATED AT LEVEL -Y1584 AND FR20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SUPPORT FLOOR LOCATED AT LEVEL -Y1584 AND FR20 AT FWD GALLEY AREA. AS PER A320 SRM 51-72-11 AND DWG D53112786, ISSUE B00.Aug 28, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090302944Floor Support · corrodedCORROSION FLOOR BEAM -Y1162.5 LOCATED BTW FR68 TO FR69 AT AFT GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1162.5 LOC BTW FR68 TO FR69 AT AFT GALLEY AREA ASPER SRM A320 51-72-11 AND DWG #D53472458 ISSUE E RELEASE DATE 09MAY11 DWG # D53472089 ISSUE L Aug 25, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090262922Seat Track · corrodedCORROSION SEAT TRACK -Y1292 LOCATED BETWEEN FR12 TO FR24 AT FWD GALLEY AREA . CORRECTIVE ACTION: REPLACED (FLOOR BEAM) SEAT TRACK -Y1292 LOCATED BETWEEN FR12 TO FR24 AT FWD GALLEY AREA ASPER SRM A320 51-72-11 AND DRAWINGS # D53112812 ISSUE E00 RELEASE DATE 08JAug 25, 2020 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020090262921Floor Support · corrodedCORROSION FLOOR BEAM -Y1225 FROM FR66 TO FR68 AFT GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1225 FROM FR66 TO FR68 AFT GALLEY AREA ASPER SRM A320 51-72-11 AND DWG # 53472845 ISSUE A RELEASE DATE 02APR98Aug 25, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090262920Seat Track · corrodedCORROSION SEAT TRACK -Y765 LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG D53112814 RELEASE DATE:14-MAR-03, ISSUE:B00 AND DWG D53110920, RELEAAug 25, 2020 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020020700974Battery Pack · inoperativeDURING S/C FOUND FWD EMER LIGHT BATTERY PAK INOP, R&R RWD BATT PAKFeb 6, 2020 · N378NW · Airbus A320211 · Emergency LightingSDR DALA2019081504803Warning Message · false activationAFTER LANDING "DOOR L AFT CABIN" SHOWED OPEN FOR 2-3 MIN THEN WENT BACK TO CLOSED. F/A SAID DOOR WAS CLOSED AT ALL TIMES. ( ALSO SMOOTH LANDING). CYCLED DOOR, INDICATIONS NORMAL AT THIS TIME, REF A320 AMM 320 AMM 52-10.Aug 13, 2019 · N378NW · Airbus A320211 · Door Warning SystemSDR DALA2018123007444Skin · dented(LP# 0883275) UPPER FUSELAGE LEFT HAND SIDE 2'X2' DENT IN FUSELAGE SKIN AT STRINGER 5L ST 1976 FR44. SEE NR FOR ADDITIONAL INFORMATION. CUT OUT DENTED SKIN. FABRICATED DOUBLER. INSTALLED STRINGER SPLICE AND DOUBLER REPAIR IAW SRM 53-31-11-300-01,Dec 29, 2018 · N378NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA201812307443Skin · damaged(LP# 0878548) UPPER FUSELAGE SURROUNDING SKIN AT FORWARD GPS ANTENNA MISSING PAINT AND PRIMER WITH DISCOLORATION IN SKIN. SEE NR FOR ADDITIONAL INFORMATION PREPPED AND PAINTED AREA.Dec 26, 2018 · N378NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2017011700420Slat · wornWEAR ON TRAILING EDGE SLAT 3 IB SIDE ON LT WING. PERFORMED PERMANENT REPAIR ON SLAT NR 3 ON LT WING PER ER/A 553516-14 REVISION ORIGINAL.Jan 16, 2017 · N378NW · Airbus A320211 · Leading Edge DevicesSDR DALA2016100507070Power Supply · inoperativeEMERGENCY LIGHT FWD L EPSU UNIT FAULT, REPLACED FWD LEFT EPSU 10WLOct 5, 2016 · N378NW · Airbus A320211 · Emergency LightingSDR DALA2016032002203Connector · damagedSEAT ROW EMERGENCY LIGHT INOPERATIVE AT SEAT ROWS 1AB, 11ABC, 13ABC. REPAIRED THE CONNECTORS AT SEATS 1AB, 11ABC AND 13ABC.Mar 19, 2016 · N378NW · Airbus A320212 · Light System WiringSDR DALA2015012200569Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB, FRAMES 62 - 63 STRINGER 38R. REPLACED THE IAW SRM 51-72-11 AND DWG E53470321.Jan 21, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015012200568Plate · misinstalledDURING INSTALLATION OF ACCESS PANEL 540HB BETWEEN RIB 13 AND RIB 14, FOUND BRIDGE PLATE IMPROPERLY INSTALLED. PERFORMED PERMANENT REPAIR, BRIDGING PLATE, ON INTERNAL AREA OF FUEL TANK BETWEEN RIB 13 TO RIB 14 ON POSITION OF ACCESS PANEL NR 540HB, LT WING IAJan 21, 2015 · N378NW · Airbus A320211 · Wing Main, Frame StructureSDR DALA2015012100406Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB -Y1732 BETWEEN FRAMES 12 TO 16. REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53112545.Jan 20, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015011900378Fitting · wornDURING INSPECTION, FOUND WEAR ON FWD MLG DOOR FITTING LT LOCATED ON MLG BAY. REPLACED FWD FITTING MLG DOOR ATTACHMENT LT SIDE LOCATED ON MLG BAY, SRM 51-72-11 AND DWGS N. D53370600 AND D53370622.Jan 18, 2015 · N378NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2015011800376Fitting · wornDURING INSPECTION, FOUND WEAR ON LT WING NR 4 SPOILER CENTER FITTING STOP BOLT. REPAIRED THE FITTING STOP BOLT IAW SRM 57-70-00, PAR 5C, FIG 