# Service difficulty reports: Airbus A319-114

A list on [Airbus A319-114](https://openairdocs.org/model/airbus-a319-114.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 205 · 10,210 reports

- [SDR DALA2026102605859](https://openairdocs.org/sdr/DALA2026102605859.md): Engine · vibration · Oct 25, 2026 · N314NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > DECLARED AN EMERGENCY AND DIVERTED TO BWI DUE TO RIGHT ENGINE HIGH VIBRATION. INSPECTION PERFORMED BORESCOPE OF LPT WITH NO FINDINGS. PERFORMED FAN LUBE AND FAN TRIM BALANCE. COMPLETED WORK CARD 0550-2004. (LP: 9454672, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026102605860](https://openairdocs.org/sdr/DALA2026102605860.md): Proximity Switch · faulty · Oct 23, 2026 · N358NB · Airbus A319114 · Door Warning System
  > ATB TO ATL, DUE TO AFT CARGO DOOR ECAM MESSAGE. DOOR AFT CARGO IN FLIGHT SHOWED OPEN. FWD TO MCO/PLAC PER MEL 52-70-01K. M PROCESS C/W. T/S PER A319 TSM 32-31-00-810-886-A, PERFORMED OPS TEST OF AFT CARGO DOOR PER AMM 52-32-00-710-001, NO FAULTS FOUND. REMOVE
- [SDR DALA2026102605849](https://openairdocs.org/sdr/DALA2026102605849.md): Proximity Sensor · faulted · Oct 22, 2026 · N302NB · Airbus A319114 · Landing Gear Position and Warning
  > LANDING GEAR NOT UP AND LOCKED MSG ON ECAM AFTER TAKEOFF. FOLLOWED ECAM PROCEDURE TO REMAIN BELOW 220 KTS LOWERED & RAISED MLG LEVER THEN RETRACTED NORMALLY. FIRST TIME IT SEEMED THE WHEELS WERE UP BUT DOORS WERE OPEN. DUE TO NLG PROX SENSOR (24GA) FAULT REPL
- [SDR DALA2026102305834](https://openairdocs.org/sdr/DALA2026102305834.md): Light · inoperative · Oct 21, 2026 · N330NB · Airbus A319114 · Emergency Lighting
  > DURING SVC FOUND ONE FLOOR PROXIMITY LIGHT INOP. REQUIRES FURTHER TROUBLESHOOTING. FWD TO MEL PLACARD INSTALLED, NO "M" PROCEDURES. OK FOR SERVICE. RESEATED FLOOR PROXIMITY LIGHT AT SEAT 14DEF. OK FOR SVC PER A319 AMM 33-51. MEL AND PLACARD REMOVED. (LP: 9485
- [SDR DALA2026102205809](https://openairdocs.org/sdr/DALA2026102205809.md): Unknown · odor · Oct 21, 2026 · N369NB · Airbus A319114 · Air Distribution System
  > DECLARED AN EMERGENCY DUE TO DIRTY SOCK ODOR IN FWD CABIN. NO TROUBLE FOUND. LEVEL B DECONTAMINATION BEING PERFORMED. MAINTENANCE STILL IN PROGRESS. (LP: 9203806, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026102005761](https://openairdocs.org/sdr/DALA2026102005761.md): Unknown · odor · Oct 20, 2026 · N369NB · Airbus A319114 · Air Distribution System
  > FUME EVENT AT 23,000 FT DESCENDING- DIRTY SOCK ODOR IN COCKPIT. CALLED CABIN, FA SAID NO SMELL. FA'S CALLED AT 14,000FT AND CONFIRMED DIRTY SOCK. RAN EQRH FUMES, FUMES DISSIPATED AT 10,000 W/ VENTILATION OVRD. C/A: PERFORMED WALKAROUND OF A/C, FOUND NO EVIDENC
- [SDR DALA2026102005760](https://openairdocs.org/sdr/DALA2026102005760.md): Fan · failed · Oct 20, 2026 · N348NB · Airbus A319114 · Air Distribution Fan
