N348NW

Service difficulty reports · 272

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 = 'N348NW' 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 DALA2022010500087None · noneSHIP 3248 WEAR ON FITTING KEEL BEAM FWD ATTACHMENT DOOR FWD LUG FWD FACE RH SIDE IN MAIN WHEEL WELL. CORRECTIVE ACTION: COMPLIED WITH PRI 595828-14AD REV 0. (2075428)Jan 4, 2022 · N348NW · Airbus A320212 · Fuselage, Door HingeSDR DALA2022010500086None · noneSHIP 3248 WEAR ON FITTING KEEL BEAM ACTUATOR ATTACHMENT FWD LUG FWD FACE IN MAIN WHEEL WELL. CORRECTIVE ACTION: COMPLIED WITH PRI 595828-14AD REV 0. (2075418)Jan 4, 2022 · N348NW · Airbus A320212 · Fuselage, Door HingeSDR DALA2022010500085None · noneSHIP 3248 CRACK INBOARD THRUST REVERSER LOC. AT 3 OCLOCK PIVOT FITTING UPPER FLAGE ON ENGINE 1. CORRECTIVE ACTION: COMPLIED WITH CMM REPAIR 87 78-32-35 AND ER/A 596072-14AD REV. ORIGINAL. (2075278)Jan 4, 2022 · N348NW · Airbus A320212 · Engine Thrust ReverserSDR DALA2022010500089None · noneSHIP 3248 CORROSION STRINGER 38R BTW FR 32 AND FR 33 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: FOUND AREA WITHIN LIMITS. CONTINUE ON MON. (2073933)Jan 3, 2022 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2022010400066None · noneSHIP 3248 CRACK PROFILE LOCATED BTW FR 50 TO FR 54 LEVEL STR 35L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A #559065-14MA REV. ORIGINAL (2073939)Jan 3, 2022 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2022010400065None · noneSHIP 3248 CORROSION STRINGER SPLICE LOCATED STR26R AT LEVEL FR67 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER SPLICE PER A320 SRM 51-72-11. (2074229)Jan 3, 2022 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2022010400064None · noneSHIP 3248 CRACK INDICATION ON FRAME 35 BULKHEAD TO SKIN ATTACHMENT AREA LH SIDE AT OPEN FASTENER HOLE H16. CORRECTIVE ACTION: REPAIRED PER ER/A 595693-14AD REV ORIGINAL. (2074203)Jan 3, 2022 · N348NW · Airbus A320212 · Fuselage Main, BulkheadSDR DALA2022010400063None · noneSHIP 3248 CRACK INDICATION ON FRAME 35 LH SIDE AT OPEN FASTENER HOLE COMMON TO BULKHEAD AND MILLED COUPLING H6. CORRECTIVE ACTION: REPAIRED PER ER/A 595693-14AD REV ORIGINAL. (2074200)Jan 3, 2022 · N348NW · Airbus A320212 · Fuselage Main, BulkheadSDR DALA2022010400062None · noneSHIP 3248 CORROSION INTERNAL STRUCTURE STRAP LOCATED AT FR 67 BTW STR 27L TO STR 28L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ERA 596106-14AD REV ORIGINAL. (2074183)Jan 3, 2022 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2022010400061None · noneSHIP 3248 CORROSION FRAME 67 SUPPORT ANGLE LOCATED BTW STR42R TO STR42L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE PER A320 SRM 51-72-11. (2074120)Jan 3, 2022 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2022010400060None · noneSHIP 3248 CORROSION STRINGER 43L BTW FR32 AND FR 34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ERA 596001-14 REV ORIGINAL. (2073932)Jan 3, 2022 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2022010400059None · noneSHIP 3248 CORROSION STRINGER 43R LOC. BTW FR 31 AND FR 33 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ERA 596001-14 REV ORIGINAL. (2073931)Jan 3, 2022 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2022010300027None · noneSHIP 3248 WEAR ON UPPER SPAR WEB RH SIDE CANTILEVER ON RH PYLON. CORRECTIVE ACTION: REPAIRED PER ER/A 596055-14 REV ORIGINAL. (2073069)Jan 2, 2022 · N348NW · Airbus A320212 · Nacelle/Pylon, Frame/Spar/RibSDR DALA2022010300026None · noneSHIP 3248 CORROSION FLOOR