N357NW

Service difficulty reports · 219

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 = 'N357NW' 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 DALA2019081504807Pressure Panel · damagedLH PRESSURE PANEL - FRAME 36 FOUND HOLE 12 CRACK EXCEEDS REPAIR AREA. REPAIRED PER PRI 580246-14 REV. 0, 1, 2, 3 AND 4, AND ER/A 580246-14 REV ORIGINAL.Aug 14, 2019 · N357NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2019081504806Pressure Panel · damagedLH PRESSURE PANEL - FRAME 36 FOUND HOLE 4 CRACK EXCEEDS REPAIR AREA. REF. AA5311-011171, SB A320-53 -1263, AD2018--06-04. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 147-0001:5311-01171- 04A/004 00213 REPAIRED PER PRI 580246-14 REV. 0, 1, 2, 3 AND 4, AND ER/A 58Aug 14, 2019 · N357NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2019081504805Pressure Panel · damagedLH PRESSURE PANEL - FRAME 36 FOUND HOLE 2 CRACK EXCEEDS REPAIR AREA. REF. AA5311-011171, SB A320-53 -1263, AD2018--06-04. REPAIRED PER PRI 580246-14 REV. 0, 1, 2, 3 AND 4, AND ER/A 580246-14 REV ORIGINAL.Aug 14, 2019 · N357NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2019081504804Pressure Panel · damagedLH PRESSURE FLOOR PANEL FASTENER HOLES AT FRAME 35 TO 36, CRACK FOUND AT HOLE "A". REPAIR IN ACCORDANCE WITH WORK CARD 5311- 01171-04A PRIOR TO FURTHER FLIGHT. "AA 5311-01171" "SB A320-53 -1264" "AD-2018-06-04". SUMMARY SEE NR FOR ADDITIONAL INFORMATION 056-00Aug 14, 2019 · N357NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2019081204703Frame · crackedLH PRESSURE PANEL - FRAME 36 FOUND HOLES 7,8,9,10 CRACKED. MODIFIED PER AMDS WORK CARD 5311-01171-04A.Aug 12, 2019 · N357NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2019071204193Light · inoperativeLEFT FORWARD OVERWING DOOR PULL HANDLE LIGHT HAS ONE BULB INOP, RELAMPED LT FWD OVERWING DOOR PULL HANDLE BULBS.Jul 11, 2019 · N357NW · Airbus A320212 · Emergency LightingSDR DALA2018081305053Relay · faultedEMERGENCY LIGHTS DO NOT COME ILLUMINATE WITH WHEELS DOWN, SWITCH OK. CHECKED ALL WIRING AT TB871VT. FOUND POWER SUPPLY RELAY 8WL AT FAULT. REMOVED AND REPLACED THE RELAY. OPS CHECKED OK.Aug 2, 2018 · N357NW · Airbus A320212 · Emergency LightingSDR DALA2018060903918Light · inoperativeEMERGENCY SEAT MOUNTED LIGHTING INOPERATIVE AT 4C. REINSTALLED.Jun 7, 2018 · N357NW · Airbus A320212 · Emergency LightingSDR DALA2017083106484Pin · wornAFT PINTLE PIN ON MLG THREADS WORN. REMOVED AND REPLACED ON CARD 3210-9601-LT.Aug 29, 2017 · N357NW · Airbus A320212 · Main Landing GearSDR DALA2016121809958Power Supply · inoperativeEMERGENCY LIGHT FAULTING, AFT LEFT ESPU AND BATTERY PACK REPLACED.Dec 17, 2016 · N357NW · Airbus A320212 · Emergency LightingSDR DALA2016101107226Power Supply · inoperativeEPSU INT LOAD AFT LT INDICATION, REPLACED AFT LT EMERGENCY POWER SUPPLY UNITOct 10, 2016 · N357NW · Airbus A320212 · Emergency LightingSDR DALA2015111707103Skin · burnedBURN MARK ON SKIN BS 385, 6" BELOW LAP SKIN, RT SIDE, DRILLED OUT DAMAGE TO .1562" RLW 744338. HFEC CHECKED IAW NTM 51-10-01. DAMAGE REMOVED QC1976 INSTALLED SOLID FASTENER IAW SRM 53-11-11, FIG 211.Nov 16, 2015 · N357NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015092505921Stringer · corrodedCORROSION ON STR 41R LOCATED BETWEEN FRAME 59 TO FRAME 63 MEASURE ARE L=2.100" , W=0.750", D=0.010", APPROXIMATELY SSI 534107 IN AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 41R LOCATED BETWEEN FRAME 59 TO FRAME 63 IN AFT CARGO COMPARTMENT ISep 24, 2015 · N357NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015092305985Shear Tie · deformedR & R DEFORMED SHEAR TIE FROM FRAME 73 BETWEEN STR 32L TO 32R. REPAIRED IAW ERA 506865-14, REV ORIGINAL SECTION IV, SRM 51-72-11 AND PRI 506865-14, REV.0 AND 1.Sep 22, 2015 · N357NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015092305917Access Panel · corrodedCORROSION ON ACCESS PANEL 640LB COUNTERSINK HOLES ON RT WING. REPLACED ACCESS PANEL 640LB ON RT WING DUE TO NOT FOUND ALLOWABLE DAMAGE IAW SRM 51-27-11 AND THE INSTALLATION IS DOCUMENTED ON AMDS 5730-6013.Sep 22, 2015 · N357NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2015092305916Stringer · corrodedCORROSION ON STR 42L LOCATED BETWEEN FR 61 TO FR 63 MEASURE ARE L=1.150", W=0.310", D=0.010" SSI 534107 IN AFT CARGO COMPARTMENT. REPLACED STR SECTION 42L LOCATED BETWEEN FRAME 61 TO FRAME 64 AND FASTENERS IAW SRM 51-72-11, DWG D53470345, PRI 539100-14 REV 0 Sep 22, 2015 · N357NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015092305795Stringer · corrodedCORROSION ON STRINGER 42R BETWEEN FRAMES 61 - 63. REPLACED THE STRINGER IAW SRM 51-72-11, DWG D53470345, PRI 539100-14, REV 0, AND ER/A 539100-14, REV ORIGINAL.Sep 22, 2015 · N357NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015092305794Stringer · corrodedCORROSION ON STRINGER 43L BETWEEN FRAMES 61 - 63. REPLACED THE STRINGER IAW SRM 51-72-11, DWG D53470330, PRI 539100-14, REV 0 AND ERA 539100-14, REV ORIGINAL.Sep 22, 2015 · N357NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015092005768Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1292 BETWEEN FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53110900 AND D53110984.Sep 19, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015091605686Seat Track · corrodedSEAT TRACK, -Y1292, FRAME 47 - 64 CORRODED. FOUND OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 DWG D53472831 AND D53472830.Sep 15, 2015 · N357NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015091605685Seat Track · corrodedSEAT TRACK, +Y1292, FRAME 47 TO 64 CORRODED OUT LIMITS IAW AMDS. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DWG D53472030 AND D53472831.Sep 15, 2015 · N357NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015091605684Seat Track · corrodedSEAT TRACK +Y765 FRAME 47 TO 64 CORRODED OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72 -11 AND DWGS, D53472030 AND D53472831.Sep 15, 2015 · N357NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016111808975Stringer · corrodedCORROSION ON STRINGER 40R LOCATED BTW FR 58 TO FR 59 IN AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 40R LOCATED BTW FR58 TO FR59 IN AFT CARGO COMPARTMENT AS PER SRM.Sep 13, 2015 · N357NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015092405864Skin · not reportedPERFORM PERMANENT REPAIR AROUND SAFETY JACK POINT EXTERNAL SKIN AT LOWER FUSELAGE FROM FRAME 73 TO FRAME 74 BETWEEN STR 32L TO STR 32R. IAW ER/A 506865-14, REV B, REF LOGS 0589859, 2134193, 2147703, 8836824.Sep 13, 2015 · N357NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015091205632Fitting · corrodedCORROSION ON CENTER FITTING BETWEEN FRAMES 66 TO 68 AT STR 23L. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480009.Sep 11, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015091205630Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y765 BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.Sep 11, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015091205629Door Sill · corrodedCORROSION ON LOWER DOOR SILL FRAMES 66 TO 68. REPLACED THE DOOR SILL IAW SRM 51-72-11, DWG D53480019, AND D53474250.Sep 11, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015091205628Door Sill · corrodedCORROSION ON LOWER DOOR SILL. REPLACED THE DOOR SILL IAW SRM 51-72-11 AND DWG D53480019. REPAIR CLASSIFIED MAJOR.Sep 11, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015091205627Fitting · corrodedCORROSION ON CORNER FITTING FRAME 68 AT STR 23L. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480009.Sep 11, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015091205626Fitting · corrodedCORROSION ON CORNER FITTING, FRAME 68 AT STRINGER 23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480009.Sep 11, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015091205625Frame · damagedELONGATED HOLES ON FITTING AT FWD GALLEY AREA ON FRAME 12 AND -Y 1292. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53112758. MAJOR REPAIR.Sep 11, 2015 · N357NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2015091205624Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y1292, LOCATED BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112813.Sep 11, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015091105574Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y1225 MEASURES APPROXIMATELY L=0.960", W=0.700", D=0.003", AT AFT GALLEY AREA FROM FRAME 66+5" TO FRAME 67+15. REPLACED THE FLOOR SUPPORT IAW SRM A320 51-72-11 DWG D53472800.Sep 10, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015091105578Angle · crackedCRACK ON EMERGENCY EXIT DOOR ANGLE. REPLACED THE ANGLE IAW SRM 51-72-11 AND DWG D52279040.Sep 9, 2015 · N357NW · Airbus A320212 · Emergency ExitsSDR DALA2015091105577Angle · crackedCRACK ON EMERGENCY EXIT DOOR ANGLE . REPLACED THE ANGLE IAW SRM 51-72-11 AND DWG D52279040.Sep 9, 2015 · N357NW · Airbus A320212 · Emergency ExitsSDR