# Service difficulty reports: IAE V2500-A1

A list on [IAE V2500-A1](https://openairdocs.org/engine/iae-v2500-a1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 7 · 306 reports

- [SDR 2026FA0000291](https://openairdocs.org/sdr/2026FA0000291.md): Case · unserviceable · Apr 24, 2026 · Engine (Turbine/Turboprop)
  > IBERIA MAINTENANCE HAS RECEIVED A NOTIFICATION FROM AN EXTERNAL REPAIR STATION (FAA DLAY225D LUFTHANSA TECHNIK AG (“LHT”) TO INFORM OF AN OCCURRENCE STATING THAT A NUMBER OF INDIVIDUAL COMPONENTS WERE IDENTIFIED WHERE A FINAL, FULL FLUORESCENT PENETRANT INSP
- [SDR 2025FA0000822](https://openairdocs.org/sdr/2025FA0000822.md): Unknown · unknown · Dec 12, 2025 · N678MK · Airbus A320231 · Standard Practices/Structures
  > THE PARTS RECORDED UNDER EASA FORM 1 TRACKING NR 44543 AND 44538 HAVE BEEN DETECTED AS SUSPICIOUS. DISCREPANCY ON MISSING SIGNATURE, (SECTION 14B), APPROVAL/CERTIFICATE NO (SECTION 14C) AND ORGANIZATION NAME AND ADDRESS (SECTION 4) HAVE BEEN DETECTED. AUTHORI
- [SDR CALA2024083000519](https://openairdocs.org/sdr/CALA2024083000519.md): Engine · unknown · Aug 28, 2024 · N471UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > REJECTED TAKE OFF AT 60 KNOTS. ON T/O ENGINES DI D NOT COME UP T OGETHER A ND WERE SPLIT AT FLEX UPON ARRIVAL TO COCKPIT, NO STATUS MESSAGE WAS PRESENT. PRINTED A PFR. FOUND FAILURE "DMC2: NO ADF1 DATA" AND "DMC3: NO EEC2B DATA SOURCE EIS 3 AT 01:31 GMT ( SAME
- [SDR CALA2022112803241](https://openairdocs.org/sdr/CALA2022112803241.md): Module · damaged · Nov 28, 2022 · N409UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > *EMERGENCY DECLARED* BIRDSTRIKE ENG 2 ENGINE #2 SN V10989 HAD BIRDSTRIKE ON TAKEOFF. ONLY PARAMETERS CHANGE WAS VIBRATION. ENGINE WAS NOT SHUTDOWN, BROUGHT BACK TO IDLE UNTIL LANDING. TRANSFERRED TO OFF #2 ENG SN V10989 AC 8802 LP3191823. ONLY PARAMETERS CHA
- [SDR CALA2022112503227](https://openairdocs.org/sdr/CALA2022112503227.md): Drain Line · damaged · Nov 25, 2022 · N433UA · Airbus A320232 · Engine Drains
  > PDA 3 ENGINE #1 ZONE F DRAIN TUBE, APPROXIMATELY 8 INCHES, MISSING FROM AIRCRAFT. INSTALLED LH ZONE F DRAIN TUBE. REF AMM 54-51-29.
- [SDR CALA2022112103193](https://openairdocs.org/sdr/CALA2022112103193.md): Harness · failed · Nov 21, 2022 · N831UA · Airbus A319131 · Cylinder Head Temperature (CHT) Indicating System
  > ENG 2 EGT OVERTEMP ONT/O ROLL.TEMP APROX 890C 77-20-00-810-802-B. TOMC-MEREDITH UPDATED MAA CODE FIX USING VENDOR MAA SCREEN CREW REPORTED LOW SPEED ABORTED TAKEOFF AND EGT INDICATION POST FLIGHT REPORTS. SEE ATTACHED PICTURES. PLEASE CONTACT TOMC BEFORE COMME
- [SDR CALA2022103102993](https://openairdocs.org/sdr/CALA2022103102993.md): Actuator · fault message · Oct 30, 2022 · N813UA · Airbus A319131 · Compressor Bleed Valve
  > COMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. - ENG ENG 1 ON INITIAL TO ROLL PERFORMED FADEC 1A&B BITE AND FOUND CHA AND CHB VSV ACT/HC/EEC1 REMOVED #1 ENG VSV ACTUATOR AS PER AMM 75-32-41-000-010-A. INSTALLED VSV ACTUATOR PER AMM 75-32-41-400-010..NEED TO P
- [SDR CALA2021100601806](https://openairdocs.org/sdr/CALA2021100601806.md): Engine · none · Oct 6, 2021 · N485UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > 4285-2 ESN V10979 DUE TO IFSD ACCOMPLISH WINDMILL INSPECTION PER AMM 72-00-00-200-021 4.A.(2)(B). REPORT FINDINGS TO TOMC EMC. FLAGGING SDR FOR FLT 2369-01 PERFORMED WINDMILL INSPECTION PER AMM 72-00-00-200-0214. A (2) (B), REPLACED MAIN PUMP OIL FILTER AND SC
- [SDR YENA2020121700606](https://openairdocs.org/sdr/YENA2020121700606.md): Engine · vibration · Dec 13, 2020 · N635JB · Airbus A320232 · Engine (Turbine/Turboprop)
  > FLT 280, PBI-BOS. RETURNED TO FIELD. ABNORMAL AIRFRAME VIBRATION ON CLIMBOUT THROUGH FL250 UP TO LEVEL OFF AT FL310. ENGINE 2 N1 VIB 1.8, ENGINE 1 N1 BIV.4. FELT MORE LIKE FLT CONTROL FLUTTERING. NO ABNORMAL ECAMS. HYD, FLT CONTROLS READ NORMAL. SUPPLE
- [SDR AALA202011149001](https://openairdocs.org/sdr/AALA202011149001.md): Beam · cracked · Nov 13, 2020 · N802AW · Airbus A319132 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE. NR 1 ENGINE PYLON AFT BEAM HANGER IS CRACKED. REPLACED NR 1 ENGINE PYLON AFT INBOARD HANGER BEAM, PER AMM 54-51-17.