  > IN DESCENT OUT OF FL330 GOT BURNING ELECTRICAL AND RUBBER ODOR THROUGHT ACFT. AMBER FAN ON CONDITION PAGE. REMOVED CABIN RECIREULATION FAN 15HG PER AMM 21-21-51. WATTING ON NEW FAN FOR NOW. BEFORE RECIRC FAN REMOVAL PERFORMED TEST AND SMELLED ELECTRICAL ODER
- [SDR DALA2026102605850](https://openairdocs.org/sdr/DALA2026102605850.md): Amu · inoperative · Oct 19, 2026 · N335NB · Airbus A319114 · Crew Oxygen System
  > CREW REPORTS F/O'S O2 MASK MIC IS INOP. T/S IAW TSM 23-51, REPLACED AMU PERFORMED OP CK, OK FOR SVC. (LP: 9100196, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026101405630](https://openairdocs.org/sdr/DALA2026101405630.md): Brake Assy · overheated · Oct 13, 2026 · N314NB · Airbus A319114 · Landing Gear Brake System
  > ABORTED TAKE OFF AT 80 KTS, DUE TO HOT BRAKES ECAM, ON THE RIGHT (3,4) SIDE, TEMP THROUGH 600 C QUICKLY BEFORE LEAVING RUNWAY. R & R NR 3 & 4 BRAKE ASSY IAW AMM 32-42. NO FURTHER DAMAGE NOTED. OK FOR SVC. (LP: 9459622, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026102605848](https://openairdocs.org/sdr/DALA2026102605848.md): Oxygen Mask · no test · Oct 12, 2026 · N363NB · Airbus A319114 · Crew Oxygen System
  > CA SIDE OXYGEN MASK FAILED TEST. FREE FLOWING AIR. NOT ABLE TO SHUT OFF / SELECTED CREW SUPPLY OFF TO STOP AIR FLOW. REMOVED AND REPLACED CA O2 MASK REF A319 AMM 35-12. OP CHECK NORMAL. NO LEAKS NOTED. RFID INDUCTION C/W. (LP: 9478930, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026101005578](https://openairdocs.org/sdr/DALA2026101005578.md): Engine · bird ingestion · Oct 8, 2026 · N353NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > ON T/O ROLL POSSIBLE BIRD INGESTION ON RT ENGINE. HIGH VIBRATION MESSAGE ON ROTATION & CLIMB. N1 AS HIGH AS 9.0 IN CRUISE N1 VIB AROUND 5.2. PERFORM BIRD STRIKE INSPECTION IAW AMM 72-00-00-200-001-001-A. FOUND NR 2 ENGINE WITH FAN BLADE DAMAGE. INSTALLED PE
- [SDR DALA2026100705552](https://openairdocs.org/sdr/DALA2026100705552.md): Landing Gear · faulted · Oct 5, 2026 · N355NB · Airbus A319114 · Landing Gear Retraction/Extension System
  > ATB - DUE TO LANDING GEAR NOT RETRACTING, L/G SHOCK ABSORBER FAULT, L/G GEAR NOT UPLOCKED, AND L/G DOORS NOT CLOSED ECAM WARNINGS. MAINTENANCE STILL IN PROGRESS. (LP: 9539601, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100305476](https://openairdocs.org/sdr/DALA2026100305476.md): Transmission · faulted · Oct 2, 2026 · N319NB · Airbus A319114 · Trailing Edge Flap Control System
  > DIV - TO AUS DUE TO F/CTL FLAPS FAULT. WTB RESET AND INSPECTED FLAP TRANSMISSION, NO TROUBLE FOUND. (LP: 9499366, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026102005759](https://openairdocs.org/sdr/DALA2026102005759.md): Skin · dented · Oct 1, 2026 · N325NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > ER/A 633023-14 REV A: UPPER REAR FUSELAGE SKIN WITH DENT AT FR55 470MM, STRG 6/7LT. SUBJECT REQUIRES FOLLOW ON ACTIONS. ACCOMPLISH SEC. II WITHIN 33,700 FLIGHT HOURS OR 16,800 FLIGHT CYCLES THRESHOLD (WITHIN AIRCRAFT TOTAL TIME OF 93,219 FH OR 47,634 FC) FRO
