N353NW
Service difficulty reports · 183
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 = 'N353NW' 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 = 'N353NW' 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 DALA2026092705364Computer · malfunctionedDURING DECENT FOR APPROACH, WITH SPEED BRAKES DEPLOYED. AIRCRAFT MADE AN UNCOMMANDED RIGHT ROLL WITH NOTICEABLE BANK. T/S IAW TSM 27-10-00-810-842A, PERFORMED OPS TEST OF BOTH ELACS 1 & 2. TESTED OK. PERFORMED ELAC TEST IAW AMM 27-93-00-710-001-A. PERFORMEDSDR DALA2026092105249Door Sill · corrodedPAX CABIN, PASSENGER DOOR CUTOUT, LOWER SILL BEAM I/B FLANGE WITH CORROSION LOC. AT FR67+450MM. REPLACED LOWER SILL BEAM P/N: 5348004320601, LOCATED AT PAX CABIN, PASSENGER DOOR CUTOUT I/A/W A320 SRM 51-72-11-911-001 PARAG 2 REV: 158.00 DATED: 01-JUN-26 AND RSDR DALA2026092105246Door Sill · corrodedPAX CABIN, CREW DOOR CUTOUT, LOWER SILL BEAM I/B FLANGE WITH CORROSION LOC. AT FR67+450MM. C/A: PERFORMED REPAIR AT PASSENGER CABIN, CREW DOOR CUTOUT LOWER SILL BEAM I/B FLANGE FROM FR67+290MM TO FR68 I/A/W DELTA ER/A #636581-14 SECTION I REV ORIGINAL DATED 11SDR DALA2026092105245Beam · corrodedPAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR67+430MM Y1292. REPLACED LONGITUDINAL BEAM P/N: D5347218820400 AT Y1292 BTW FR68 TO FR69 I/A/W A 320 SRM TASK 51-72-11-911-001 PARAG 2 REV: 158.00 DATED 01-JUN-26. AND REF DWGS: 53474180, D534SDR DALA2026091705192Floor Support · corrodedLEVEL 2 CORROSION, PASSENGER CABIN LONGITUDINAL BEAM -Y1292, FR68 (COUPLING AREA), UPPER I/B AND AT FR66 UPPER AND LOWER I/B COUPLING ANGLES WITH ELONGATED HOLES AND CORROSION. NOTE: FOUND DURING PROCESS WITH ORNRC 200-378. C/A: REPLACED COUPLINGS AT LONGITUDISDR DALA2026091705191Floor Support · corrodedLEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC.BTW FR66+220MM TO FR68-Y1292. REPLACED LONGITUDINAL FLOOR SUPPORT D5347218920200 LOC.BTW FR66 TO FR69 AT -Y1292 I/A/W A320 SRM TASK 51-72-11-911-001 PARAG 2 REV 158.00 DATED 01-JUSDR DALA2026091705190Skin · dentedNOSE FWD EXTERNAL FUSELAGE, AT FR11 BETWEEN -Z 88 AND -Z 263, L/ H SIDE, SKIN WITH DENTS. C/A: PERFORMED REPAIR AT FWD EXTERNAL FUSELAGE SKIN SECTION AT FR11 BETWEEN -Z 88 AND -Z 263 L/H SIDE AS PER DELTA ER/A NO 636719-14 REV ORIGINAL SECTION I PART A, PART BSDR DALA2026091705189Skin · scratchedNOSE FWD EXTERNAL FUSELAGE, AT FR10 -Z361 L/H SIDE, SKIN WITH SCRATCH. PERFORMED REPAIR AT FWD EXTERNAL FUSELAGE SKIN SECTION AT FR 10 -Z361 LH SIDE AS PER DELTA ER/A NO. 636719-14 REV ORIGINAL SECTION I PART A, PART B STEP 15, 19 AND 20, DATED 11-SEP-26. NOTSDR DALA2026091705188Coupling · corrodedLEVEL 2 CORROSION, PAX CABIN LONGITUDINAL BEAM AT FR68 Y1292 COUPLING AREA, I/B UPPER COUPLING ANGLE WITH CORROSION. FOUND DURING PROCESS WITH ORNRC 200-337. REPLACED