# Service difficulty reports: N376NW

A list on [N376NW](https://openairdocs.org/aircraft/N376NW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 160 reports

- [SDR DALA2026081204630](https://openairdocs.org/sdr/DALA2026081204630.md): Display · shorted · Aug 12, 2026 · N376NW · Airbus A320212 · Central Display
  > SMOKE 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)
- [SDR DALA2026070503913](https://openairdocs.org/sdr/DALA2026070503913.md): Brake Assy · overtemp · Jul 4, 2026 · N376NW · Airbus A320212 · Landing Gear Brake System
  > RTO 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 WAS
- [SDR DALA2025111908442](https://openairdocs.org/sdr/DALA2025111908442.md): Outflow Valve · faulted · Nov 16, 2025 · N376NW · Airbus A320212 · Pressure Regulator/Outflow Valve
  > ATO - 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)
- [SDR DALA2025091706826](https://openairdocs.org/sdr/DALA2025091706826.md): None · none · Sep 14, 2025 · N376NW · Airbus A320212 · Standard Practices/Structures
  > INSPECTION 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,
- [SDR DALA2025081606132](https://openairdocs.org/sdr/DALA2025081606132.md): Wire Harness · unsecure · Aug 10, 2025 · N376NW · Airbus A320212 · Light System Wiring
  > FLOOR 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.
- [SDR DALA2025072305525](https://openairdocs.org/sdr/DALA2025072305525.md): Oxygen Mask · unwanted deploy · Jul 20, 2025 · N376NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 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)
- [SDR DALA2025042403197](https://openairdocs.org/sdr/DALA2025042403197.md): Fitting · not reported · Apr 20, 2025 · N376NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 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 CO
- [SDR DALA2025042103038](https://openairdocs.org/sdr/DALA2025042103038.md): Fitting · cracked · Apr 19, 2025 · N376NW · Airbus A320212 · Fuselage Main, Structure
  > CRACK 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 A
- [SDR DALA2025042103042](https://openairdocs.org/sdr/DALA2025042103042.md): Fitting · damaged · Apr 18, 2025 · N376NW · Airbus A320212 · Fuselage Main, Structure
  > PERFORM 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 ON
- [SDR DALA2025042103041](https://openairdocs.org/sdr/DALA2025042103041.md): Window Frame · cracked · Apr 18, 2025 · N376NW · Airbus A320212 · Fuselage Main, Structure
  > CRACK 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.
- [SDR DALA2025041702978](https://openairdocs.org/sdr/DALA2025041702978.md): Skin · corroded · Apr 15, 2025 · N376NW · Airbus A320212 · Wing, Plate/Skin
  > SHIP 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 INSTRU
- [SDR DALA2025041702985](https://openairdocs.org/sdr/DALA2025041702985.md): Not Reported · not reported · Apr 14, 2025 · N376NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 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 5311-012
- [SDR DALA2025041702984](https://openairdocs.org/sdr/DALA2025041702984.md): Window Frame · damaged · Apr 14, 2025 · N376NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 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 A
- [SDR DALA2025041702983](https://openairdocs.org/sdr/DALA2025041702983.md): Window Frame · damaged · Apr 14, 2025 · N376NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 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 D
- [SDR DALA2025041702980](https://openairdocs.org/sdr/DALA2025041702980.md): Skin · damaged · Apr 4, 2025 · N376NW · Airbus A320212 · Wing, Plate/Skin
  > SHIP 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
- [SDR DALA2025040602610](https://openairdocs.org/sdr/DALA2025040602610.md): Seat Track · corroded · Apr 3, 2025 · N376NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 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
- [SDR DALA2025040602609](https://openairdocs.org/sdr/DALA2025040602609.md): Floorbeam · corroded · Apr 3, 2025 · N376NW · Airbus A320212 · Fuselage Main, Floor Beam
  > SHIP 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: 0893568
- [SDR DALA2025040402552](https://openairdocs.org/sdr/DALA2025040402552.md): Seat Track · corroded · Apr 1, 2025 · N376NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 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,
- [SDR DALA2025040102466](https://openairdocs.org/sdr/DALA2025040102466.md): Crossbeam · bent · Mar 31, 2025 · N376NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 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)
- [SDR DALA2025033002336](https://openairdocs.org/sdr/DALA2025033002336.md): Door Frame · cracked · Mar 29, 2025 · N376NW · Airbus A320212 · Fuselage Main, Structure
  > AIRCRAFT 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 RESOLUT
- [SDR DALA2025033002335](https://openairdocs.org/sdr/DALA2025033002335.md): Door Frame · cracked · Mar 29, 2025 · N376NW · Airbus A320212 · Fuselage Main, Structure
  > AIRCRAFT 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 RESOLUT
- [SDR DALA2025032702245](https://openairdocs.org/sdr/DALA2025032702245.md): Seat Track · corroded · Mar 26, 2025 · N376NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 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)
- [SDR DALA2025032702244](https://openairdocs.org/sdr/DALA2025032702244.md): Fitting · corroded · Mar 25, 2025 · N376NW · Airbus A320212 · Nacelle/Pylon, Main Frame
  > AIRCRAFT 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)
- [SDR DALA2025032702243](https://openairdocs.org/sdr/DALA2025032702243.md): Floor Support · corroded · Mar 25, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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 51-7
- [SDR DALA2025032702242](https://openairdocs.org/sdr/DALA2025032702242.md): Floor Support · corroded · Mar 25, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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 51-7
