Airbus A320-212

Service difficulty reports · 8,181

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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 aircraft_model_key = 'A320212'
  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 DALA2026061803631Computer · faultyATB, AFTER T/O WHEN RETRACTING FLAPS TO 0 RECEIVED F/CTL FLAPS FAULT MSG AND FLAPS STUCK AT 0 ON LANDING WHEN HANDLE SET TO FLAPS 2 FLAPS EXTENDED. REF LOG 1652816 FOR WORK PERFORMED(146991) REMOVED AND REPLACED SFCC 1 IAW AMM 27-51. NO FAULTS NOTED AT THIS TJun 18, 2026 · N345NW · Airbus A320212 · Trailing Edge Flap Control SystemSDR DALA2026062203692Oxygen Panel · openPASSENGER OXYGEN MASK PANEL OPENED IN FLIGHT ABOVE SEATS 2C AND D. FWD TO MEL 35- 21-01A. M PROCEDURE C/W AND PLACARD INSTALLED. SEATS 2 C AND D UNUSABLE. RESECURED O2 CONTAINER DOOR AT 2CD PER AMM 35-21. M PROCEDURES REVERSED. MEL PLACARD REMOVED. OK FOR SEJun 17, 2026 · N341NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2026061803629Strut · corrodedCORROSION INTERCONNECTING STRUT IB FLAP LH WING (REFER TO AMDS CARD 27 51-9202 RII). REMOVED INTERCONNECTING STRUT LT WING UNSERVICEABLE CONDITION IAW FAM AMM 27-51-44-000-001- A STEP 1 THRU 3.D(1) & 4.A JOB IN PROGRESS. FINAL REPAIR RESOLUTION: PERFORMED OPEJun 12, 2026 · N375NC · Airbus A320212 · Trailing Edge Flap Control SystemSDR DALA2026061503566Oil System · overservicedSMOKE/FUME EVENT AFT GALLEY (10K THROUGH LANDING). C/A: PERFORMED INITIAL INSPECTION OF NR 1 , NR 2 ENG AND APU COMPARTMENT NO EXTERNAL LEAKS NOTED. (WIP D.P 098218). PERFORMED W/C 0550- 2001, LOGGED DATA WITH PTRAK , RESULTS SUBMITTED TO SMOKE AND FUMES GROUPJun 12, 2026 · N356NW · Airbus A320212 · APU Oil SystemSDR DALA2026071504144Elec Connector · corrodedCORROSION ELECTRICAL CONECTOR OF ESCAPE SLIDE OF PASSENGER CREW DOOR 842 (REFERENCE RII AMDS CARD 5210-7089-RA). REMOVED ESCAPE SLIDE OF PASSENGER CREW DOOR 842 IN UNSERVICEABLE CONDITION P/N D31517-717 S/N A12730RP AS PER AMDS CARD 5210- 7089-RA JOB IN PROGRJun 11, 2026 · N375NC · Airbus A320212 · Equipment/Furnishings WiringSDR DALA2026061803630Psu · looseOXYGEN PANEL LOOSE, AT THE TOP OF 2L EXIT DOOR, COVER POPPED OPEN. SIGN SHOWS, MASK PACKING, O2 GENERATOR & MASK SCHEMATIC. HOT INTERIOR. RESECURED CLOSED. NO FURTHER DEFECTS NOTED. IAW AMM 35-22. (LP: 1642116, AIRCRAFT WAS GROUNDED)Jun 11, 2026 · N340NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2026061103522Dampener · failedDID NOT PASS OPS TEST OF DOOR DAMPER ON PASSENGER CREW DOOR 832. REMOVED DOOR DAMPER FROM PASSENGER CREW DOOR 832 IN UNSERVICEABLE CONDITION JOB IN PROGRESS. REPLACED UNSERVICEABLE DOOR DAMPER PN FE174-004 SN NO869 FOR NEW DOOR DAMPER PN FE240-006 SN RFM29991Jun 9, 2026 · N375NC · Airbus A320212 · Passenger/Crew DoorsSDR DALA2026061103523Unknown · odorWALKED INTO THE AIRCRAFT, APU WAS ON AS WELL AS APU BLEED. AIRCRAFT SMELLED LIKE DIRTY SOCKS. MTX AND CLEANERS SMELLED IT AS WELL. (APU NOT SOURCE OF ODOR. (LP: 8678685, AIRCRAFT WAS GROUNDEDJun 8, 2026 · N356NW · Airbus A320212 · Air Distribution SystemSDR DALA2026060803417Blade · bird ingestionON DEPT OUT OF HOU, BIRDSTRIKE ON RT ENG, HIGH VIB INDICATION ON ECAM MAX 8.8 N1, ENG CONT TO RUN WITH THRUST PULLED BACK. C/W BIRDSTRIKE INSP IAW 72-00. FOUND MULTIPLE BLADES DAMAGED BEYOND REPAIR, ACOUSTIC PANES DAMAGE & RUB STRIP OUT OF LIMITS PER 72-21. RJun 8, 2026 · N362NW · Airbus A320212 · Turbine Engine Compressor SectionSDR DALA2026060903449Warning Message · illuminatedATO AT 2 KTS DUE TO