COUPLING AT FR68 Y1292 LOCATED I/B UPPER IAW SRM 51-72-11-911-001 PARAG 2. REV 158. AND DWGSDR DALA2026091505146Seat Track · corrodedPAX CABIN, LONGITUDINAL BEAM WITH CORROSION AT SEAT TRACK CROWN AREA LOC. BTW FR65 TO FR 66 -Y765. REPLACED SEAT TRACK BEAM P/N 14N00031-103 AT Y-765 BETWEEN FR64 AND FR66 I/A/W A320 SRM 51-72-911-001 PARAG 2 REV 158.00 DATED 01-JUN-26 AND REFERENCE NAT DRAWISDR DALA2026091505145Beam · corrodedLEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR66 Y765. C/A: REPLACED SEAT TRACK BEAM P/N 14N00031-103 AT Y 765 BETWEEN FR64 AND FR66 I/A/W A320 SRM 51-72-911-001 PARAG 2 REV 158.00 DATED 01-JUN-26 AND REFERENCE NAT DRAWISDR DALA2026091505144Beam · corrodedLEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR66+70MM Y1292. C/A: REPLACED SEAT TRACK BEAM P/N 14N00031-101 AT Y1292 BETWEEN FR64 AND FR66 I/A/W A320 SRM 51-72-911-001 PARAG 2 REV 158.00 DATED 01-JUN-26 AND REFERENCE NATSDR DALA2026091305112Skin · corrodedLEVEL 2 CORROSION, LOWER FUSELAGE AFT CARGO COMPARTMENT FROM FR56 TO FR 57 BETWEEN STRG-42L AND STRG-43L AFT ATG4 ANTENNA INTERNAL DOUBLER WITH CORROSION. PERFORMED REPAIR AT LOWER FUSELAGE AFT CARGO COMPARTMENT SKIN PANEL SECTION FROM FR 56 TO FR 57, BETWEENSDR DALA2026091305111Shear Plate · corrodedLEVEL 2 CORROSION, PAX CABIN, LATERAL SHEAR PLATE WITH CORROSION LOC.BTW FR 69 TO FR 70 STR 23L. REPLACED SHEAR PLATE AT PAX CABIN BETWEEN FR 69 TO FR 70 STG 23L AS PER A320 SRM 51-72-11-911-001 PARAG 2, REV 158.00 DATED 01-JUN-26 AND REFERENCE DRAWING D5347SDR DALA2026091705193Skin · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR FUSELAGE SKIN R EPAIR AT FR11LH, -Z88 & -Z263 PER ER/A 636719-14. C/A: SECTION I IS LIMITED TO SOONER OF 60000FC OR 120000FH. ER/A TO B E REVISED PRIOR TO THIS DATE ELSE REMOVE A/C FROM SERVICE. . (LP: 1807237,SDR DALA2026091305108Shear Plate · corrodedLEVEL 2 CORROSION, PAX CABIN, LATERAL SHEAR PLATE WITH CORROSION LOC. BTW FR69 TO FR70 STGR 23R. REPLACED SHEAR PLATE P/N: D5347112420300 LOCATED BTW FR69 TO FR70, STGR 23R IAW SRM 51-72-11-911-001 PARAG 2 REV 158.00 DATED 01-JUN-26 AND REF DWG A320 #D534741SDR DALA2026091305105Skin · damagedER/A 636728-14 IS ISSUED FOR FUSELAGE SKIN REPAIR INSTALLED AT F R56/57, S42/43LH WHICH WAS INSTALLED PER SRM 53-00-11-300-013. F OLLOW ON ACTION IS REQUIRED. SECTION II, AS REQUIRED IAW SRI 53-00-11-205-035, REQUIRED PRIOR TO SOONER OF 33600FC OR 67200FH & ESDR DALA2026091305107Anchor Fitting · corrodedLEVEL 2 CORROSION, LOWER FUSELAGE, RT MLG ANCHORAGE FITTING WITH CORROSION. REPAIRED RH MLG RETRACTION JACK ANCHORAGE FITTING LUG BARE, UPPER AND LOWER BEARING FACES AND EDGE CHAMFER I.A.W. A320 SRM TASK 57-26-13-300-008 REV. 158 DATED 01 JUN, 26. THIS IS REPSDR DALA2026091305106Anchor Fitting · corrodedLEVEL 2 CORROSION, LOWER