N343NW

Service difficulty reports · 259

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 = 'N343NW' 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 DALA2020120904030Hinge Fitting · deterioratedDETERIORATED PASSENGER CREW DOOR 831 UPPER HINGE FITTING AT FR 16, FWD GALLEY AREA. CORRECTIVE ACTION:REPLACED UPPER HINGE FITTING AT FR 16 OF PASSENGER CREW DOOR. OK FOR SERVICE.Dec 8, 2020 · N343NW · Airbus A320212 · Fuselage, Door HingeSDR DALA2020120904029Floor Support · corrodedCORROSION ON FLOOR BEAM -Y765 AT LEVEL OF FR 68 AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOCATED FR 66+5" TO FR 70 AFT GALLEY AREA, AS PER SRM A320 51-72-11.Dec 8, 2020 · N343NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2020121804148Damper · malfunctionedPASSENGER CREW DOOR 841 DAMPER NOT WORKING CORRECTLY DURING OPENING AND CLOSING. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR DAMPER.Dec 7, 2020 · N343NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020120703984Bushing · excess playEXCESSIVE PLAY ON PASSENGER CREW DOOR 841 ON BONDED BUSHINGS OF UPPER CONNECTION LINK AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED BONDED BUSHINGS OF UPPER CONNECTION LINK OF PASSENGER CREW DOOR 841. OK FOR SERVICE.Dec 6, 2020 · N343NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020120103928Bushing · excess playEXCESSIVE PLAY IN PASSENGER CREW DOOR 842 ON BUSHINGS OF UPPER CONNECTION LINK. CORRECTIVE ACTION: REPLACED BUSHINGS. OK FOR SERVICE.Nov 30, 2020 · N343NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020112703884Roller · deterioratedFOUND DETERIORATED PASSENGER CREW DOOR 831 LOWER GUIDE ROLLERS FWD AND AFT POSITIONS. CORRECTIVE ACTION: REPLACED LOWER GUIDE ROLLERS FWD AND AFT POSITIONS AT DOOR 831. OK FOR SERVICE.Nov 24, 2020 · N343NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020112703883Door · out of adjustPASSENGER CREW DOOR 831 OUT OF ADJUSTMENT. CORRECTIVE ACTION: PERFORMED ADJUSTMENT ON PASSENGER CREW DOOR NUMBER 831. OK FOR SERVICE.Nov 24, 2020 · N343NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020112703882Torsion Bar · out of adjustOUT OF ADJUSTMENT TORSION BAR BELLCRANK PASSENGER CREW DOOR 832. CORRECTIVE ACTION: PERFORMED ADJUSTMENT OF RIGGING POINT OF TORSION BAR BELLCRANK OF PASSENGER/CREW DOOR 832 AT AFT GALLEY.Nov 24, 2020 · N343NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020112703881Door · out of rigPASSENGER CREW DOOR 841 WAS OUT OF RIG. CORRECTIVE ACTION: PERFORMED ADJ OF PASSENGER CREW DOOR 841. OK FOR SERVICE.Nov 24, 2020 · N343NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020112403854Roller · deterioratedDETERIORATED ROLLER PASSENGER CREW DOOR 842 FWD AND AFT LOWER POSITIONS. CORRECTIVE ACTION: REPLACED ROLLER PASSENGER CREW DOOR FWD AND AFT LOWER POSITIONS AT AFT GALLEY AREA DOOR 842. OK FOR SERVICE.Nov 23, 2020 · N343NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020112403853Roller · deterioratedDETERIORATED ROLLER PASSENGER CREW DOOR 832 FWD AND AFT LOWER POSITION. CORRECTIVE ACTION: REPLACED ROLLERS ON PASSENGER CREW DOOR 832 FWD AND AFT LOWER POSITIONS AT AFT GALLEY AREA. OK FOR SERVICE.Nov 23, 2020 · N343NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2019052103161Light · inoperativeONE OVERWING EXIT HANDLE LIGHT INOP, R/R LIGHT ASSY.May 20, 2019 · N343NW · Airbus A320212 · Emergency LightingSDR DALA2019030501474Access Panel · missingPDA PART DEPARTING AIRCRAFT. LOG 5580746 RIGHT WING ANTI-ICE VALVE ACCESS COVER MISSING, PANEL 622WB, PERFORMED ERA 576058-14MA REV ORIGINAL. ACCOMPLISHED SEC 1, NO LEAK NOTED, NO SECOUNDARY DEFECTS NOTED. INSTALLED PLATE AND SPEED TAPE AS REQUIRED PER ERA.Mar 4, 2019 · N343NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2019020700838Attach Bracket · corrodedLEFT WING NR 1 PYLON INBOARD SIDE, FAIRING ATTACH BRACKET HAS CORROSION ON FRONT AND BACK SIDES, LOCATED BELOW REAR SPAR. REPLACED BRACKET IAW DWG D54530251.Feb 5, 2019 · N343NW · Airbus A320212 · Nacelle/Pylon Miscellaneous StructureSDR DALA2019020700837Bracket · corrodedCORROSION ON ADJACENT BRACKET FOUND ON N/R 97. REMOVED AND REPLACED BRACKET IAW DWG D54510054.Feb 5, 2019 · N343NW · Airbus A320212 · Wing Miscellaneous StructureSDR DALA2019020400835Pressure Deck · crackedLEFT HAND PRESSURE DECK HOLE A CRACKED. INSTALLED REPAIR IAW EM5311-01171-04A AND ERA 594797-14AD REV O.Feb 3, 2019 · N343NW · Airbus A320212 · Fuselage Main, BulkheadSDR DALA2018070504388Computer · faultyEXPERIENCED AN ELAC 1 FAULT WITH AN UNCOMMANDED AIRCRAFT ROLL, DISCONNECTED ELAC 1 PER QRH AND CONTINUED THE FLIGHT. REPLACED ELAC 1.Jul 3, 2018 · N343NW · Airbus A320212 · Elevator Control SystemSDR