DALA2015091105576Door Frame · crackedCRACK ON EMERGENCY EXIT DOOR FRAME. REPLACED THE DOOR FRAME IAW SRM 51-72-11 AND DWG D52279040.Sep 9, 2015 · N357NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2015091105575Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y1162 FROM FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM A320 51-72-11, DWG D53472800.Sep 9, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015091005573Dummy Rail · corrodedCORROSION ON RAIL DUMMY -Y81 LOCATED BETWEEN FRAME 12 TO FRAME 16 MEASURE ARE: L=0.500", W=0.250", D=0.010", APPROXIMATELY SSI 531189 AT FWD GALLEY AREA. REPLACED RAIL DUMMY -Y81 LOCATED BETWEEN FRAME 12 TO FRAME 16 FWD GALLEY AERA FLOOR STRUCTURE IAW SRM 51-Sep 9, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015090905571Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y512 FROM FRAMES 65 - 67. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.Sep 8, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015090905570Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1162 FROM FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472800.Sep 8, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015090905569Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1225 FROM FRAMES 66+5 - 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472800.Sep 8, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015090805524Floor Support · corrodedCORROSION ON FLOORBEAM -Y765 MEASURES APPROXIMATELY L=0.193", W=-0.114", D=0.003" AT AFT GALLEY AREA FROM FRAME 66+5" TO FRAME 70. REPLACED FLOORBEAM -Y765 LOCATED FROM FRAME 66+5" TO FRAME 70 AND FASTENERS IAW SRM 51-72-11 AND DWG D53472816.Sep 7, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015090805523Seat Track · corrodedCORROSION ON SEAT TRACK +Y1292 ON CENTER WING BOX FROM FRAME 41 TO FRAME 47. REPLACED SEAT TRACK +Y1292 ON CENTER WING BOX FROM FRAME 41 TO FRAME 47 IAW SRM 51-72-11 AND DWG D53371112.Sep 7, 2015 · N357NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015090805522Seat Track · corrodedCORROSION ON SEAT TRACK -Y765 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24. REPLACED ON SEAT TRACK =Y765 AT FWD GALLEY AREA FORM FRAME 12 TO FRAME 24 IAW SRM 51-72-11 AND DWG D53110984.Sep 7, 2015 · N357NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015090805521Floor Support · corrodedCORROSION ON FLOORBEAM -Y765 MEASURES APPROXIMATELY L=0.300", W=0.178", D=0.003" AT AFT GALLEY AERA FROM FRAME 64 TO FRAME 67+10". REPLACED FLOORBEAM -Y465 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 67+10" IAW SRM 51-72-11 AND DWG D53472816.Sep 7, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015090805520Seat Track · corrodedCORROSION ON SEAT TRACK +Y765 ON CENTER WING BOX FROM FRAME 36 TO FRAME 41. REPLACED SEAT TRACK +Y765 ON CENTER WING BOX FROM FRAME 36 TO FRAME 41, SRM 51-72-11 AND DWG D53370500.Sep 7, 2015 · N357NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015090805519Floor Support · corrodedCORROSION ON FLOORBEAM, +Y765 MEASURES APPROXIMATELY L=0.280", W=0.214", D=0.00 2" AT AFT GALLEY AREA FROM FRAME 66+5" TO FRAME 70. REPLACED FLOORBEAM Y765 AT AFT GALLEY AREA FROM FRAME 66 + 5" TO FRAME 70 IAW SRM 51-72-11 AND DWG D53472800.Sep 7, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015090705510Shear Tie · corrodedCORROSION ON CLEAT FR 30 RT BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT L=0.960", W=0.375", D=0.001". REPLACED CLEAT FR 30, RT BETWEEN. STR 40R TO STR 41R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231586 MEASURE OF CORROSION ARE: L=0.960",Sep 6, 2015 · N357NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015090505517Structure · corrodedCORROSION ON INTERNAL STRUCTURE COUPLING IN FWD CARGO COMPARTMENT FROM FRAME 30 TO FRAME 31 AND STRINGER 41R, L=1.160", W=0.350", D=0.001". REPLACED COUPLING ON INTERNAL STRUCTURE IN FWD CARGO COMPARTMENT FORM FRAME 30 TO FRAME 31 AND STR 41R IAW SRM 51-72-11Sep 4, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015090405514Support · corrodedCORROSION ON WEB SUPPORT LOCATED AT LEVEL STR 23 AND BETWEEN FRAME 20 TO FRAME 24, RT SIDE AT FWD GALLEY AERA. REPLACED WEB SUPPORT LOCATED AT LEVEL STR 23R AND BETWEEN FR 20 TO FR 24 RT SIDE AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG NR D53114392, REPAIRED Sep 3, 2015 · N357NW · Airbus A320212 · Fuselage Miscellaneous Structure
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