# Service difficulty reports: Airbus A318-111

A list on [Airbus A318-111](https://openairdocs.org/model/airbus-a318-111.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 8 · 353 reports

- [SDR ANCF2019021801](https://openairdocs.org/sdr/ANCF2019021801.md): Transducer · faulty · Feb 18, 2019 · N592EL · Airbus A318111 · APU Bleed Air System
  > FEB 18. DURING DESC TO SKPS THE APU BLEED ON ECAM APPEARS AIR APU BLEED FAULT. CORRECTIVE ACTIONS: FEB 18. IN ACCORDANCE WITH MEL 36-12-01 CAT "C" THIS REPORT IS DEFERRED TO DMI W/O:2130037 CNMCC-2019-AV0925 FEB 21. IN ACCORDANCE WITH TSM 36-12-00-810-801-A FA
- [SDR ANCF2019011701](https://openairdocs.org/sdr/ANCF2019011701.md): Transducer · out of adjust · Jan 17, 2019 · N592EL · Airbus A318111 · Pneumatic Indicating System
  > JAN 17. DURING DESCENT TO SKPS APU BLEED FAULT. CORRECTIVE ACTION: JAN 17. THIS ITEM IS DEFERRED TO DMI WO 2094888 IN ACCORDANCE WITH MEL 36-12-01 CAT C. CNMCC-2019-AV0280 // IN ACCORDANCE WITH TSM 49-00-81-810-860-A STEP 3.A. THE APU LAST LEG REPORT AND GROUN
- [SDR ANCF201812270402](https://openairdocs.org/sdr/ANCF201812270402.md): Unknown · warning message · Dec 4, 2018 · N593EL · Airbus A318111 · AC Generator-Alternator
  > DURING TAXI AND PERFORMING ONE ENGINE TAXI DEPATURE PROCEDURE WITH ENGINE AVAIL MESSAGE ON ECAM:ELEC GEN 2 FAULT.PERFORMED ECAM PROCEDURE UNSUCCESFULL // CORRECTIVE ACTION: DEC 4. THIS REPORT IS DEFERRED TO DMI WO 1822567 LOG PAGE RED BOOK 18495. N593EL-CNMCC-
- [SDR ANCF2018FA0000385](https://openairdocs.org/sdr/ANCF2018FA0000385.md): Proximity Sensor · faulty · Sep 24, 2018 · N593EL · Airbus A318111 · Landing Gear Position and Warning
  > SHOCK ABSORBER FAULT IN LANDING GEAR EXT PROX SN SR 25GATGT POS IN LFEXT PROX SN SR (24GA) TGT POS. IAW AMM 32-31-73-000-005A PROXIMITY SENSORS 24GA / 25GA WERE REPLACED.
- [SDR ANCF2018FA0000379](https://openairdocs.org/sdr/ANCF2018FA0000379.md): Unknown · odor · Sep 17, 2018 · N592EL · Airbus A318111 · Air Distribution System
  > STRONG SMELL OF HYDRAULIC CABIN PASSENGERS.
- [SDR ANCF2018FA0000372](https://openairdocs.org/sdr/ANCF2018FA0000372.md): Shock Absorber · faulted · Sep 14, 2018 · N593EL · Airbus A318111 · Main Landing Gear Strut/Axle/Truck
  > PILOT REPORT UNABLE TO RAISE LANDING GEAR AFTER LIFTOFF, LT SHOCK ABSORBER FAULT ON ECAM.
- [SDR ANCF2018FA0000359](https://openairdocs.org/sdr/ANCF2018FA0000359.md): Warning System · activated · Sep 10, 2018 · N594EL · Airbus A318111 · Landing Gear Position and Warning
  > DURING TAKE OFF MESSAGE APPEAR L/G DOORS NOT CLOSED. DMI WAS CREATED 32-31-00 CAT B.
