N340NW

Service difficulty reports · 216

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 = 'N340NW' 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 DALA2015042702988Floor Panel · delaminatedDELAMINATED FLOOR PANEL 241FF IN PASSENGER CABIN. FOUND OUT LIMITS IAW SRM 53-02-00, TABLE 103 AND WAS REPLACED IAW SRM 53-02-00, PAR 8H, FIG 209 .Apr 26, 2015 · N340NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2015042702987Floor Panel · delaminatedDELAMINATED FLOOR PANEL 211HF IN THE COCKPIT. FOUND OUT LIMITS IAW SRM 53-12-00, DIAGRAM 101, SHEET 1. REPLACED IAW SRM 53-12-00, PAR 5F, FIG 206 .Apr 26, 2015 · N340NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2015042702986Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231TF IN PASSENGER CABIN. FLOOR PANEL FOUND OUT LIMITS IAW SRM 53-02-00, TABLE 103 AND WAS REPLACED IAW SRM 53-02-00, PAR 8H, FIG 209 AND IRM 9701, REV G.Apr 26, 2015 · N340NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2015042702985Floor Panel · crackedCRACK ON FLOOR PANEL 241JF IN THE CABIN. FLOOR PANEL FOUND OUT LIMITS. REPLACED IAW SRM 53-02-00, PAR 8H, FIG 209 AND IRM 9701, REV G.Apr 26, 2015 · N340NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2015042702984Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y512 FRAMES 64 TO 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472230.Apr 26, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2016112209101Web · corrodedCORROSION ON WEB STRINGER 38R BETWEEN FRAMES 51 TO 52. REPLACED THE WEB IAW SRM.Apr 25, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042702991Seat Track · corrodedCORROSION ON SEAT TRACK +Y765, FRAMES 36 TO 41. FOUND OUT OF LIMITS IAW AMDS 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Apr 25, 2015 · N340NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015042702990Seat Track · corrodedCORROSION ON SEAT TRACK +Y1292, FRAMES 41 TO 47. FOUND OUT OF LIMITS IAW AMDS 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Apr 25, 2015 · N340NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015042602978Floor Support · corrodedCORROSION ON FLOORBEAM +Y1225 BETWEEN. FR 66+5" AND FR 67+15 AT AFT GALLEY AREA, L=0.800 W=0.500", D=0.003". REPLACED FLOORBEAM Y1225 BETWEEN FR 66+5" AND FR67+15" AT AFT GALLEY AREA IAW SRM 51-72-11 DWG D53472000.Apr 25, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042602977Web · crackedCRACK ON WEB AT +Y765 BETWEEN FRAMES 8 AND 11 IN COCKPIT. REPLACED WEB IAW SRM 51-72-11 AND DWG D53113219.Apr 25, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042602941Seat Track · corrodedDURING INSPECTION, FOUND EVALUATED SEAT TRACK +Y765 FRAME 47 TO 64 POINT 1, FR50+9" UPPER FLANGE D.0.043, W.0.379. L.4. 229, POINT 2, FR 48+2" UPPER FLANGE D.0.049, W .0.370, L . 3.532, POINT 3, FRAME 59+8" UPPER FLANGE D.0.048, W.0.379, L.3.139, POINT 4, FRAApr 25, 2015 · N340NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015042602940Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1162 BETWEEN FRAME 67+15 AND FRAME 69 AT AFT GALLEY AREA L=0.700", W=0.400, D=0.002". REPLACED FLOORBEAM +Y1162 BETWEEN FRAME 67+15" AND FRAME 69 AT AFT GALLEY AREA IAW SRM A320 51-72-11, DWG D53472000.Apr 25, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042602939Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +1292 BETWEEN FRAME 64 AND FRAME 66+5" AT AFT GALLEY A REA L=1", W=0.500", D=0.003". REPLACED FLOORBEAM +1292 BETWEEN FRAME 64 AND FRAME 66+5" AT AFT GALLEY AERA SRM 51-72-11 AND DWG D53472000.Apr 25, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042602938Web · corrodedDURING INSPECTION, FOUND CRACK ON WEB -Y765, BETWEEN FR 8 AND FR 11 IN COCKPIT. REPLACED