N363NW

Service difficulty reports · 222

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 = 'N363NW' 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 DALA2026090104921Light · inoperativeSEAT 10D EMERGENCY LIGHT INOP. R & R 10D EMER ESCAPE PATH LIGHT IAW AMM 33-51-19. LIGHT OPERATES NORMALLY, OKAY FOR SERVICE. (LP: 8828773, AIRCRAFT WAS GROUNDED)Aug 26, 2026 · N363NW · Airbus A320212 · Emergency LightingSDR DALA2026082404778Indication Sys · inoperativeATB - DUE TO FUEL QTY IMBALANCE, RIGHT INBOARD TANK READ 1,200 LBS HIGHER THAN LEFT INBOARD TANK. REPLACED FQIC. (LP: 8828758, AIRCRAFT WAS GROUNDED)Aug 23, 2026 · N363NW · Airbus A320212 · Fuel Indicating SystemSDR DALA2026060203357Oxygen Mask · unwanted deployAFT RIGHT LAV O2 MASK DEPLOYED AT CRUISE PAX IN LAVATORY. FWD TO MCO AND PLACARD PER MEL 35-21-02 AFT RIGHT LAVATORY OXY INOP, (M) PROCEDURES C/W. MCO AND PLACARD INSTALLED. R/R AFT RIGHT LAV EMERGENCY OXY CONTAINER PER AMM 35-21. OPTS CHECK GOOD. OK FOR SERVMay 26, 2026 · N363NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2025032302157Battery Pack · no testSHIP 3263 DISC: DURING SVC FOUND CABIN EMERGENGY LIGHTS AT ROWS 24-25, 28-29 AND 30. INOP. C/A: PER A320 AMM 33-51. R/R POWER UNIT BATTERY PACK AT 11WL. OPS CHECK GOOD. OK FOR SVC. (LP: 7215020)Mar 22, 2025 · N363NW · Airbus A320212 · Emergency LightingSDR DALA2025021601168Outlet · smokeSHIP 3263 DISC: DURING BOARDING, SEAT 3A +3B ELECTRICAL OUTLET SMOKING/ ONCE POWERED DOWN SMOKE STOPPED. C/A: R/R SPM P/N RD-FA3622-01 S/N OFF/ON 333933/427987, R/R DC-SEB , R/R PED OUTLET AT SEAT 3AB REF PAC A320 AIPC (SPM) 23-81-08, (DC-SEB) 23-32-07, (PED OFeb 16, 2025 · N363NW · Airbus A320212 · AC Power Distribution SystemSDR DALA2024100109585Filter · odorSHIP 3263 DISC: BOARDING ONTO THE AIRCRAFT THE CREW SMELLED DIRTY SOCK SMELL. C/A: PERFORMED WORK CARD 2100-2005. ALL OPS TESTS GOOD. AS PRECAUTION R+R RECIRCULATION FILTERS PER A320 AMM 21-21. ODI STEPS C/W REF LOG 0583248. (LP: 6653438)Sep 30, 2024 · N363NW · Airbus A320212 · Air Distribution SystemSDR DALA2024052105382Proximity Sensor · faultedSHIP 3263 - DIV - TO BWI DUE TO LANDING GEAR FAILING TO RETRACT. SYSTEM FAULTING NLG EXTEND PROX SENSORS. CORRECTIVE ACTION: MAINTENANCE IN PROGRESS.May 20, 2024 · N363NW · Airbus A320212 · Landing Gear Position and WarningSDR DALA2024031403322Light · detachedSHIP 3263 DISC: EMERGENCY PATH LIGHT AT SEAT 27F IS DETACHED FROM THE SEAT. C/A: RESECURED SAME. OK FOR SERVICE. (LP: 5273818)Mar 8, 2024 · N363NW · Airbus A320212 · Emergency LightingSDR DALA2024022102450Module · failedSHIP 3263 DISC: ROW 15 AISLE SEAT FWD EMERGENCY LIGHT INOP. C/A: REMOVED FWD LIGHT MODEUL PER A320 MM 33-51 412796. INST LITE MODULE CKS OK PER A320MM 33-51. (LP: 4897943)Feb 18, 2024 · N363NW · Airbus A320212 · Emergency LightingSDR DALA2024021502253Anti-Ice Valve · faultedSHIP 3263 - ATB - DUE TO ANTI ICE ENG2 VALVE CLSD ECAM MESSAGE. CANNOT CONTINUE INTO ICING CONDITIONS. CORRECTIVE ACTION: R/R #2 ENGINE ANTI-ICE VALVE. NO HELP. ITEM PLACED ON MEL PROCEDURES C/W (LOCKED VALVE IN OPEN POSITION). (LP: 4897922)Feb 13, 2024 · N363NW · Airbus A320212 · Engine Anti-Icing SystemSDR DALA2024020901762Extinguisher · dischargedSHIP 3263 DISC: FWD CARGO FIRE EXTINGUISHER DISCHARGED. C/A: BEGAN RESTORATION OF FES SYS PER A320 AMM 26-23 (889397) REMOVED AND REPLACED FWD CARGO FIRE BOTTLE PER A319-320 AMM 26-16. RFID PENDING (221599) RFID TAGE INSTALLED. MEL/PLAC RMVD. OK FOR SERVICE. (Feb 7, 2024 · N363NW · Airbus A320212 · Extinguishing SystemSDR DALA2024012200909Oxygen Mask · unwanted deploySHIP 3263 DISC: O2 MASKS CAME DOWN AT 13DFE UPON LANDING. C/A: REPACK