N376NW

Service difficulty reports · 160

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 = 'N376NW' 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 DALA2026081204630Display · shortedSMOKE IN THE COCKPIT DUE TO UPPER ECAM DISPLAY SHORTED, CREW TURNED OFF DISPLAY AND SMOKE DISSIPATED. REPLACED UPPER ECAM DU (4WT1). (LP: 9588150, AIRCRAFT WAS GROUNDED)Aug 12, 2026 · N376NW · Airbus A320212 · Central DisplaySDR DALA2026070503913Brake Assy · overtempRTO AT 15 KTS, BRAKE TEMPERATURE MONITORING UNIT. WARN MSG- BRAKES HOT. FLIGHT CREW PLACARD VALIDATION IS ACCOMPLISHED. AS PER MCC REQUEST RESET SYS BRAKE TEMP NRML AT THIS TIME M PROC REVERSED MCC CONTACTED PLAC REMOVED OK FOR SVC. (LP: 1681021, AIRCRAFT WASJul 4, 2026 · N376NW · Airbus A320212 · Landing Gear Brake SystemSDR DALA2025111908442Outflow Valve · faultedATO - BELOW 80KTS DUE TO A VENT SKIN VALVE FAULT. DEFERRED THE AVIONICS COOLING SKIN AIR OUTLET VALVE PER MEL AND CONTINUED. LATER REPLACED THE SKIN AIR OUTLET VALVE. (LP: 8022576)Nov 16, 2025 · N376NW · Airbus A320212 · Pressure Regulator/Outflow ValveSDR DALA2025091706826None · noneINSPECTION ER/A 624251-14AD REVISION ORIGINAL. REPAIR AT TOP SKIN PANEL 2, UPPER SURFACE, BETWEEN RIBS 14-16 REQUIRES FOLLOW ON INSPECTIONS PER ER/A 624251-14AD SECTION II PRIOR TO 46,131 TOTAL FLIGHT CYCLES OR 94,851 TOTAL FLIGHT HOURS, WHICHEVER COMES FIRST,Sep 14, 2025 · N376NW · Airbus A320212 · Standard Practices/StructuresSDR DALA2025081606132Wire Harness · unsecureFLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHT INOPERATIVE AT ROW 18 D/E/F. 18 D/E/F ESCAPE PATH MARKING LIGHT INOPERATIVE. DEFERRED PER MEL 33-50- 03A. INSPECTED AND FOUND LIGHT HARNESS UNSECURE. SECURED. HARNESS IAW AMM 33-51. OPS CHECKED GOOD.Aug 10, 2025 · N376NW · Airbus A320212 · Light System WiringSDR DALA2025072305525Oxygen Mask · unwanted deploySHIP 3276, OXY MASKS DEPLOYED ON T.O. AT SEATS 1C/D. RESTOWED O2 MASKS + SECURED COVER. O2 GEN NOT ACTIVATED. IAW A320 AMM 35-21. (LP: 7324770)Jul 20, 2025 · N376NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2025042403197Fitting · not reportedSHIP 3276 DISC: PERFORM ER/A 624308-14 FOR GAIN ACCESS TO REPLACE CONTINUITY FITTINGS ON WINDSHIELD AREA. C/A: COMPLIED WITH ER/A 624308-14 REV ORIGINAL MATCHES WITH ALL STEPS OF ER/A 624308-14 PRI REV 0 IT IS BEEN VALIDATED. PERFORMEDREPAIR INSTRUCTIONS ON COApr 20, 2025 · N376NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2025042103038Fitting · crackedCRACK FIN 80VU IS IN CONTACT WITH STRUCTURE LOWER LATERAL FITTING RH SI DE. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. (REFER TO AMDS 2515-01014-02B AD RELATED). C/A: ER/A 623985-14AD REV A APPROVED DATE: 04/APR/25 WAS VERIFIED AApr 19, 2025 · N376NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2025042103042Fitting · damagedPERFORM ER/A 624309-14 FOR REPLACE CONTINUITY FITTINGS ON WINDSHIELD A REA. COMPLIED WITH ER/A 624309-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF ER/A 624309-14AD PRI REV 0 IT IS BEEN VALIDATED. PERFORMEDREPAIR INSTRUCTIONS ON CONTINUITY FITTINGS RH AND LH ONApr 18, 2025 · N376NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2025042103041Window Frame · crackedCRACK INDICATION ON WINDSHIELD CENTER POST UPPERT TENSION BOLT L /H SI DE CRACK LOCATION 12 OCLOCK , LARGE APPROX 0.141 INCH AD 2020-17-03/ WO RKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE AC COMPLISHED PRIOR TO FURTHER FLIGHT.Apr 18, 2025 · N376NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2025041702978Skin · corrodedSHIP 3276 DISC: SECUNDARY FINDING CORROSION UPPER SKIN LOWER SURFACE AT LEVEL RIB15 T RAILING EDGE ON RH WING. C/A: COMPLIED WITH ER/A 624251-14 REV ORIGINAL MATCHES WITH ALL STEPS OF PRI 624251-14 REV 0,1 AND REV 2 IT IS BEEN VALIDATED.PERFORMED REPAIR INSTRUApr 15, 2025 · N376NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2025041702985Not Reported · not reportedSHIP 3276 DISC: DTE ERA 624310-14AD REV ORIGINAL. REPAIR AT AREA 3 PER ERA 624310-14AD REQUIRES DTE FOLLOW UP PRIOR TO 91,131 TOTAL FLIGHT CYCLES. C/A: REVISE / UPDATE ERA 624310-14AD WITH DTE RESULTS PRIOR TO 91,131 TOTAL FLIGHT CYCLES. ASSOCIATED AA 5311-012Apr 14, 2025 · N376NW · Airbus A320212 · Standard Practices/StructuresSDR DALA2025041702984Window Frame · damagedSHIP 3276 DISC: INSPECTION ERA 624310-14AD REV ORIGINAL. REPAIR AT WINDSHIELD FRAMING (MIRROR FITTINGS) REQUIRES FOLLOW ON INSPECTIONS PRIOR TO 58,131 TOTAL FLIGHT CYCLES AND EVERY 4,700 FLIGHT CYCLES THEREAFTER. C/A: ACCOMPLISH INSPECTION AT MIRROR FITTINGS AApr 14, 2025 · N376NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2025041702983Window Frame · damagedSHIP 3276 DISC: DTE ERA 624309-14AD REV ORIGINAL. REPAIR AT THE AREA OF WINDSHIELD FRAMING REQUIRES DTE FOLLOW UP PRIOR TO 60,631 TOTAL FLIGHT CYCLES. C/A: REVISE / UPDATE ERA 624309-14AD WITH DTE RESULTS PRIOR TO 60,631 TOTAL FLIGHT CYCLES. REFERENCE AIRBUS DApr 14, 2025 · N376NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2025041702980Skin · damagedSHIP 3276 DISC: DTE ER/A 624251-14AD. REPAIR AT RH WING TOP SKIN, TE OVERHANG REQUIRES DTE FOLLOW UP PRIOR TO 21SEP2025. C/A: REVISE / UPDATE ER/A 624251-14AD WITH DTE RESULTS PRIOR TO 21SEP2025. AIRBUS DOSSIER 81551722. ASSOCIATED ER/A 14-624251 ADDED FOR AC Apr 4, 2025 · N376NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2025040602610Seat Track · corrodedSHIP 3276 DISC: CORROSION SEAT TRACK +Y765 BTW FR64 TO FR65 AFT GALLEY AREA (SSI 534147). C/A: REPLACED SEAT TRACK Y765 LOCATED BTW FR64 TO FR66 AFT GALLEY AREA AS PER A320 SRM 53-41-15-283-002, A320 SRM 51-42-11, A320 SRM51-44-11, A320 SRM 51-46-11, A320 SRM Apr 3, 2025 · N376NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025040602609Floorbeam · corrodedSHIP 3276 DISC: CORROSION FLOOR BEAM -Y1162.5 AT LEVEL FR68 AFT GALLEY AREA (SSI 534147). C/A: REPLACED FLOOR BEAM -Y1162.5 AT LEVEL FR68 AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11, DWG D53472780, DWG D53474250, AND DWG D53474180. (LP: 0893568Apr 3, 2025 · N376NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2025040402552Seat Track · corrodedSHIP 3276 DISC: CORROSION SEAT TRACK +Y1292 BTW FR64 TO FR65 AFT GALLEY AREA ( SSI 534147). C/A: REPLACED SEAT TRACK Y1292 BTW FR64 TO FR65 AFT GALLEY AREA AS PER A320 SRM 53-41-15-283-002, A320 SRM 51-42-11, A320 SRM 51-44-11, A320 SRM 51-21-11, DWG 14N00031,Apr 1, 2025 · N376NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025040102466Crossbeam · bentSHIP 3276 DISC: BENT FRAME 26 CROSSBEAM STR38L TO STR38R IN FWD CARGO COMPARTMENT. C/A: REPLACED CROSSBEAM FRAME 26 STR38L TO STR38R IN FWD CARGO COMPARTMENT AS PER A320 SRM 51-42-11 AND A320 SRM 51-72-11 AND DWGD53230829. (LP: 0888319)Mar 31, 2025 · N376NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2025033002336Door Frame · crackedAIRCRAFT 3276, CRACK INDICATION ON FR 66 AT AFT GALLEY AREA, DOOR STOOP FITTING 1, LOWER INBOARD HOLE, LH SIDE, CRACK POSITION AT 7 OCLOCK, CRACK DEPTH 0.115 INCHES, HOLE DIAMETER 0.250 INCHES, AA 5311-01216, AD RELATED. CORRECTIVE ACTION: FINAL REPAIR RESOLUTMar 29, 2025 · N376NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2025033002335Door Frame · crackedAIRCRAFT 3276, CRACK INDICATION ON FR 66 AT AFT GALLEY AREA, DOOR STOOP FITTING 1, LOWER INBOARD HOLE, LH SIDE, CRACK POSITION AT 7 OCLOCK, CRACK DEPTH 0.115 INCHES, HOLE DIAMETER 0.250 INCHES, AA 5311-01216, AD RELATED. CORRECTIVE ACTION: FINAL REPAIR RESOLUTMar 29, 2025 · N376NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2025032702245Seat Track · corrodedAIRCRAFT 3276, CORROSION SEAT TRACK -Y765 BTW FR64 TO FR66 AFT GALLEY AREA (SSI 534147). CORRECTIVE ACTION: REPLACED SEAT TRACK -Y765 AT LEVEL FR66 AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG: 10N01048, ISSUE: E, RELEASE DATE: 18/MAY/15. (LP 0878815)Mar 26, 2025 · N376NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025032702244Fitting · corrodedAIRCRAFT 3276, CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A320 SRM 54-51-12-300-001 AND AS PER A320 FAM AMM 54-51-41-400-001-A. (LP 0877370)Mar 25, 2025 · N376NW · Airbus A320212 · Nacelle/Pylon, Main FrameSDR DALA2025032702243Floor Support · corrodedAIRCRAFT 3276, CORROSION FLOOR STRUCTURE WEB FRAME LOCATED FROM FR69 TO FR70 AND STR 23LH AT AFT GALLEY AREA (SSI:534147). CORRECTIVE ACTION: REPLACED WEB AND FASTENERS LOC ON FR69 TO FR70 AT LEVEL STR23LH AFT GALLEY AREA AS PER A320 SRM 51-42-11 A320 SRM 51-7Mar 25, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2025032702242Floor