- [SDR ANCF2017122401](https://openairdocs.org/sdr/ANCF2017122401.md): Warning Light · false activation · Dec 24, 2017 · N590EL · Airbus A318111 · Central Warning
  > AFTER TAKEOFF, FLIGHT CONTROL GROUND SPOILER 1 & 2 FAULT WARNING APPEARED ON ECAM. IAW TSM 27-60-00-810-805-A CHECK OF THE WIRING FROM SEC 3 AND THROTTLE CONTROL UNIT WAS PERFORMED AND FOUND OK. AMM 27-94-34-PB 401 TH SEC 3 WAS REMOVED AND REPLACED OPS TESTE
- [SDR ANCF2016042901](https://openairdocs.org/sdr/ANCF2016042901.md): Hinge Fitting · vibration · Apr 29, 2016 · N594EL · Airbus A318111 · Elevator Structure
  > SEVERE ACFT VIBRATION FELT AT FL 290 WITH A SPEED OF APROX 290 KTS & THROUGHOUT 260 KTS VIBRATION STOPPED. IAW TSM 05-50-00-810-801-A IDENTIFICATION OF THE CAUSE OF INFLIGHT AIRFRAME VIBRATIONS & OR NOISES WAS ACCOMPLISHED IAW TSM TASK 27-30-00-810-850-A. AI
- [SDR ANCF2016011202](https://openairdocs.org/sdr/ANCF2016011202.md): Engine · bird ingestion · Jan 12, 2016 · N592EL · Airbus A318111 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF RNWY 34, SKCC ENG NR 2 HAD THE STRIKE, N1 INCREASED UP TO 4,7 VIB WHILE N2 VIB REMAINED UNCHANGED. PARAMETERS WERE LOOKED IN QRH PAGE 70,09A & NOT EXCEED THOSE VLVS. IAW AMM 05-51-19-200-601A INSPECTION OF THE ENG AFTER A BIRD STRIKE OR SLUSH
- [SDR ANCF2015121101](https://openairdocs.org/sdr/ANCF2015121101.md): Engine · failed · Dec 11, 2015 · N595EL · Airbus A318111 · Engine (Turbine/Turboprop)
  > DURING FLIGHT, ENG 1 FAIL, ENG 1 STALL & ENG 1 SHUTDOWN. REPLACE ENG 1 IN PROGRESS. ENG PN CFM56-5B, SN 577194, TSN 26542 141, CSN 19697. REMAINING TIME IN ORDER TO GO TO THE SHOP, 303 FC.
- [SDR ANCF2015080201](https://openairdocs.org/sdr/ANCF2015080201.md): Warning System · false activation · Aug 2, 2015 · N590EL · Airbus A318111 · Autopilot System
  > DURING ENG START AUTO FLIGHT YAW DAMPER SYS FAULT MSG ON ECAM. IAW AMM TASK 22-91-00-710 -001 & AMM 22-96-710-001-A THE AFS GND SCAN & TEST WAS PERFORMED. TESTED SATISFACTORY.
- [SDR ANCF2015071401](https://openairdocs.org/sdr/ANCF2015071401.md): Ecu · faulty · Jul 14, 2015 · N596EL · Airbus A318111 · Fuel Controlling System
  > DURING ENG 1 START THE ENG 1 ING A FAULT APPEAR. THE FADEC MADE A NEW ENG START WITH IGN AB WITHOUT POSITIVE SUCCESS, ENG REMAIN HUNG STAR. IAW AMM 73-21-60-000 400-001-B THE ECU ON ENG 1 WAS R & R. THE FUNCTIONAL TEST OF THE ECU WAS SATISFACTORY PN 2123M56
- [SDR ANCF2015071301](https://openairdocs.org/sdr/ANCF2015071301.md): Starter · malfunctioned · Jul 13, 2015 · N596EL · Airbus A318111 · Engine Starter
  > DURING ENG 1 START WHEN MASTER SWITCH TO NR N 2 MOVEMENT, BLEED PRESS NORMAL, START VLV OPEN. IAW AMM 80-11-10 PB 401 THE STARTER WAS REPLACED, O TEST WAS PERFORMED SATISFACTORY PN 3505582-27, SN OFF YG439040-H & SN ON Y6336238-AC.
- [SDR ANCF2015060101](https://openairdocs.org/sdr/ANCF2015060101.md): Igniter · failed · Jun 1, 2015 · N596EL · Airbus A318111 · Spark Plug/Igniter
  > DURING ENG 1 START, ENG 1 IGNITER A FAULT. IAW TSM 74-00-00-810-801A THE OPERATIONAL OF IGNITION SYS WAS ACCOMPLISHED THE RT IGNITER PLUG CANNOT HEARD. IAW AMM 71-21-30 PB401 THE SPARK IGNITER A WAS REPLACED. OPERATIONAL TESTED SATISFACTORY.