- [SDR DALA2026100705551](https://openairdocs.org/sdr/DALA2026100705551.md): Dampener · leaking · Oct 1, 2026 · N317NB · Airbus A319114 · Passenger/Crew Doors
  > R1 DOOR DAMPNER NOT HOLDING CHARGE. REMOVED DOOR DAMPNER IAW AMM 52-11-14-000-001-B. INSTALLED A REPLACEMENT DOOR DAMPNER IAW AMM 52-11-14-400-001-B. REF IPC 52-13-04-01B ALL RII TASKS COMPLIED. (LP: 9608069, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100105457](https://openairdocs.org/sdr/DALA2026100105457.md): Light · missing · Sep 29, 2026 · N361NB · Airbus A319114 · Emergency Lighting
  > DURING CAV FOUND FLOOR PROZIMITY EMERGENCY ESCAPE PATH MARKING LIGHT LENS MISSING NEXT TO CLOSET 302. FWD TO MEL 33-50-03A. MEL PLACARD INSTALLED. MEL REMARKS C/W. NO "M" PROCEDURES. CONTACTED MCC. REQURES MPN BR9471-11 STOCK # 33-3300-3-0127. REF CMM 25-31-9
- [SDR DALA2026100105456](https://openairdocs.org/sdr/DALA2026100105456.md): Oxygen Box · leaking · Sep 28, 2026 · N345NB · Airbus A319114 · Crew Oxygen System
  > WORKING CREW O2 LEAK MSG. FO MASK BOX LEAKING. R & R MASK STOWING BOX PER AMM 35-12. NO LEAKS NOTED AT THIS TIME. OK SVC. R/R MASK PER AMM 35-12. NO LEAKS NOTED OK SVC. (LP: 6797929, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100405477](https://openairdocs.org/sdr/DALA2026100405477.md): Oxygen Mask · leaking · Sep 27, 2026 · N345NB · Airbus A319114 · Crew Oxygen System
  > SUSPECTED CREW 02 LEAK. CA MASK AND BOX REPLACED. C/A: REFER TO LOG 6797929 FOR CORRECTIVE ACTION, OK TO CLOSE LOG. (LP: 1835948, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092705360](https://openairdocs.org/sdr/DALA2026092705360.md): Unknown · odor · Sep 27, 2026 · N370NB · Airbus A319114 · Air Distribution System
  > UNUSUAL ODOR REPORTED BY FLIGHT ATTENDANT & CAPTAIN BEFORE BOARDING. SEEMED TO SUBSIDE, CALLED MAINT, NOTHING DESCOVERED. PUSHED BACK & STARTED ENGINES, NOW SMELLED AGAIN BY MULTIPLE CREW MEMBERS. SMELLED IS LIKE BURNING PLASTIC. DETERMINED TO BE TYPE 9 OD
- [SDR DALA2026092705362](https://openairdocs.org/sdr/DALA2026092705362.md): Windshield · out of tolerance · Sep 26, 2026 · N331NB · Airbus A319114 · Windshield/Door Rain/Ice Removal
  > DIVERTED DUE TO, DURING CLIMB, ANTI-ICE WINDSHIELD CAUTION APPEARED. ATTEMPTED RESET BUT CAUTION MESSAGE REMAINED. TROUBLESHOT IAW TSM 30-42-00-810-803-A. FOUND LT WINDSHIELD AT 362 K OHMS. R & R LEFT WINDSHIELD IAW AMM 56-11. WHC BITE & WINDOW HEAT OPS NOR
- [SDR DALA2026092805367](https://openairdocs.org/sdr/DALA2026092805367.md): Oxygen Panel · unsecure · Sep 25, 2026 · N327NB · Airbus A319114 · Passenger Oxygen System
  > SEATS 10E, 10D, & 10F OXYGEN PANEL CAME LOOSE DURING TAKE OFF. SECURED THE PANEL. NOW CHKD GOOD. (LP: 1831789, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092705361](https://openairdocs.org/sdr/DALA2026092705361.md): Unknown · odor · Sep 25, 2026 · N348NB · Airbus A319114 · Air Distribution System