O2 MASKS AT 13DEF PER A 320 AMM 35-21. (LP: 8914028)Jan 20, 2024 · N363NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2024011400564Unknown · unknownSHIP 3263 DISC: AD RELATED:(5311-01244-01A) PREVIOUS REPAIR PART INSTALL AT L/H FR. 68, STGR 22LH, REQUESTING DELTA LIASON ENGINEERING TO DETERMINE IF SRM 53-41-12-300-011- STOP FTG HOLES OF LH AFT DOOR - REPAIR PART INSTALLATION WAS ACOMPLISHED WITH OR WITHOUJan 11, 2024 · N363NW · Airbus A320212 · Standard Practices/StructuresSDR DALA2024011400563Unknown · unknownSHIP 3263 DISC: BATHTUB FITTING ON FR.68 LOWER L/H SIDE, FOUND GOUGED DURRING INSPECTION. REF BY AIRBORNE/PEMCO NR.14821.0068. C/A: REMOVED AND REPLACED BATHTUB FITTING ON FR 68 LOWER L/H SIDE (#1 DOOR STOP AREA) AIW A320 SRM 53-41-12-300-011. SEALANT P/N PS87Jan 11, 2024 · N363NW · Airbus A320212 · Fuselage Main, Attach FittingsSDR DALA2024011400566Unknown · unknownSHIP 3263 DISC: AD RELATED:(5311-01244-01B) PREVIOUS REPAIR PART INSTALL AT R/H FR. 68, STGR 22RH, REQUESTING DELTA LIASON ENGINEERING TO DETERMINE IF SRM 53-41-12-300-011- STOP FTG HOLES OF RH AFT DOOR - REPAIR PART INSTALLATION WAS ACOMPLISHED WITH OR WITHOUJan 10, 2024 · N363NW · Airbus A320212 · Standard Practices/StructuresSDR DALA2023051003669Unknown · unknownSHIP 3263 #2 ENGINE PYLON AFT MOUNT INBD SIDE DAMAGED. CORRECTIVE ACTION: COMPLIED WITH ERA 603758-14. (2492432)Nov 12, 2022 · N363NW · Airbus A320212 · Nacelle/Pylon, Attach FittingsSDR DALA2022082205659None · noneSHIP 3263 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:32D. CORRECTIVE ACTION: SECURED 32D EMERG LIGHT IN PLACE. OK FOR SERVICE. (2372165)Aug 19, 2022 · N363NW · Airbus A320212 · Emergency LightingSDR DALA2021123008174None · noneCRACK FOUND ON WINDSHIELD FRAME RH SIDE, CRACK LENGTH: 0.200 INCH, CRA CK AT 11 O CLOCK . AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING R EPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. SIDE AS PER ER/A 595453-14AD REV. ORIGINAL ANDDec 29, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908147None · noneCRACK FOUND ON CONTINUITY FITTING LH SIDE , CRACK LENGTH: 0.190 INCH APPROX, VERTICAL DIRECTION. AD 2020-17-03/ WORKCARD 5311-01226- 01 REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. PERFORMED REPAIR INSTRUCTION ON CONTINUIDec 29, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908146None · noneCRACK FOUND ON CONTINUITY FITTING RH SIDE, CRACK LENGTH: 0.190 INCH, V ERTICAL CRACK. AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. PERFORMED REPAIR INSTRUCTIONS FOR CONTINUITY FITTINDec 29, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908139None · noneCRACK INDICATION FOUND IN OPEN FASTENER HOLE (1EA) LOCATED AT UPPER AT TACHMENT FRAME 4 SIDE POST AREA RH SIDE, CRACK DIRECTION: 07 O CLOCK ( D1-D2=0.075 INCH). PERFORMED PERMANENT REPAIR ON UPPER ATTACHMENT FRAME 4 SIDE POST AREA RH SIDE AS PER ER/A 543313-14Dec 28, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908138None · noneCRACK INDICATION FOUND IN OPEN FASTENER HOLE (1EA) LOCATED AT UPPER AT TACHMENT FRAME 4 SIDE POST AREA LH SIDE, CRACK DIRECTION: 01 O CLOCK APPROX (D1-D2=0.0665 INCH). PERFORMED PERMANENT REPAIR ON UPPER ATTACHMENT FRAME 4 SIDE POST AREA LH SIDE AS PER ER/A 54Dec 28, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908133None · noneOUT LIMIT FRAME 68 DOOR STOP FITTING 1L DIAMETER HOLE ?1= 0.252INCH,?2= 0.254INCH,?3=0.251INCH ,?4=0.258INCH AA 5311 -01216 AD RELATED ACTIONS R EQUIRED PRIOR TO FURTHER FLIGHT AT AFT GALLEY AREA (4 EA). PERFORMED PERMANENT REPAIR FRAME 68 DOOR STOP FITTING 1LDec 28, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908132None · noneOUT