BRAKE SYS 1 FAULT ON ECAM. RESET PER RESET PROCEDURE COMPLETED SUCCESSFULLY. INFO NOTED & RECORDED. NO 10 DAYS HISTORY. (LP: 8678676, AIRCRAFT WAS GROUNDED)Jun 5, 2026 · N356NW · Airbus A320212 · Landing Gear Brake SystemSDR DALA2026060703412Engine · making metalRETURNED TO MSP DUE TO REPORT OF #2 ENGINE EGT OVERLIMIT. METAL FOUND IN TAILPIPE, ENGINE CHANGE REQUIRED. (LP: 8940774, AIRCRAFT WAS GROUNDED.)Jun 5, 2026 · N361NW · Airbus A320212 · Engine (Turbine/Turboprop)SDR DALA2026060503399Window Frame · crackedCRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHM ENT AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH, AD RE LATED, AA 5311-01226, AD 2020-17-03, WORK CARD 5311-01226-01. REQUESTI NG REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHJun 4, 2026 · N341NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026060503398Window Frame · nonePERFORM ER/A 633637-14AD FOR WINDSHIELD FRAMING CENTER POST LT AND RT SIDE AT COCKPIT AREA. COMPLIED WITH ER/A 633637-14AD REV. ORIGINAL APPROVED DATE 28- MAY-26 MATCHES WITH ALL STEPS ON PRI 633637-14AD REV. 0; REV. 1; ITHAS BEEN VALIDATED. PERFORMED REPAIR IJun 4, 2026 · N341NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026060903450Oxygen Mask · unwanted deployOXYGEN PANEL MASK DEPLOYED / LOCATIONS:18D FRC35230318D - ADDITIONAL LOCATIONS 18E,18F - OXYGEN MASK IN SEATS 18DEF DEPLOYED ON TAKEOFF / INTERIOR. APPLIED MEL 35-21-01A TO SEAT ROW 18DEF PLACARDS INSTALLED. FOUND OB HINGES BROKEN, R/R HINGES PER CMM 25-28-02,Jun 3, 2026 · N335NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2026060203349Window Frame · crackedCRACK INDICATION FOUND IN FASTENER HOLE LOCATED AT THE LT FR4 LATERAL WINDOW UPPER JUNCTION. CRACK DEPTH = 0.138 INCHES, CRACK DIRECTION 10 O CLOCK. IN COCKPIT. AA NUMBER 5311-01236-01. AD RELATED, WORK CARD 53 11-01236-01. REQUESTING REPAIR DISPOSITION. REPAIJun 1, 2026 · N341NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026060203348Fitting · damagedAVIONICS COMPARTMENT RACK 80VU, LH AND RH LATERAL PYRAMIDS FITTINGS WITH ELONGATED HOLES.AIRBUS MUST BE CONTACTED BEFORE FURTHER FLIGHT, REPAIRED FWD FUSELAGE EQUIPMENT / RACK 80VU LH AND RH LOWER LATERAL SUPPORT FOR MATERIAL BURRED (OVALIZATION) IAW ER/A 634Jun 1, 2026 · N351NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026060103313Unknown · odorSMOKE + FUMES IN FLIGHT DECK, ELECTRICAL BURNING SMELL. EMERGENCY DELCARED. FOUND LEFT PACK ACM FAILED WITH SEIZED SHAFT, PACK OVERHEAT EVENT. ACM WAS REPLACED REF LOG 8668857, RAN PACKS FOR 20 MINUTES AND NO SMELL NOTED. (LP: 8668858, AIRCRAFT WAS GROUNDED)May 31, 2026 · N355NW · Airbus A320212 · Air Distribution SystemSDR DALA2026060203350Door · unsecureRETURN TO GATE EVENT-DURING T/O, AFT CARGO DOOR INDICATED NOT CLOSED. T/O WAS ABORTED. INSPECTED AFT CARGO DOOR IAW A320 TSM 52-32-00-810-801-A & A320 AMM 52-71-00-820-004-A. IMMEDIATELY NOTICED AFT CARGO DOOR HANDLE NOT FULLY LOCKED/LATCHED. LATCHED DOOR, INMay 30, 2026 · N345NW · Airbus A320212 · Door Warning SystemSDR DALA2026053103303Floorbeam · crackedAD RELATED AA 5711-01036-CENTER WING FRONT SPAR VERTICAL STRINGERS, CRACKS FOUND ON FLOORBEAM SIDE VERTICAL RADIUS AT-Y765 ZONE 1 CRACK L= 0.250 INCHES APPROX AT ZONE 2 CRACK L= 0.400 INCH APPROX, REPAIR IS R EQUIRED PRIOR TO FUTHER FLIGHT. COMPLIED WITH ER/AMay 30, 2026 · N341NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2026053103302Structure · damagedDURING DVI WAS FOUND EXISTENT REPAIR BUSHING LOCATED ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND 2 -Y765 ( AD RELATED AA 5711-01036). PERFORMED REPAIR INSTRUCTION ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND ZONE 2 ON -Y765 AS PER ER/A 587692-14AD REV. B SMay 30, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026053103301Structure · damagedDURING DVI WAS FOUND EXISTENT REPAIR BUSHING LOCATED ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND 2 -Y254 (AD RELATED AA 5711-01036). PERFORMED REPAIR INSTRUCTIONS ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND ZONE 2 ON -Y254 AS PER ER/A 587692-14AD REV. B SMay 30, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026060103311Door Sill · corrodedLEVEL 2 CORROSION, AFT PASSENGER CABIN, LH DOOR LOWER CUT OUT SILL BEAM AREA CENTER ANGLE WITH CORROSION. REPLACED (SHAPE) CENTER ANGLE P/N: D5348004820203 AT AFT PASSENGER CABIN L/H DOOR LOWER CUT OUT SILL BEAM IAW A320 SRM 51 -72-11-911-001 REV 157.00 DATEDMay 29, 2026 · N351NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026053103300Hinge Arm · corrodedLEVEL 2 CORROSION, CORROSION SSI:553006 RUDDER HINGE ARM NR 7 STUD HOLES L/R SIDES WITH CORROSION. REPAIRED VERTICAL STABILIZER RUDDER HINGE ARM BR1 OVERSIZED HOLE AND HINGE BR7 REPLACEMENT IAW DELTA ER/A 634168-14 REVISION ORIGINAL DATED 27-MAY-26. NOTE: FORMay 29, 2026 · N351NW · Airbus A320212 · Vertical StabilizerSDR DALA2026053103299Stop Fitting · damagedEXISTING REPAIR FR68, INNER CAP & FR FLANGE, STRG 22 RH AT LEVEL DOOR STOP FITTING 1. CONTACT DELTA LIAISON ENGINEERING FOR ALTERNATE INSPECTION INSTRUCTIONS THAT MAY BE REQUIRED TO COMPLETE WORK CARD 5311-0124 4-02B DUE TO PREVIOUS REPAIR IN THE INSPECTION ARMay 29, 2026 · N341NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026053103298Filter · odorWITH INOP APU AND NO JET BRIDGE AIR,UTILIZING HUFFER TO RUN PACKS. FUMEES BEGAN IN CABIN. SECURED PACKS AND HUFFER CART. R/R RECIRC FILTERS AND #2 RECIRC FAN PER A320 AMM 21-21. NO FURTHER SCENT NOTED. (LP: 8668980, AIRCRAFT WAS GROUNDED)May 29, 2026 · N372NW · Airbus A320212 · Air Distribution SystemSDR DALA2026053103297Floorbeam · crackedDURING M2 AND WHILE ACCOMPLISHING EM 5711-01036-03B, PREVIOUSLY REPAIRED HOLES FOUND AT -Y254 AND -Y765 ALONG WITH CRACK INDICATION FOUND IN THE RADIUS OF HORIZONTAL FLOOR BEAM AT -Y765. PER SECTION IV OF 587692-14AD REV B, ACCOMPLISH SECTION IV REPETITIVE INMay 29, 2026 · N341NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2026053103290Door Sill · corrodedLEVEL 2 CORROSION, AFT PASSENGER CABIN, AFT R/H DOOR CUTOUT AT Y-1235MM FR68 SILL BEAM WITH CORROSION. FOUND DURING PROCESS WITH ORNRC 200- 278. PERFORMED REPAIR AFT PASSENGER CABIN AFT RH DOOR CUT OUT SILL BEAM BETWEEN FR 67 +335MM AND FR 68 +35MM I/A/W A32May 29, 2026 · N351NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026053103296Support Fitting · not reportedER/A 634037-14AD ISSUED FOR REPAIR TO LT & RT LOWER LATERAL SUPPORT FITTINGS OF THE 80VU RACK. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 19500FC OF SECTION I AND EVERY 1000FC THEREAFTER. ASSOCIATED AA 2515-01014 ADDED FOR AC 3251 ASSOCIATED ER/AMay 28, 2026 · N351NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026053103295Window Frame · cracked*DTE* DURING M2 AND WHILE INSPECTING PER EM 5311-01236-01 CRACK INDICATIONS FOUND IN LH LATERAL WINDOW FRAME UPPER JUNCTION FASTENER HOLE #1 AND HOLE #3. *DTE* PER SECTION DTE OF 633473-14, THE REPAIR OF SECTION I IS LIMITED TO 20,700 FC FROM SECTION I (18MAYMay 28, 2026 · N341NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026053103285Window Frame · crackedCRACK INDICATION FOUND IN OPEN FASTENER HOLE LOCATED ON FRAME 4 LATERA L WINDOW UPPER JUNCTION RT SIDE. CRACK DEPTH: 0.078 INCH, CRACK DIRECTION: 3 O`CLOCK VIEW LOOKING FWD. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. A.A 5311 -01236-02. COMPLIED WIMay 28, 2026 · N336NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026052803240Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND (1 EA) ON RH CONTINUITY FITTING OF THE WINDSHIE LD LOWE R ATTACHMENT AREA, L= 0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 5311-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RMay 28, 2026 · N336NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026052803239Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND ON LH CONTINUITY FITTING OF THE WINDSHIELD LOWE R ATTACHMENT AREA, L=0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 53 11-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RH FRONT May 28, 2026 · N336NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026052803238Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND ON LH CONTINUITY FITTING OF THE WINDSHIELD LOWE R ATTACHMENT AREA, L= 0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 53 11-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RH FRONTMay 28, 2026 · N336NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026052803237Window Frame · crackedAIRCRAFT 3241, CRACK INDICATION FOUND IN FASTENER HOLE LOCATED AT THE RH FR4 LATERAL WINDOW UPPER JUNCTION. CRACK DEPTH = 0.079 INCHES, CRACK DIRECTION 2 O CLOCK. IN COCKPIT. AA NUMBER 5311-01236-02. AD RELATED, WORK CARD 531 1-01236-02. CORRECTIVE ACTION: PERMay 28, 2026 · N341NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2026052803230Window Frame · crackedAIRCRAFT 3236, DURING M2 CHECK AT AEM (SAL), WHILE EXECUTION OF HFEC INSPECTION OF THE WINDSHIELD CENTRAL NODE CONTINUITY FITTINGS AND WINDSHIELD FRAMES ON LH AND RH SIDES AS PER JOB CARD 5311-01226-01 (IN ORDER TO COMPLY WITH FAA AD 2020-17-03 AND SB A320-53-May 28, 2026 · N336NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026060103310Skin · damagedDURING CURRENT HEAVY CHECK PERFORMED ON AEM SAL, AN EXISTING REPAIR WAS FOUND ON THE BUTT JOINT LOCATED AT FR24 BETWEEN STGR23LH AND STGR24LH ON THE SKINS PN D53112242202 AND PN D53231369200. THE REPAIR WAS EVALUATED AGAINST THE SRM 53-00-11 TABLE 203. SRM 53-May 27, 2026 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2026053103294Fitting · cracked*DTE* DURING M2 WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALED HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA. C/A: *DTE* PER SECTION DTE OF 633637-14AD THE May 27, 2026 · N341NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026053103293Fitting · crackedDURING M2 AND WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALED THAT HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA. PER SECTION II OF 633637-14AD, ACCOMPLISH May 27, 2026 · N341NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026053103292Fitting · crackedDURING M2 AND WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALE D THAT HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA. PER SECTION II OF 633308-14AD, ACCOMPLISHMay 27, 2026 · N341NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026052803241Union · leakingSHIP 3262 - MISC - DECLARED EMERGENCY DUE TO PARTIAL LOSS OF THE GREEN SYSTEM HYDRAULIC FLUID. AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. CORRECTIVE ACTION: FOUND