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 DALA2026081404666Windshield · crackedCRACK APPEARED ON THE RIGHT WINDSHIELD FOLLOWED BY A ANTI-ICE RT WINDSHIELD ECAM MESSAGE, R & R FIRST OFFICER`S WINDSHIELD IAW A320 AMM 65-11-11-400-001-A. (9170340) (AIRCRAFT GROUNDED).Aug 13, 2026 · N340NW · Airbus A320212 · Flight Compartment WindowsSDR DALA2026081404665Frame · crackedFOUND CRACK IN FR16 LT, OUTBBOARD FLANGE, UPPER AREA ABOVE DOOR STOP 7, AT HOLE NR 6, COMPLIED WITH ER/A 567055-14. (1753281) (AIRCRAFT GROUNDED).Aug 12, 2026 · N362NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2026081204632Coffeemaker · faultedAFT INBD COFFEEMAKER WILL NOT SECURE. BOTH COFFEEMAKER CIRCUIT BREAKERS PULLED IN AFT GALLEY AS PRECAUTION DUE TO LOG 9170338. R & R AFT INBD COFFEEMAKER DISPENSER IAW AMM 25-35, OPS CHK GOOD. (LP: 9170339, AIRCRAFT WAS GROUNDED)Aug 12, 2026 · N340NW · Airbus A320212 · Buffet/GalleysSDR 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 DALA2026081104624Brake · bindingUPON LDG IN ATL AUTOBRAKES SELECTED LOW. AC TOUCHDOWN AT 2000 APPROACHING 2ND HIGH SPEED TURN OFF AC WAS DOING 100 KTS. MANUAL BRAKES APPLIED TO FURTHER DECEL. UPON MANUAL BRAKING AC VEERED HARD LEFT. FULL RUDDER DEFLECTION WAS INSUFFICIENT. TILLER USED TO MAIAug 8, 2026 · N368NW · Airbus A320212 · Landing Gear Brake SystemSDR DALA2026081004595Bracket · damagedFO CONSOLE / FLOOR LIGHT MAKES BURNING ELECTRICAL SMELL WHEN TURNED ON. C/W MD LOG 1744592 STEPS A,B,C,D,E. INSP FLT DECK FOUND FO UNDER SEAT LIGHT BRACKET DAMAGED CAUSING BULB TO BURN OBJECT UNDER SEAT CREATING BURN ODOR, R&R F/O SEAT IAW A320 AMM 25-11. RE-Aug 8, 2026 · N334NW · Airbus A320212 · Emergency LightingSDR DALA2026080704568Window Frame · crackedAD 2020-17-03 / A.A WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT . FLIGHT DECK, WINDSHIELD FRAMING, L/H R/H CONTINUITY FITTING CRACKED. CONTACT LIAISON ENGINEERING FOR FURTHER DISPOSITION. PERFORMEAug 6, 2026 · N352NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026080604536Skin · damagedIMPACT DAMAGE BETWEEN FR63-64 FROM S-39L TO S-42R. THE DAMAGE CONSISTS OF DENTS AND GOUGES TO THE SKIN PANEL. COMPLIED WITH ER/A 635883-14 PRI REV 0, ER/A 635883-14 PRI REV 1, ER/A 635883-14 PRI REV 2, ER/A 635883-14 PRI REV 3, ER/A 635883-14 PRI REV 4, ER/AAug 5, 2026 · N357NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2026080604535Stringer Splice · fomLEVEL 2 CORROSION, DISPLACE STGR 41R AND SPLICE SPLICE BETWEEN FR 60-63 AS REQUIRED TO FOM ON SKIN LAP CUTOUT. REMOVED AND REPLACED IAW SRM 51-42-11. CORROSION IS LEVEL 2, PART REPLACED. (LP: 1738901, AIRCRAFT WAS GROUNDED)Aug 4, 2026 · N357NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2026080604534Stringer · corrodedLEVEL 2 CORROSION, 2 DOUBLE FLUSH RIVETS AND CORROSION FOUND ON STGR 42R FWD OF FR 63 AND 64. R & R, IAW SRM 51-42-11-801. CORROSION FOUND TO BE LEVEL 2. REPLACED PART. (LP: 1738877, AIRCRAFT WAS GROUNDED)Aug 4, 2026 · N357NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2026080204455Shear Plate · corrodedLEVEL 2 CORROSION, UPPER FUSELAGE, AFT PAX CABIN, SHEAR PLATE CORRODED AT -Y1150 BETWEEN FR 69 TO FR 