  > FLIGHT ATTENDANTS SMELLED STRONG DIRTY SOCK FUME ODOR DURING CLIMB OUT. FRP,10K FEET TO 32K FEET. SCENT WENT AWAY BY OP OF CLIMB. NO SYMPTOMS. MCC AND DISPATCH NOTIFIED. PERFORMED VISUAL INSPECTION OF APU INLET. NO CONTAMINATION FOUND. RAN BOTH ENGINES, PAC
- [SDR DALA2026092705359](https://openairdocs.org/sdr/DALA2026092705359.md): Lanyard · misinstalled · Sep 25, 2026 · N343NB · Airbus A319114 · Emergency Equipment
  > ALL FOUR CABIN DOORS (L1, R1, L2, R2) SURVIVAL KIT ATTACH LANYARDS INSTALLED BACKWARDS. C/A: REINSTALLED ATTACH LANYARD UPRIGHT & "LANYARD" NOW VISIBLE. REF A319 SVC CK. (LP: 8900283, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092705363](https://openairdocs.org/sdr/DALA2026092705363.md): Unknown · missing · Sep 24, 2026 · N332NB · Airbus A319114 · Emergency Equipment
  > F/A REPORTED UPK MISSING. DEFERRED PER NEF 25-20-13. (LP: 9333435, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092405333](https://openairdocs.org/sdr/DALA2026092405333.md): Autobrake Sys · faulted · Sep 23, 2026 · N359NB · Airbus A319114 · Landing Gear Brake System
  > AUTOBRAKES DISCONNECTED ABRUPTLY AND HARSHLY AT 60 KNOTS ( AFTER BRAKES WERE ALREADY APPLIED). ON TAXI IN, NOTICED AUTOBRAKES STILL SET TO MEDIUM TURNED OFF AUTOBRAKES MANUALLY WITH PUSH BUTTON. PERFORMED BITE TEST OF THE BSCU IAW AMM 32-46-00, NO FAULTS NOT
- [SDR DALA2026092405334](https://openairdocs.org/sdr/DALA2026092405334.md): Unknown · unknown · Sep 22, 2026 · N366NB · Airbus A319114 · Landing Gear System
  > STOPPED ON TAXIWAY AND AIRCRAFT WOULDN'T MOVE UNDER OWN POWER WITH BOTH ENGINES RUNNING. NEEDED A TOW BACK INTO GATE. ACFT STOPPED ON UNEVEN TAXIWAY SURFACE. TOWED TO GATE AND PERFORMED GVI OF NLG AND MLG IAW AMM 32-11 AND AMM 32-21. NO DEFECT NOTED. A/C OK F
- [SDR DALA2026092405335](https://openairdocs.org/sdr/DALA2026092405335.md): Blades · dented · Sep 21, 2026 · N327NB · Airbus A319114 · Turbine Engine Air Inlet Section
  > FOUND TWO BLADES DENTED ON NR 2 ENG. FOUND BLADES 29 AND 30 DENTS TO BE OUT OF LIMITS IAW AMM 72 -21-00-320-001-Q, DAMAGE EXCEEDS A DEPTH OF 1 INCH IN SECTION D INTO SECTION C. REROMVED SPINNER FRONT & REAR CONE IAW AMM 72-21 REMOVED AND REPLACED THE FAN B
- [SDR DALA2026092205297](https://openairdocs.org/sdr/DALA2026092205297.md): Oxygen Mask · broken · Sep 21, 2026 · N348NB · Airbus A319114 · Crew Oxygen System
  > FO OXYGEN MASK PUSH TO TEST SWITCH BROKEN. SWAPPED FO O2 MASK AND BOX WITH 3RD OBS SEAT PER MEL 25-11-06A M PROCEDURES C/ W PLACARD INSTALLED. R & R FLIGHT CREW MASK STOWGE BOX IAW AMM 35-12 MEL CLEARED PLACARD REMOVED A/C OK FROR SERVACE. (LP: 6791268, AIRC
- [SDR DALA2026092205296](https://openairdocs.org/sdr/DALA2026092205296.md): Oxygen Gen · wrong part · Sep 21, 2026 · N339NB · Airbus A319114 · Passenger Oxygen System
  > DURING 60 DAY RFID CHECK FOUND WRONG OXYGEN GENERATORS INSTALLED AT JS 104 AND GAL 401. REPLACED OXYGEN GENERATORS AT JS 104 AND GAL 401. IAW AMM 35-21. (LP: 9118720, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092205265](https://openairdocs.org/sdr/DALA2026092205265.md): Hydraulic Line · leaking · Sep 21, 2026 · N322NB · Airbus A319114 · Hydraulic System, Main
