N339NW

Service difficulty reports · 177

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 = 'N339NW' 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 DALA2021020500685Frame · crackedSHIP 3239 CRACK INDICATION ON FRAME 36 R -Y1292 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON FRAME PER PRI 589227-14AD REV 0, REV 1, REV 2, AND ERA 589227-14AD REV ORIGINAL. (1722889)Feb 4, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021020500684Frame · crackedSHIP 3239 CRACK INDICATION ON FRAME 36 L Y1292 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON FRAME PER PRI 589227-14AD REV.0 REV1, REV2 AND ERA 589227-14D REV. ORIGINAL. (1722885)Feb 4, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021020500683Pressure Deck · crackedSHIP 3239 CRACK INDICATION FOUND AT FASTENER HOLE A. PRESSURE FLOOR PANEL RH SIDE 7 OCLOCK POSITION. CORRECTIVE ACTION: REPAIRED IN ACCORDANCE WITH DELTA WORK CARD 5311-01171-04B. (1722882)Feb 4, 2021 · N339NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021020500682Frame · crackedSHIP 3239 CRACK INDICATION ON FRAME 36 L Y1292 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON FRAME PER PRI 589227-14AD REV.0 REV1, REV2 AND ERA 589227-14D REV. ORIGINAL. (1722881)Feb 4, 2021 · N339NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021020500681Pressure Deck · crackedSHIP 3239 CRACK INDICATION FOUND AT FASTENER HOLE A. PRESSURE FLOOR PANEL LH SIDE 12 OCLOCK POSITION. CORRECTIVE ACTION: REPAIRED IN ACCORDANCE WITH DELTA WORK CARD 5311-01171-04A. (1722880)Feb 4, 2021 · N339NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021020500680Frame · crackedSHIP 3239 CRACK INDICATION ON FRAME 36 R -Y1292 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON FRAME PER PRI 589227-14AD REV.0 REV1, REV2 AND ERA 589227-14D REV. ORIGINAL. (1722879)Feb 4, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021020400672Frame · crackedSHIP 3239 CRACK INDICATION ON FRAME 68 RT SIDE ON OPEN FASTENER HOLE 4 AT DOOR S TOP 1 POSITION. CORRECTIVE ACTION PERFORMED REPAIR PER PRI 589181-14 REV. O AND REV 1 ERA/: 589181-14 AD REV. ORIGINAL.Feb 3, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021020400668Stringer · crackedSHIP 3239 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 4 AT FR 36. R. CORRECTIVE ACTION PERFORMED PERMANENT REPAIR PER ER/A 589108-14AD REV. ORIGINAL PRI 589108-14AD REV.0 AND REV. 1.Feb 3, 2021 · N339NW · Airbus A320212 · Wing, Center BoxSDR DALA2021020400667Frame · crackedSHIP 3239 CRACK INDICATION ON FRAME 35 HOLE 6 LT IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION PERFORMED REPAIR PER PRI REV.0, REV.1, REV.2 ER/A 589152-14AD REV. ORIGINAL.Feb 3, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021020400665Fuel Tank · corrodedSHIP 3239 CORROSION INTERNAL STRUCTURE UPPER SKIN OF CENTER FUEL TANK LOCATED FR 40 BETWEEN Y1292 AND Y1732 IN PASSENGER CABIN. CORRECTIVE ACTION PERFORMED REPAIR PER PRI 589264-14 REV 0 AND ER/A REV ORIGINAL.Feb 3, 2021 · N339NW · Airbus A320212 · Fuel StorageSDR DALA2021020300649Rib · crackedSHIP 3239 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR 36. R. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER ER/A 589108-14AD REV. ORIGINAL PRI 589108-14AD REV 0. (1721483)Feb 3, 2021 · N339NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021020300648Rib · crackedSHIP 3239 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR 36. R. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER ER/A 589108-14AD REV. ORIGINAL PRI 589108-14AD REV 0. (1721480)Feb 3, 2021 · N339NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021020300647Rib · crackedSHIP 3239 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36. R. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER ER/A 589108-14AD REV. ORIGINAL PRI 589108-14AD REV 0. (1721477)Feb 3, 2021 · N339NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021020300646Rib · crackedSHIP 3239 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36. R. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER ER/A 589108-14AD REV. ORIGINAL PRI 589108-14AD REV 0. (1721476)Feb 3, 2021 · N339NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021020300645Rib · crackedSHIP 3239 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 4 AT FR 36. R. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER ER/A 589108-14AD REV. ORIGINAL PRI 589108-14AD REV 0. (1721474)Feb 3, 2021 · N339NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021020400674Slide Raft · failedSHIP 3239 SLIDE RAFT AT PASSENGER CREW DOOR 842 DID NOT PASS TEST WHILE TESTING. CORRECTIVE ACTION REPLACED SLIDE RAFT PER DELTA WORK CARD AMDS 2561 -4002-RA. OK FOR SERVICE.Feb 2, 2021 · N339NW · Airbus A320212 · Life RaftSDR DALA2021020300642Stringer · corrodedSHIP 3239 CORROSION STRINGER 31R FROM FR65 TO FR66 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-72-11 AND SRM 51-42-11. (1720956)Feb 2, 2021 · N339NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2021020400675Bulkhead · crackedSHIP 3239 FUSELAGE, BULKHEADS, FR35LT BTW STGR28 AND STGR31 CRACK AT HOLE 6. CORRECTIVE ACTION ACCOMPLISHED ER/A 589152-14 SECTION II INSPECTION. CONT ON MON.Jan 29, 2021 · N339NW · Airbus A320212 · Fuselage Main, BulkheadSDR DALA2021020200622Floorbeam · crackedSHIP 3239 WINGS / CENTER WING / FRONT SPAR AT FR36 / FLOOR BEAM & VERTICAL STIFFENER / CRACKS. CORRECTIVE ACTION: ACCOMPLISH ER/A 589108-14. CONT ON MON. (1718034)Jan 29, 2021 · N339NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2021020100587Frame · crackedSHIP 3239 CRACK INDICATION ON FRAME 16 LT SIDE ON OPEN FASTENER HOLE C. PERFORMED REPAIR PER PRI N 589064-14AD REV 0 AND REV 1 AND ERA 589064-14 REV ORIGINAL.Jan 29, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021020100582Floorbeam · corrodedSHIP 3239 CORROSION FLOOR BEAM -Y254 AT LEVEL FR12 AT FWD GALLEY AREA. CORRECTIVE ACTION REPLACED FLOOR BEAM PER A320 SRM 51-72-11.Jan 29, 2021 · N339NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2021020100581Skin · corrodedSHIP 3239 CORROSION EXTERNAL SKIN UPPER SURFACE LOCATED AT 3.5 INCHES OF FRONT SPAR RIB 7 ON RT WING. CORRECTIVE ACTION PERFORMED REPAIR PER PRI 589191- 14AD REV 0 AND ERA 589191-14 REV ORIGINAL.Jan 29, 2021 · N339NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2021020100580Skin · corrodedSHIP 3239 CORROSION EXTERNAL SKIN UPPER SURFACE LOCATED AT 2.5 INCHES OF FRONT SPAR AND BTW RIB 1 TO RIB 2 ON RT WING. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 589191-14 REV.0 AND ERA 589191-14 REV ORIGINAL.Jan 29, 2021 · N339NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2021012900551Skin · dentedDENT EXTERNAL SKIN LOCATED FR 65 BETWEEN STR 40R AND STR 41R LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR ON EXTERNAL SKIN, PER ER/A 589496-14 REV ORIGINAL AND PRI 589496-14 REV 0 AND REV 1.Jan 28, 2021 · N339NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2021012900550Fastener · crackedCRACK INDICATION FRAME 16 RT SIDE ON OPEN FASTENER HOLE B. CORRECTIVE ACTION: PERFORMED REPAIR, PER PRI NR 589066-14AD REV 0 AND REV 1 AND ER/A NR 589066-14 REV ORIGINAL.Jan 28, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021012900548Fastener · crackedCRACK INDICATION ON FRAME 16 RT SIDE ON OPEN FASTENER HOLE C. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI NO, 589066-14AD REV 0 AND REV 1 AND ER/A NR 589066-14 REV ORIGINAL.Jan 28, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021012700505Floor Support · corrodedCORROSION FLOOR BEAM +Y765 LOCATED BETWEEN FR 66 TO FR 70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER A320 SRM 51-72-11.Jan 26, 2021 · N339NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021012700504Floor Support · corrodedCORROSION FLOOR BEAM -Y160 FROM FR 66 TO FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER A320 SRM 51-72-11.Jan 26, 2021 · N339NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021012700503Floorbeam · corrodedCORROSION FLOOR BEAM -Y765 AT LEVEL FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER A320 SRM 51-72-11.Jan 26, 2021 · N339NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2021012600490Shear Tie · corrodedCORROSION SHEAR TIE LOCATED AT FR 34 AND BETWEEN STR 42L TO STR 43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED AT FR 34 AND BETWEEN STR 42L TO STR 43L IN FWD CARGO COMPARTMENT.Jan 25, 2021 · N339NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2021012600488Support · corrodedCORROSION LOWER SILL LOCATED AT FR 68 AND STR 23L AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED LOWER SILL, PER A320 SRM 51-72-11.Jan 25, 2021 · N339NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021012600487Web · corrodedCORROSION INTERNAL STRUCTURE ON WEB LOCATED BETWEEN FR 56 TO FR 57 AT LEVEL STR 38R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED WEB, PER A320 SRM 51-72-11.Jan 25, 2021 · N339NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021012600486Stringer · corrodedCORROSION