- [SDR ANCF2015042601](https://openairdocs.org/sdr/ANCF2015042601.md): Acm · seized · Apr 26, 2015 · N591EL · Airbus A318111 · Cabin Cooling System
  > DURING INITIAL CLIMB AFTER TAKEOFF PROX AT 3500 FT THE FLIGHT ATTENDANT CALLED TO THE COCKPIT & INFORMED SMELL & SMOKE IN THE CABIN. THE CREW PERFORMED THE SMOKE PROCEDURE & RETURNED TO DEPARTURE AIRPORT. AFTER LANDING AIR PACK 1 OVHT APPEARED ON ECAM. IAW
- [SDR ANCF2015042001](https://openairdocs.org/sdr/ANCF2015042001.md): Ignition Sys · malfunctioned · Apr 20, 2015 · N596EL · Airbus A318111 · Ignition System
  > DURING ENG START, IGNITION A, ENG 1 FAULT. IAW AMM TASK 74-21-20-000-400-002-A ON ENG NR 1 IGNITION A WAS REPLACED. IAW AMM 74-00- -00-710-043-A OPERATIONAL TEST OF THE IGNITION SYS WAS PERFORMED WITH RESULT SATISFACTORY.
- [SDR ANCF2015033001](https://openairdocs.org/sdr/ANCF2015033001.md): Warning System · false activation · Mar 30, 2015 · N592EL · Airbus A318111 · Pneumatic Indicating System
  > DURING TAXI OUT WITH ENG 1 STARTED AIR RT WING LEAK WAS PRESENTED ON ECAM. IAW AMM 36-11-00-740-001 TEST OF THE BMC ON GND WAS ACCOMPLISHED SATISFACTORY. IAW AMM 36-11-00-720-809-A 808-A CHECK FOR LEAK WITH ENGS RUN UP SATISFACTORY.
- [SDR ANCF2015032601](https://openairdocs.org/sdr/ANCF2015032601.md): Sensor · dirty · Mar 26, 2015 · N595EL · Airbus A318111 · Door Warning System
  > AFTER TAKEOFF ON ECAM EMER SLIDES, COMES ON CORRECTIVE ACTION. IAW AMM 52-21-00-810-806-A CLEANED SENSOR & IAW AMM 52-71-13-400-001 INSTALL LT HANDLE FLAP & ADJUSTED.
- [SDR ANCF2015031601](https://openairdocs.org/sdr/ANCF2015031601.md): Unknown · malfunctioned · Mar 16, 2015 · N592EL · Airbus A318111 · Electrical Power System
  > AFTER ENG START AUTO FLIGHT AUTO THRUST OFF WAS PRESENTED ON ECAM. IAW AMM 24-00-00 RESET TO FMEC 1 & 2 WAS PERFORM WITH SATISFACTORY RESULTS.
- [SDR ANCF2015030805](https://openairdocs.org/sdr/ANCF2015030805.md): Ignition Sys · faulted · Mar 8, 2015 · N598EL · Airbus A318111 · Ignition Switching
  > ENG 2 IGN FAULT. IAW AMM 74-00-00-710-043A OPERATIONAL TEST OF IGN SYS WAS PERFORMED & THE IGNITERS WERE CYCLED DURING TEST. IAW TSM 71-50-00-810-804A OPERATIONAL TEST OF FADEC 2A & 2B WAS PERFORMED. NO FAULTS RECORDED.
- [SDR ANCF2015022001](https://openairdocs.org/sdr/ANCF2015022001.md): Servo Control · faulty · Feb 18, 2015 · N594EL · Airbus A318111 · Elevator Control System
  > DURING CLIMB AT FLIGHT LEVEL 320 STRONG HARMONICS VIBRATION WAS FELT ON THE ENTIRE ACFT. IAW AMM 27-34-00-200-001A & 27-24-00-200-002A, ELEVATOR & RUDDER, THE TOO MUCH PLAY CHECK OF THE BEARING & HINGES WERE PERFORMED. REQUIRE REPLACE ELEVATOR SERVO CONTROL
- [SDR ANCF2015021401](https://openairdocs.org/sdr/ANCF2015021401.md): Seal · vibration · Feb 14, 2015 · N594EL · Airbus A318111 · Aerodynamic Fairings
  > DURING CLIMB PASSING FL300, CLIMB SPEED NOTING CONDITION & NO TURBULENCE. THE ACFT HAD A VERY STRONG VIBRATION FOR ABOUT 30 SECONDS. AFTER REDUCING SPEED & DISCONNECTING AP THE VIBRATIONS STOPPED. THE AP WAS CONNECTED AGAIN WITH A/T & WITH SPEED TURBULENCE.