FUSELAGE, LH MLG ANCHORAGE FITTING WITH CORROSION. C/A: REPAIRED LH MLG RETRACTIION JACK ANCHORAGE FITTING LUG BARE UPPER AND LOWER BEARING FACES AND EDGE CHAMFER I.A.W. A320 SRM TASK 57-26-13-300-008 REV. 158 DATED 01 JUN, 26. THIS ISSDR DALA2026091005067Skin · damagedUPPER FUSELAGE FROM FR 29 TO FR 30 BETWEEN STRG 1L TO STGR 1R PCS/TIMING ANTENNA AREA BELOW COVER PLATE WITH SCRATCHES. PERFORMED PERMANENT MAJOR REPAIR AT FWD UPPER FUSELAGE SKIN SECTION AROUND PCS/TIMING ANTENNA BETWEEN FR 29 AND FR 30 AT STGR 1L - 1R I.A.WSDR DALA2026091005066Beam · corrodedLEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR 68 Y765. REPLACED LONGITUDINAL P/N D5347219220000 AT Y 765 BTW FR66 TO FR70 I/A/W SRM TASK 51-72-11-911-001 PARAG 2 REV 158.00 DATED 01 -JUN-26. AND REFERENCE A 320 DWGS: DSDR DALA2026091005065Skin · damagedER/A 636530-14 ISSUED FOR SKIN REPAIR INSTALLED BETWEEN FR29 & F R30, S1 LH & RH. PERFORM SECTION II THE SOONER OF 30600FC/61200FH AFTER SECTION I AND EVERY SOONER OF 1200FC/2400FH THEREAFTER. ASSOCIATED ER/A 00-636530 ADDED FOR AC 3253. (LP: 1801765, AIRCRAFSDR DALA2026090705012Seat Track · corrodedLEVEL 2 CORROSION, PASSENGER CABIN BETWEEN FR 16 - 20, Y-1292 SEAT TRACK CORRODED. REPLACED THE SEAT TRACK BTWN FR 12 - 24 IAW SRM 53-11-15- 01A, FIG 001, ITEM 040-A, REV 158.00, & INSTALLED IAW DWG D53112812, ISSUE E, SHEET 01, DWG D53110900, ISSUE L, SHEESDR DALA2026090705011Light · corrodedLEVEL 2 CORROSION, UPPER FUSELAGE, PASSENGER CABIN ON FR16 AT Y254 SEAT TRACK CORRODED. REPLACED THE SEAT TRACK BTWN FR 12 TO FR 24, AT Y:254 IAW SRM 53-11-14-08B, FIG 008, ITEM 005B, REV 158.00, DRAWING D53112816, SHEET 01, ISSUE G. ITEM 000, & DWG D53110900SDR DALA2026090705009Seat Track · corrodedLEVEL 2 CORROSION, UPPER FUSELAGE, PASSENGER CABIN, FR 20 AT Y 765 SEAT TRACK CORRODED. REPLACED THE SEAT TRACK, FR 12 & FR 24 IAW SRM 53-11-15-01A, FIGURE 001, ITEM 015-A, REV 158.00 AND INSTALLED IAW DWG D53112812, ISSUE E, SHEET 01, DWG D53110900, ISSUE LSDR DALA2026090705008Seat Track · corrodedLEVEL 2 CORROSION, UPPER FUSELAGE, PASSENGER CABIN ON FR 20 AT Y-765 SEAT TRACK WITH CORROSION. REPLACED PASSENGER CABIN SEAT TRACK AT Y-765 BETWEEN FR12 AND FR24 IAW SRM 53-11-15-01A FIG 001 ITEM 040-A, SRM REV 158-00 AND INSTALLED IAW DWG D53112812, ISSUE SDR DALA2026072804386O-Ring · crackedON CLIMB OUT THROUGH HIGH 20'S GOT A HYD Y RSVR LO LVL ECAM. SYSTEM PAGE SHOWED Y HYD QUANTITY DECREASING. FOUND O-RING / PACKING ON SOLENOID / PRIORITY VALVE CRACKED. CAUSING THE LEAK. R/R PACKING PER A320 AMM 20-29. PERFORMED YELLOW HYD SYS LEAK CHECK PER WSDR DALA2026031701841Slat · damagedPILOTS REPORTED FOUND DAMAGE ON RT #1 SLAT & FUSELAGE FROM FUELER STAIRS CONTACT. REPAIR DAMAGE ON RT #1 SLAT PER A320 SRM 57-40-00-283-002 PARA. 2.A(2). NO FURTER DAMAGE