Airbus A319-114

Service difficulty reports · 10,218

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'A319114'
  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 DALA2026070803984Unknown · odorFA'S ALERTED US OF DIRTY SOCK ODOR, ROWS 10-17. ODOR WENT AWAY INITIALLY WITH SMOKE/FUMES CHECKLIST. MX HAS US RESTORE VENTILATION ABOUT 30 MIN LATER ODOR CAME BACK AND WE COMPLIED WITH FUMES CHECKLIST. DEBRIEFED FLIGHT CREW AND ENSURED THE LOG IS ACCURATE. RJul 6, 2026 · N333NB · Airbus A319114 · Air Distribution SystemSDR DALA2026070904018Sleeve · damagedNR 3 AND 4 MLG AXLE SLEEVE DAMAGED. R & R NR 3 & 4 MLG AXLE ADAPTER SLEEVES PER AMM 32-42. OK FOR SVC. (LP: 8924695, AIRCRAFTT WAS GROUNDED)Jul 5, 2026 · N355NB · Airbus A319114 · Main Landing Gear Strut/Axle/TruckSDR DALA2026070603916Engine · no discrepancyATB, #2 ENG OVER LIMIT ON TAKEOFF. REMOVED CRANKPAD AND S17 BOROSCOPE PLUG ON NR 2 ENG PER A319 AMM 72-00. C/W OVERTEMP BSI ON #2 ENG PER A319 AMM 72-00 -00-200-003-A. NO DEFECTS NOTED. REINSTALLED CRANKPAD AND S17 BOROSCOPE PLUG ON #2 ENG PER A319 AMM 72-00.Jul 5, 2026 · N355NB · Airbus A319114 · Engine (Turbine/Turboprop)SDR DALA2026070503905Skin · dentedL1 LOWER FORWARD SKIN SECTION REQUIRES PERMANENT REPAIR DENT TYPE 1, ZONE 1, AREA 1, REPAIR SOLUTION PERMANENT WITHIN 8000FC. REFERENCE SRM 52-10-00-283-002 PAGE 17 007 DEF CHECK AIRCRAFT WAS GROUNDED.Jul 4, 2026 · N331NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2026071004044Fairing · missingENG 1 TOP OTBD LOCKOUT FAIRING MISSING. FWD TO CDL 78-00-11, M PROC C/W. REMOVED TOP OTBD THRUST REVERSER LOCKOUT FAIRING, PLACARDS INSTALLED, DISPATCH APPROVED, OK FOR SVC. INSTALLED NR 1 ENG TOP OTBD LOCKOUT FAIRING IAW AMM 78-30 -00. (LP: 8820078, AIRCRAJul 2, 2026 · N346NB · Airbus A319114 · Engine Thrust ReverserSDR DALA2026071304081Cover · missingLT WING 1 FLAP TRACK MOVEABLE FAIRING PIVOT COVER MISSING. FWD TO CDL 27-00-16. C/W "M" PROCEDURES. PLACARDS INSTALLED, MCC NOTIFIED. ACFT OK FOR SVC. RETAINER ALREADY INSTALLED. R & R FAIRING PIVOT COVER AS PER A319 AMM 57-55. OK TO CLOSE. (LP: 8199436, AIRCJul 1, 2026 · N348NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2026070503906Oxygen Box · openSHIP 3140 DISC: OXYGEN MASK COMPARTMENT OPENED UP ON LANDING IN FORWARD LAV. RESET O2 CONTAINER IN FWD LAV PER A319 AMM 35-21. OK FOR SERVICE. (LP: 8641230, AIRCRAFT WAS GROUNDED)Jul 1, 2026 · N340NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2026070803983Latch · missing11DEF PASSENGER OXYGEN STORAGE, FOUND FWD LATCH FOR O2 GENERATOR PANEL MISSING. FWD TO MEL 35-21 -01A. -M- PROCEDURES C/W. WILL NEED LATCH. REPLACED PASSENGER SERVICE UNIT AT ROW 11DEF IAW AMM 25-25. OPS CHKD GOOD. M PROCEDURE REVERSED. MEL AND PLACARD REMOJun 30, 2026 · N335NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2026070603918Wire · disconnectedDURING