STRINGER 41L LOCATED AT LEVEL FR 66 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON STRINGER, PER A320 SRM 53-41-13-300-004.Jan 25, 2021 · N339NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2021012600485Floorbeam · corrodedCORROSION FLOOR BEAM +Y1292 AND FR 16 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER A320 SRM 51-72-11.Jan 25, 2021 · N339NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2021012600484Floor Support · corrodedCORROSION FLOOR BEAM -Y1162.5 FROM FR 68 TO FR 69 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER SRM A320 51-72-11.Jan 25, 2021 · N339NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021012600483Floor Support · corrodedCORROSION FLOOR BEAM -Y1225 FROM FR 66 TO FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER SRM A320 51-72-11.Jan 25, 2021 · N339NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021012600482Seat Track · corrodedCORROSION SEAT TRACK -Y1292 BETWEEN FR 18 TO FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER SRM 51-72-11.Jan 25, 2021 · N339NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2021012600481Web · crackedCRACK INTERNAL STRUCTURE ON WEB LOCATED BETWEEN FR 56 TO FR 57 AND STR 38L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED WEB LOCATED, PER A320 SRM 51-42-11 AND 51-72-11.Jan 25, 2021 · N339NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021012600480Web · corrodedCORROSION SUPPORT FRAME WEB LOCATED BETWEEN FR 69 TO FR 70 AT LEVEL STR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SUPPORT FRAME WEB, PER A320 SRM 51-72-11.Jan 25, 2021 · N339NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2024032103599Door Frame · noneSHIP 3239 DISC: DTA MONITOR INSPECTION, FUSELAGE / FRAMES / FR68 RH / DOOR STOP FITTING # 1 / LOWER INBOARD HOLE / CRACKS. C/A: REF ERA 589181-14.Jan 22, 2021 · N339NW · Airbus A320212 · Standard Practices/StructuresSDR DALA2024032103598Door Frame · noneSHIP 3239 DISC: DTA MONITOR FUSELAGE / FRAMES / FR68 RH / DOOR STOP FITTING # 1 / LOWER INBOARD HOLE / CRACKS. C/A: ER/A 589181-14. (LP: 1712233)Jan 22, 2021 · N339NW · Airbus A320212 · Standard Practices/StructuresSDR DALA2021020100592Damper · no testSHIP 3239 DURING DOOR TEST DAMPER ON PASSENGER CREW DOOR 832 FAILED TEST. CORRECTIVE ACTION REPLACED DAMPER PER A320 FAM AMM 52-13-14-400-001-A.Jan 22, 2021 · N339NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2021012900557Stop Fitting · crackedFUSELAGE FRAMES FR 68 RT DOOR STOP FITTING NR 1 LOWER INBOARD HOLE CRACKS. CORRECTIVE ACTION: ACCOMPLISHED ER/A 589181-14 SECTION II INSPECTION. CONT ON INSP MON.Jan 22, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021012200441Shear Tie · corrodedCORROSION SHEAR TIE LOCATED AT FR 32 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE, PER A320 SRM 51-72-11.Jan 21, 2021 · N339NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2021012000366Frame · crackedCRACK INDICATION ON FRAME 16 DOOR STOP FITTING 1 LT SIDE HOLE 3. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 589046-14AD REV 0, REV 1 AND ERA 589046-14AD REV ORIGINAL.Jan 19, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021012000365Frame · crackedCRACK INDICATION ON FRAME 16 DOOR STOP FITTING 7 RT SIDE HOLE 3. CORRECTIVE ACTION: PERFORMED REPAIR ON FRAME, PER PRI 589130-14AD REV 0 AND ERA 589130-14AD REV ORIGINAL.Jan 19, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021012000364Frame · crackedCRACK INDICATION ON FRAME 16 DOOR STOP FITTING 1 LT SIDE HOLE 1. CORRECTIVE ACTION: PERFORMED REPAIR ON FRAME, PER PRI 589046-14AD REV 0, REV 1 AND ERA 589046-14AD REV ORIGINAL.Jan 19, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021012000363Frame · crackedCRACK INDICATION ON FRAME 16 DOOR STOP FITTING 7 RT SIDE HOLE 1. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 589130-14AD REV 0 AND ERA 589130-14AD REV ORIGINAL.Jan 19, 2021 · N339NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021012000362Support Frame · corrodedCORROSION SUPPORT FRAME FROM FR 69 TO FR 70 AND STR 23L AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SUPPORT FRAME, PER A320 SRM 51-72-11.Jan 19, 2021 · N339NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2021011900281Floor Support · corrodedCORROSION FLOOR BEAM -Y464.8 FROM FR 67 TO FR 70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM, PER A320, SRM 51-72-11.Jan 16, 2021 · N339NW · Airbus A320212 · Fuselage Miscellaneous Structure
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