NOTED. OK FOR SVC. (LP: 8275520)SDR DALA2026012800694Repair · noneEXISTING REPAIR DOUBLER ON AREA FR68 RT AT LEVEL DOOR STOP 1, S22R. REFERENCE WORK CARD 5311-01244-02B AND SB A320-53-1491. COMPLIED WITH ER/A 616797-14AD REV B, NOT MATCHES WITH ALL STEPS ON PRI 616797-14A, REV 0 DUE TO SECTION III REPETITIVE INSPECTION SUPSDR DALA2026012800693Frame · damagedINSPECTION ERA 616797-14 REV. B. REPAIR AT FR68 & STR22R, FRAME WEB HORIZONTAL FLANGE REQUIRES FOLLOW ON INSPECTIONS PRIOR TO 54,670 TFC AND EVERY 16,200 FC THEREAFTER. ACCOMPLISH FOLLOW ON INSPECTIONS PER ERA 616797-14AD SECTION III PRIOR TO 54,670 TFC AND ESDR DALA2025100807318Microphone · inoperativeFO'S O2 MASK MICROPHONE NOT WORKING. RESET MASK, OPS CKS NORMAL. (LP: 7376134)SDR DALA2025100707311Microphone · inoperativeF.O O2 MASK MICROPHONE NOT TESTING. C/A: REPACKED O2 MASK OPS CKD PER A320 AMM35-13 CKD NORMAL. (LP: 7276102)SDR DALA2025090106464Ecs · contaminatedAFTER START OF BOTH ENGINES FA NOTIFIED CREW OF BURNT RUBBER SMELL IN BACK OF CABIN THRU CENTER OF CABIN. SECURED BOTH PACKS AND COMPLIED WITH EQRH. SMELL DISCIPATED WITHIN 1 MIN OF PACKS OFF. PERFORMED T/S AND MTC PER AMDS W/C 0550-2002. PERFORMED LEVEL A DESDR DALA2025071805419Hydraulic Line · brokenSHIP 3253 - ATB - DUE TO LOSS OF THE GREEN HYDRAULIC SYSTEM SHORTLY AFTER TAKE-OFF. FOUND BROKEN HYDRAULIC LINE AT RH MLG LOCKSTAY ACTUATOR SWIVEL FITTING. MAINTENANCE IN PROGRESS. (LP: 7283138)SDR DALA2025011000206Cable · brokenSHIP 3253 DISC: DURING SERVICE, MANUAL RELEASE HANDLE CABLE BROKE ON RIGHT SIDE. C/A: FWD RT MLG DOOR GROUND OPEN CABLE TO MEL 32-12-01 CAT C PLACARDS INSTALLED M PROCEDURES C/W WILL REQ. STK# 32-3200-3-1509 IAW A320 IPC 32-12-16-01A ITEM 50 P/N TLH466L70 PARTSDR DALA2024101310017Flange · noneSHIP 3253 DISC: WEB HORIZONTAL FLANGE / CRACK. ER/A 616797-14AD REV A REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. C/A: ER/A 616797-14AD REV A SECTION II FOLLOW-ON INSPECTIONS ARE REQUIRED ON OR BEFORE 55,400 TOTAL AIRFRAME FSDR DALA2024101310016Frame · crackedSHIP 3253 DISC: DTE, ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL. A320 / 3253 / FUSELAGE / FRAMES/FORMERS / FR68 & STR22R / FRAME WEB HORIZONTAL FLANGE / CRACK. C/A: ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL ON OR BEFOR E 72,600 TOTAL AIRFRSDR DALA2024101310015Frame · crackedSHIP 3253 DISC: DTE, ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL. A320 / 3253 / FUSELAGE / FRAMES/FORMERS / FR68 & STR22R / FRAME WEB HORIZONTAL FLANGE / CRACK. C/A: ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL ON OR BEFOR E 97,200 TOTAL AIRFRSDR DALA2024101310014Frame · crackedSHIP 3253 DISC: DTE, ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL. A320 / 3253 / FUSELAGE / FRAMES/FORMERS / FR68 & STR22R / FRAME WEB HORIZONTAL