70. REPLACED SHEAR PLATE AT PAX CABIN -Y1150 BETWEEN FR 69 TO FR 70 IAW SRM 51-72-11-977-001, PARA 2, SRM REV 158.00, & AIRBUS REF DWG D53474180. (LP: 172925Jul 30, 2026 · N352NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026073004395Priority Valve · leakingHYD - DUE TO GREEN HYDRAULIC SYSTEM PRESSURE AND QUANTITY LOSS, HYD G RSVR LO LVL AND HYD G SYS LO PR. FOUND PRIORITY VALVE ON PTU LEAKING, REPLACED SAME. (LP: 8898723, AIRCRAFT WAS GROUNDED)Jul 29, 2026 · N372NW · Airbus A320212 · Hydraulic System, MainSDR DALA2026072804387Elec Connector · looseEXIT LIGHT AT 2R IS OUT. FOUND CONNECTOR LOOSE AT HARNESS 4026VB, RE-SECURED CONNECTOR IAW ESPM 20-44. OPS CHECK GOOD, IAW AMM 33-51. (LP: 8871680, AIRCRAFT WAS GROUNDED)Jul 25, 2026 · N335NW · Airbus A320212 · Light System WiringSDR DALA2026072804385Oxygen Mask · unwanted deployFWD LAV O2 MASK DEPLOYED IN FLIGHT. REPACKED OXYGEN MASK ASSY IAW AMM 35-21 PROCEDURES. OK FOR SVC. (LP: 9583816, AIRCRAFT WAS GROUNDED)Jul 24, 2026 · N336NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2026072804384Fitting · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPLACEMENT CENTER WINDOW FRAMES AND CONTINUITY FITTINGS PER ER/A 635072-14AD. SECTION I IS LIMITED TO 60000 TOTAL AIRCRAFT FLIGHT CYCLES. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE ASSJul 24, 2026 · N352NW · Airbus A320212 · Fuselage Main, StructureSDR 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 WJul 23, 2026 · N353NW · Airbus A320212 · Hydraulic System, MainSDR DALA2026072304308Blades · damagedBIRDSTRIKE NR 2 ENGINE SIGNIFICANT FAN BLADE DISTORTION. C/W AMM 05-51 BIRDSTRIKE INSPECTION, NO OTHER DAMAGE NOTED ON FUSELAGE. INSPECTED NR 2 ENG IAW AMM 72-00-00-200 -001-A. REMOVED BOROSCOPE PLUGS NR 1, 4, AND 8 IAW AMM 72-31 -00-290-001-A. REMOVED CRANJul 21, 2026 · N344NW · Airbus A320212 · Turbine Engine Compressor SectionSDR DALA2026072304302Alternator · detachedRETURNED TO DTW DUE TO LOSS OF NBR 2 ENGINE OIL QUANTITY AND PRESSURE. CREW SHUT ENGINE DOWN WHEN QUANTITY AND PRESSURE WENT TO ZERO. MTC FOUND ENGINE CONTROL ALTERNATOR DETACHED FROM AGB MOUNTING PAD. MAINTENANCE IN PROGRESS. (LP: 8844868. AIRCRAFT WAS GROUJul 21, 2026 · N361NW · Airbus A320212 · Accessory GearboxesSDR DALA2026072004244Sensor · out of adjustAIRCRAFT PULLS RT WHILE TAXIING BOTH RT BRAKES REACHED 550 AFTER BLOCK IN BUT LT BRAKES ONLY 230. JACKED RT GEAR OPERATED BRAKE PEDALS SET & RELEASED PARKING BRAKE WHEELS SPIN FREELY. CHECKED NOSE WHEEL ALIGNMENT IAW AMM 32-51-00. ALIGNMENT GOOD. PERFORMED BIJul 16, 2026 · N354NW · Airbus A320212 · Landing Gear Brake SystemSDR DALA2026072004241Frame · damagedSHIP 3252 DISC: NIV STEPS 6 AND 16 IF DAMAGE FOUND CONTACT ENGINEERING UPPER FUSELAGE PAX CABIN AT FR 20 RH DOUBLE JOGGLE AREA AT HOLES NR 5 AND 6 FOUND WITH BURR DAMAGE INDICATION AT FRAME LAYER. NOTE: PER MONITOR LOG PAGE 0252469 RELATED TO ER/A #550431-14ADJul 16, 2026 · N352NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2026071504158Sign · no testFOUND R1 DOOR LOWER EXIT SIGN INOP DURING SERVICE CHECK. FOUND LIGHT ASSY. DISCONNECTED. RECONNECTED LIGHT ASSY. OPS CHECK GOOD. IAW AMM 33-51. (LP: 