- [SDR AALA202011149002](https://openairdocs.org/sdr/AALA202011149002.md): Beam · cracked · Nov 13, 2020 · N802AW · Airbus A319132 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE. NR 1 ENGINE PYLON CENTER INBOARD BEAM HANGER IS CRACKED. REPLACED NR 1 ENGINE PYLON CENTER INBOARD HANGER BEAM, PER AMM 54-51-17.
- [SDR AALA202011149003](https://openairdocs.org/sdr/AALA202011149003.md): Beam · cracked · Nov 13, 2020 · N802AW · Airbus A319132 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE. NR 1 ENGINE PYLON AFT OUTBOARD BEAM HANGAR IS CRACKED. REPLACED NR 1 ENGINE PYLON AFT OUTBOARD BEAM HANGER, PER AMM 54-51-17-401.
- [SDR AALA2019120549008](https://openairdocs.org/sdr/AALA2019120549008.md): Actuator · faulty · Dec 3, 2019 · N657AW · Airbus A320232 · Turbine Engine Compressor Section
  > AIRCRAFT WAS GROUNDED: PILOT REPORTS APPLIED T/O POWER ENG 2 COMPRESSOR VANE FAULT. EXIT RWY AND SHUTDOWN. CLASS 2 MESSAGE, ENGINE 2 FADEC. MAINTENANCE PERFORMED REMOVAL AND INSTALLATION OF ENGINE 2 VSV ACTUATOR IAW JOB CARD 26T40075005 AND 26L00071014. OKAY F
- [SDR YENA2019120280685](https://openairdocs.org/sdr/YENA2019120280685.md): Relay · failed · Nov 28, 2019 · N613JB · Airbus A320232 · Engine Pressure Ratio (EPR)
  > FT # 1416, LGB-AUS. RETURNED TO FIELD. ENG 2 EPR MODE FAULT ON CLIMBOUT; R & R RELAY BOX 4100KS ENG #2 AS PER AMM 71-51-49. IDLE RUN NO FAULT BITE PASS.
- [SDR GTIA2016072101511](https://openairdocs.org/sdr/GTIA2016072101511.md): Seal · leaking · Jul 21, 2016 · N512NK · Airbus A319132 · Turbine Engine Oil System
  > ODORIN CABIN AND COCKPIT DURING TAXI IN ON NR 1 ENGINE, COCKPIT CREW SMELLED EXHAUST FUMES, ASKED FA'S ABOUT ODORS. THEY ALL SAID THEY SMELLED ODORS OF MUSTY, DIRTY SOCKS. THE 2 AFT F/A'S THEN SAID THAT DURING CLIMBOUT, THERE WAS A MUSTY ODOR. DE-BRIEFED CAP
- [SDR GTIA2016070101497](https://openairdocs.org/sdr/GTIA2016070101497.md): Packing · leaking · Jul 1, 2016 · N504NK · Airbus A319132 · Turbine Engine Oil System
  > AFT F/A REPORTS BURNING RUBBER ODOR IN CABIN. ODOR DISAPPEARED ONLY WHEN NR 2 BLEED CLOSED. RAN NR 1 & 2 ENGINES WITH BOTH PACKS ON AND CYCLED BOTH ENGINE BLEEDS. NO ODOR NOTICED AT THIS TIME. AFTER SHUTTING DOWN ENGINES, NOTICED EXCESSIVE POOLING OF OIL
- [SDR USAA2014080400012](https://openairdocs.org/sdr/USAA2014080400012.md): Door · loose · Aug 1, 2014 · N644AW · Airbus A320231 · Fluid Service Doors
  > ON REACHING LEVEL OFF AT 35000 FT, NR 1 ENGINE VIBRATION EXCEEDED 5.0 N1, IT REACHED A MAXIMUM OF 6.2. REDUCED POWER TO KEEP VIBRATION BELOW 5.0 IAW TSM 77-30-00-810-826A. FOUND NR 1 ENG OIL SERVICE DOOR LOOSE & HAS PLAY. REPLACED ENGINE OIL SERVICE DOOR &
- [SDR IU5R2014032800001](https://openairdocs.org/sdr/IU5R2014032800001.md): Fuel Nozzle · cracked · Mar 21, 2014 · Airbus A320* · Fuel Injector Nozzle