- [SDR ANCF2015021101](https://openairdocs.org/sdr/ANCF2015021101.md): Bleed Valve · faulty · Feb 11, 2015 · N593EL · Airbus A318111 · Compressor Bleed Valve
  > ENGINE 1 COMPRESSOR ARE DISPLAY ON ECAM DESCENT, A STRONG NOISE ON ENG 1, STALL ON ECAM FOLLOWED BY ENG 1 STALL ON ECAM FOLLOWED BY ENG 1 COMPRESSOR VANE DURING THE REST. OF THE FLIGHT, WE HAD 2 COMPRESSOR STALL EVENTS. IAW AMM 75-31-50-000 400-A THE BLEED V
- [SDR ANCF2015012601](https://openairdocs.org/sdr/ANCF2015012601.md): Proximity Switch · out of adjust · Jan 26, 2015 · N594EL · Airbus A318111 · Door Warning System
  > DOOR AFT AVIONICS OPEN ON ECAM DURING INITIAL CLIMB THROUGH 11.000 FT. RETURNED, WAS REQUIRED BY ECAM DUE TO MEMO. ACCOMPLISHED VISUAL CHECK OF AVIONICS COMPARTMENT DOOR & WAS FOUND CORRECTLY CLOSED IAW 52-70-00-040- 004-A. IAW AMM 52-71-00-820-008 -A01 ADJ
- [SDR ANCF2015012301](https://openairdocs.org/sdr/ANCF2015012301.md): Smoke Detector · damaged · Jan 23, 2015 · N595EL · Airbus A318111 · Smoke Detection
  > DURING ARRIVAL THE ACFT WAS DECLARED IN EMER BY AFT CARGO SMOKE. DURING MX CHECK IAW TSM 26-16-00-810-809-AA, FOUND SMOKE DETECTOR 5WH DAMAGED. FALSE FIRE WARNING DURING FLIGHT WAS DETERMINED. SMOKE DETECTOR WAS REPLACED IAW AMM 26-16-15-000-001 400-001.
- [SDR 2014FA0000588](https://openairdocs.org/sdr/2014FA0000588.md): Slide · twisted · Oct 2, 2014 · Airbus A318111 · Escape Slide
  > DURING DEPLOYMENT OF OVERWING SLIDE ONE OF THE ROPES WAS ENTANGLED RESULTING IN AN IMPROPER DEPLOYMENT.