SVC CHECK FOUND L2 DOOR EMER LIGHT INOP. REMOVED LIGHT AND FOUND WIRING TO CONNECTOR HAD DISCONNECTED FROM LIGHT. RECONNECTED AND TESTED REF A319 AMM 33-50. OPS CHECK GOOD OK FOR SVC. (LP: 8477148, AIRCRAFT WAS GROUNDED)Jun 30, 2026 · N317NB · Airbus A319114 · Light System WiringSDR DALA2026070103871Computer · faultyREJECTED TAKE OFF AT LOW SPEED BELOW 50 KNOTS DUE TO FLIGHT CONTROL CAUTION MSG. BITE TEST SFCC 1 FAULTS SLTS SFCC 1. R & R IAW TSM 27-51 AND AMM 27-51 BITE TEST NO FAULTS NOTED RESET SYS IAW AMM 27-51 NO FAULTS NOTED OK FOR SVC. (LP: 8651838, AIRCRAFT WAS Jun 30, 2026 · N357NB · Airbus A319114 · Flight Management Computing Hardware SystemSDR DALA2026070603917Cover · missingLEFT WING #2 FAIRING I/B COVER MISSING. DEFERRED #2 FAIRING PIVOT COVER PER CDL 27-00-16 PLACARD INSTALLED A/C OK FOR SERVICE M PROCEDURE C/W. INSTALLED I/B COVER ON THE #2 FLAP FAIRING PER A319 AMM 27-54. THIS CLOSES CDL 27-00-16. A/C OK FOR SVC. PLACARD REMJun 28, 2026 · N348NB · Airbus A319114 · Wing Miscellaneous StructureSDR DALA2026070103870Unknown · odorON TAXI OUT IN EYW, ENGINES RUNNING, APU BLEED ON, SULFUR ODOR THROUGH OUT CABIN. PILOTS MASK USED RETURNED TO GATE. PERFORMED INSPECTION OF ENGINES 1 AND 2 INLETS NO OIL FOUND AS WELL AS APU INLET AND SURROUNDING AREA. WITH SULFUR SMELL REPORTED AND SEAWEED Jun 28, 2026 · N370NB · Airbus A319114 · Air Distribution SystemSDR DALA2026070103869Drain Mast · missingNR 2 ENGINE ARRIVED WITH DRAIN MAST MISSING. INSTALLED NR 2 ENGINE DRAIN MAST IAW AMM 71-71-42. (LP: 8906834, AIRCRAFT WAS GROUNDED)Jun 25, 2026 · N360NB · Airbus A319114 · Engine (Turbine/Turboprop)SDR DALA2026062703819Oxygen Mask · damagedSCRATCHED CREW OXYGEN MASK OBSERVER POSITION ON COCKPIT. REMOVED CREW OXYGEN MASK POSITION 3RD OCCUPANT ON COCKPIT ON UNSERVICEABLE CONDITION IAW AMM 35-12-41-000-002A STEP 4. . REPLACED CREW OXYGEN MASK OBSERVER POSITION ON COCKPIT IAW FAM AMM 35-12-41-000Jun 24, 2026 · N369NB · Airbus A319114 · Crew Oxygen SystemSDR DALA2026062503772O-Ring · leakingEMERGENCY DECLARED, Y HYD RESERVOIR LEVEL CONTINUALLY DECREASES IN FLIGHT. HYD Y RSVR LO LVL ECAM DISPLAYED. MSI / ODI EVENT. FOUND BAD O-RING ON YELLOW SYSTEM SIDE OF PTU MANIFOLD, FIN 3015GM. R/R O-RING PER A-319 AMM 20-20. LEAK CHECK OK. C/W A-319 AMM 29-0Jun 24, 2026 · N301NB · Airbus A319114 · Hydraulic System, MainSDR DALA2026062403743Secu · faultedDIV TO BOS DUE TO F/CTL SEC 3 FAULT. REPLACED SEC 3 AND RELAY 41CE3. (LP: 8320072, AIRCRAFT WAS GROUNDED)Jun 24, 2026 · N336NB · Airbus A319114 · Flight Control SystemSDR DALA2026062403744Unknown · odorUPON REACHING CRUISE ALTITUDE FL360 RECEIVED CALL FROM FWD. FA ( S) VERY STRONG (C) FORWARD CABIN (E) NO PHYSICAL EFFECTS (N) DIRTY SOCK SMELL (T) LASTED FROM INITIAL CLIMB, COMPLETED QRH SMOKE/FUMES/AVNCS SMOKE WITH AIR COND SMOKE/FUMES SUSPENDED. AFTER CAB FJun 23, 2026 · N339NB · Airbus A319114 · Air Distribution SystemSDR DALA2026062503771Brake Assy · overheatedRIGHT SIDE LEFT INBOARD BRAKE TEMP 470 / 295 LEFT SIDE INBD & OTBD BRAKES 290/320. THIS OCCURRED ON LANDING BUT DURING TAKEOFF BRAKES TEMPS SHOW A VAST DIFFERENCE BETWEEN INBOARD AND OUTBOARD. INSP NBR 3 MLG BRAKE FOUND DRAGGING. REPLACED SAME PAR A319 AMM 3Jun 20, 2026 · N341NB · Airbus A319114 · Landing Gear Brake SystemSDR DALA2026062203691Light · unknownEMERGENCY LIGHTS IN CABIN COME ON WHEN ENG ANTI ICE IS TURNED ON. IT HAPPENED EVERY TIME THE ANTI -ICE SWITCHES WERE CYCLED IN FLIGHT. PERFORMED EMERGENCY LIGHTING TEST IAW TSM 33-52-00-810-881A . TEST PASSED. PERFORMED OPS CHECK OF ENG ICE PROTECTION SYSTEMJun 19, 2026 · N359NB · Airbus A319114 · Emergency LightingSDR DALA2026062203690Slide · unserviceableWHILE WORKING SLIDE CHANGE AT FWD L/H DOOR NEW SLIDE WAS FOUND TO BE UNSERVICEABLE. REMOVED AND REINSTALLED ORIGINAL SLIDE PER AMDS TASK CARD 2561- 4003-LF. RII COMPLETE. (LP: 8851540, AIRCRAFT WAS GROUNDED).Jun 19, 2026 · N322NB · Airbus A319114 · Escape SlideSDR DALA2026062103687Stiffener · unsecureDURING M2 AND WHILE INSPECTING PER 5316-01052-05B THE HORIZONTAL STIFFENER OF LATERAL WINDOW FR4 RHS WAS FOUND COMPLETELY REMOVED DUE TO PREVIOUS REWORK PER THIS ER/A ORIGINAL REVISION. PER SECTION IV OF 573692-14 REV B, ACCOMPLISH SECTION IV REPETITIVE INSPEJun 17, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026061503569Unknown · odorSULFUR ODOR IN COCKPIT AND CABIN ON TAXI OUT. PERFORMED LEVEL A DECONTAMINATION PER AMM 21-00-00. NO FURTHER SMELLS NOTED. OK FOR SERVICE. (LP: 9073650, AIRCRAFT WAS GROUNDED)Jun 14, 2026 · N314NB · Airbus A319114 · Air Distribution SystemSDR DALA2026062003683Light · damagedEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. AISLE LIGHT HANGING FROM SEAT. RE-SECURED 21D LIGHT ASSY, ALL OPS NORMAL. (LP: 1645205, AIRCRAFT WAS GROUNDED)Jun 13, 2026 · N331NB · Airbus A319114 · Emergency LightingSDR DALA2026061503564Computer · faultedBOTH ENGINES RUNNING, REJECTED TAKEOFF DUE TO ELAC 1 PITCH FAULT MESSAGE AT 10 KNOTS. DUE TO HISTORY - APPLING ELAC 1 TO MEL & PLAC PER A319/320/321 MEL 27-93-01. M PROC C/W, MCC NOTIFIED. (LP: 8778668, AIRCRAFT WAS GROUNDED)Jun 13, 2026 · N353NB · Airbus A319114 · Flight Control SystemSDR DALA2026061503563Unknown · odorFA REPORTED STRONG ELECTRICAL BURNING ODOR NEAR AFT GALLEY JUST AFTER STARTING BOTH ENGINES. ODOR DISSIPATED 5-10 MIN LATER. NO VISIBLE SMOKE OBSERVED. RETURNED TO GATE. INSPECTED COFFE MAKERS IN AFT GALLEY. NO DEFECTS NOTED. CHECKED AFT LAVS AND NO DEFECTS NOJun 12, 2026 · N355NB · Airbus A319114 · Air Distribution SystemSDR DALA2026062003684Psu · broken29ABC OXYGEN PANEL MASKS DEPLOYED, DROPPED ON THEIR OWN DURING SERVICE. MOVED TO MEL 35-21-01A, PLAC & MEL INSTALLED, M PROC C/W. SECURED PSU PANEL AND O2 MASKS REF A319 