N351NW
Service difficulty reports · 257
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 = 'N351NW' 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.
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 = 'N351NW' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2021012700506Stringer · not reportedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE STRINGER 43L LOCATED BETWEEN FR 54 TO FR 60 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER. WORK WAS DOCUMENTED ON NON-ROUTINE CARD 224/100.SDR DALA2021012700502Stringer · corrodedCORROSION STRINGER 42L AND SPLICES LOCATED FROM FR 55 TO FR 58 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER, PER A320 SRM 51-72-11.SDR DALA2021012700501Stringer · not reportedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE ON STRINGER 42L BETWEEN FR 55 TO FR 58 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER 42L LOCATED BETWEEN FR 55 TO FR 60 IN AFT CARGO COMPARTMENT WAS DOCUMENTED ON NON-ROUTINE CASDR DALA2021012700500Shear Tie · corrodedCORROSION SHEAR TIE FR 30 AND BETWEEN STR 39/40 RT IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE, PER A320 SRM 51-72-11.SDR DALA2021012500467Stringer · corrodedCORROSION STRINGER 43R LOCATED AT FR 32 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: EVALUATED REWORK AREA STR 43R LOCATED AT FR 32 IN FWD C.C. FOUND WITHIN LIMITS ALLOWABLE, AS PER A320 SRM 53- 21-13-283-004. CONT ON MON.SDR DALA2021012500464Stringer · corrodedCORROSION STRINGER 40L LOCATED AT FR 32 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON STRINGER 40L LOCATED AT FR 32 IN FWD CARGO COMPARTMENT, AS PER SRM 53-00-13-300-001. RECHECK REQUIRED AT 60,000 FC/ 120,000 FH INSPECTION THRESHOLD FROM SDR DALA2021012500463Stringer · corrodedCORROSION STRINGER 40R LOCATED BETWEEN FR 31 TO FR 32 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON STRINGER 40R LOCATED BETWEEN FR 31 TO FR 32 IN FWD CARGO COMPARTMENT, AS PER SRM A320 53-00-13-300-001. RECHECK REQUIRED AT 60,000 FC/ 120,SDR DALA2021012500468Door Frame · crackedFUSELAGE FRAME 16 NOSE FWD LT DOOR STOP 1 & DOOR STOP 7 CRACKED HOLES. CORRECTIVE ACTION: ACCOMPLISHED ER/A 589094-14 SECTION II INSPECTION. CONT ON MON.SDR DALA2021012200443Washer · missingPASSENGER CREW DOOR 831 ADJUSTMENT WASHER ON UPPER LINK MISSING. CORRECTIVE ACTION: INSTALLED WASHER, ADJ DOOR, OK FOR SERVICE.SDR DALA2021012200436Frame · crackedCRACK INDICATION ON FRAME 4 LT SIDE UPPER SIDE POST LOWER FACE AT OPEN FASTENER HOLE SECOND MOST FWD. CORRECTIVE ACTION: REPLACED FITTING, PER A320 SRM 51-72-11.SDR DALA2021012200432Web · corrodedCORROSION INTERNAL STRUCTURE WEB LOCATED FROM FR 54 TO FR 55 AND STR 38L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED NEW WEB AND FASTENERS, PER A320 SRM 51-72-11.SDR DALA2021012000372Skin · corrodedCORROSION FRAME 33 TO FR 34 INTERNAL SKIN AND BETWEEN STR 40R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: INSPECTED AREA, AS PER SRM A320 53-21-11-283-007.SDR DALA2021012000371Skin · corrodedCORROSION FRAME 33 TO FRAME 34 INTERNAL SKIN BETWEEN STR 42R TO STR 44 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: INSPECTED AREAS, PER SRM A320 53-21-11-283-007. CONT IN SERVICE.SDR DALA2021012000361Frame · crackedCRACK INDICATION ON FRAME 20 RT SIDE ON DOOR STOP 1, OPEN FASTENER HOLE 3. CORRECTIVE ACTION: REPLACED INTERCOSTAL FITTING, PER SRM A320 51-72-11. OK FOR SERVICE.SDR DALA2021012000360Frame · crackedCRACK INDICATION ON FRAME 20 RT SIDE ON OPEN FASTENER HOLE C. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 589068-14 AD PRI. REV 0, REV 1 AND ER/A 589068-14 REV.ORIGINAL.SDR DALA2021011900302Door Frame · crackedCRACK INDICATION ON FRAME 68 LT DOOR STOP 1 LOWER OUTBOARD HOLE. CORRECTIVE ACTION: PERFORMED REPAIR ON FRAME 68 LT DOOR STOP 1 LOWER OUTBOARD HOLE IN PASSENGER CABIN, AS PER A320 SRM 53-41-12-300-010 RECHECK REQUIRED AT 37,700 FC.SDR DALA2021011900301Frame · crackedCRACK INDICATION ON FRAME 16 RT SIDE ON DOOR STOP 7, OPEN FASTENER HOLE 1 ON FRAME AND INTERCOSTAL FITTING LAYER. CORRECTIVE ACTION: REPLACED INTERCOSTAL FITTING, PER SRM A320 51-72-11.SDR DALA2021011900300Frame · crackedCRACK INDICATION ON FRAME 16 RT SIDE ON DOOR STOP 7, OPEN FASTENER HOLE 3 ON INTERCOSTAL FITTING LAYER FWD GALLEY AREA. CORECTIVE ACTION: REPLACED INTERCOSTAL FITTING, PER SRM A320 51-72-11.SDR DALA2021011900286Shear Tie · corrodedCORROSION INTERNAL STRUCTURE SHEAR TIE LOCATED AT FR 28 BETWEEN STR 41L TO STR 42L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE SHEAR TIE, PER SRM A320 51-72-11.SDR DALA2021011900285Door Frame · crackedCRACK INDICATION ON FRAME 16 RT SIDE ON DOOR STOP 1, OPEN FASTENER HOLE 3 ON FRAME LAYER. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 589110-14AD PRI REV 0, REV 1 AND ER/A 589110-14AD REV ORIGINAL.SDR DALA2021011900308Door Frame · crackedCRACK AT FR 20RT AT DOOR STOP NO 7 LEVEL/DOUBLE JOGGLE. CORRECTIVE ACTION: ACCOMPLISH ER/A 589068-14 SECTION II INSPECTION. CONTINUE TO MONITOR.SDR DALA2021011900283Frame · crackedCRACK INDICATION ON FRAME 16 RT SIDE OPEN FASTENER HOLE A ON UPPER DOUBLE JOGGLE AREA. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 589100 REV ORIGINAL AND ER/A 589100-14QD PRI REV 0 AND REV 1.SDR DALA2021011900282Frame · crackedCRACK INDICATION ON FRAME 16 RT SIDE OPEN FASTENER HOLE C ON UPPER DOUBLE JOGGLE AREA. CORRECTIVE ACTION: PERFORMED REPAIR ON FRAME 16RT SIDE OPEN FASTENERS HOLE C ON UPPER DOUBLE JOGGLE AREA AT FWD GALLEY AREA, AS PER ER/A 589100-14 REV ORIGINAL AND ER/A 589SDR DALA2021011500247Door Frame · crackedFUSELAGE NOSE FWD RT FRAME 16 DOOR STOP 1 HOLE 3 CRACKED. CORRECTIVE ACTION: MON INSP PER ERA 589110-14AD SECTION II INSPECTION.SDR DALA2021011300189Not Reported · not reportedHOLES REQUIRE COLD WORK HOLE A AND HOLE B IN ACCORDANCE WITH WORK CARD 5311- 01171-03B, AA 5311-01171, SB A320-53-1264, AD-2018-06-04. CORRECTIVE ACTION: PERFORMED COLD WORK OF HOLES. OK FOR SERVICE.SDR DALA2021011300188Not Reported · not reportedCOLD WORK REQUIRED FOR HOLE A AND HOLE B IN ACCORDANCE WITH WORK CARD 5311- 01171-03A, AA 5311-01171, SB A320-53-1264, AD-2018-06-04. PERFORMED COLD WORK OF HOLES. OK FOR SERVICE.SDR DALA2021011100160Floor Support · corrodedCORROSION FLOOR BEAM Y503.2 LOCATED BETWEEN FR 12 TO FR 16 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER A320 SRM 51-42-11 AND SRM 51-72-11.SDR DALA2021011100159Floor Support · corrodedCORROSION FLOOR BEAM +Y1292 BETWEEN FR 66 TO FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND SRM 51-72-11.SDR DALA2021011100155Frame · crackedCRACK INDICATION ON FRAME 68 LT DOOR STOP 1 LOWER INBOARD HOLE. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 SRM 53-41-12-300-010 RECHECK REQUIRED AT 37,700 FC.SDR DALA2021011100142Frame · crackedCRACK INDICATION ON FRAME 20 LT SIDE ON DOOR STOP 1, OPEN FASTENER HOL E 3 ON FRAME. CORRECTIVE ACTION: PERFORMED ROTOTEST INSPECTION ON COMMON AFFECTED HOLES AFTER SEPARATION OF LAYERS ON DOOR STOP 1 LOCATE FR 20 LT AND DID NOT FIND CRACKS. OK FOR SERVICE.SDR DALA2021010800119Support · corrodedCORROSION LOWER SILL LT SIDE LOCATED AT LEVEL FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON LOWER SILL LT SIDE LOCATED AT LEVEL FR 68 AT AFT GALLEY AREA, AS PER A320 SRM 53-41-14.SDR DALA2021010800118Floor Support · corrodedCORROSION FLOOR BEAM -Y1292 LOCATED BETWEEN FR 66 TO FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER SRM A320 51-72-11-911-001.SDR DALA2021010800117Seat Track · corrodedCORROSION SEAT TRACK -Y1292 LOCATED AT LEVEL FR 20 AT FWD GALLEY. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER A320 SRM 51-42-11 AND SRM 51-72-11.SDR DALA2021010800116Floor Support · corrodedCORROSION FLOOR BEAM -Y1162.5 LOCATED BETWEEN FR 68 TO FR 69 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER SRM A320 51-72-11-911-001.SDR DALA2021010600068Floor Support · corrodedCORROSION FLOOR BEAM +Y765 LOCATED BETWEEN FR 66 TO FR 70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM +Y765 LOCATED BETWEEN FR 66 TO FR 70 AT AFT GALLEY AREA, AS PER A320 SRM 51-72-11.SDR DALA2021011900305Damper · no testDURING TEST PASSENGER CREW DOOR 842 DAMPER DID NOT PASS TEST. CORRECTIVE ACTION: REPLACED DAMPER, PER A320 AMM 52-13-14-400-001-B.SDR DALA2021011100161Damper · no testPASSENGER CREW DOOR 832 DAMPER DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DAMPER, PER AMM 52-13-14-400-001-B AND 52-13-14-000-001-B.SDR DALA2020122404252Door · out of adjustPASSENGER CREW DOOR 842 OUT OF ADJUSTMENT. CORRECTIVE ACTION: PERFORMED ADJUSTMENT OF DOOR, PER A320 FAM AMM 52-13-21-400-001-A. OK FOR SERVICE.SDR DALA2020122304200Door · out of adjustPASSENGER CREW DOOR 841 OUT OF ADJUSTMENT. CORRECTIVE ACTION: ADJUST PASSENGER CREW DOOR 841, PER A320 FAM AMM 52-11-21-400-001-A. OPERATIONS CHECK GOOD.SDR DALA2020122304199Shackle · corrodedCORROSION ON SHACKLES AFT BEARING ATTACH FITTING ON LT PYLON (2 EA). CORRECTIVE ACTION: REPLACED SHACKLES AFT BEARING ATTACH FITTING ON LT PYLON (2 EA), AS PER A320 FAM AMM 54-51-17-400-003-A.SDR DALA2019052603182Light · inoperativeEPSU EXT LOAD EMER L MESSAGE ON EMERGENCY LIGHTS TEST, RELAMPED OVERWING LIGHTS.SDR DALA2018121707294Light · damagedFOUND BOTH LEFT HAND OVERWING EXIT HANDLE EMERGENCY LIGHTS DAMAGED. REPLACED FORWARD AND AFT LEFT HAND OVERWING EXIT HANDLE LIGHT. OPERATION CHECKS GOOD.SDR DALA2018121097118Connector · incorrect(LP# 4597696) L1 EMERGENCY LIGHT ON WHEN SWITCH IN ARMED POSITION. ROUND 41WL AND 21WL PLUGGED IN REVERSED. SWITCHED PLUGS IAW AVM. OPERATION CHECKS GOOD.SDR DALA2018110606490Structure · crackedCRACK EMERGENCY EXIT DOOR 834 AFT SEGMENT. REPLACED SEGMENT IAW 572630-14AD, REV O.SDR DALA2018110606489Structure · crackedCRACK EMERGENCY EXIT DOOR 834 FWD SEGMENT. REPLACED SEGMENT IAW PRI/ERA 572630-14AD REV O.SDR DALA2018100906001Unknown · odorAFTER LIFTOFF SMELLED STRONG RUBBER TIRE SMELL IN COCKPIT AND REPORTS FROM ROW 12-24. DISSIPATED WITHIN 2 MINUTES. COMPLY WITH NO GO ODI PREVENTION PER MCC INSPECTED AIRCRAFT. NO HYDRAULIC , ENGINE AND APU COMPARTMENT LEAKS. ALL CLEAR. HIGH POWER ENGINE RUN WISDR DALA2016111408764Angle · corrodedCORROSION ANGLE ON INTERNAL STRUCTURE AT FR 67 BTW STR 43L AND STR 43R IN AFT CARGO COMPARTMENT. REPLACED ANGLE ON INTERNAL STRUCTURE AT FR 67 BTW STR 43L AND STR 43R IN AFT CARGO COMPARTMENT AS PER SRM 51-72-11 AND DRAWING D53480212.SDR DALA2017080105820Skin · corrodedCORROSION ON SKIN BETWEEN STRINGERS 41 AND 43 LEFT, FRAME 56 AND 57, 3 SPOTS. REMOVED AREA OF CORROSION IAW SRM 51-73-00.SDR DALA2016020100834Stringer · corrodedCORROSION ON STRINGER 43L AT FRAMES 56 AND 57, REPLACED STR SPLICE 42L IAW SRM 53-00-13, FIG 201.SDR DALA2016020100833Stringer · corrodedSTRINGER CORROSION ON 42L AT FRAME 56 AND 57, REPLACED STRINGER SPLICE 42L IAW SRM 53-00-13, FIG 201.
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