WEB -Y765 BETWEEN FR 8 AND FR 11 IN COCKPIT IAW SRM 51-72-11 AND DWG D53113219.Apr 25, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042602937Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 68 AT AFT GALLEY AREA AND STRINGER 23L, L=0.475", W=0.100", D=0.001". SSI 534136. REPLACED CORNER FITTING FRAME 68 AT AFT GALLEY AREA AND STRINGER 23L IAW SRM 51-72-11, DWG D53480019.Apr 25, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042602936Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 66 AT AFT GALLEY AREA AND STR 23L, L=0.270", W=0.160", D=0.001", SSI 534136. REPLACED CORNER FITTING FRAME 66 AT AFT GALLEY AREA AND STR 23L IAW SRM 51-72-11 DWG D53480019.Apr 25, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042602935Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STRINGER 23L, L=2", W=1", D=0.003". SSI 534147. REPLACED LOWER SILL LOCATED AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STRINGER 23L IAW SRM 51-72-11 AND Apr 25, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042602944Support Angle · corrodedDURING INSPECTION, FOUND CORROSION ON SUPPORT ANGLE IN AFT CARGO COMPARTMENT ON STR 44 BETWEEN FRAME 64 TO FRAME 65. REPLACED SUPPORT ANGLE IN AFT CARGO COMPARTMENT ON STR 44 BETWEEN FRAME 64 TO FR65 IAW SRM 51-72-11 AND DWG D53470150.Apr 24, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042602943Seat Track · corrodedDURING INSPECTION, FOUND CORRODED SEAT TRACK +Y1292 FRAME 47 TO 64 POINT 1 FRAME 47+7" UPPER FLANGE D.0.036, W.0.379, L.4 437, POINT 2 FRAME 52" UPPER FLANGE D.0.037, W.0.379, L. 3.845, POINT 3 FR 57+19" UPPER FLANGE D.0.050, W.0.379L 3.791, POINT 4, FRAME 6Apr 24, 2015 · N340NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015042502934Frame Splice · corrodedDURING INSPECTION, FOUND CORROSION ON SPLICE AT AFT GALLEY AREA ON STR 31 ON FRAME 67 L=0.437", W=0.218", D=0.002". MEASURES APPROXIMATELY, SSI 534144. REPLACED SPLICE AT AFT GALLEY AREA ON STRINGER 31 AND FRAME 67 IAW SRM 51-72-11 AND DWGS D53480020 AND D53Apr 24, 2015 · N340NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2015042402925Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y 189 AT FWD GALLEY AREA BETWEEN FRAME 20 TO FRAME 23. L=1.250", W=0.900", D=0.003", MEASURES APRROXIMATELY SSI 531189. REPLACED FLOORBEAM -Y189 AT FWD GALLEY AREA BETWEEN FRAME 20 TO FRAME 23 IAW SRM 51-72-11Apr 23, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042402924Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB AT AFT GALLEY AREA FROM FRAME 69 TO FRAME 70 AND STR 23R, L=2", W=1", D=0.002". SSI 534147. REPLACED WEB AT AFT GALLEY AREA FROM FRAME 69 TO FRAME 70 AND STR 23R IAW SRM 51-72-11 AND DWG D53470100.Apr 23, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042402905Stringer Splice · corrodedDURING INSPECTION, FOUND CORROSION ON SPLICE AT AFT GALLEY AREA ON STR 30R ON FRAME 67, L=0.300", W=0.250", D=0.008". MEASURES APPROXIMATELY, SSI 534144. REPLACED SPLICE AT AFT GALLEY AREA ON STRINGER 30R AND FRAME 67 IAW SRM 51-72-11 AND DWG D53480020 ANApr 23, 2015 · N340NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015042402904Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y310 BETWEEN FR 65 TO FR 67 AT AFT GALLEY AREA L=5", W=3", D=0.003". SSI 534147. REPLACED FLOORBEAM -Y318 BETWEEN FR 65 TO FR 67 AT AFT GALLEY AREA IAW SRM 51-72-11 DWG D53472305.Apr 23, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042302897Stringer Splice · corrodedDURING INSPECTION, FOUND CORROSION ON SPLICE AT AFT GALLEY ARA ON STR 29L ON FRAME 67 L=0.540", W=0.100", D=0.002", MEASURES APPROXIMATELY, SSI 534144. REPLACED SPLICE AT AFT GALLEY AREA ON STR 29L ON FRAME 67L IAW SRM 51-72-11 