201, SHEET 2.Jan 17, 2015 · N378NW · Airbus A320211 · SpoilersSDR DALA2015011800375Fitting · wornDURING INSPECTION, FOUND WEAR ON RT WING NR 4 SPOILER CENTER FITTING STOP BOLT. REPAIRED IAW SRM 57-70-00, PARAGRAPH 5.C, FIG 201, SHEET 2.Jan 17, 2015 · N378NW · Airbus A320211 · SpoilersSDR DALA2015011800374Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y254 BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53111461 AND D53110984.Jan 17, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015011800373Fitting · wornDURING INSPECTION, FOUND WEAR ON FWD MLG DOOR FITTING RT LOCATION ON MLG BAY. REPLACED FWD MLG DOOR FITTING RT LOCATION ON MLG BAY IAW 51-72-11 AND DWG D53370600.Jan 17, 2015 · N378NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2015011800372Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER FLOOR SUPPORT BETWEEN FRAME 66 AND 68. REPLACED IAW SRM 51-72-11, DWG D53480505, AND D53470150.Jan 17, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015011700371Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER FLOOR SUPPORT BETWEEN FRAMES 66 AND 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53480505.Jan 16, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016112209168Frame · corrodedCORROSION ON AFT FACE FRAME 16 AT LEVEL STRINGER 23R. REPAIRED IAW ER/A.Jan 15, 2015 · N378NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2016112209171Floor Panel · corrodedCORROSION ON FLOOR PANEL 261FF. REPLACED THE FLOOR PANEL.Jan 14, 2015 · N378NW · Airbus A320211 · Fuselage Floor PanelSDR DALA2016112209170Floor Panel · corrodedCORROSION ON FLOOR PANEL 262FF. REPLACED FLOOR PANEL.Jan 14, 2015 · N378NW · Airbus A320211 · Fuselage Floor PanelSDR DALA2016112209169Floor Panel · corrodedCORROSION ON CABIN FLOOR PANEL 221FF. REPLACED THE FLOOR PANEL.Jan 14, 2015 · N378NW · Airbus A320211 · Fuselage Floor PanelSDR DALA2015011500326Seat Track · corrodedCORROSION ON SEAT TRACK -Y765 LOCATED BETWEEN FRAMES 64 - 66+5. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472229.Jan 14, 2015 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015011500325Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y765 BETWEEN, FRAMES 66+5 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Jan 14, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015011500324Support Frame · corrodedAFTER REMOVAL OF SHEAR PLATE, FOUND CORROSION ON SUPPORT FRAME LOCATED BETWEEN FRAMES 69 - 70 STRINGER 23R. REPLACED THE SUPPORT FRAME IAW SRM 51-72-11 AND DWG D53470100.Jan 14, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016112209174Floor Panel · corrodedCORROSION ON CABIN FLOOR PANEL 222FF. REPLACED THE CABIN FLOOR PANEL.Jan 12, 2015 · N378NW · Airbus A320211 · Fuselage Floor PanelSDR DALA2015011100225Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN -Y1162 TO -Y1292 AND FRAMES 66+5 - 67+17. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.Jan 10, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015011100224Fitting · corrodedFOUND CORROSION ON AFT LOWER CORNER FITTING ON FRAME 68 AT STRINGER 23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480505.Jan 10, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015011100223Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292 BETWEEN FRAMES 64 - 66+5. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472832.Jan 10, 2015 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015011100222Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+17 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.Jan 10, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015011100221Coupling · corrodedDURING INSPECTION, FOUND CORROSION ON COUPLING AT STRINGER 44 AND FRAME 27+12. REPLACED THE COUPLING IAW SRM 51-72-11 AND DWG D53231598.Jan 10, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015011100220Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB Y1732 BETWEEN FRAMES 20 - 24. REPLACED THE WEB IAW SRM 51-72-11, D53112783 AND D53112545 .Jan 10, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015011100219Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB -Y1732 BETWEEN FRAMES 20 - 24. REPLACED THE WEB IAW SRM 51-72-11, DWG D53112783, D53112545 AND D53110920.Jan 10, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015011100218Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING BETWEEN FRAMES 66 - 68 . REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D534 80019 .Jan 10, 2015 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
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