- [SDR DALA2025032502204](https://openairdocs.org/sdr/DALA2025032502204.md): Floor Support · corroded · Mar 24, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > SHIP 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: 0
- [SDR DALA2025032502203](https://openairdocs.org/sdr/DALA2025032502203.md): Floor Support · corroded · Mar 24, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > SHIP 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)
- [SDR DALA2025032302155](https://openairdocs.org/sdr/DALA2025032302155.md): Floor Support · corroded · Mar 22, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION 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
- [SDR DALA2025032302154](https://openairdocs.org/sdr/DALA2025032302154.md): Floor Support · corroded · Mar 22, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION 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 D5347
- [SDR DALA2025032002102](https://openairdocs.org/sdr/DALA2025032002102.md): Floor Support · corroded · Mar 20, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION 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-
- [SDR DALA2025032002099](https://openairdocs.org/sdr/DALA2025032002099.md): Seat Track · corroded · Mar 19, 2025 · N376NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 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- 11-15-283-010
- [SDR DALA2025032002097](https://openairdocs.org/sdr/DALA2025032002097.md): Seat Track · corroded · Mar 15, 2025 · N376NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 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
- [SDR DALA2025031501994](https://openairdocs.org/sdr/DALA2025031501994.md): Fitting · corroded · Mar 14, 2025 · N376NW · Airbus A320212 · Nacelle/Pylon Miscellaneous Structure
  > SHIP 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, AND
- [SDR DALA2025020200769](https://openairdocs.org/sdr/DALA2025020200769.md): Support Fitting · none · Jan 30, 2025 · N376NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 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. A
- [SDR DALA2025020200768](https://openairdocs.org/sdr/DALA2025020200768.md): Fitting · damaged · Jan 30, 2025 · N376NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > SHIP 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 T
- [SDR DALA2025012100510](https://openairdocs.org/sdr/DALA2025012100510.md): Switch · failed · Jan 18, 2025 · N376NW · Airbus A320212 · Flight Control System
  > SHIP 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)
- [SDR DALA2025011900437](https://openairdocs.org/sdr/DALA2025011900437.md): Warning Message · illuminated · Jan 18, 2025 · N376NW · Airbus A320212 · Central Warning
  > SHIP 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)
- [SDR DALA2024091508992](https://openairdocs.org/sdr/DALA2024091508992.md): Unknown · odor · Sep 12, 2024 · N376NW · Airbus A320212 · Air Distribution System
  > SHIP 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 PRESENT
- [SDR DALA2024053005674](https://openairdocs.org/sdr/DALA2024053005674.md): Controller · faulted · May 29, 2024 · N376NW · Airbus A320212 · Engine Bleed Air System
  > SHIP 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)
- [SDR DALA2024040804148](https://openairdocs.org/sdr/DALA2024040804148.md): Oxygen Mask · unsecure · Apr 4, 2024 · N376NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 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)
- [SDR DALA2024031403324](https://openairdocs.org/sdr/DALA2024031403324.md): Fcu · faulted · Mar 11, 2024 · N376NW · Airbus A320212 · Engine Fuel and Control
  > UNSATISFACTORY 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.
- [SDR DALA2024030803147](https://openairdocs.org/sdr/DALA2024030803147.md): Brake · faulted · Mar 7, 2024 · N376NW · Airbus A320212 · Landing Gear Brake System
  > SHIP 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
- [SDR DALA2024030503022](https://openairdocs.org/sdr/DALA2024030503022.md): Oxygen Mask · unwanted deploy · Mar 3, 2024 · N376NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 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)
- [SDR DALA2024030402926](https://openairdocs.org/sdr/DALA2024030402926.md): Container · open · Mar 2, 2024 · N376NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 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)
- [SDR DALA2024072907533](https://openairdocs.org/sdr/DALA2024072907533.md): Strake · missing · Feb 11, 2024 · N376NW · Airbus A320212 · Nacelle/Pylon, Main Frame
  > SHIP 3276 DISC: NBR 1 ENGINE INB STRAKE MISSING. C/A: DEFER TO CDL 54-00-01C, PLACARD INSTALLED. (LP: 5451710)
- [SDR DALA2024021301993](https://openairdocs.org/sdr/DALA2024021301993.md): Oxygen Mask · unwanted deploy · Feb 10, 2024 · N376NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 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 REVERSED
- [SDR DALA2024020801682](https://openairdocs.org/sdr/DALA2024020801682.md): Fitting · gouged · Feb 5, 2024 · N376NW · Airbus A320212 · Fuselage, Door Hinge
  > SHIP 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
- [SDR DALA2023120810069](https://openairdocs.org/sdr/DALA2023120810069.md): Unknown · unknown · Dec 7, 2023 · N376NW · Airbus A320212 · Fire Detection
  > SHIP 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 ASSE
- [SDR DALA2023051904002](https://openairdocs.org/sdr/DALA2023051904002.md): Unknown · unknown · May 18, 2023 · N376NW · Airbus A320212 · Emergency Lighting
  > SHIP 3276 ROW 12 DEF EMERGENCY FLOOR ILLUMINATION LT AND ASSY MISSING. CORRECTIVE ACTION: REPLACED LIGHT ASSY. OK FOR SERVICE. (9734714)
- [SDR DALA2023020300845](https://openairdocs.org/sdr/DALA2023020300845.md): Not Entered · not entered · Jan 31, 2023 · N376NW · Airbus A320212 · Emergency Lighting
  > SHIP 3276 FOUND RH FWD OVERWING EMERGENCY EXIT HANDLE LIGHTS INOP. CORRECTIVE ACTION: R/R LIGHT ASSY PER A320 AMM 33-51. (9889557)

Next page: https://openairdocs.org/aircraft/N376NW/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N376NW/reports

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