AMM 35-20. OPS CHK NML. PLACARD REMOVED. "M" PROC REV. (LP: 1642084, AIRCRAFT WAS GROUNDEJun 11, 2026 · N314NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2026061503562Access Panel · corrodedLEVEL 2 CORROSION, NR 2 ENGINE, RT UPPER PYLON, ACCESS PANEL 424CR WITH CORROSION. REPAIRED EXTERNAL SKIN IN ACCESS PANEL 424CR, ENGINE NR 2 RT UPPER PYLON AREA IAW SRM 54-52-11-300-003 PARAG 2.A FIG 001, REV 158. THIS REPAIR IS CATEGORY A WITH NO ADDITIONAL Jun 11, 2026 · N340NB · Airbus A319114 · Nacelle/Pylon, Plate/SkinSDR DALA2026061103521Wire Harness · damagedDECLARED EMERGENCY DUE TO A LANDING GEAR DISAGREE MESSAGE AFTER GEAR EXTENSION FOR APPROACH. GEAR DOORS STAYED OPEN DUE TO A RT DOWN LOCK 14GA PROX SENSOR FAULT. ALL NORMAL AFTER SECOND GEAR EXTENSION. CORRECTIVE ACTION: FOUND SENSOR HARNESS STUCK BETWEEN SENSJun 10, 2026 · N343NB · Airbus A319114 · Landing Gear System WiringSDR DALA2026061103520Control Valve · contaminatedFO SMELLED WET SOCK SMELL ON TAXI - IN WHEN SWITCHING TO APU BLEED. SMELLED IN FLIGHT DECK ONLY NOT IN CABIN. REMOVED LOAD CTL VLV PER A319 AMM 49-51 INSP FOUND OIL CONTAMINATE. CLEANED AND REINSTALLED (KH 384158) PERFORMED LEVEL B DECONTAMINATION WITH REF TOJun 9, 2026 · N346NB · Airbus A319114 · APU Oil SystemSDR DALA2026061103519Fitting · not reportedPERFORM ER/A 633646-14AD FOR REPLACEMENT OF CONTINUITY FITTINGS LH AND RH. COMPLIED WITH ER/A 633646-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF ER/A 633646-14AD PRI REV 0 AND PRI REV 1 IT IS BEENVALIDATED. PERFORMED REPAIR INSTRUCTIONS ON CONTINUITY FITTINGSJun 9, 2026 · N366NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026060903445Window Frame · crackedCRACK INDICATION FOUND ON CENTER POST UPPER TENSION BOLT LH AREA AT 1 OCLOCK, CRACK LENGTH 0.125 IN APPROX AND RH AREA AT 11 OCLOCK, CRACK L ENGTH 0.187 IN APPROX LOOKING INBOARD.MORE OVER CRACK INDICATION FOUN D ON CENTER POST LOWER CORNER LH. CRACK LENGT 0.3Jun 6, 2026 · N366NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026060903444Stringer · corrodedCORROSION STRINGER 38RH FROM FR59 TO FR60 IN AFT CARGO COMPARTMENT (SS I: 534150). REPLACED STRINGER SECTION 38RH BTW FR 59 TO FR 63 IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DRAWING E53476330 ISSUE AD, RELEASE DATE 11/JUL/18, MJun 6, 2026 · N369NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2026060503397Unknown · odorPASSANGERS IN 15 D AND 15E REPORTED OCCASIONAL WHIFS OF BURNING OIL SMELL THAT THEY REPORTED AT TOP OF DESCENT TO THE FLIGHT ATTENDANT. I SPOKE TO THE PASSANGERS AND THEY SAID THEY HAD NO ILLNESS SYMPTOMS AND CONFIRMED INTERMITTANT WHIFFS. INSPECTED PSU PANELJun 1, 2026 · N357NB · Airbus A319114 · Air Distribution SystemSDR DALA2026060503396Oxygen Mask · deployedOXYGEN MASKS OVER 17 A,B,C NEED TO BE RESTOWED. FOUND 17 ABC O2 GENERATOR PIN PULLED AND DEPLETED. R & R O2 