- [SDR ANCF2014092601](https://openairdocs.org/sdr/ANCF2014092601.md): Controller · malfunctioned · Sep 26, 2014 · N590EL · Airbus A318111 · Cabin Pressure Controller
  > PIREP DURING CLIMB REACHING 360 CABIN PRESS EXCESS CABIN ALT WAS PRESENTED & CABIN PRESS SYS 2 & DURING DESCEND CABIN PRESS LOW DIF PRESS WAS PRESENTED. IAW AMM 21-31-00-040-006-A DEACTIVATION CPC 2 WAS PERFORMED IN NORMAL CONDITION TEST OK, CB Y22 IS POSITIO
- [SDR ANCF2014083101](https://openairdocs.org/sdr/ANCF2014083101.md): Valve · faulty · Aug 31, 2014 · N593EL · Airbus A318111 · Pneumatic Distribution System
  > GROUND RETURN TO GATE DUE TO INTERMITTENT ECAM MSG AIR BLEED 1 & AIR BLEED 2 FAULT WHEN APPLYING FLEX TO THRUST THE PACKS WERE OFF & THE TAKEOFF WAS DISCONTINUED AT 40 KNOTS REVERSE THRUST WAS NOT APPLIED & AUTO BRAKES SYS DID NOT ACTIVATE. IAW AMM 36-12-52-
- [SDR ANCF2014080101](https://openairdocs.org/sdr/ANCF2014080101.md): Fan · malfunctioned · Aug 1, 2014 · N593EL · Airbus A318111 · Air Distribution Fan
  > AFTER APPROX 2 MINUTES INFLIGHT, A STRONG NOISE WAS FELT ON THE NOSE AREA, THEN A STRONG RUBBER SMELT WAS FELT IN THE COCKPIT & PAX CABIN. THE BLOWER & EXTRACT FAULT WAS PRESENTED ON THE OVERHEAD PANEL WITHOUT ECAM ALERT. THE RUBBER SMELT DISAPPEAR ABOUT 5 M
- [SDR ANCF2014FA0000331](https://openairdocs.org/sdr/ANCF2014FA0000331.md): Unknown · vibration · May 16, 2014 · N593EL · Airbus A318111 · Standard Practices/Structures
  > DURING CRUISE, AT FL 390 AND MACH 0.78, THE CABIN CREW INFORMED ABOUT A HIGH VIBRATION IN THE TAIL, TSM 53-35-00-810-801 WAS ACCOMPLISHED AND NO DAMAGES WERE FOUND.
- [SDR ANCF2014FA0000243](https://openairdocs.org/sdr/ANCF2014FA0000243.md): Windshield · damaged · Apr 5, 2014 · N595EL · Airbus A318111 · Flight Compartment Windows
  > DURING CLIMB, ANTI-ICE RT WINDSHIELD ANNUNCIATION REPORT COME IN ECAM IAW AMM 56-11-11, PB 401, CONF 00. THE RT WINDSHIELD WAS REMOVED IAW AMM 56-11-11-400-001A. THE RT WINDSHIELD WAS INSTALLED, OPS TEST WAS SATISFACTORY.
- [SDR 2014FA0000190](https://openairdocs.org/sdr/2014FA0000190.md): Display · malfunctioned · Mar 22, 2014 · N593EL · Airbus A318111 · Central Display
  > REJECTED TAKEOFF DUE TO NO FMA ANNUNCIATIONS ON PFD, NO FLEX AND NO A/P 1 AND 2, NO AUTOTHROTTLE. PERFORMED BITE TEST AT FAC NR 1 AND NR 2 IAW AMM 22-60-00-710-001A AND OPS TEST AT AUTO PILOT SYSTEM IAW AMM 22-90-00-710-001. GROUND TEST SATISFATORY.
- [SDR ANCF201401100175](https://openairdocs.org/sdr/ANCF201401100175.md): Elevator System · out of tolerance · Jan 10, 2014 · N598EL · Airbus A318111 · Elevator Control System
  > DURING CLIMB, LEAVING FL 230 WITH 340 KNOTS, EXTREME VIBRATION IN STRUCTURE, VIBRATION STOPPED, SPEED REDUCED TO 250 KNOTS & RETURNED TO FL 230 IAW TSM FIGURE 05-50-00-991-00400-C SHEET 1, DECISION TABLE WAS ACCOMPLISHED TYPE 13, 12, 11 & 10. THE PAX DOOR
- [SDR ANCF2013190900167](https://openairdocs.org/sdr/ANCF2013190900167.md): Coffeemaker · failed · Sep 19, 2013 · N595EL · Airbus A318111 · Buffet/Galleys
  > ON GROUND, COFFEMAKER 1 STARTED TO PRODUCE SMOKE. COFFEMAKER REPLACED IAW AMM 25-85-12-000/400-001-A, TESTED OK.
- [SDR ANCF2013080700163](https://openairdocs.org/sdr/ANCF2013080700163.md): Unknown · vibration · Aug 7, 2013 · N591EL · Airbus A318111 · Fuselage Main, Structure
  > HIGH VIBRATION DURING CLIMBING AT 25,000 FT AND 27,000 FT, IAW TSM 53-35-00-810-801. A VIBRATION AND/OR NOSE FELT AND TSM 05-50-00-810-801-A IDENTIFICATION OF THE CAUSE OF IN-FLIGHT AIRFRAME VIBRATIONS AND/OR NOISES WERE PERFORMED, VIBRATION REPORTING SHEET A
- [SDR F3LA2013071700885](https://openairdocs.org/sdr/F3LA2013071700885.md): Unknown · vibration · Jul 9, 2013 · N803FR · Airbus A318111 · Flight Control System
  > AIR TURN BACK DUE TO SEVERE AIRFRAME VIBRATION. BEGAN AT 25,500 FT AND AROUND 330 KIAS. DID NOT STOP UNTIL SPEED MANUALLY FLOWN LESS THAN 300 KIAS. EMERGENY DECLARED. R & R LT AND RT ELEVATOR ATTACH HARDWARE AND BEARINGS REF AMM 27-34-41, PAGE BLOCK 401.