DALA2018030101302Stringer · corrodedCORROSION FOUND ON STRINGER 43L BETWEEN FRAMES 56 AND 57. REPLACED THE STRINGER IAW SRM 53-00-13, FIG 201.Feb 27, 2018 · N343NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2017041202954Power Supply · no testEPSU UNIT FWD L MESSAGE FOR EMERGENCY LIGHTS SYS CHECK. R & R FWD EPSU UNIT 10WL.Apr 12, 2017 · N343NW · Airbus A320212 · Emergency LightingSDR DALA2017021101176Frame · corrodedCORROSION ON FRAME 16, STRINGER 23R. REPAIRED THE FRAME IAW ERA 532404-14AD REV A.Feb 10, 2017 · N343NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2017021101175Frame · crackedCRACK INDICATION FOUND AT RADIUS ON FRAME 68 AT STRINGER 8R. REPAIRED THE FRAME IAW ER/A 553542-14AD REV ORIGINAL.Feb 10, 2017 · N343NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2017012500609Web · corrodedCORROSION ON WEB IN AFT GALLEY AREA, STRINGER 23L BETWEEN FRAME 69 TO FRAME 70. REPLACED THE WEB AND FASTENERS IAW SRM 51-72-11 AND DRAWING D53470100Jan 24, 2017 · N343NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2017010800184Lens · damagedEMERGENCY LIGHT LENS DAMAGED, REPLACED THE LENSJan 5, 2017 · N343NW · Airbus A320212 · Emergency LightingSDR DALA2016111308760Frame · crackedLEFT SIDE WING BOX FRAME 43 CRACK INDICATION. REPAIRED PER WORKCARD 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.Nov 12, 2016 · N343NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2020121504102Door Frame · damagedFR 20 LT ELONGATED HOLE AT DOOR STOP 1, REPAIRED PER ER/A 532986-1. CORRECTIVE ACTION: PERFORMED REPETITIVE INSPECTION ON FR 20 LT AT DOOR STOP 1 HOLE NR 16, AS PER ER/A 532986-14. OK TO CONTINUE.Mar 6, 2016 · N343NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2015122107687Skin · corrodedAFT ATG4 ANTENNA STEP 2A AN AREA OF POSSIBLE CORROSION, C/W PRI ERA 542338-14AD, REV 0 STEP 2, WORKED THE CORROSION IAW SRM CH 51-73-00.Dec 19, 2015 · N343NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015031402137Door Frame · corrodedDURING INSPECTION, FOUND CORROSION ON DOOR AFT FACE FRAME 66 STRINGERS 22L - 23L. PERFORMED TIME LIMITED REPAIR IAW ERA 532979-14 REV. ORIGINAL AND PRI 532979-14 REV. 0, 1 AND 2.Mar 13, 2015 · N343NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2015031102116Skin · bentDURING INSPECTION, FOUND BENT PASSENGER CREW DOOR EXTERNAL SKIN, 841 DOOR, UPPER PLATE ON UPPER FUSELAGE. REPLACED UPPER PLATE LOCATED ON UPPER FUSELAGE, AT PASSENGER CREW DOOR EXTERNAL SKIN, 841 DOOR, IAW SRM 51-72-11 AND DWG 52111475.Mar 10, 2015 · N343NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2015030902115Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 41R TO STR 42R, L=0.800", W=0.300", D=0.004". REPLACED CLEAT LOCATED FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 41R TO STR 42R IAW SRM 51-72-11 AND DWG D53231586.Mar 8, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030802086Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION SHEAR TIE ON FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STRINGERS 41R TO 42R. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG D53231586.Mar 7, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030802085Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 27L BETWEEN FRAMES 67 AND 68 IN BULK CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 27L IAW ERA 533417-14 REV.ORIGINAL SEC.1 AND PRI 533417-14 REV.O.Mar 7, 2015 · N343NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015030702084Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 40R ON FWD CARGO COMPARTMENT BETWEEN FRAME 29 TO FRAME 31 L=1" W=0.5" D=0.003. PERFORMED PERMANENT REPAIR ON STRINGER IAW SRM 53-0013 FIG 201(SHEET 2).Mar 6, 2015 · N343NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015030702083Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON FWD CARGO COMPARTMENT ON STRINGER 43L BETWEEN FRAME 31 TO FRAME 34 L=1" W=0.5" D=0.003. REPLACED STRINGER ON FWD CARGO COMPARTMENT ON STRINGER 43L BETWEEN FRAME 30+15" TO FR 34+6" IAW SRM 51-72-11 AND DRAWING D5323162Mar 6, 2015 · N343NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015030602082Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STRINGER 39R TO STRINGER 40R L=1.000" W=0.500" D=0.004". REPLACED SHEAR TIE IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STRINGER 39R TO STRINGER 40R IAW SRM 51-72-1Mar 5, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030602081Skin · dentedDURING INSPECTION, FOUND DENT ON EXTERNAL SKIN AT FR.25+8.5" AND STR.42L ON LOWER FUSELAGE. PERFORM PERMANENT REPAIR ON EXTERNAL SKIN AT LEVEL FR 25+8.5" ON LOWER FUSELAGE IAW SRM 53-00-11, PARAGRAPH 4W, STEP 7, FIG 239.Mar 5, 2015 · N343NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015030602080Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 34 BETWEEN STRINGER 43R TO STRINGER 44, L=0.850", W=0.500", D=0.003. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 34 BETWEEN STR 43R TO STR 44R IAW SRM 51-72-11 AND DWG D53231Mar 5, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030602079Stringer · corrodedDURING INSPECTION, FOUND CORROSION STR ON FWD CARGO COMPARTMENT ON STR 41L BETWEEN FRAME 31 TO FRAME 34, L=1", W=0.5", D=0.003" . REPLACED STR LOCATED ON FWD CARGO COMPARTMENT ON STR 41L BETWEEN FRAME 31 TO FR 34 IAW SRM 51-72-11 AND DWG D53231626.Mar 5, 2015 · N343NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015030602078Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STR 43L TO STR 44, L=0.850", W=0.300", D=0.005", SSI532180. REPLACED CLEAT LOCATED IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STR 43L TO STR 44 IAW SRM 51-72-11 AND DWGMar 5, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030602077Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STRINGER 41 TO STRINGER 42R, L=0.900", W=0.550", D=0.002. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 41R TO STR 42R IAW SRM A320 51-72-11, DWG D532Mar 5, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030502054Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 40L TO STR 41L, L=0.600", W=0.400", D=0.002, SSI 532180. REPLACED CLEAT LOCATED IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 40L TO STR 41L IAW SRM 51-72-11 AND DMar 4, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030502053Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STR 41L TO STR 42L, L=1.000", W=0.400", D=0.004, SSI 532180. REPLACED CLEAT LOCATED IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STR 41L TO STR 42L IAW SRM 51-72-11 AND DMar 4, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030502052Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y254 AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 21, L=1" W=0.200", D=0.003", SSI 531189. REPLACED FLOORBEAM -Y254 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24 IAW ER/A NR 532969-14, PRI 532969-14 AND SRM 51-72-1Mar 4, 2015 · N343NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015030502051Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 34 BETWEEN STR 42R TO STR 43R, L=1.000", W=0.450", D=0.003", SSI532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FR 34 BETWEEN STR 42R TO STR 43R IAW SRM 51-72-11.Mar 4, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030502050Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 33 BETWEEN STRIN GER 42R TO STRINGER 43R L=0.800 W=0.400 D=0.004 .(SSI 532180). REPLACED CLEAT IN FWD CARGO COMPARTMENT FR 33 BETWEEN STR 42R TO STR 43R IAW SRM 51-72-11. DWG D5323Mar 4, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030502049Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 42L TO STR 43L, L=0.950", W=0.600", D=0.004", SSI 532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 42L TO STR 43L IAW SRM 51-72-11 AND DWG D532Mar 4, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030502048Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 40L TO STR 41L, L=1.000", W=0.300", D=0.003". SSI 532180). REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 40L TO STR 41L IAW SRM 51-72-11 AND DWG D53Mar 4, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030502047Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 33 BETWEEN STR 43R TO STR 44, L=0.950, W=0.300, D=0.002. SSI 532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON EXACT LOCATION, FRAME 33 BETWEEN STR 43 LT SIDE TO STR 43 RT IAW SRMMar 4, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030502046Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STR 40L TO STR 41L L=1.000", W=0.800", D=0.008", SSI532180. REPLACED CLEAT ON FWD CARGO COMPARTMENT LOCATED FRAME 29 BETWEEN STR 40L, TO STR 41L IAW SRM 51-72-11 AND DWG Mar 4, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015030502045Fitting · wornDURING INSPECTION, FOUND WEAR ON MAIN DOOR FITTING FORWARD POSITION ON LT MLG. REPLACED FITTING ON MAIN DOOR FORWARD POSITION ON LT MLG IAW SRM 51-72-11 AND DWG D53370600.Mar 4, 2015 · N343NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2015030502044Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT IN FRAME 32 BETWEEN STR 41L TO STR 42L L=0.900", W=0.400", D=0.004", SSI532180. REPLACED CLEAT LOCATED ON FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 41L TO STR 42L IAW SRM 51-72-11 AND DWMar 4, 2015 · N343NW · Airbus A320212 · Fuselage Internal Mounting Structure
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