GENERATOR AND STOWED MASKS PER AMM 35-21. (LP: 8925703, AIRCRAFT WAS GROUNDED)Jun 1, 2026 · N301NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2026060503395Fitting · not reportedER/A 633553-14AD HAS BEEN ISSUED FOR WINDSHIELD CENTER POST MIRR OR FITTING REPAIR. FOLLOW ON ACTION IS REQUIRED. SECTION I IS LIMITED TO 17700FC FROM SECTION I WHICH IS APPROVED AS CATEGORY 'C'. SECTION II IS TBD AT THIS TIME NEEDING ADDITI ONAL EVALUATION FOJun 1, 2026 · N366NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026060503394Fitting · not reportedER/A 633646-14AD ISSUE FOR WINDSHIELD CENTER POST CONTINUITY FIT TING REPLACEMENT. FOLLOW ON ACTION IS REQUIRED. SECTION I IS LIMITED TO 17700FC FROM SECTION I. SECTION II IS TB D AT THIS TIME AS ORIGINAL APPROVAL IS CATEGORY 'C'. ASSOCIATED ER/A 14-633646 ADJun 1, 2026 · N366NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026053103284Fitting · corrodedLEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001. TOOK MEASURE INITIAL CORROSION SPIGOT FITTINGWAS: P1: L:2.418 INCH, P2: L: 2.872 INCH, SEE INDIVIDUAL SIGN OFFMay 30, 2026 · N369NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2026053103283Fitting · corrodedLEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER A319 SRM 54-51-12-300-001. TOOK MEASURE INITIAL ON CORROSION SPIGOT FITTING RECEPTACLE WAS: P1: L:3.058 INCH, P2: L: 1.602 INCH. SEE INDIMay 30, 2026 · N369NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2026053103305Transponder · failedATC REPORTED INTERMITTENT MODE C. ALTITUDE REPORTING FAILURES IN ROUTE. ATC TRANSPONDER/AUTOMATIC ALTITUDE REPORT SYS AND A/C VACATED RVSM AIRSPACE. USE FLT AWARE TO VERIFY DATA GAPS FOR THIS FLIGHT. C/A: R/R ATC TRANSPONDER 1 +2 IAW A319 AMM 34-52 BITE TEST PMay 28, 2026 · N370NB · Airbus A319114 · ATC Transponder SystemSDR DALA2026053103304Idg · faultedON APPRAOCH IDG 1 REACHED 147 AND WAS FLASHING GREEN. TEMPERATURE COOLED BACK DOWN GRADUALLY AND WAS BACK TO NORMAL TEMP AFTER LANDING. T/S PER TSM 24-20. FOUND IDG 1 OVER SERVICED, PROPERLY SERVICED IDG 1 IAW A319 AMM 12-13 RAN ENGINE & PERFORMED OP CK, FOUNMay 28, 2026 · N354NB · Airbus A319114 · AC Generator-AlternatorSDR DALA2026053003281Power Supply · faultedEMERGENCY EXIT SIGNS INOPERATIVE. THE EXIT SIGNS ABOVE DOORS 2L AND 2R DO NOT ILLUMINATE WHEN THE GEAR IS DOWN, INSTEAD THE SMALL EMERGENCY LIGHTS BETWEEN THE EXIT SIGN AND DOOR COME ON. R & R EPSU AND EPSU POWER SUPPLY REF A319/320 AMM 33-51. FAULT STILL PREMay 27, 2026 · N325NB · Airbus A319114 · Emergency LightingSDR DALA2026052903250Warning Message · illuminatedREJECTED TAKEOFF AT APPROX.30 KTS DUE TO A COMMUNICATION ECAM. (F/O'S PTT SWITCH.) MAINTENANCE IN PROGRESS. (LP: 1616037) AIRCRAFT WAS GROUNDEDMay 27, 2026 · N355NB · Airbus A319114 · Communications SystemSDR DALA2026052803231Window Frame · brokenDURING THE M2 CHECK (D