LIMIT FRAME 68 DOOR STOP FITTING 1 RH HOLE DIAMETER ?1= 0.257IN, ?2 =0.258IN, ?3=0.256IN, ?4=0.256IN AA 5311-01216 AD RELATED. ACTIONS REQ UIRED PRIOR TO FURTHER FLIGHT AT AFT GALLEY AREA (4 EA). ERFORMED PERMANENT REPAIR FRAME 68 DOOR STOP FITTING 1 RH ATDec 28, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908131None · noneWEAR ON FITTING KEEL BEAM FWD , FWD LUG ,FWD FACE RH SIDE IN MAIN WHEE L WELL (1 EA). PERFORMED REPAIR LOC. ON FITTING KEEL BEAM FWD , FWD LUG ,FWD FACE RH SIDE IN MAIN WHEEL WELL (1 EA). AS PER PRI 595936-14AD, REV. 0. AND ER/A 595936-14AD, REV. ORIGINAL. APPDec 28, 2021 · N363NW · Airbus A320212 · Fuselage Main, KeelSDR DALA2021122808096None · noneSHIP 3263 ER/A 595940-14AD DTA REQUIRED FOR THE LH FRAME 68 INSPECTING FOR CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA. CONTINUE ON MON. (2066495)Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122808095None · noneSHIP 3263 ER/A 595940-14AD DTA REQUIRED FOR LH & RH FRAME 68. CORRECTIVE ACTION: COMPLIED WITH ERA. (2066491)Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122808094None · noneSHIP 3263 ER/A 595940-14AD DTA REQUIRED FOR RH FRAME 68 INSPECTING FOR CRACKS. CORRECTIVE ACTION: COMPLIED WITH ERA. CONTINUE ON MON. (2066486)Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122808093None · noneSHIP 3263 ER/A 595940-14AD DTA REQUIRED FOR THE FRAME 68 LH & RH INSPECTING FOR CRACKS. CORRECTIVE ACTION: COMPLIED WITH ERA. (2066483)Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122808092None · noneSHIP 3263 ER/A 595940-14AD SEC III REQUIRED FOR THE RH FRAME 68. CORRECTIVE ACTION: COMPLIED WITH ERA. CONTINUE ON MON. (2066476)Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122808091None · noneSHIP 3263 ER/A 595940-14AD SEC II REQUIRED FOR LH AND RH FRAME 68 INSPECTING FOR CRACKS. CORRECTIVE ACTION: COMPLIED WITH ERA. CONTINUED ON MON. (2066465)Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122708048None · noneSHIP 3263 CORROSION INTERCONNECTING STRUT OB FLAP ON CONNECTOR LH WING. CORRECTIVE ACTION: REMOVED AND REPLACED CONNECTOR ON INTERCONNECTING STRUT LH WING AS PER A320 AWM 27-51-12. (2063606)Dec 24, 2021 · N363NW · Airbus A320212 · Trailing Edge FlapsSDR DALA2021122708043None · noneSHIP 3263 GOUGE SHEAR TIE LOCATED FR32 BTW STR 43L TO STR 44 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER 51-42-11 AND 51-72-11. (2063686)Dec 24, 2021 · N363NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2021122708047None · noneSHIP 3263 SEAT TRACK Y1292 AT LEVEL FR64 TO FR66 AT AFT GALLEY AREA OUT OF LIMITS. CORRECTIVE ACTION: FABRICATED AND REPLACED SEAT TRACK PER ER/A 595627-14 REV. ORIGINAL. (2062573)Dec 23, 2021 · N363NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2021122708046None · noneSHIP 3263 SEAT TRACK -Y1292 AT LEVEL FR 64 TO FR66 AT AFT GALLEY AREA OUT OF LIMITS. CORRECTIVE ACTION: FABRICATED AND REPLACED SEAT TRACK PER ER/A 595630-14 REV. ORIGINAL. (2062571)Dec 23, 2021 · N363NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2021122908155None · noneDTA MONITOR INSPECTION LOG REFERENCE ER/A 595412-14 SECTION II REQUIRES DTA APPROVAL WITHIN 30600 CYCLES. ASSOCIATED ER/A 00-595412 ADDED FOR AC 3263. (LP# 2067204)Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908154None · noneDTA MONITOR INSPECTION LOG REFERENCE ER/A 595453-14 SECTION II REQUIRES DTA APPROVAL WITHIN 30600 CYCLES. DISCONTINUE REVENUE SERVICE WITHIN 30600 CYCLES AFTER SECT I PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-595453 ADDED FOR AC 3263. (Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908153None · noneDTA MONITOR INSPECTION LOG REFERENCE ER/A 543312-14 