- [SDR ANCF2013042900158](https://openairdocs.org/sdr/ANCF2013042900158.md): Unknown · smoke · Apr 29, 2013 · N589AV · Airbus A318111 · Air Distribution System
  > DURING INITIAL CLIMB, ACCORDING TO THE F/A THERE WAS SMOKE WITH ELECTRICAL ODOR AND THE SAME CONDITION WAS REPORTED BY THE CABIN CREW AFTER ENGINE SHUTDOWN IAW AMM TASK 21-61-00-710-001A. THE OPS TEST OF PACKS 1 AND 2 WERE PERFORMED DURING TWENY FIVE MINUTES
- [SDR ANCF2013042000157](https://openairdocs.org/sdr/ANCF2013042000157.md): Control Unit · malfunctioned · Apr 20, 2013 · N596EL · Airbus A318111 · Landing Gear Steering System
  > DURING LANDING ROLL CROSSING ABOUT 70KTS WHEEL NOSE WHEEL STEERING FAULT AND BRAKES SYSTEM 1 FAULT WAS PRESENTED NWS REMAINS INOPERATIVE UNTIL FINAL STOP IN THE RWY. ACCORDING TSM 32-51-00-810-818A THE BSCU MUST BE REPLACED FOLLOWING AMM 32-42-34PB401. THE
- [SDR ANCF2013041200155](https://openairdocs.org/sdr/ANCF2013041200155.md): Oven · smoke · Apr 12, 2013 · N597EL · Airbus A318111 · Buffet/Galleys
  > NR 2 OVEN IN REAR GALLEY HAS A BURNING SMOKE. NR 2 OVEN REAR GALLEY WAS REMOVED AND REPLACED IAW AMM 25-35-19-PB 401.
- [SDR ANCF2013040100153](https://openairdocs.org/sdr/ANCF2013040100153.md): Connector · loose · Apr 1, 2013 · N591EL · Airbus A318111 · Door System Wiring
  > DOOR FWD CARGO INDICATION DURING CLIMB -- IN ACCORDANCE WITH AMM 52-71-00-200-001- A VISUAL INSPECTION ON THE FWD CARGO SENSOR CONNECTOR LOOSE. THIS ITEM IS DEFERRED TO DMI #262 IN ACCORDANCE WITH MEL 52-70-01-3 CAT "C". IAW AMM 52-71-12-400-001-A ADJUST OF
- [SDR ANCF2013030200151](https://openairdocs.org/sdr/ANCF2013030200151.md): Smoke Detector · damaged · Mar 3, 2013 · N590EL · Airbus A318111 · Smoke Detection
  > DURING CRUISE SMOKE AFT CARGO WAS PRESENTED THE AGENT WAS DISCHARGED -IAW AMM 26-23-00-200-005A RESTORATION OF THE FIRE EXTINGUISHING SYSTEM AFTER ACTUATION WAS PERFORMED. ALSO IAW AMM 26-23-41 PB 401 BOTTLE FIRE EXT WAS REPLACED AND SMOKE DETECTOR WAS REPLAC
- [SDR ANCF2013012300147](https://openairdocs.org/sdr/ANCF2013012300147.md): Warning System · activated · Jan 23, 2013 · N593EL · Airbus A318111 · Door Warning System
  > DURING CLIMB, DOOR RIGHT EMERGENCY EXIT AMBER CAUTION PRESENTED DURING CLIMB. IN ACCORDANCE WITH AMM 52-21-11-400-001-A THE COVER FLAP WAS INSTALLED PROPERLY.