AND DWG D53480020.Apr 22, 2015 · N340NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015042302896Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -465 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 67, L=1.5", W=0.500", D=0.002", SSI 534147. REPLACED FLOORBEAM -Y465 AT AFT GALLEY AREA FROM FR 64 TO FR 67+ 5" IAW SRM 51-72-11 DWG D53472000.Apr 22, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042302892Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y765 BETWEEN FR 66+5" AND FR 70 AT AFT GALLEY AREA L=2", W=1", D=0.033", SSI 534147. REPLACED FLOORBEAM +Y765 BETWEEN FR 66+5" AND FR 70 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000.Apr 22, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042202882Seat Track · corrodedDURING INSPECTION, FOUND OUT LIMIT SEAT TRACK -Y1292 FLOOR STRUCTURE AFTER EVALUATION IAW AMDS 2500-2030 AT FWD GALLEY AREA FROM FRAME 20 TO FRAME 24, 3 EA, L=1.586 , W=0.376 , D=0.050. L=3.304, W=0.367, D=0.034, L=1.824, W=0.365, D=0.049". REPLACEDApr 21, 2015 · N340NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015042202873Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y765 AT AFT GALLEY AREA FROM FRAMES 64 TO 66. REPLACED FLOOR SUPPORT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472230.Apr 21, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042202872Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y765 AT AFT GALLEY AREA FORM FRAMES 66 TO 70REPLACED FLOOR SUPPORT -Y765 AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 70 IAW SRM 51-72-11 AND DWG D53472000.Apr 21, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042202871Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y765 BETWEEN FRAMES 64 AND 66+5" AT AFT GALLEY AREA L=3", W=2", D=0.004", SSI 534147. REPLACED FLOORBEAM +Y765 BETWEEN FRAME 64 AND FRAME 66+5" AT AFT GALLEY AREA IAW SRM 51-72-11.Apr 21, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042202870Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM LOCATED BETWEEN +Y254 TO +Y180 AT AFT GALLEY AREA L=0.500", W=0.300", D=0.002", SSI 534147. REPLACED FLOORBEAM LOCATED BETWEEN +Y254 TO +Y180 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000.Apr 21, 2015 · N340NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2015042102839Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y765 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24, L=0.987", W=0.675", D=0.002", APPROX SSI 531189. REPLACED FLOORBEAM +Y765 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24 IAW SRM 51-72-11 AND DWG D53112812 AND Apr 20, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042102838Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y512 BETWEEN FR 64 AND FR 70 AT AFT GALLEY AREA L=4", W=3", D=0.004". SSI 534147. REPLACED FLOORBEAM Y512 BETWEEN FR 64 AND FR 70 AFT GALLEY AREA IAW SRM 51-72-11 DWG D53472000.Apr 20, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042102843Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING AT FWD GALLEY AREA ON STRINGER 23R BETWEEN FRAME 16 TO FRAME 20, L=0.300", W=0.150", D=0.003". MEASURES APPROXIMATELY, SSI 531189. REPLACED CENTER FITTING AT FWD GALLEY AREA ON STR 23R BETWEEN FRAME 16 TApr 19, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042102842Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 20 AT FWD GALLEY AREA ON STRINGER 23L, L=0.200", W=0.100", D=0.004". MEASURES APPROXIMATELY SSI 531189. REPLACED CORNER FITTING FRAME 20 AT FWD GALLEY AREA ON STR 23L IAW SRM 51-72-11 AND DWG D5311222Apr 19, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015042102841Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING AT FWD GALLEY AREA ON STR 