FLANGE / CRACK. C/A: ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL ON OR BEFOR E 73,600 TOTAL AIRFRSDR DALA2024091508991Life Raft · out of positionSHIP 3253 DISC: DURING 1A AIRFRAME CHECK FOUND LIFE RAFT AT OVERHEAD BIN 32ABC UNABLE TO SEE PRESSURE GAUGE. C/A: REMOVED AND REPLACED LIFE RAFT ASSEMBLY REF A320 AMM 25-66.SDR DALA2024071307097Lens · damagedSHIP 3253 DISC: PATH WAY LIGHT LENS DAMAGED AT 1C AND 4C. C/A: REPLACED LIGHT LENS PER CMM 25-20-148. (LP: 0430284)SDR DALA2024071207054Lamp · inoperativeSHIP 3253 DISC: 16F EMERGENCY EXIT HANDLE LIGHT INOP. C/A: RELAMPED EMERGENCY EXIT HANDLE LIGHT REF A320 AMM 33-51-11-000- 001-A. OPS CK GOOD. (LP: 6204543)SDR DALA2024071207055Light · inoperativeSHIP 3253 DISC: 13D EMERGENCY LIGHT INOP. C/A: REPLACED LIGHT ASSEMBLY OPS CK GOOD REMOVED PLACARDS, CLEARED MEL. OK FOR SVC. (LP: 6204542)SDR DALA2024061406074Line · chafedSHIP 3253 - MISC/DE - DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM (HYD Y RSVR LO LVL ECAM). CORRECTIVE ACTION: FOUND #2 ENGINE T/R LOCK ACTUATOR LINE DAMAGED (CHAFFED) AT THE CLAMP, R/R BOTH LINES UNDER SAME CLAMP. ALSO, R/R EDP DUE TO POSSIBLE CAVITATION. OPS CHECSDR DALA2024041904582Frame · crackedSHIP 3253 DISC: CRACK INDICATION FOUND ON FRAME WEB HORIZONTAL FLANGE LOCATED ON FR68 AT LEVEL OF STRINGER 22R, CRACK LENGHT= 1.0 INCH APPROX. C/A: ACCOMPLISHED ER/A 616797-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI 616797-14AD REV 0 THRU REV. 5. IT HAS SDR DALA2024041904577Frame · crackedSHIP 3253 DISC: CRACK INDICATION FOUND ON FRAME WEB HORIZONTAL FLANGE LOCATED ON FR68 AT LEVEL OF STRINGER 22R, CRACK LENGHT= 1.0 INCH APPROX. C/A: ACCOMPLISHED ER/A 616797-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI 616797-14AD REV 0 THRU REV. 5. IT HAS SDR DALA2024041904579Frame · crackedDURING C-CK AND WHILE ACCOMPLISHING 5311-01244-01B, CRACK FOUND IN FR68 RT, WEB AT STR 22R. PER ER/A 616797-14AD REV A, DTE STAGE 2 ACCOMPLISHED. DTE STAGE 3 IS TRACKED ON NEW LOG PAGES 0598549, 0598554, AND 0598560. PLEASE CLOSE THIS LOG PAGE, 0297395. DTE* SDR DALA2024041504404Pin · brokenBROKEN PIN INTERNAL MECHANISM EVACUATION SLIDE AT PASSENGER DOOR 831. REMOVED SLIDE RAFT IN UNSERVICEABLE CONDITION PN D30664-705 SN A6282RP. AS PER AMDS CARD 2561-4003-LF. JOB IN PROGRESS.SDR DALA2024022602585Oxygen Mask · no testSHIP 3253 DISC: F/O MASK IS NOT TESTING. C/A: SWAPPED F/O'S AND PRIMARY OBSERVERS O2 MASK STORAGE BOX R/R PRIMARY OBERSERVERS O2 MASK STOWAGE BOX PER A320 AMM 35-12. (LP: 5576994)SDR DALA2023032302195Unknown · unknownSHIP 3253 - ATO - DUE TO BRAKE SYS 2 FAULT. CORRECTIVE ACTION: PLACED ON MEL DEFERRAL. LATER, WIRING CHECK C/W AND R/R BSCU PER A320 AMM 32-42-34. OPS CHECK GOOD. OK FOR SERVICE. (4818436)
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