  > DIV - TO BOS DUE TO GREEN SYSTEM HYDRAULIC QUANTITY LOSS (HYD G RSVR LO LVL ECAM WARNING). FOUND HYDRAULIC LEAK COMING FROM HYDRAULIC LINE IN NR 1 ENGINE PYLON, REPLACED SAME, AND DURING CHECKS FOUND NEW LINE LEAKING AT THE T-FITTING TO HCU. MAINTENANCE STIL
- [SDR DALA2026092205298](https://openairdocs.org/sdr/DALA2026092205298.md): Unknown · odor · Sep 20, 2026 · N320NB · Airbus A319114 · Air Distribution System
  > AT 3,000 FT MSL, PRETTY STRONG ODOR (DIRTY SOCK). STAY ON UNTIL GATE. DOOR OPEN AND WINDOW. C/A: WORK IN CONJUNCTION WITH LP 1821932 MSI. RAN BOTH ENGINES, BOTH PACKS, AND APU BLEED. ISOLATED EACH SYS. NO SMELLS. RAN BOTH ENGINES AT POWER FOR 15 MINS. CHANGED
- [SDR DALA2026092105253](https://openairdocs.org/sdr/DALA2026092105253.md): Unknown · odor · Sep 20, 2026 · N336NB · Airbus A319114 · Air Distribution System
  > ON THE PREVIOUS FLIGHT FROM DTW TO AUS, A BURNING ELECTRICAL ODOR WAS OBSERVED IN FLIGHT DECK ON CLIMB OUT FROM 5000-15000 AND THEN DISSAPATED. UPON ARRIVAL AND AFTER DISCUSSION WITH MCC, IT WAS DETERMINED THE PLANE WAS OKAY FOR SERVICE. DURING ENGINE START IN
- [SDR DALA2026092105244](https://openairdocs.org/sdr/DALA2026092105244.md): Unknown · odor · Sep 18, 2026 · N344NB · Airbus A319114 · Air Distribution System
  > VERY STRONG PAINT/CHEMICAL ODOR IN FLIGHT DECK. INITIALLY AFTER APU BLEED ON. SHORTLY AFTER SMELL WAS ALSO NOTICEABLE IN AFT GALLEY. SCENT REMAINED UNTIL BLEED SELECTED OFF. SMOKE AND FUMES REPORT SENT TO MCC. ACCOMPLISHED W/C 0550-2002 EVENT CONSIDERED TYPE
- [SDR DALA2026092105243](https://openairdocs.org/sdr/DALA2026092105243.md): Engine · power loss · Sep 18, 2026 · N336NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > RTO - RIGHT ENG DID NOT SPOOL UP AS FAST AS THE LEFT ENGINE. NR 1 ENG REACHED 80% N1 WHILE END #2 WAS MUCH SLOWER. PERFORMED TSM 71-00-00-810-807-A, ENG SLOW TO ACCEL; PERFORMED A319 AMM 73-21-60-740-028-A, CORRECT FAULTS OF ENG SCHED MAINT RPTS; NO FAULTS RE
- [SDR DALA2026091805197](https://openairdocs.org/sdr/DALA2026091805197.md): Engine · vibration · Sep 18, 2026 · N336NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > ATB- RETURNED TO AUS DUE TO ENGINE 1 VIBES ABOVE 4.0. CREW ALSO REPORTED FEELING A PULSE. MTC REPORTED HIGHEST N1 VIBE OBSERVED ON NUMBER ONE ENGINE WAS 4.2 UNITS. C/W FAN LUBE PER WORK CARD 7221-9601-01. C/W VIBE SURVEY PER AMM 71-00, N1 VIBES WITHIN LIMITS
- [SDR DALA2026092105242](https://openairdocs.org/sdr/DALA2026092105242.md): Skin · cracked · Sep 17, 2026 · N325NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > ER/A 632717-14 REV A: A319 / 3125 / REAR FUSELAGE SKIN PANEL / BTW FR65-66 & STGR31RH-32RH / CORRODED AND CRACKED. SUBJECT REQUIRES FOLLOW ON ACTIONS. ACCOMPLISH SECTION III EXTERNAL INSPECTIONS AT DOUBLER AT A THRESHOLD OF 99,500 TOTAL FLIGHT HOURS OR 50,800