9072518, AIRCRAFT WAS GROUNDED)Jul 14, 2026 · N359NW · Airbus A320212 · Emergency LightingSDR DALA2026071504153Fitting · corrodedLEVEL 2 CORROSION, FWD CARGO BAY, DOOR CUTOUT AT FR 24A & 25MM, DOOR SILL CORRODED. REPLACED CORNER FITTING AT FWD CARGO BAY DOOR CUT OUT FR 24A LOWER SILL AREA IAW SRM 51-72-11-911-001, REV 158.00 AND DRAWING D53231725. (LP: 1699971, AIRCRAFT WAS GROUNDED).Jul 14, 2026 · N352NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026071504150Door Sill · corrodedLEVEL 2 CORROSION, FWD CARGO COMPARTMENT DOOR CUTOUT AT FR 28 - 25MM, DOOR SILL WITH CORROSION. REPLACED CORNER FITTING AT FWD CARGO COMPARTMENT DOOR CUTOUT FR28 LOWER SILL AREA IAW SRM 51-72- 11-911-001 REV 158.00 AND REFERENCE DRAWING 532 31725. (LP: 169793Jul 13, 2026 · N352NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026071504157Oxygen Mask · unwanted deployFA REPORTED IN FLIGHT 2 02 MASKS DROPPED BY 2R DOOR. CONSULTED MCC AND OCC ELECTED TO CONTINUE TO DESTINATION. RESECURED 2R DOOR O2 GEN MASKS IAW AMM 35-21. (LP: 8871613, AIRCRAFT WAS GROUNDED).Jul 12, 2026 · N335NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2026071504156Light · detachedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED, HANGING ON BY THE WIRES. MOUNTING BRACKETS BROKEN, 26D AND 30D. REPLACED 26D AND 30D EEPLS LIGHTS REF A320 AMM 33-51. (LP: 1692939, AIRCRAFT WAS GROUNDED)Jul 10, 2026 · N375NC · Airbus A320212 · Emergency LightingSDR DALA2026071504155Brake · draggingAFTER LANDING WITH MINOR BRAKING, NR 1 BRAKE HEATED TO 520 WHILE ALL OTHER BRAKES REMAINED NORMAL (GREEN). 200 DEGREES DIFFERENCE NR 1 & NR 2. FOUND NR 1 BRAKE DRAGGING. REPLACED NR 1 BRAKE IAW AMM 32 -42. (LP: 9205971, AIRCRAFT WAS GROUNDED).Jul 9, 2026 · N373NW · Airbus A320212 · Landing Gear Brake SystemSDR DALA2026071304084Skin · scratchedFWD UPPER FUSELAGE AROUND PCS/TIMING ANTENNA CUTOUT AT FR29+ 195MM AND BETWEEN STRINGER 1L-1R SKIN PANEL WITH SCRATCH. C/A: PERFORMED FUSELAGE SKIN REPAIR BETWEEN FR 29 AND FR 30 AT STGR 1R IAW DELTA ER/A # 635410-14 REV: ORIGINAL DATED 03-JUL-26. NOTE: PERFORJul 9, 2026 · N352NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2026071304083Skin · nickedFWD FUSELAGE FR13+65MM AND 400MM ABOVE OF LEFT SIDE STRG SKIN PANEL WITH NICK. PERFORMED PERMANENT FUSELAGE SKIN REPAIR AT FWD FUSELAGE FROM FR 12 +238MM TO FR 13 +155MM, BETWEEN Z-520 AND Z-742 L/H SIDE I.A.W A320 SRM 53-11-11-300-041 PARAG 1 AND PARAG 2A FIJul 9, 2026 · N352NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2026071004045Fairing · missingRIGHT WING .5 ROOT FILLET FAIRING MISSING. DEFERRED RT ROOT FILLET FAIRING PER A320 CDL 53-00-03. M PROCEDURE C/W. PLACARD INSTALLED. (LP: 8820352, AIRCRAFT WAS GROUNDED)Jul 8, 2026 · N349NW · Airbus A320212 · Aerodynamic FairingsSDR DALA2026070904017Brake Assy · faultedBRAKES AUTO BRK FAULT BRAKE RELEASED ECAM ON LANDING. LEFT OUTSIDE MAIN TIRE BLOWN. R & R NR 1 TIRE AND WHEEL 32-41. MPN ON/OFF A319-A320M S/M OFF DL 6874 S/N ON DL6855.