Support · corrodedAIRCRAFT 3276, CORROSION FLOOR STRUCTURE WEB FRAME LOCATED FROM FR69 TO FR70 AND STR23RH AT AFT GALLEY AREA (SSI: 534147). CORRECTIVE ACTION: REPLACED WEB AND FASTENERS LOC ON FR69 TO FR70 AT LEVEL STR23RH AFT GALLEY AREA AS PER A320 SRM 51-42-11 A320 SRM 51-7Mar 25, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2025032502204Floor Support · corrodedSHIP 3276 DISC: CORROSION FLOOR BEAM +Y1162.5 AT LEVEL FR68 AFT GALLEY AREA (SSI 534147). C/A: REPLACED FLOOR BEAM Y1162.5 AT LEVEL FR68 TO FR69 AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11, DWG D53472788, DWG D53474250 AND DWG D53474180. (LP: 0Mar 24, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2025032502203Floor Support · corrodedSHIP 3276 DISC: CORROSION LOWER SILL LOCATED AT LEVEL FR68 RH SIDE AFT GALLEY AREA (SSI 534147). C/A: PERFORMED PERMANENT REPAIR ON LOWER SILL LOCATED AT LEVEL FR68 RH SIDE AFT GALLEY AREA AS PER A320 SRM 53-41-14-300-001. (LP: 0875044)Mar 24, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2025032302155Floor Support · corrodedCORROSION FLOOR BEAM -Y765 LOCATED FROM FR66 TO FR70 AT AFT GALLEY AREA (SSI: 534147). REPLACED FLOOR BEAM -Y765 AND FASTENERS LOCATED FROM FR66 TO FR70 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11 51-44-11,SRM 51-21-11,SRM 53-11-15-283-010 DWG D53472093, DWG Mar 22, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2025032302154Floor Support · corrodedCORROSION FLOOR BEAM -Y464.8 LOCATED FROM 67 PLUS 10 INCH TO FR70 AT AFT GALLEY AREA (SSI: 534147). REPLACED FLOOR BEAM -Y464.8 LOCATED FROM FR.67 TO FR.70 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11. DWG D53472816 RELEASE DATE 18-DEC-06 ISSUE F AND DWG D5347Mar 22, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2025032002102Floor Support · corrodedCORROSION FLOOR BEAM +Y254 BTW FR16 TO FR20 FWD GALLEY AREA (SSI 531189). C/A: REPLACED FLOOR BEAM LOCATED Y254 BTW FR16 TO FR24 FWD GALLEY AREA AS PER A320 SRM 51-44-11, A320 SRM 51-21-11, SRM 53-11- 15-283-010 DWG D53110920, DWG D53112816, AND ESPM 20-33-Mar 20, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2025032002099Seat Track · corrodedSHIP 3276 DISC: CORROSION SEAT TRACK -Y765 LOCATED FROM FR12 TO FR24 AT FWD GALLEY AREA (SSI: 531189). C/A: REPLACED SEAT TRACK -Y765 LOC. FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-44-11, A320 SRM 51-21-11,A320 SRM 53- 11-15-283-010Mar 19, 2025 · N376NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025032002097Seat Track · corrodedSHIP 3276 DISC: CORROSION SEAT TRACK -Y1292 FROM FR12 TO FR24 AT FWD GALLEY AREA (SSI: 531189). C/A: REPLACED SEAT TRACK -Y1292 LOC. FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-44-11, A320 SRM 51-21-11,A320 SRM 53- 11-15-283-010, DWG Mar 15, 2025 · N376NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025031501994Fitting · corrodedSHIP 3276 DISC: CORROSION SPIGOT FITTING RECEPTACLE BORE ON LH PYLON. C/A: REPLACED LOWER FITTING SPIGOT ON LH PYLON AS PER A320 SRM 54-51- 12-300-001 AND PERFORMED DETAIL VISUAL INSPECTION ON AREA AND NOTFOUND ADDITIONAL DAMAGE AS PER AIRBUS NTM 51-90-00, ANDMar 14, 2025 · N376NW · Airbus A320212 · Nacelle/Pylon Miscellaneous StructureSDR DALA2025020200769Support Fitting · noneSHIP 3276 DISC: ERA 623985-14AD REV ORIG FOR 80VU AVIONICS RACK SUPPORT FITTINGS REQUIRES FOLLOW ON ACTIONS. C/A: ACCOMPLISH SECTION II REPEAT INSPECTIONS EVERY 500 FC UNTIL SECT ION III PERMANENT REPAIR. PERMANENT REPAIR SECTION III REQUIRED WITHIN 4500 FC. AJan 30, 2025 · N376NW · Airbus A320212 · Standard Practices/StructuresSDR DALA2025020200768Fitting · damagedSHIP 3276 DISC: PER AMDS 2515-01014-07, FOUND R/H LOWER FITTING P/N D53910657201000 (FORK) OUTBD HOLE IS ELONGATED. C/A: REMOVED BOLT AND COMPLETED STEPS 2 THRU 4 ON ER/A 623985-14AD PRI REV. O (WIP 874493). RE-INSTALLED LOWER RH BOLT. RA 623985-14AD REV 0 TJan 30, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2025012100510Switch · failedSHIP 3276 - MISC/DE - DUE TO F/CTL SEC 3 FAULT. CORRECTIVE ACTION: SEC 3 PLACED ON MEL. R/R P/B SWITCH FOR SEC#3. OK FOR SERVICE. (LP: 6555042)Jan 18, 2025 · N376NW · Airbus A320212 · Flight Control SystemSDR DALA2025011900437Warning Message · illuminatedSHIP 3276 DISC: DECLARED EMERGENCY INTO LAX DUE TO SEC 3 FAULT. C/A: FWD TO MEL 27-94-01. MEL & PLACS INSTALLED. MCC NOTIFIED. OK FOR SVC. (LP: 6555044)Jan 18, 2025 · N376NW · Airbus A320212 · Central WarningSDR DALA2024091508992Unknown · odorSHIP 3276 DISC: AFTER LEVEL OFF AT 370 F/A CALLED TO REPORT A RUBBER SMELL AROUND ROW 15. ALL INDICATIONS IN FLIGHT DECK WERE NORMAL AFTER 10 MIN. CAPT PROCEEDS TO GO BACK TO CHECK SMELL. SAW NO EVIDENCE OF SMOKE OR MIST IN THE CABIN. THERE WAS A SMELL PRESENTSep 12, 2024 · N376NW · Airbus A320212 · Air Distribution SystemSDR DALA2024053005674Controller · faultedSHIP 3276 DISC: AIRBLEED CLASS 2 ECAM MSG. C/A: REMOVED AND REPLACED BMC 2 IAW A320 AMM 36-11. OPS CHECK GOOD. THIS CLEARED MEL 36-00-00C. PLACARDS REMOVED. (LP: 5983666)May 29, 2024 · N376NW · Airbus A320212 · Engine Bleed Air SystemSDR DALA2024040804148Oxygen Mask · unsecureSHIP 3276 DISC: O2 MASK INOP AT SEAT 1CD. C/A: RESECURED O2 MASK DOOR @1CD PER A320 AMM 35-21. DOOR SECURE. MEL & PLACARDS REMOVED 'M' PROC. REVERSED. (LP: 5276123)Apr 4, 2024 · N376NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2024031403324Fcu · faultedUNSATISFACTORY ACFT PERFORMANCE AT ALTITUDE. WITH MORE THAN 2000 FT BUFFER ACFT UNABLE TO CLIMB, UNABLE AT CRUISE OR TO MAINTAIN AIRSPEED 15 TO 20 KYS SLOW. ENG PARAMETERS SHOW NORMAL, PERFORMANCE REQTS UNSAT. ENG SLOW TO RESPOND TO REQUEST FOR PERFORMANCE. Mar 11, 2024 · N376NW · Airbus A320212 · Engine Fuel and ControlSDR DALA2024030803147Brake · faultedSHIP 3276 DISC: AFTER TAKE-OFF RECEIVED ECAM "BRAKES HOT" COMPLIED W/ ECAM AND QRH. BRAKES COOLED AND WITH CONCURRENCE OF MX + DISPACH PROCEEDED TO DESTINATION. C/A: AFTER TAKE OFF PILOT REPORTS ECAM BRAKES HOT AND AFTER LANDING PILOT REPORTS LEFT SIDE BRAKES Mar 7, 2024 · N376NW · Airbus A320212 · Landing Gear Brake SystemSDR DALA2024030503022Oxygen Mask · unwanted deploySHIP 3276 DISC: O2 MASKS DROPPED FROM PSEU AT SEATS 11A,B,C. TUBE WASN"T PULLED, NO O2 FLOW. C/A: REPACKED 02 MASK AT SEAT 11A,B,C PER A320 AMM 35-21, A/C OK FOR SVC. (LP: 5451796)Mar 3, 2024 · N376NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2024030402926Container · openSHIP 3276 DISC: OXYGEN MASK COMPARTMENT OPENED SEAT ROW 22ABC. C/A: R/R 02 CONTAINER ASSY IN REF WITH A320 CMM 25-28-02. OPS NORMAL. MEL & PLACARD REMOVED. M PROCEDURES REVERSED. OK FOR SVC. (LP: 5451786)Mar 2, 2024 · N376NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2024072907533Strake · missingSHIP 3276 DISC: NBR 1 ENGINE INB STRAKE MISSING. C/A: DEFER TO CDL 54-00-01C, PLACARD INSTALLED. (LP: 5451710)Feb 11, 2024 · N376NW · Airbus A320212 · Nacelle/Pylon, Main FrameSDR DALA2024021301993Oxygen Mask · unwanted deploySHIP 3276 DISC: OXY MASKS ROW 32ABC FELL OUT. C/A: C/W MEL 35-21-01A. PROCEDURES. SEATS 32A,32B,32C WERE NOT TAKEN OUT OF SERVICE. SEATS HAVE NOW BEEN BLOCKED OFF. RESECURED PANEL ON 02 BOX, COULD NOT DUPLICATE FAULT. MEL AND PLACARD REMOVED. "M" PROC REVERSEDFeb 10, 2024 · N376NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2024020801682Fitting · gougedSHIP 3276 DISC: ERA 615578-14AD ISSUED FOR ACCIDENTAL GOUGE DAMAGE TO LH MLG DOO KEEL FITTING. FOLLOW ON ACTION REQUIRED. AD RELATED NO DEVIATION OR SUBSTITUTE. C/A: UPDATING THE MASK TO REMOVE THE TERMINATING ACTION. THERE IS NO TERMINATING ACTION ASSOCIATED Feb 5, 2024 · N376NW · Airbus A320212 · Fuselage, Door HingeSDR DALA2023120810069Unknown · unknownSHIP 3276 - (SUPPLEMENTAL INFORMATION 12/07 DCA) ATO - AT THROTTLE UP DUE TO AN ENG 2 FIRE DETECION LOOP A FAULT. C/A: DEFERRED FIRE DETECTION SYSTEM PER MEL AND CONTINUED. FOUND ENG 2 FAN FIRE DETECTOR LOOP A (4000WD1) DAMAGED. R/R #2ENGINE FAN LOOP RAIL ASSEDec 7, 2023 · N376NW · Airbus A320212 · Fire DetectionSDR DALA2023051904002Unknown · unknownSHIP 3276 ROW 12 DEF EMERGENCY FLOOR ILLUMINATION LT AND ASSY MISSING. CORRECTIVE ACTION: REPLACED LIGHT ASSY. OK FOR SERVICE. (9734714)May 18, 2023 · N376NW · Airbus A320212 · Emergency LightingSDR DALA2023020300845Not Entered · not enteredSHIP 3276 FOUND RH FWD OVERWING EMERGENCY EXIT HANDLE LIGHTS INOP. CORRECTIVE ACTION: R/R LIGHT ASSY PER A320 AMM 33-51. (9889557)Jan 31, 2023 · N376NW · Airbus A320212 · Emergency Lighting
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