- [SDR DALA2026091705194](https://openairdocs.org/sdr/DALA2026091705194.md): Structure · damaged · Sep 15, 2026 · N353NB · Airbus A319114 · Passenger/Crew Doors
  > DURING GVI OF FR68 LH AFT PASSENGER DOOR INNER CAP AND FLANGE, A REPAIR PART WAS IDENTIFIED. PER ER/A 605954-14AD REV A, SRM 53- 41-12-300-011 WAS ACCOMPLISHED WITHOUT DEVIATION. DUE TO LOCATION OF GUSSET ON TOP OF REPAIR PART FLANGE, UNABLE TO PERFO COMPLETED
- [SDR DALA2026091505143](https://openairdocs.org/sdr/DALA2026091505143.md): Access Panel · corroded · Sep 14, 2026 · N345NB · Airbus A319114 · Aerodynamic Fairings
  > LEVEL 2 CORROSION, APU EXHAUST TAIL CONE AT FR 86, ACCESS PANEL 317AL WERE FOUND FRAME AUXILIARY, TRANSFORMER REAR NAVIGATION LIGHT AND BONDING ANGLE WITH CORROSION AND AT FUSELAGE AREA FOUND FR 86 LOWER FRAME SECTION (CHANNEL) WITH CORROSION. (LP: 1813002, AI
- [SDR DALA2026091305110](https://openairdocs.org/sdr/DALA2026091305110.md): Panel · detached · Sep 12, 2026 · N337NB · Airbus A319114 · Passenger Oxygen System
  > OXYGEN PANEL IN AFT GALLEY FELL OFF. FOUND RUBBER SEAL TUBE MISSING FROM BOTH SIDES, NO DMG TO MODULE. INSTALLED NEW SEALS AS REQ'D, MODULE SECURED. MEL & PLACARDS REMOVED, OK FOR SVC. (LP: 9118950, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092805366](https://openairdocs.org/sdr/DALA2026092805366.md): Strut · corroded · Sep 9, 2026 · N360NB · Airbus A319114 · Wing Main, Frame Structure
  > CORROSION ON INTERNAL BARREL OF INTERCONNECTING STRUT OF LT WING. REMOVED & REPLACED THE INTERCONNECTING STRUT IAW AMM 27-51-44-000-001- A, STEP 1, THRU 3.D(1), & 4.A.
- [SDR DALA2026092805365](https://openairdocs.org/sdr/DALA2026092805365.md): Strut · corroded · Sep 9, 2026 · N360NB · Airbus A319114 · Wing Main, Frame Structure
  > CORROSION ON INTERNAL BARREL OF INTERCONNECTING STRUT ON RT WING. REMOVED INTERCONNECTING STRUT OF RT WING IAW FAM AMM 27-51-44-000-001-A, STEP 1, THRU 3.D(1) AND 4.A. REPLACED INTERCONNECTING STRUT IAW AMM 27-51 -44-000-001-A, & AMM 27-51-44-400-001-A. (LP
- [SDR DALA2026091005064](https://openairdocs.org/sdr/DALA2026091005064.md): Rudder · no discrepancy · Sep 8, 2026 · N343NB · Airbus A319114 · Rudder Structure
  > WEIGH RUDDER IAW AMDS WORKCARD 5540-01015-02. WEIGHED RUDDER IAW AMDS WORKCARD 5540-01015-02 AND IAW AMDS WORK CARD 2721-4001 FOR REMOVAL AND REINSTALL. NO FINDINGS NOTED. (LP: 1801737, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091005063](https://openairdocs.org/sdr/DALA2026091005063.md): Frame · damaged · Sep 6, 2026 · N315NB · Airbus A319114 · Fuselage Main, Frame
  > S.B A320-53-1491-WORK CARD 5311-01244-02B R/H FRAME 68 FLANGE HAS PREVIOUS REPAIR REQUIRING FURTHER ENGINEERING TO COMPLETE WORK CARD. CURRENT ERA 603003-14AD. REV 0. C/A: COMPLIED WITH ERA 6365560-14 REV 0 FOR THE R/H FR 68 FLANGE NO DEFECTS NOTED. JOB COMPLE
- [SDR DALA2026091005062](https://openairdocs.org/sdr/DALA2026091005062.md): Frame · damaged · Sep 6, 2026 · N315NB · Airbus A319114 · Fuselage Main, Frame