CHECK) AT COO (SJO), AND WHILE EXECUTING A DELTA TASK CARD INSTRUCTIONS RELATED TO SB A320-53-1331 R01 AND AD 2020-17-03, THE LT CONTINUITY FITTING AND WINDSHIELD FRAMING WITH CRACK WERE FOUND. CORRECTIVE ACTION: PERFORMED WINDSHIELD FRAMay 27, 2026 · N368NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2026052703189Seat Track · corrodedLEVEL 2 CORROSION, CORROSION SEAT TRACK -Y1292 LOC. FR 64 TO FR 66 AT AFT GALLEY AREA (SSI:534147). REPLACED SEAT TRACK -Y1292 AND FASTENERS LOC. BETWEEN FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AS PER A319 SRM51-72-11 AND DWG 10N01048 ISSUE:AMay 27, 2026 · N369NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026052703186Floor Support · corrodedSHIP 3168 DISC: LEVEL 2 CORROSION, TASK 5310-3040, CORROSION SSI: 531189, CPCP TASK 2021-2001. FWD PASSENGER CABIN BETWEEN FR 16-20, Y 254, FLOOR BEAM WITH CORROSION. REPLACED FLOOR BEAM P/N: D5311281820401 BETWEEN FR12 AND FR24, Y254 IAW A319 SRM 53-11-14-08May 26, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026052703185Seat Track · corrodedPAX CABIN AFT SECTION FLOOR STRUCTURE, BETWEEN FR64 AND FR66 AT Y-765 SEAT TRACK WITH CORROSION IN SEVERAL PLACES. C/A: REPLACED SEAT TRACK AT PAX CABIN BETWEEN FR64 AND FR66, Y-765 IAW ER/A #633966-14 REV ORIGINAL DATED 19/MAY/26, NAT DWG #14N00031 REV E AND May 25, 2026 · N368NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026052703184Flap Track · excess playLEVEL 2 CORROSION, LH WING I/B FLAP TRACK NR 2 SUPPORT ECCENTRICAL BEARING WITH PLAY. REPAIRED LT WING I/B FLAP TRACK NR 2 SUPPORT I/B AND OTBD FITTING FACES AND AL BORE HOLES IAW DELTA ERA 633957-14 REV ORIGINAL APPROVED DATE 19/MAY/26. THIS REPAIR APPROVAL May 25, 2026 · N368NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2026052703183Shear Plate · corrodedLEVEL 2 CORROSION, SHEAR PLATE STR 23 R LOC. FR 69 TO FR 70 AT AFT GALLEY AREA. APPLIED PROTECTIVE TREATMENT IN NEW HOLES ON SHEAR PLATE IAW SRM 51-21-11,.AND REPLACED SHEAR PLATE LOCATED BTW FR69 TO FR70 AT LEVEL STR23R AT AFT GALLEY AREA IAW SRM 51-42 -11, May 25, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026052703182Fitting · corrodedLEVEL 2 CORROSION, CORROSION CENTER FITTING FR 66 TO FR 68 RH SIDE AT AFT GALLEY AREA ( SSI:534147). REPLACED CENTER FITTING LOCATED FR 66 TO FR 68 RH SIDE AT AFT GALLEY AREA. INITIAL MEASURE OF CORROSION WAS: L:0.4930 IN W: 0.2075 IN D:0.040 IN AS PER A319 SMay 24, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026052703181Seat Track · corrodedLEVEL 2 CORROSION, CORROSION SEAT TRACK -Y765 LOC. FR 12 TO FR 24 AT FWD GALLEY AREA (SSI : 531189). REPLACED SEAT TRACK -Y765 LOC. FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 A319 SRM 51-42-11 DWG D53112812 ISSUE: E00 RELEASE DATE: 22-MAR-06 DMay 24, 2026 · N369NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
Back to Airbus A319-114