REV A SECTION VI REQUIRES DTA APPROVAL WITHIN 48000 CYCLES AFTER SECT III. DISCONTINUE REVENUE SERVICE WITHIN 48000 CYCLES AFTER SECT III PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-5433Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908152None · noneFUSELAGE / FRAMES / RHS LATERAL WINDOW FRAME & GUSSET / REPLACEMENT, SECTION V. ACCOMPLISH ER/A 543312-14 REV A SECTION V INSPECTION WITHIN 3,299 CYCLES AFTER SECTION III REPAIR, AND THEREAFTER WITHIN EVERY 11,000 CYCLES. (LP# 2067128)Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908151None · noneFUSELAGE / FRAMES / LHS LATERAL WINDOW FRAME & GUSSET / REPLACEMENT. ACCOMPLISH ER/A 543312-14 REV A SECTION IV INSPECTIONS WITHIN 21,100 CYCLES AFTER SECTION III AND THEREAFTER WITHIN EVERY 5,200 CYCLES. ASSOCIATED ER/A 00-543312 ADDED FOR AC 3263. (LPL# 2067Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908150None · noneDTA MONITOR INSPECTION LOG REFERENCE ER/A 543313-14 REV A SECTION VI REQUIRES DTA APPROVAL WITHIN 48000 CYCLESAFTER SECT III. DISCONTINUE REVENUE SERVICE WITHIN 48000 CYCLES AFTER SECT III PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-54331Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908149None · noneFUSELAGE / FRAMES / RHS LATERAL WINDOW FRAME & GUSSET / REPLACEMENT WITH DEVIATIONSFOR SECTION V. ACCOMPLISH ER/A 543313-14 REV A SECTION V INSPECTION WITHIN 3,299 CYCLES AFTER SECTION III REPAIR, AND THEREAFTER WITHIN EVERY 11,000 CYCLES. ASSOCIATED ER/A 00-5Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122908148None · noneFUSELAGE / FRAMES / RHS LATERAL WINDOW FRAME & GUSSET / REPLACEMENT WITH DEVIATIONS. ACCOMPLISH ER/A 543313-14 REV A SECTION IV INSPECTIONS WITHIN 21,100 CYCLES AFTER SECTION III AND THEREAFTER WITHIN EVERY 5,200 CYCLES. ASSOCIATED ER/A 00-543313 ADDED FOR AC Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122308007None · noneSHIP 3263 CORROSION INTERNAL STRUCTURE SKIN LAP JOINT AREA BTW STR 40/42 R AND BTW FR 33/34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 595841-14 REV. 0. AND ER/A 595841-14AD REV. ORIGINAL. (2061442)Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2021122308006None · noneSHIP 3263 CORROSION SHEAR TIE LOCATED FR29 BTW STR44 TO STR43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-42-11 AND 51-72-11. (2061439)Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2021122308005None · noneSHIP 3263 CORROSION STRINGER 42R LOCATED BTW FR30 TO FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-42-11 AND 51-72-11. (2061434)Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2021122308004None · noneSHIP 3263 CORROSION SHEAR TIE LOCATED FR33 BTW STR42R TO STR43R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11 AND 51-42-11. (2061424)Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2021122207983None · noneSHIP 3263 CRACK INDICATION FOUND IN OPEN HOLE 07 LOCATED AT FRAME 16 LH SIDE. CORRECTIVE ACTION: REPAIRED PER PRI #595385-14AD REV.0, REV.1 AND ER/A #595385-14AD REV.ORIGINAL. (2060316)Dec 21, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122207982None · noneSHIP 3263 CRACK INDICATION FOUND IN OPEN HOLE 06 LOCATED AT FRAME 16 LH SIDE. CORRECTIVE ACTION: COMPLIED WITH PRI #595385-14AD REV.0, REV.1 AND ER/A #595385-14AD REV.ORIGINAL. (2060311)Dec 21, 2021 · N363NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021122207968None · noneSHIP 3263 CORROSION STRINGER 44 LOCATED BTW FR31 TO FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON STRINGER PER A320 SRM 53-00-13. (2060446)Dec 21, 2021 · N363NW · Airbus A320212 · Fuselage Floor Panel
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