LEAK AT GREEN SYSTEM HP MANIFOLD UNION. REMOVED PRESSURE SWITCH AND REPLACED O'RING AND RE-May 27, 2026 · N362NW · Airbus A320212 · Hydraulic System, MainSDR DALA2026052803236Skin · damagedAIRCRAFT 3236, DURING CURRENT HEAVY CHECK PERFORMED AT AEM (SAL), AN EXISTING REPAIR WAS FOUND ON THE EXTERNAL SKIN AT LEVEL OF FR29 AND STGR4L. THE REPAIR WAS EVALUATED AGAINST THE SRM 53-00-11 FIGURE 204 AND THE PITCHES THAT FIGURE 1 SHOWS WERE FOUND OUT OF May 27, 2026 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2026052803235Stop Fitting · scratchedAIRCRAFT 3251, UPPER FUSELAGE PAX CABIN BETWEEN FR15 AND FR16 R/H SIDE AT STOP FITTING #1, INTERCOSTAL WITH SCRATCHES AND TOOL MARK. CORRECTIVE ACTION: ACCOMPLISHED INTERCOSTAL REPLACEMENT AT FR16 RH DOOR STOP #1 IAW ER/A #589110-14AD REV A. (LP 1615986 - AIRCMay 27, 2026 · N351NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026052803234Seat Track · corrodedAIRCRAFT 3251, UPPER FUSELAGE, FWD ENTRY AREA SEAT TRACK BETWEEN FR 20 AND FR 21 Y-1292 WITH CORROSION LEVEL 2. CORRECTIVE ACTION: REPLACED SEAT TRACK P/N: D5311281400200 AT Y-1292 BTWN FR12 AND FR24 IAW A320 SRM 51-72-11-911-001 PARG 2 REV 157.00 DATED 15/APRMay 27, 2026 · N351NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026052803233Floor Support · corrodedAIRCRAFT 3251, AFT PASSENGER CABIN BETWEEN FR 66-68, -Y 765 FLOOR BEAM WITH LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FLOOR BEAM P/N: 5347219320000 AT Y-765 BTW FR66 TO FR70 IAW A320 SRM TASK 51-72-11-911-001 PARAG 1A (1) REV 157.00 DATED 15/APR/26 AND AIMay 27, 2026 · N351NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026052803232Floor Support · corrodedAIRCRAFT 3251, AFT PASSENGER CABIN BETWEEN FR 66-68, -Y 1292, FLOOR BEAM WITH LEVEL 2 CORROSION. REPLACED FLOOR BEAM P/N: D5347217220390, P/N: D5347218920200, COUPLING P/N: D5347210220600, D5347210220400, D5347210220200, BTW FR66 TO FR69 AT -Y1292 IAW A320 SMay 27, 2026 · N351NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026052703217Actuator · wornATO- DUE TO RIGHT ENGINE COMPRESSOR VANE FAULT. FOUND VBV MASTER BALLSCREW ACTUATOR WORN AND NOT FUNCTIONING. REPLACED ACTUATOR, MECHANICAL STOP, GEAR MOTOR AND POSITION SENSOR. (LP: 8881690) AIRCRAFT WAS GROUNDEDMay 27, 2026 · N374NW · Airbus A320212 · Compressor Bleed ControlSDR 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 DALA2026053103291Skin · damagedDURING M2 AND WHILE PERFORMING AAI INSPECTIONS EXISTING REPAIR, INSTALLED PER 547923-14 REV B WAS FOUND INSTALLED ON EXTERNAL FUSELAGE SKIN AT FR24 BETWEEN STGR20LH AND STGR23LH WITH FASTENERS INSTALLED INCORRECTLY ON CHEM-MILLED POCKET. *DTE* PER SECTION DTEMay 26, 2026 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2026052703210Web · damagedA.A. WORK CARD 5311-01244-02B, REQUESTING REPAIR DISPOSITION. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED, AND REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. REFER TO EM 5311- 01244 AND SB A320-53-1491. INSTRUCTIONS TO LIASON IN EARTH FOLDER "DELTA May 26, 2026 · N351NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026052703209Seat Track · corrodedLEVEL 2 CORROSION, A1R116 2-79 (200-336). AFT PASSENGER CABIN AT FR66 Y-765, SEAT TRACK WITH CORROSION. NOTE: FOUND DURING PROCESS OF ORNRC 200- 277. C/A: REPLACED SEAT TRACK P/N: 14N00031-103 FROM FR64 TO FR66 -Y 765 WET AREA, DUE TO CORRODED OUT-LIMITS I/A/WMay 26, 2026 · N351NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
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