N355NW

Service difficulty reports · 185

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 = 'N355NW' 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 DALA2021031801532Floor Support · corrodedSHIP 3255 CORROSION FLOOR BEAM -Y1292 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11, 51-72-11. (1757390)Mar 17, 2021 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2020123104351Psu · no testRT FWD ENTRY DOOR PSU PANEL FAILED TO OPEN ON OXY MASK TEST. CORRECTIVE ACTION: FOUND PSU OXY PANEL MOUNTING SCREWS MISSING. REPLACED SCREWS. TEST OK.Dec 30, 2020 · N355NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2020123104350Psu · no testDURING TEST PSU AT SEAT 32R FAILED TO OPEN. CORRECTIVE ACTION: REPACKED PSU AND PERFORMED SECOND TEST. OPERATIONS CHECK GOOD.Dec 30, 2020 · N355NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2020123004345Psu · no testROW 32RH SIDE PSU PANEL FAILED TO OPEN ON OXY MASK TEST. CORRECTIVE ACTION: ON SECOND TEST PSU PANEL PASSED TEST. OK FOR SERVICE.Dec 29, 2020 · N355NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2020123004344Psu · no testROW 1LH PSU PANEL FAILED TO OPEN ON OXY MASK TEST. CORRECTIVE ACTION: REPACKED PSU. OPERATIONS CHECK GOOD.Dec 29, 2020 · N355NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2020100503279Pressure Deck · crackedRIGHT SIDE FR 35/36 PRESSURE FLOOR PANEL HOLE NR 6 & 7 HAVE HFEC CRACK INDICATIONS. CORRECTIVE ACTION: REPAIRED PER AMDS NR 5311-01171-04B.Oct 3, 2020 · N355NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2019071204192Light · inoperativeLT AFT OVERWING EXIT DOOR PULL HANDLE LIGHT INOP, RELAMPED LT AFT OVERWING EXIT DOOR PULL HANDLE LIGHT.Jul 12, 2019 · N355NW · Airbus A320212 · Emergency LightingSDR DALA2019061293529Housing · brokenEMERGENCY LIGHT HOUSING BROKEN AT SEAT 12D, REPLACED HOUSINGJun 7, 2019 · N355NW · Airbus A320212 · Emergency LightingSDR DALA2019040752279Housing · detachedSEAT 16 DEF EMERGENCY LIGHT HOUSING NOT INSTALLED UNDER SEAT, REPLACED HOUSING ASSEMBLYMar 27, 2019 · N355NW · Airbus A320212 · Emergency LightingSDR DALA2019021300948Light · unsecureEMERGENCY LIGHT IN AISLE SEAT 28D LOOSE AND HANGING BY WIRES.Feb 10, 2019 · N355NW · Airbus A320212 · Emergency LightingSDR DALA2018122407381Light · unsecure(LP# 3993482) SEAT 18D MOUNTED EMERGENCY LIGHT KEEPS FALLING OFF. RESECURED. OPERATION CHECKS OKAY.Dec 22, 2018 · N355NW · Airbus A320212 · Emergency LightingSDR DALA2018091005535Light · brokenEMERGENCY LIGHT BROKEN 28D. RESECURED LIGHT.Sep 6, 2018 · N355NW · Airbus A320212 · Emergency LightingSDR DALA2018022001026Housing · damaged11DEF EMERGENCY LIGHT HOUSING DAMAGED, REPLACED THE LIGHT.Feb 20, 2018 · N355NW · Airbus A320212 · Emergency LightingSDR DALA2017090706751Power Supply · no testFWD EPSU FAILED EMERGENCY LIGHT TEST, REPLACED FWD EPSU.Sep 6, 2017 · N355NW · Airbus A320212 · Emergency LightingSDR DALA2021041202115Door Frame · crackedSHIP 3255 CRACK INDICATIONS ON FR16L AT HOLES #7, #8, #A, AND #B ABOVE DOOR STOP 7. CORRECTIVE ACTION: REPAIRED PER ER/A 554956-14AD REV.A. (0066446)Jun 13, 2017 · N355NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2019030701526Frame · crackedCRACK INDICATION ON FRAME 16 JOOGLE AREA IN OPEN HOLE NR 5 RIGHT SIDE CRACK DIRECTION: 3 O'CLOCK APPROX AND HOLE NR 6 ABOVE NR 7 DOOR STOP FITTING AT FWD GALLEY AREA; REPLACE DOOR FRAME FR16RH PER PRI 554957-14AD REV 0, REV 1, REV 2 AND ER/A 554957-14AD REV C May 8, 2017 · N355NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2017031802182Skin · dentedDENT SKIN BTW FR 80 AND FR 81 STR 1R TO STR 2R AT RUDDER AREA ON UPPER FUSELAGE.Mar 17, 2017 · N355NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2017031802181Skin · dentedDENT SKIN AT FR 79 BTW STR 4L AND STR 5L APPROX ON UPPER FUSELAGE, PERMANENT REPAIR ON THIS AREA AS PER SRM 53-51-11 FIG 20102 PAG 8.Mar 17, 2017 · N355NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2017011000267Wire Harness · disconnectedSEAT EMERGENCY LIGHT INOPERATIVE ROWS 12 AND 19, RECONNECTED AND SECURED HARNESSJan 9, 2017 · N355NW · Airbus A320212 · Light System WiringSDR DALA2016121809960Wire · looseEMERGENCY LIGHT AT SEAT ROW 14 INOPERATIVE, FOUND LOOSE WIRE AT SEAT SPLICE. REPLACED SPLICE.Dec 15, 2016 · N355NW · Airbus A320212 · Light System WiringSDR DALA2019030101322Box