23L BETWEEN FRAME 16 TO FRAME 20. L=0.200", W=0.150", D=0.003". MEASURES APPROXIMATELY, SSI 531189. REPLACED CENTER FITTING AT FWD GALLEY AREA ON STR 23L BETWEEN FRAME 16 TO FRAApr 19, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2016112209104Seat Track · corrodedCORROSION ON SEAT TRACK +Y765, FRAMES 41 - 47. REPLACED THE SEAT TRACK.Apr 18, 2015 · N340NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015041902806Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1292 AT FWD GALLEY AREA FROM FRAME 12 TO FR AME 24, L=0.895, W=0.679, D=0.002. APPROXIMATELY SSI 531189. REPLACED FLOOR BEAM +Y1292 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24 SRM 51-72-11 AND DWG D53112812Apr 18, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015041802805Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB FRAME 20 -Y1732 AT FWD GALLEY AREA L=0.895 W=0.658, D=0.002. APROXIMATELY SSI531189. REPLACED WEB LOCATED ON FR 20 -Y1732 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53112783.Apr 17, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015041802804Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y 81 AT FWD GALLEY AREA BETWEEN FRAME 12 TO FRAME 16. L=1.500", W=1.000", D=0.003". MEASURES APPROXIMATELY. REPLACED FLOORBEAM -Y81 AT FWD GALLEY AREA BETWEEN FRAME 12 TO FRAME 16 IAW SRM 51-72-11 AND DWG D5Apr 17, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015041702802Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM Y 503 AT FWD GALLEY AREA BETWEEN FRAME 12 TO FRAME 16. L=3.000", W=2.000", D=0.004". MEASURES APPROXIMATELY. REPLACED FLOORBEAM Y503 AT FWD GALLEY AREA BETWEEN FRAME 12 TO FRAME 16 IAW SRM 51-72-11 AND D531128Apr 16, 2015 · N340NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA1501443240Skin · damagedFUSELAGE SKIN HAS BIRD STRIKE DAMAGE. REPLACED THE SKIN IAW ERA 525216-14.Apr 24, 2014 · N340NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA14014033240Wire · damagedDURING A NON-ROUTINE CHECK, CAPTAIN FOUND ROW 16 AND 17 EMERGENCY SEAT MOUNTED LIGHTS INOPERATIVE. FOUND WIRE OUT OF SPLICE UNDER SEAT 16, REPLACED AND CRIMPED CONNECTOR, FUNCTIONAL CHECK WAS NORMAL.Feb 27, 2014 · N340NW · Airbus A320211 · Light System WiringSDR DALA13030553240Battery · faultedDURING SERVICE CHECK, FOUND FORWARD EPSU BATTERY FAULT. MX REPLACED FORWARD EPSU BATTERY AND OPS CHECK WAS NORMAL.Jun 20, 2013 · N340NW · Airbus A320212 · Emergency LightingSDR DALA1209193240Connector · damagedDURING NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 8C INOPERATIVE. MAINTENANCE REPINNED AND REPLACED CONNECTOR UNDER SEAT AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Feb 16, 2012 · N340NW · Airbus A320212 · Light System WiringSDR DALA1141773240Wire · brokenDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT 4L INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND FUNCTIONAL CHECK IS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jun 26, 2011 · N340NW · Airbus A320212 · Light System WiringSDR DALA1501413240Skin · damagedFUSELAGE SKIN HAS A LIGHTNING STRIKE, FRAMES 28-29, S41L. REPAIRED IAW SRM 53-21-11.Apr 16, 2011 · N340NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA1030043240Wire · disconnectedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 7C AND 25C INOPERATIVE. MAINTENANCE RECONNECTED WIRES AT BOTH SEAT AND FUNCTIONAL CHECK WAS NORMAL. (2010-00829)Oct 29, 2010 · N340NW · Airbus A320212 · Light System WiringSDR DALA109823240Wire · brokenDURING TEST PATH LIGHT SEAT 4B WAS INOP, REPAIRED BROKEN WIRE AND SECURED CONNECTION AND CHECKS OK.May 12, 2010 · N340NW · Airbus A320212 · Light System Wiring
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