(909446) R/R #2 WHEEL AND TIRE ASSY IAW AMM 32-41. MPN ON/OFF A319-A320M S/N OFF DL6723 SNJul 8, 2026 · N366NW · Airbus A320212 · Landing Gear Brake SystemSDR DALA2026071304087Cover · missingLT WING INBD FLAP PIVOT COVER MISSING. INSTALLED LT WING INBD PIVOT COVER PER A320 AMM 57-54. (LP: 8498046, AIRCRAFT WAS GROUNDED)Jul 7, 2026 · N364NW · Airbus A320212 · Trailing Edge FlapsSDR DALA2026070803985Cover · dislodgedATB - DUE TO A LEFT AFT OVERWING EXIT OPEN MESSAGE. HANDLE COVER FOUND PARTIALLY DISLODGED. REINSTALLED THE EXIT HANDLE COVER FLAP. (LP: 9600128, AIRCRAFT WAS GROUNDED)Jul 7, 2026 · N354NW · Airbus A320212 · Emergency ExitsSDR DALA2026071304090Oxygen Mask · unwanted deployO2 MASKS DROPPED AT 10A-C. RESET O2 MASK COVER PER AMM 35-12. ACFT OK. FOR SERVICE. (LP: 8441468, AIRCRAFT WAS GROUNDED)Jul 6, 2026 · N341NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2026070803982Unknown · odorDIRTY SOCK ODOR ON APPROACH TO LANDING. PERFORMED INSPECTION OF NR 1, 2 & APU NO DEFECTS/LEAKS NOTED IAW AMM 79-00 & AMM 49-51. C/W LEVEL A CONTAMINATION W/C 2100-2007, W/C 0550-2001 & W/C 0550-2002, NO DEFECTS NOTED NO ODORS THROUGHOUT ENG RUNS NOTED. ACFTJul 6, 2026 · N356NW · Airbus A320212 · Air Distribution SystemSDR DALA2026070803981Compressor · crackedATB - DUE TO A LT WING BLEED LEAK MESSAGE, LT ENG BLEED FAULT, AND A LT PACK COMPRESSOR FAULT. FOUND RT ACM WITH A LARGE CRACK AT THE COMPRESSOR OUTLET BLOWING DIRECTLY ON OVERHEAT LOOPS OF THE LT WING. REPLACED RT ACM. (LP: 9589043, AIRCRAFT WAS GROUNDED)Jul 6, 2026 · N344NW · Airbus A320212 · Cabin Cooling SystemSDR DALA2026070603923Control Valve · leakingDIV, ON CLIMB OUT THROUGH 16,000', AIR R WING LEAK. COMPLETED ECAM ACTIONS AND FAULT NEVER CLEARED. T/S PER A320 TSM 36-22-00-810-802. UNDER PANEL 622AB FOUND PNEUMATIC LEAK OUTBOARD OF THE WING ANTI-ICE CONTROL VALVE. . RESECURED PANELS 192AB, 192FB, 192EB, 6Jul 5, 2026 · N360NW · Airbus A320212 · Pneumatic Distribution SystemSDR 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 DALA2026071004046Oxygen Box · openMASK COMPARTMENT OPENED OVER ROW 28DEF. INSPECTED ROW 28 DEF OXYGEN COMPARTMENT PER AMM 35-21, NO DEFECTS NOTED. PERFORMED MASK REPACKING IAW AMM 35-21. OK FOR SVC. (LP: 8640773, AIRCRAFT WAS GROUNDED)Jul 3, 2026 · N359NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2026070603921Repair · not reportedER/A 635410-14 PERFORMS A REPAIR AT FR29 & S-1 LH & RH PER SRM T ASK 53-21-11-300-087. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN THE SOONER OF 40000FC OR 80000FH FROM SECTION I AND EVERY SOONER OF 2900FC OR 5800FH THEREAFTER. ASSOCIATED ER/A 14-Jul 3, 2026 · N352NW · Airbus A320212 · Fuselage Structure (General)SDR DALA2026070603920Support Fitting · damagedER/A 635102-14AD ISSUED FOR REPAIR TO LH & RH LOWER LATERAL SUPPORT FITTINGS OF THE 80VU RACK. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 19500FC FROM SECTION I AND EVERY 1000F C THEREAFTER. ASSOCIATED AA 2515-01014 ADDED FOR AC 3252 ASSOCIATED EJul 3, 2026 · N352NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026070904011Seat Track · corrodedLEVEL 2 CORROSION, UPPER FUSELAGE, AFT PAX CABIN, LONGITUDINAL SEAT TRACK CORRODED AT Y1292, FR 66. REPLACED LONGITUDINAL FLOOR SEAT TRACK (ORIGINAL P/N: 14N00031- 101) AT Y1292 FROM FR64 TO FR 66 IAW A320 SRM TASK 51-72-11-911- 001 