Beam · crackedCRACK FOUND IN ONE OPEN HOLE OF FUSELAGE CENTER BOX BEAM AT FR43 AND Y1650. FOUND DURING ACCOMPLISHMENT OF NTM 51-10-01-PB 6, PERFORMED TIME LIMITED REPAIR ON FLOOR STRUCTURE SIDE BOX BEAM UPPER FLANGE AT FR 43 LT SIDE ON CENTER WING BOX AS PER PRI N.535313-14May 4, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050303101Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STR 23R, L=1", W=0.50", D=0.003". REPLACED LOWER SILL AT AFT GALLEY AREA FROM FR 66 TO FR 68 AND STR 23R IAW SRM 51-72-11 AND DWG D53480505.May 2, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050303100Skin · corrodedDURING INSPECTION, FOUND CORROSION ON DOUBLER SKIN IN FWD CARGO COMPARTMENT FROM FRAME 27 TO FRAME 28 ON STR 43R L=1.110", W=0.210", D=0.001. REPLACED DOUBLER SKIN IN FWD CARGO COMPARTMENT FROM FRAME 27 TO FRAME 28 ON STR 43R IAW SRM 51-42-11 AND DWG D532315May 2, 2015 · N355NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015050203097Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STR 41R IN AFT CARGO COMPARTMENT BETWEEN FRAME 58+12" TO FRAME 59+3.5", L=6", W=1.5", D=0.004". MEASURES APPROXIMATELY SSI 534107. REWORKED AREA MECHANICALLY IAW SRM 51-74-00. EVALUATED REWORKED AREA ON STRINGER 41R IMay 1, 2015 · N355NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015050203096Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB FRAME 16 AT FWD GALLEY AREA AND STRINGER 23R L=1.640"; W=0.875"; D=0.002". REPLACED WEB FRAME 12 TO 16 AT FWD GALLEY AREA AND STR 23R IAW SRM 51-72-11 AND DWG NR D53112570.May 1, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050103036Coupling · corrodedCORROSION ON COUPLING IN FWD CARGO COMPARTMENT FROM FRAMES 27 TO 28 ON STRINGER 43R. REPLACED THE COUPLING IAW SRM 51-72-11 AND DWG D53231598.Apr 30, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015043003035Floor Panel · delaminatedDELAMINATED FLOOR PANEL 262EF AT AFT GALLEY AREA. REPLACED THE FLOOR PANEL IAW 53-02-00, PAR 8.H, FIG 209.Apr 29, 2015 · N355NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2015043003034Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221DF AT FWD GALLEY AREA. REPLACED THE FLOOR PANEL IAW 53-12-00, FIG 206.Apr 29, 2015 · N355NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2015043003033Floor Panel · delaminatedDELAMINATED FLOOR PANEL 262BG AT AFT GALLEY AREA. REPLACED FLOOR PANEL IAW 53-02-00, PAR 8.H, FIG 209.Apr 29, 2015 · N355NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2015043003011Floor Panel · delaminatedDELAMINATED FLOOR PANEL 222EF AT FWD GALLEY AREA. REPLACED THE FLOOR PANEL IAW SRM 53-12-00, FIG 101, DIAGRAM 101.Apr 29, 2015 · N355NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2015043003010Floor Panel · corrodedCORROSION ON FLOOR PANEL 221FF AT FWD GALLEY AREA, REPLACED THE FLOOR PANEL IAW AMM 53-42-12.Apr 29, 2015 · N355NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2015042903004Structure · corrodedCORROSION ON LOWER SILL LOCATED BETWEEN FRAME 66 TO FRAME 68 AT STR. 23L AT AFT GALLEY AREA, L=1", W=0.500", D=0.003". REPLACED LOWER SILL LEFT SIDE LOCATED BETWEEN FRAME 66 TO FRAME 68 AT LEVEL STR 23L AT AFT GALLEY AREA IAW STEP 51-72-11 AND DWG D53480505.Apr 28, 2015 · N355NW · Airbus A320212 · Fuselage Structure (General)SDR DALA2016112209100Access Panel · corrodedCORROSION ON ACCESS PANEL 540KB COUNTERSINK HOLES LT WING. REPLACED THE ACCESS PANEL .Apr 26, 2015 · N355NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2015042602983Floor Panel · corrodedCORROSION ON FLOOR PANEL 262FF AT AFT GALLEY AREA. REPLACED THE FLOOR PANEL IAW AMM 53-42-12-400-002-A .Apr 25, 2015 · N355NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2015042602982Stringer · corrodedCORROSION ON STRINGER 43L IN AFT CARGO BAY FRAME 56+11. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53470345.Apr 25, 2015 · N355NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015042602981Stringer · corrodedCORROSION ON STRINGER 42L IN AFT CARGO BAY BETWEEN FRAMES 56+10 TO 58+9. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53470345.Apr 25, 2015 · N355NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015042602980Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y1162 BETWEEN FRAMES 67+15 TO 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472800.Apr 25, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042602979Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y1292 BETWEEN FRAMES 64 TO 66+5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.Apr 25, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042602942Structure · corrodedDURING INSPECTION, FOUND CORROSION ON UNDERFLOOR STRUCTURE SECTION-CONNECTION AT STR 29L AND AT FRAME 67 AT AFT GALLEY AREA, L=3", W=0.200", D=0.003". SSI 534144. REPLACED SECTION-CONNECTION LOCATED ON UNDERFLOOR STRUCTURE AT STR 29L AND AT FRAME 67 AFT GALLApr 25, 2015 · N355NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2015042502933Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB FRAME 20 AT FWD GALLEY AREA AND STR 23R L=1.860", W=0.860", D=0.002". SSI 531189. REPLACED WEB, LOCATED BETWEEN FR 20 TO FR 24 AT LEVEL OF STR 23R FWD GALLEY AREA IAW SRM 51-72-11 AND DWG N.D53112783 AND DWG N, DApr 24, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042502932Skin · dentedDURING INSPECTION, FOUND DENT ON EXTERNAL SKIN AT LOWER FUSELAGE ON FRAME 69+9" BETWEEN STRINGER 19L TO STR 20L. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN AT LOWER FUSELAGE AT FR 69+9" BETWEEN STR 19L TO STR 20L IAW SRM 53-41-11 PARA 5.M, FIG 215.Apr 24, 2015 · N355NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015042502931Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 40R TO STRINGER 41R L=1.115", W=0.310", D=0.001". SSI 532180. REPLACED CLEAT AND FASTENERS LOCATED IN FWD CARGO COMPARTMENT ON FR 32 BETWEEN STR 40R TO STR 41R IAW Apr 24, 2015 · N355NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015042502930Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 20 AND STRINGER 23L L=0.325", W=0.150", D=0.002". SSI 531189, REPLACED CENTER FITTING AND FASTENER LOCATED AT FWD GALLEY AREA FROM FR 16 TO FR 20 AND STR 23L IAW Apr 24, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042502929Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK +Y1292, FRAME 47 TO 64 EVALUATED AND FOUND OUT LIMITS ON JOB CAR 2500-203 2-DE IN PASSENGER CABIN. REPLACED SEAT TRACK Y1292 FR 47 TO FR 64 IAW SRM 51-72-11 AND DWG: D53472000.Apr 24, 2015 · N355NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015042502928Dummy Rail · corrodedDURING INSPECTION, FOUND CORROSION ON RAIL DUMMY Y503.2 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 16 L=1.278", W=0.870", D=0.002". SSI 531189. REPLACED RAIL DUMMY Y503.2 LOCATED BETWEEN FR 12 TO FR 16 FWD GALLEY AREA IAW SRM 51-72-11 AND DWG N, D53112825 ANApr 24, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042502927Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y512 BETWEEN FR 64 TO FR 67+10" AT AFT GALLEY AREA L=2", W=1", D=0.004". SSI 534147. REPLACED FLOORBEAM +Y512 BETWEE FR 64 TO FR 67+10" AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472815.Apr 24, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042302901Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1292 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24, L=0.178", W=0.055", D=0.001". SSI 531189. REPLACED FLOORBEAM -Y1292 LOCATED BETWEEN FR 12 TO FR 24 SRM 51-72-11 AND DWS D53112812, D53110984 , D5311Apr 22, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042302900Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y81 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 16, L=0.381", W=0.160", D=0.001". SSI 531189. REPLACED FLOORBEAM -Y81 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 16 AND FASTENERS IAW SRM 51-72-11 AND DWG D5311Apr 22, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042302899Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24, L=1.375", W=0.810", D=0.002". SSI 531189. REPLACED FLOORBEAM -Y765 LOCATED AT FWD GALLEY AREA FROM FR 12 TO FR 24 IAW SRM 51-72-11 AND DWG D53110422.Apr 22, 2015 · N355NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042302898Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765, FRAME 47 TO 64 EVALUATED AND FOUND LIMITS ON JC 2500- 2032-DE IN PASSENGER CABIN. P1, FR 49=3.785", W=0.350", D=0.063", P2 FR.53+12", L=2.603", W=0.348", D=0.043, "P3 FR .62+10", L=4.100", W=0.350", D=0.Apr 22, 2015 · N355NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
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