STRUCTURE WEB BTW FR 56/57, STR 38R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: R/R PER ERA 596303-14 PRI REV.0 AND ER/A 596303-14 REV. ORIGINAL. (2073056)Jan 2, 2022 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2022010300025None · noneSHIP 3248 CORROSION INTERNAL STRUCTURE SUPPORT ANGLE LOCATED BTW FR 56 TO FR 57 AND STR 42L TO STR 43L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: R/R INTERNAL STRUCTURE SUPPORT ANGLE PER A320 SRM 51-72-11. (2072880)Jan 2, 2022 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2022010300017None · noneSHIP 3248 CRACK INDICATION ON FRAME 68 LH DOOR STOP FITTING HOLE 1. CORRECTIVE ACTION: REPAIRED PER ER/A 596000-14AD REV. ORIGINAL. (2072462)Jan 2, 2022 · N348NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2022010300016None · noneSHIP 3248 CORROSION STRINGER 41R LOC.BTW FR 32 AND FR 34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-72-11. (2072435)Jan 2, 2022 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2022010300029None · noneSHIP 3248 NEED TO PERFORM DTA MONITOR CRACK INSPECTION ER/A 596106-14. CORRECTIVE ACTION: COMPLIED WITH ERA. OK TO CONTINUE ON MON. (2072344)Jan 1, 2022 · N348NW · Airbus A320212 · Fuselage Main, BulkheadSDR DALA2022010300013None · noneSHIP 3248 DENT EXTERNAL SKIN ON DOUBLER REPAIR LOCATED AT FR74 AND BTW STR 30R TO STR 31R AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A #496943-14 REV.B. (2070969)Dec 31, 2021 · N348NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2022010300012None · noneSHIP 3248 CRACK INDICATION FOUND IN OPEN HOLE (H2) ON CROSSBEAM SPLICING AREA AT FRAME 16 LH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 595688-14AD REV ORIGINAL. (2070932)Dec 31, 2021 · N348NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2022010300011None · noneSHIP 3248 CRACK INDICATION FOUND ON HOLE #8 LOC. REAR EMERGENCY EXIT DOOR CUTOUT EXTERNAL FUSELAGE LH STR20 BTW FR40 AND FR41. CORRECTIVE ACTION: COMPLIED WITH PRI 595702-14AD. (2070925)Dec 31, 2021 · N348NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2022010308203None · noneSHIP 3248 CRACK EMERGENCY EXIT DOOR 833 ON LH LOAD TRANSMITTING PROFILE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED LH SEGMENT ANGLE AND FASTENERS PER A320 SRM 51-42-11, AND 51-72-11. (2070205)Dec 30, 2021 · N348NW · Airbus A320212 · Emergency ExitsSDR DALA2022010308202None · noneSHIP 3248 CRACK INDICATION ON FRAME 16 LH DOUBLE JOGGLE AREA HOLE C IN COCKPIT. CORRECTIVE ACTION: REPAIRED PER ER/A #595611-14AD REV.ORIGINAL. (2070176)Dec 30, 2021 · N348NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2022010308201None · noneSHIP 3248 CORROSION STRINGER 41L BTW FR 27 AND FR 31 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ERA 596001-14 REV ORIGINAL. (2069966)Dec 30, 2021 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2022010308200None · noneSHIP 3248 CRACK FOUND IN OPEN FASTENER HOLE #13 FRAME 20 RH SIDE DOOR STOP #1 LOWER CORNER. CORRECTIVE ACTION: REPAIRED PER ER/A #595607-14AD REV. ORIGINAL. (2069788)Dec 30, 2021 · N348NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2022010308199None · noneSHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT OPEN FASTENER HOLE ZONE 2. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD REV. ORIGINAL. (2069667)Dec 30, 2021 · N348NW · Airbus A320212 · Wing SparSDR DALA2022010308198None · noneSHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT OPEN FASTENER HOLE ZONE 1. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD, REV.ORIGINAL. (2069638)Dec 30, 2021 · N348NW · Airbus A320212 · Wing SparSDR DALA2022010300024None · noneSHIP 3248 WEAR ON LOWER SKIN SLAT 3 ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A #599222-14 REV.ORIGINAL. (2069578)Dec 30, 2021 · N348NW · Airbus A320212 · Wing SparSDR DALA2022010300023None · noneSHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT OPEN FASTENER HOLE ZONE 2. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD, REV. ORIGINAL. (2069702)Dec 30, 2021 · N348NW · Airbus A320212 · Wing SparSDR DALA2022010300022None · noneSHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT OPEN FASTENER HOLE ZONE 1. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD, REV. ORIGINAL. (2069674)Dec 30, 2021 · N348NW · Airbus A320212 · Wing SparSDR DALA2022010300021None · noneSHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 4 AT OPEN FASTENER HOLE ZONE 1. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD REV. ORIGINAL. (2069663)Dec 30, 2021 · N348NW · Airbus A320212 · Wing SparSDR DALA2022010300020None · noneSHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT OPEN FASTENER HOLE ZONE 1. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD REV. ORIGINAL. (2069651)Dec 30, 2021 · N348NW · Airbus A320212 · Wing SparSDR DALA2022010300031None · noneSHIP 3248 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT OPEN FASTENER HOLE ZONE 2. CORRECTIVE ACTION: REPAIRED PER ER/A #595656-14AD REV. ORIGINAL. (2069659)Dec 30, 2021 · N348NW · Airbus A320212 · Wing SparSDR DALA2022010300030None · noneSHIP 3248 NEED TO COMPLY WITH ERA INSPECTION ER/A 595693-14. CORRECTIVE ACTION: COMPLIED WITH ERA (CRACK INSPECTION) OK TO CONTINUE. (2072092)Dec 29, 2021 · N348NW · Airbus A320212 · Fuselage Main, BulkheadSDR DALA2021123008177None · noneDTA MONITOR INSPECTION LOG REFERENCE ER/A 596000-14 SECTION IV REQUIRES DTA APPROVAL WITHIN 60000 CYCLES AFTER SECTION I. CONTACT ENABLING TECHNOLOGIES DOUG JURY, 404-714-2928. DISCONTINUE REVENUE SERVICE WITHIN 60000 CYCLES AFTER SECT I PENDING A DAMAGE TOLERDec 29, 2021 · N348NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021123008176None · noneDTA MONITOR INSPECTION LOG REFERENCE ER/A 596000-14 SECTION III REQUIRES DTA APPROVAL WITHIN 37900 CYCLES AFTER SECTION I REPAIR CONTACT ENABLING TECHNOLOGIES DOUG JURY, 404-714-2928. DISCONTINUE REVENUE SERVICE WITHIN 37900 CYCLES AFTER SECT I PENDING A DAMAGDec 29, 2021 · N348NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021123008175None · noneREAR FUSELAGE / FRAME - FR 68LH - DOOR STOP FITTING #1 - HOLE 4 - CRACK. ACCOMPLISH ER/A 596000-14 SECTION II INSPECTION WITHIN EVERY 19700 CYCLES AFTER ACCOMPLISHMENT OF THE SECTION I REPAIR. ASSOCIATED ER/A 00-596000 ADDED FOR AC 3248. (LP# 2068997)Dec 29, 2021 · N348NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908144None · noneCORROSION STRINGER 40L BTW FR33 AND FR34 IN FWD CARGO COMPARTMENT (SSI 532180). PERFORMED REPAIR INSTRUCTION LOC. ON STRINGER 40L LOC AT FR33 AND FR34 IN FWD CARGO COMPARTMENT AS PER SRM A320 53-00-13- 300-001 PARAGRAGH 2, FIG 001. MEASUREMENT OF REWORK ARE P1Dec 28, 2021 · N348NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2021122908143None · noneCORROSION STRINGER 39R LOC AT FR33 IN FWD CARGO COMPARTMENT (SSI 532180). PERFORMED REPAIR INSTRUCTIONS LOC ON STRINGER 39R LOC AT FR32 PLUS 13.750 INCH TO FRAME 35 LESS 3 INCHES IN FWD CARGO COMP- ARTMENT AS PER SRM A320 53-00-13-300-001 PARAGRAPH 2, FIG 00. Dec 28, 2021 · N348NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2021122908142None · noneCORROSION STRINGER 42L BTW FR33 AND FR34 IN FWD CARGO COMPARTMENT (SSI 532180). PERFORMED REPAIR INSTRUCTIONS LOC ON STRINGER 42L LOC AT FR33 AND FR34 IN FWD CARGO COMPARTMENTS AS PER SRM A320 53-00-13- 300-001 PARAGRAPH 2, FIG 001. MEASUREMENT OF REWORK ARE PDec 28, 2021 · N348NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2021122908141None · noneCORROSION SEAT TRACK +Y765 FR20 AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK Y765 AND FASTENERS LOC BTW FR12 TO FR24 FWD PASSENGER CABIN AS PER A320 SRM 51-72-11 AND DWGS #D53112812, ISSUE E00, RELEASE DATE:22-MAR-06, DWG D53110900, ISSUE L00, RELEASE Dec 28, 2021 · N348NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2021122908140None · noneCORROSION SEAT TRACK -Y765 LOC FR46+8 INCHES IN PASSENGER CABIN (MEASUREMENT ARE L=4.364 INCHES, W=0.380 INCHES, D=0.040). REPLACED SEAT TRACK -Y765 LOC FR41 TO FR47 IN PASSENGER CABIN AS PER A320 SRM 51-42-11, 51-72-11 AND DWG D53370500, RELEASE DATE:11-JAN-0Dec 28, 2021 · N348NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2021122908136None · noneCORROSION FLOOR BEAM +Y765 LOC. FR64 TO FR66 AT AFT GALLEY AREA (1EA)(SSI 534147). REPLACED SEAT TRACK Y765 LOC BTW FR64 TO FR66 AFT GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG 10N01474. RII INSPECTION COM- PLETE 0113782 (AE262QC) JOB COMPLETE. (LP# 2067298)Dec 28, 2021 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2021122908135None · noneBENT FITTING DOOR LOWER CORNER AFT POSITION IN FWD CARGO COMPARTMENT. INSTALLED NEW CORNER AFT POSITION IN FWD CARGO COMPARTMENT AS PER A320 SRM 51-42-11, 51-71-11 AND DWG D532371810, ISSUE W, RELEASE DATE:16-JUN-20. RII INSPECTION COMPLETE 0294551 (AE166QC) JDec 28, 2021 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2021122908134None · noneCORROSION DOOR AFT CORNER LOCKING HOOK AREA IN AFT CARGO COMPARTMENT (SSI 523113). REPLACED CORNER LOCKING HOOK AREA LOC. AT AFT CARGO COMPARTMENT AS PER A320 SRM 51-42-11, 51-72-11 AND DWG 52371700 ISSUE G, RE- LEASE DATE:26-JUL-21. RII INSPECTION COMPLETE 16Dec 28, 2021 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2021122708044None · noneSHIP 3248 CORROSION INTERNAL STRUCTURE WEB AT STR 38R BTW FR33 AND FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER A320 SRM 51-42-11, AND 51-72-11. (2063728)Dec 24, 2021 · N348NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2021122207981None · noneSHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIP, BETWEEN FRAMES 73 AND 74, BETWEEN STRINGERS 34 AND 33L. CORRECTIVE ACTION: REPLACED CLIP PER A320 SRM 51-72-11. (2060599)Dec 21, 2021 · N348NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2021122207980None · noneSHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIP, BELOW FRAME 73, BETWEEN 73, BETWEEN STRINGERS 31L AND 30L. CORRECTIVE ACTION: REPLACED CLIP PER A320 SRM 51-72-11. (2060597)Dec 21, 2021 · N348NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2021122207979None · noneSHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIPS BELOW FRAME 74 BTW STR 30L 29L AND STR 30R AND 29R. CORRECTIVE ACTION: REPLACED CLIPS PER A320 SRM 51-72-11. (2060595)Dec 21, 2021 · N348NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2021122207978None · noneSHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIPS (5EA) BELOW FRAME 75 BTW STR 39L AND STR 39R. CORRECTIVE ACTION: REPLACED CLIPS PER A320 SRM 51-72-11. (2060588)Dec 21, 2021 · N348NW · Airbus A320212 · Fuselage Main, Plate/Skin
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