N345NW

Service difficulty reports · 204

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 = 'N345NW' 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 DALA2021041302159Psu · no testSHIP 3245 DURING TEST SEAT 21ABC PSU/O2 PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (3998093)Apr 13, 2021 · N345NW · Airbus A320212 · Emergency EquipmentSDR DALA2021041302158Psu · no testSHIP 3245 DURING TEST SEAT 18ABC PSU/O2 PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (3998092)Apr 13, 2021 · N345NW · Airbus A320212 · Emergency EquipmentSDR DALA2021041302157Psu · no testSHIP 3245 DURING TEST SEAT 13ABC PSU/O2 PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (3998091)Apr 13, 2021 · N345NW · Airbus A320212 · Emergency EquipmentSDR DALA2021041302156Psu · no testSHIP 3245 DURING TEST SEAT 12DEF PSU/O2 PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (3998090)Apr 13, 2021 · N345NW · Airbus A320212 · Emergency EquipmentSDR DALA2021030901343Fire Warning · false activationSHIP 3245 - ATB - DUE TO ENGINE 1 FIRE- ECAM WARNING ON CLIMB OUT. REVERTED TO JUST LOOP A FAULTING AFTER THROTTLE BACK TO IDLE. FIRE DEPT. CLEARED AIRCRAFT AFTER LANDING WITH NO FIRE OR EVIDENCE OF OVER HEAT. CORRECTIVE ACTION: R AND R FDU PER A320 AMM 26 -12Mar 8, 2021 · N345NW · Airbus A320212 · Fire DetectionSDR DALA2021010700090Damper · inoperativePASSENGER CREW DOOR 841 ON DOOR DAMPER NOT DAMPING CORRECTLY. CORRECTIVE ACTION: REPLACED DAMPER. OK FOR SERVICE.Jan 6, 2021 · N345NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020122904328Window Frame · crackedCRACK INDICATION ON FRAME 4 RT SIDE LATERAL WINDOW UPPER JUNCTION OPEN FASTENER HOLE, CRACK INDICATION IS AT 4 AND 5 O`CLOCK. AD RELATED, WORK CARD 5311-01236-02. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT, IN COCKPITDec 27, 2020 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2020122804282Frame · crackedCRACK INDICATION ON FRAME 35 LOCATED AT LEVEL STR 30 L HOLE NR 6 IN FWD CARGO COMPARTMENT (1 EA). CORRECTIVE ACTION: PERFORMED TIME LIMIT REPAIR ON FRAME 35 LOCATED AT LEVEL STR 30L HOLE NR 6 IN FWD CARGO COMP, AS PER PRI REV 0, REV 1, REV 2, ER/A 588711- 14ADec 26, 2020 · N345NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2020122804280Frame · crackedCRACK INDICATION ON FRAME 36 HOLE NR 4 LOCATED 5 INCH OUT SIDE Y1292 LT IN FWD CARGO COMPARTMENT (1 EA). CORRECTIVE ACTION: PERFORMED REPAIR ON FR 36 HOLE NR 4 LOCATED SICH OUTSIDE Y1292 LT IN FWD CARGO COMPARMENT, AS PER PRI REV 0, REV 1, REV 2, ER/A 588715-Dec 26, 2020 · N345NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2020122804279Frame · crackedCRACK INDICATION ON FRAME 36 ON HOLE NR 7 LOCATED 2 IN OUT SIDE OF Y1292 LT IN FWD CARGO COMPARTMENT (1 EA). CORRECTIVE ACTION: PERFORMED REPAIR ON FR 36 HOLE NR 7 LOCATED 2 IN OUTSIDE OF Y1292 LT IN FWD CARGO COMPARTMENT, AS PER PRI REV 0, REV 1, REV 2 ER/A Dec 26, 2020 · N345NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2020122804278Frame · crackedCRACK INDICATION ON FRAME 36 HOLE NR 6 LOCATED 3 INCH OUT SIDE Y1292 LT IN FWD CARGO COMPARTMENT (1 EA). CORRECTIVE ACTION: PERFORMED REPAIR ON FR 36 HOLE NR 6 LOC 3 IN OUT SIDE Y1292 LT IN FWD CARGO COMPARTMENT, AS PER PRI REV 0, REV 1, REV 2 ER/A 588715- 14Dec 26, 2020 · N345NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2020122804277Frame · damagedOUT LIMIT FRAME 35 HOLE NR 10 STR 30L HAVING A DIMAETER THATS LARGE THAN MINIMUM SRARING DIAMETER OF 2ND OVERSIZE IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED TIME LIMIT REPAIR ON FRAME 35 HOLE NO 10 STR 30L IN FWD CARGO COMP, AS PER PRI REV 0, REV Dec 26, 2020 · N345NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2020122804321Hinge Fitting · crackedCRACK INDICATION ON MAIN DOOR FWD HINGE FITTING, L=0.052 IN AT LT MAIN LANDING GEAR (1 EA). CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS LOCATED ON MAIN DOOR FWD HINGE FITTING IN AT LT MAIN LANDING GEAR, AS PER PRI 588719-14AD.Dec 24, 2020 · N345NW · Airbus A320212 · Fuselage, Door HingeSDR DALA2020122404251Stiffener · crackedCRACK INDICATION FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 32 AT FRAME 36 Y254. CORRECTIVE ACTION: REPAIRED PER ER/A 588680-14AD REV ORIGINAL. OK FOR SERVICE.Dec 24, 2020 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2020122404250Stiffener · crackedCRACK INDICATION FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FRAME 36 Y-765. CORRECTIVE ACTION: REPAIRED PER ER/A 588680-14AD REV O. OK FOR SERVICE.Dec 24, 2020 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2020122404249Stiffener · crackedCRACK INDICATION FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FRAME 36 Y-765. CORRECTIVE ACTION: REPAIRED PER ER/A 588680-14AD REV ORIGINAL. OK FOR SERVICE.Dec 24, 2020 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021010800133Frame · crackedCRACK WAS FOUND AT HOLE NR 6 ON LT AT FR 35, BETWEEN STR 28 AND STR 31. CORRECTIVE ACTION: MONITOR CRACK, PER AA REFERENCE 32-588711.Dec 23, 2020 · N345NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021010800132Panel · crackedCRACK WAS FOUND AT THE FASTENER OF THE UPPER JUNCTION ATTACHING LATERAL PANEL TO THE FWD WINDSHIELD. CORRECTIVE ACTION: MONITOR CRACK, PER ERA 588561-14AD AND 5311-01236-02.Dec 23, 2020 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2020122404248Web · corrodedCORROSION INTERNAL STRUCTURE WEB LOCATED FROM FR 56 TO FR 57 AND STR 38R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 589020-14. OK FOR SERVICE.Dec 23, 2020 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2020122404247Skin · corrodedCORROSION UPPER SURFACE AROUND GROUND POINT AT LEVEL OF RIB 20 ON LT WING. CORRECTIVE ACTION: REPAIRED PER ER/A 588694-14AD. OK FOR SERVICE.Dec 23, 2020 · N345NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2020122404246Skin · damagedSKIN DISCREPANCIES ON FR 74 BETWEEN STR 3L AND STR 5L ON UPPER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 588902-14AD REV ORIGINAL. OK FOR SERVICE.Dec 23, 2020 · N345NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2020122404245Skin · corrodedCORROSION FOUND ON EXTERNAL SKIN LOCATED ON FR 34 BETWEEN STR 43LT AND STR 43RT. CORRECTIVE ACTION: REPAIRED PER ER/A 534543-14 REV C. OK FOR SERVICE.Dec 23, 2020 · N345NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2021010800135Skin · corrodedCORROSION SPOT WAS FOUND ON TOP SKIN OF PANEL 2 BETWEEN RIB 19 AND RIB 20 ON LT WING. CORRECTIVE ACTION: MONITOR CORROSION PER A/A 32-588694.Dec 22, 2020 · N345NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2020122304198Fairing · corrodedCORROSION FLAP TRACK FAIRING 633CB INTERNAL STRIP RT WING. CORRECTIVE ACTION: REPLACED BONDING PLATE ON FLAP TRACK FAIRING 633CB INTERNAL STRIP RT WING, AS PER ER/A 588948-14 PRI REV 0.Dec 22, 2020 · N345NW · Airbus A320212 · Trailing Edge FlapsSDR DALA2020122304197Mount · wornWEAR ON AFT MOUNT INBOARD SIDE ON RT PYLON. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON AFT MOUNT INBOARD SIDE ON RT PYLON, AS PER ER/A NR 588912-14 REV ORIGINAL.Dec 22, 2020 · N345NW · Airbus A320212 · Nacelle/Pylon, Attach FittingsSDR DALA2020122304196Door Frame · crackedCRACK INDICATION FOUND IN OPEN HOLE 3 (LOWER INBOARD POSITION) LOCATED ON FRAME 16 DOOR STOP FITTING 1 LT SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 588748-14AD REV ORIGINAL. OK FOR SERVICE.Dec 22, 2020 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021011500249Pressure Deck · crackedWHILE ACCOMPLISHING INSPECTIONS 3 CRACKS FOUND IN FASTENERS HOLES IN UPPER SURFACE OF PRESSURE DECK MEMBRANE LT SIDE, UNDER TITANIUM ANGLE CONNECTION AND CORNER BRACKET AT FR 36. CORRECTIVE ACTION: MONITOR PER ERA 588715-14 AD.Dec 21, 2020 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2020122204191Skin · not reportedSKIN DISCREPANCIES ON FR 72 BETWEEN STR 3L AND STR 5L, STR 3R AND STR 5R ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIRS, PER ER/A 588834-14AD REV ORIGINAL.Dec 21, 2020 · N345NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2020122204189Stiffener · crackedWINGS CENTER WING FRONT SPAR AT FR 36 FLOOR BEAM & VERTICAL STIFFENER CRACKS FOUND Y-765 ZONE 1, 2 Y254 ZONE 1. CORRECTIVE ACTION: COMPLIED WITH ER/A 588680-14AD.Dec 18, 2020 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2020122104157Striker · wornWORN STRIKER LEVER PASSENGER CREW DOOR 841 FWD GALLEY AREA. REPLACED BUSHINGS ON BELLCRANK OF PERCUSSION SYSTEM STRIKER LOWER, AS PER A320 FAM AMM 5210-00-915-001-A.Dec 18, 2020 · N345NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020122104156Intercostal · crackedCRACK INDICATION FOUND IN OPEN HOLE 1 (UPPER INBOARD POSITION) LOCATED ON INTERCOSTAL DOOR STOP FITTING 7 POSITION FR 16 RT SIDE. CORRECTIVE ACTION: REPLACED INTERCOSTAL FR 16 RT SIDE AT LEVEL STOP FITTING NR 7.Dec 18, 2020 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2020122104155Door Frame · crackedCRACK INDICATION FOUND IN OPEN HOLE 3 (LOWER INBOARD POSITION) LOCATED ON INTERCOSTAL AT DOOR STOP FITTING 7 AREA FR 16 RT SIDE. CORRECTIVE ACTION: REPLACED INTERCOSTAL FR 16 RT SIDE AT LEVEL STOP FITTING NR 7.Dec 18, 2020 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2020121804145Intercostal · crackedCRACK INDICATION FOUND IN OPEN HOLE 3 (LOWER INBOARD POSITION) LOCATED ON INTERCOSTAL AT DOOR STOP FITTING 7 FR 16 LT SIDE. CORRECTIVE ACTION: C/W ERA NR 588914-14AD REV ORIGINAL.Dec 17, 2020 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2020121704130Intercostal · crackedCRACK INDICATION FOUND IN OPEN HOLE 1 LOCATED ON INTERCOSTAL AT DOOR STOP FITTING 7 POSITION FR 16 LT SIDE. CORRECTIVE ACTION: REPLACED INTERCOSTAL FR 16 LT AT DOOR STOP FITTING NR 7, AS PER SRM A320 51-72-11 AND ER/A 588914-14AD REV ORIGINAL.Dec 16, 2020 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2020121404080Support Angle · crackedCRACK ON ANGLE SUPPORT BELLY FAIRING AT LEVEL BETWEEN FR 45 TO FR 46 KEEL BEAM AREA RT SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED ANGLE SUPPORT BELLY FAIRING AT LEVEL BETWEEN FR 45 TO FR 46 KEEL BEAM AREA RT SIDE AT LOWER FUSELAGE (1 EA), AS PER A320Dec 13, 2020 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2020121404079Door Frame · corrodedCORROSION ON LOWER SILL PASSENGER CREW DOOR 832 AT LEVEL OF FR 68 AFT GALLEY AREA. CORRECTIVE ACTION: REMOVED AND REPLACED LOWER SILL LOCATED BETWEEN FR 66 TO FR 68 AT LEVEL STR 23L FLOOR STRUCTURE AFT GALLEY AREA, AS PER A320 SRM 51-72-11, SRM 51-42-11. OK Dec 12, 2020 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2020121404078Stringer · corrodedCORROSION ON STRINGER 43L FROM FR 54 TO FR 60 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER 43L FROM FR 54 TO FR 60 IN AFT CARGO COMPARMENT, AS PER SRM A320 51-72-11. OK FOR SERVICE.Dec 11, 2020 · N345NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2020121404077Skin · dentedDENT ON EXTERNAL SKIN LOCATED BETWEEN FR 81 TO FR 82 AND STR 2L TO STR 3L ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BETWEEN FR 81 TO FR 82 STR 2L TO STR 3L ON UPPER FUSELAGE, AS PER SRM A320 53-51-11.Dec 11, 2020 · N345NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2020121004042Skin · dentedDENT EXTERNAL SKIN LOCATED BETWEEN FR 79 TO FR 80 AND STR 4R TO STR 5R ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON SKIN LOCATED BETWEEN FR 79 TO FR 80 AND STR 4R TO STR 5R ON UPPER FUSELAGE, AS PER A320 SRM-53-51-11-300- 002.Dec 9, 2020 · N345NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2020120703983Stop Fitting · crackedCRACK INDICATION ON FRAME 68 DOOR STOP 1 LT SIDE AT OPEN FASTENER HOLE 2. AA 5311-01216, AD RELATED. CORRECTIVE ACTION: PERFORMED REPAIR ON HOLE 2 FRAME 68 DOOR STOP 1 LT, AS PER A320 SRM 53-41-12-300-008 AND 53-41-12-300-010.Dec 4, 2020 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2020120703982Stop Fitting · crackedCRACK INDICATION ON FRAME 66 DOOR STOP FITTING NR 7 LT SIDE AT OPEN FASTENER HOLE 2. AA 5311-01216, AD RELATED. CORRECTIVE ACTION: REPAIRED HOLE NR 2 ON DOOR STOP FITTING NR 7 ON FRAME 66 LT SIDE, AS PER SRM A320 53-41-12-300-008 AND 53-41-12-300-010.Dec 4, 2020 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2020120703981Stop Fitting · crackedCRACK INDICATION ON FRAME 68 DOOR STOP 1 RT SIDE AT OPEN FASTENER HOLE 4. AA 5311-01216, AD RELATED. CORRECTIVE ACTION: PERFORMED REPAIR ON HOLE NR 4 FRAME 68 DOOR STOP 1 RT, AS PER A320 SRM 53-41-12-300-008 AND 53-41-12-300-010.Dec 4, 2020 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2020120703980Stop Fitting · crackedCRACK INDICATION ON FRAME 68 DOOR STOP 1 LT SIDE AT OPEN FASTENER HOLE 4. AA 5311-01216, AD RELATED. CORRECTIVE ACTION: PERFORMED REPAIR ON HOLE 4 FRAME 68 DOOR STOP NR 1 LT, AS PER A320 SRM 53-41-12-300-008 AND 53-41-12-300-010.Dec 4, 2020 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2020120303957Floorbeam · corrodedCORROSION ON FLOOR BEAM +Y1292 AT LEVEL OF FR 16 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM +Y1292 AT LEVEL OF FR 16 AT FWD GALLEY AREA. OK FOR SERVICE.Dec 2, 2020 · N345NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2020120203943Dummy Rail · corrodedCORROSION ON DUMMY RAIL AT Y503.2 BETWEEN FR 12 TO FR 16 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED DUMMY RAIL AT Y503.2 BETWEEN FR 12 TO FR 16 FWD GALLEY AREA. OK FOR SERVICE.Dec 1, 2020 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020120103931Hook · wornWEAR ON HOOK ON THE INNER CONTROL HANDLE PASSENGER CREW DOOR 831. CORRECTIVE ACTION: REPLACED HOOK. OK FOR SERVICE.Nov 30, 2020 · N345NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020120103930Compensator · out of adjustPASSENGER CREW DOOR 831 ON THE BELL CRANK OF THE COMPENSATION MECHANISM OUT OF ADJUSTEMENT. CORRECTIVE ACTION: PERFORMED ADJUSTMENT. OK FOR SERVICE.Nov 30, 2020 · N345NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020120103929Roller · wornWORN ROLLER ON PASSENGER CREW DOOR 831 AFT LOWER POSITION. CORRECTIVE ACTION: REPLACED ROLLER. OK FOR SERVICE.Nov 30, 2020 · N345NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020113003900Dampener · no testDAMPER DOES NOT PASS TEST AT PASSENGER CREW DOOR 842. CORRECTIVE ACTION: REPLACED DAMPER AT PASSENGER CREW DOOR 842. OK FOR SERVICE.Nov 28, 2020 · N345NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020113003901Dampener · no testPASSENGER CREW DOOR 832 WONT PASS DAMPER TEST. CORRECTIVE ACTION: REPLACED DAMPER AT PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. OK FOR SERVICE.Nov 26, 2020 · N345NW · Airbus A320212 · Passenger/Crew Doors
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