- [SDR ANCF2012112900138](https://openairdocs.org/sdr/ANCF2012112900138.md): Unknown · odor · Nov 29, 2012 · N593 · Airbus A318111 · Air Distribution System
  > FUEL SMELL DURING DESCENT COMING FROM VENTILATION. CORRECTIVE ACTION IN ACCORDANCE WITH TSM TASK 28-00-00-810-801-A. INSPECTION OF EXTERNAL FUSELAGE CENTER BOX WING AREA WAS INSPECTED, FUEL LEAK WAS NOT FOUND.
- [SDR F3LA2012112000814](https://openairdocs.org/sdr/F3LA2012112000814.md): Switch · failed · Nov 17, 2012 · N923FR · Airbus A318111 · Crew Oxygen System
  > 02 MASK DROPPED. REPLACED PASSENGER OXYGEN ALTITUDE SWITCH IAW AMM 35-23-15 PB 401.
- [SDR ANCF2012110900136](https://openairdocs.org/sdr/ANCF2012110900136.md): Wheel · failed · Nov 9, 2012 · N597EL · Airbus A318111 · Wheel/Ski/Float
  > DURING WALK AROUND, TIRE NR 4 WAS FOUND WITHOUT CANVAS AND PANEL NR 673AB ON RT WING WAS FOUND CRACKED. C/A IAW AMM 32-41-11-000-006A AND 32-41-11-400-006-A THE MAIN WHEEL 3 AND 4 WERE R & R. TIRE PRESS 189 PSI IAW AMM TASK 05-51-15-200-001-A. THE INSPECTIO
- [SDR ANCF2012102600135](https://openairdocs.org/sdr/ANCF2012102600135.md): Valve · damaged · Oct 26, 2012 · N597EL · Airbus A318111 · Pressure Regulator/Outflow Valve
  > AFTER T/O THE VENT OUT DIDN´T CLOSE WITH OVERRIDE P/B. IN ACCORDANCE WITH AMM 21-26-00-710-001 OPERATIONAL TEST OF THE AEVC SYSTEM VIA MCDU WAS ACCOMPLISHED. TEST SATISFACTORY AND SKIN AIR-INLET VALVE FIN 15HQ, AVIONICS FILTER AIR WERE REPLACED. IN ACCORDAN
- [SDR ANCF2012102500134](https://openairdocs.org/sdr/ANCF2012102500134.md): Unknown · smoke · Oct 25, 2012 · N597EL · Airbus A318111 · Air Distribution System
  > DURING CRUISE HAD PACK 1 OVERHEAT ON ECAM. PROCEDURES WERE MADE ACCORDING TO ECAM BUT WHEN WE PUT ON THE PACK 1 THERE WAS SMOKE IN THE COCKPIT. IN ACCORDANCE WITH AMM TASK 21-61-00-710-001A OPERATIONAL TEST OF THE PACK 1/2 TEMPERATURE CONTROL WAS PERFORMED S
- [SDR ANCF2012101600133](https://openairdocs.org/sdr/ANCF2012101600133.md): Unknown · odor · Oct 16, 2012 · N591EL · Airbus A318111 · Air Distribution System
  > LOW SPEED REJECTED TAKEOFF DUE TO RUBBER SMELL IN THE CABIN. IN ACCORDANCE WITH TSM 26-15-00-810-804-A CHECK BY ODOURS AND MIST IN THE CABIN, NON EXTERNAL OIL OR FUEL LEAKS WERE FOUND. THE FUMES IN THE CABIN/ OIL SMOKE AT THE APU EXAUST CHECK MUST BE PERFOR
- [SDR ANCF2012100900132](https://openairdocs.org/sdr/ANCF2012100900132.md): Oven · malfunctioned · Oct 9, 2012 · N596EL · Airbus A318111 · Buffet/Galleys
  > DURING TAXI BURNING SMELL WAS DETECTED ON AFT GALLEY (4 LEFT). IAW AMM TASK 25-35-00 WAS PERFORMED CHECK IN AFT GALLEY AND FOUND C/B OVEN NR 3 TRIPPED, OVEN NR 3 IS DEFERRED TO DMI /NEF NR 1158 AS PER MEL NEF II-5 CAT D.

Next page: https://openairdocs.org/model/airbus-a318-111/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 = 'A318111'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a318-111/reports

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