  > S.B A320-53-1491-WORK CARD 5311-01244-02A L/H FRAME 68 FLANGE HAS PREVIOUS REPAIR REQUIRING FURTHER ENGINEERING TO COMPLETE WORK CARD. CURRENT ERA 602719-14AD. REV 0. COMPLIED WITH ERA 602719-14AD, REV 0, SECTION II IAW ESR 18175. ALL STEPS OF PRI 636551-14 R
- [SDR DALA2026090805017](https://openairdocs.org/sdr/DALA2026090805017.md): Piston · intermittent · Sep 5, 2026 · N335NB · Airbus A319114 · Landing Gear Brake System
  > ON TAXI OUT CA RIGHT BRAKE PEDAL CHATTERED AND THEN WENT TO THE FLOOR. AFTER RETURNING TO GATE NOISE FROM PREVIOUS FLIGHT RETURNED. C/A: T/S IAW A319 TSM 32-42-00-810-841-A & TSM 32-42-00-810-912-A. FOUND #4 BRAKE PISTON AT 1 O'CLOCK POSITION INTERMITTENTLY GR
- [SDR DALA2026090204944](https://openairdocs.org/sdr/DALA2026090204944.md): Unknown · odor · Sep 1, 2026 · N339NB · Airbus A319114 · Air Distribution System
  > MUSTY DIRTY SOCK ODOR, STRONGER ON F/O SIDE. DESCRIBED AS A MANURE ODOR. SURVEY COMPLETED. COPY OF LOG PAGE AND SMOKE AND FUMES REPORT SENT TO MCC. C/W MSI PREVENTION FOR SMOKE/FUMES REF LOG 1788293. (LP: 9609256, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026090104920](https://openairdocs.org/sdr/DALA2026090104920.md): Computer · failed · Aug 31, 2026 · N360NB · Airbus A319114 · Pitot/Static Anti-Ice System
  > DIVERTED TO IAD DUE TO BURNING ELECTRICAL ODOR AFTER TAKEOFF WITH ASSOCIATED NR 2 PROBE HEAT, COMPUTER FAILURE MESSAGES. CONFIRMED PROBE HEAT COMPUTER FRIED. REPLACED COMPUTER AND PERFORMED A LEVEL A DECONTAMINATION OF THE ECS. (LP: 9117321, AIRCRAFT WAS GRO
- [SDR DALA2026083004890](https://openairdocs.org/sdr/DALA2026083004890.md): Wire Harness · faulted · Aug 30, 2026 · N343NB · Airbus A319114 · Landing Gear System Wiring
  > GO-AROUND, AFTER GEAR EXTENSION, LT MAIN INDICATOR LIGHT DISPLAYED UNLK WITH NO GREEN TRIANGLE. WHEEL PAGE ON ECAM DISPLAYED RED TRIANGLE ON THE LEFT SIDE OF LT MAIN GEAR & GREEN TRIANGLE ON THE RT. ON LANDING ROLLOUT GOT L/G SYSTEM DISAGREE ECAM MESSAGE. LT
- [SDR DALA2026090204942](https://openairdocs.org/sdr/DALA2026090204942.md): Tru · odor · Aug 29, 2026 · N347NB · Airbus A319114 · AC Power Distribution System
  > SHIP 3147 DISC: FLT CREW REPORTED ELECTRICAL ODOR AND A/C BUSS 2 FAULT ON THE ECAM. T/S & FOUND TR2 INOP & RT GEN GLC 2 CONTACTOR BURNED, R & R TRU 2 IAW AMM 24-32 AND GLC 2 IAW AMM 24-22. PERFORMED A GOOD OPS CHK OF DC GENERATION SYS & LT GEN IAW AMMS 24-32/
- [SDR DALA2026090204941](https://openairdocs.org/sdr/DALA2026090204941.md): Cover · broken · Aug 29, 2026 · N325NB · Airbus A319114 · Emergency Lighting
  > LIGHT COVER ABOVE 1L DOOR BROKEN/FELL OFF. SECURED LIGHT COVER ABOVE 1L DOOR. OPS CHKD GOOD. (LP: 9489242, AIRCRAFT WAS GROUNDED)

Next page: https://openairdocs.org/model/airbus-a319-114/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 aircraft_model_key = 'A319114'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a319-114/reports

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