PARAG 2C AND INSTALLED IAWJul 2, 2026 · N352NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026070503909Seat Track · corrodedLEVEL 2 CORROSION, UPPER FUSELAGE, AFT PAX CABIN, LONGITUDINAL FLOOR SEAT TRACK CORRODED AT Y765, FR65. REPLACED LONGITUDINAL FLOOR SEAT TRACK (ORIGINAL P/N 14N00031- 1003) AT Y 765 FROM FR 64 TO FR 68 IAW A320 SRM TASK 51-72-11- 911-001 PARAG 2C, AND INSTALLJul 2, 2026 · N352NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026070503908Intercostal · corrodedLEVEL 2 CORROSION, LOWER FUSELAGE, FWD CARGO COMPARTMENT, FROM FR 27 & 28, ON STR 38 LH, INTERCOSTAL LOWER SECTION WITH CORROSION. REPLACED INTERCOSTAL AT FWD CARGO COMPARMENT FROM FR27 AND FR28, AT STR 38 LT IAW A320 SRM 51-72-11-911-001 REV 158.00 DATED 01 Jul 2, 2026 · N352NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026070203879Stringer · corrodedLEVEL 2 CORROSION, LOWER FUSELAGE,FWD CARGO COMPARTMENT,FROM FR 33 & 34,ON STR 38 RH,INTERCOSTALLOWER SECTION WITH CORROSION. REPLACED INTERCOSTAL AT FWD CARGO COMPARMENT, FROM FR33 AND FR34 , AT STR 38RH IAW SRM 51-72-11-911-001, REV 158.00 DATED 01 /JUN/26 Jul 1, 2026 · N352NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2026070103873Servo Valve · faultedDE - DUE TO BRAKES AUTO BRK FAULT ECAM WARNING. REPLACED NORMAL BRAKE SERVO VALVE (15GG) AND BSCU (10GG). (LP: 8749444, AIRCRAFT WAS GROUNDED).Jul 1, 2026 · N366NW · Airbus A320212 · Landing Gear Brake SystemSDR DALA2026070603919Light · brokenROW 15DEF EPL HOUSING BROKEN. R & R 15DEF EPL HOUSING REF AMM 33-51. (LP: 8879288, AIRCRAFT WAS GROUNDED)Jun 30, 2026 · N371NW · Airbus A320212 · Emergency LightingSDR DALA2026070103872Floor Support · corrodedLEVEL 2 CORROSION, UPPER FUSELAGE, AFT PAX CABIN, LONGITUDINAL FLOOR BEAM CORRODED AT -Y254 BETWEEN FR68 TO FR69. REPLACED LONGITUDINAL FLOOR BEAM AT -Y254 BTWN FR68 TO FR70 IAW A320 SRM TASK 51-72-11-911-001 PARAG C (1) , SRM 53-41-14-01A, FIG 301, ITEM 225.Jun 29, 2026 · N352NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026062703820Frame · damagedEXISTING REPAIR FR 68 INNER CAP & FLANGE STR22 RT AT LEVEL DOOR STOP FITTING 1. CONTACT DELTA LIAISON ENGINEERING FOR ALTE RNATE INSPECTION INSTRUCTIONS THAT MAY BE REQUIRED TO COMPLETE WORK CARD 5311-01244-02B DUE TO PREVIOUS REPAIR IN THE INSPECTION AREA. ADJun 24, 2026 · N360NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2026062503773Support · corrodedLH WING, OTBD FLAP, SUPPORT AT TRACK 3, RIB 5 AND TRACK 4, BETWEEN INNER RIB 14 AND OUTER RIB 14, WITH CORROSION INTERNAL STRUCTURE. FOR REMOVAL OF THE LH WING OUTBOARD FLAP S/N: D01703, SEE DELTA WORK CARD 2750-6020-LT. (LP: 1664687, AIRCRAFT WAS GROUNDED)Jun 24, 2026 · N352NW · Airbus A320212 · Trailing Edge FlapsSDR DALA2026062403745Floor Support · corrodedLEVEL 2 CORROSION, PPER FUSELAGE, AFT PAX CABIN, LONGITUDINAL FLOOR SUPPORT CORRODED AT Y1292, BETWEEN FR67 AND FR68. REPLACED LONGITUDINAL FLOOR SUPPORT AT UPPER FUSELAGE AFT PAX CABIN BETWEEN FR66 AND FR68 Y1292 IAW SRM 51-72-11-911-001 REV 158 AND DWG D53Jun 23, 2026 · N352NW · Airbus A320212 · Fuselage Miscellaneous Structure
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