  > DURING INVESTIGATION ON FUEL NOZZLES IAW CMM 73-13-41. ENGINEERING REVIEW PRIOR REPAIR CONDITIONS OF CIRCUMFERENTIAL CRACKS, CC ON THE OUTER AIR SWIRLER, OAS, SIDE OF EB WELD JOINT TO THE END CAP BAFFLE, ECB, IT WAS APPARENT BY OAS ADJACENT MATERIAL CONDITION
- [SDR USAA2013121600018](https://openairdocs.org/sdr/USAA2013121600018.md): Unknown · odor · Dec 14, 2013 · N647AW · Airbus A320232 · Air Distribution System
  > FLT 657, VERY STRONG ODOR IN CABIN MAKING FLIGHT ATTENDANT ILL WITH RESPIRATORY IRRITATION. COMPLIED WITH JOB CARD 26L00021001 TROUBLE SHOT CABIN AIR QUALITY. FINDINGS ARE IN COMPLIANCE WITH JOB CARD.
- [SDR USAA2013121600015](https://openairdocs.org/sdr/USAA2013121600015.md): Actuator · inoperative · Dec 13, 2013 · N649AW · Airbus A320232 · Compressor Bleed Control
  > NR 1 ENGINE FAILURE AND SHUTDOWN ON DESCENT INTO IAH. RELIGHT ATTEMPTED, UNSUCESSFUL AND ENGINE SECURED FOR LANDING. PERFORMED IAW A320 TSM 71-00-00-810-808-A. REPLACED E1 VSV ACTUATOR, REPLACED 10TH STAGE SOLENOID VALVE.
- [SDR USAA2013121300011](https://openairdocs.org/sdr/USAA2013121300011.md): Vane · faulted · Dec 12, 2013 · N621AW · Airbus A320231 · Compressor Bleed Control
  > NUMBER 1 ENG COMPUTER VANE FAULT. VSV LUBE & FORCE CHECK PERFORMED IAW JOB CARD 26T40075001. ADDITIONAL TROUBLESHOOTING BEING ACCOMPLISHED IAW A320 TSM TASK 75-30-00-810-821-A. SUPPLEMENTAL TO FOLLOW FINAL CORRECTIVE ACTION.
- [SDR USAA2013022200001](https://openairdocs.org/sdr/USAA2013022200001.md): Engine · vibration · Feb 21, 2013 · N631AW · Airbus A320231 · Engine (Turbine/Turboprop)
  > IN CRUISE FL 340 NR 2 N1 VIRBRATION BRIEFLY EXCEEDED 5 UNITS, THRUST REDUCED TO KEEP VIBRATION BELOW 5. VIBRATION LEVELS RETURNED TO NORMAL AT 11-12 THOUSAND FEET. PERFORMED VIBRATION SUMMARY, NO DEFECTS NOTED, INSPECTED FOR FOD DAMAGE, NONE FOUND, INSPECTED
- [SDR USAA2012022800009](https://openairdocs.org/sdr/USAA2012022800009.md): Solenoid Valve · faulty · Feb 26, 2012 · N620AW · Airbus A320231 · Compressor Bleed Valve
  > REJECTED TAKEOFF AT 70-80 KNOTS DUE TO ENGINE 1 SYSTEM FAULT AND APPROX 645 EGT. AIRCRAFT HAD ANOTHER REJECTED TAKEOFF ON THE SAME FLIGHT JUST PRIOR TO THIS TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE HPC STAGE 10 SOLENOID VALVE (4023KS) IAW AIRBUS MAINTEN
- [SDR USAA2012011700023](https://openairdocs.org/sdr/USAA2012011700023.md): Pump · failed · Jan 12, 2012 · N632AW · Airbus A320231 · Engine Fuel Pump
  > ENGINE NR 2 MOMENTARILY FAILED DURING IDLE DESCENT AT FL200, 280 KNOTS. CREW FELT AIRCRAFT YAW AND REPORTED N2 AT APPROXIMATELY 30 PERCENT. UPON IGNITION ACTIVATION, ENGINE RELIT ITSELF AND CONTINUED TO OPERATE NORMALLY. MAINTENANCE REMOVED AND REPLACED THE
- [SDR USAA2012011000022](https://openairdocs.org/sdr/USAA2012011000022.md): Actuator · failed · Jan 8, 2012 · N632AW · Airbus A320231 · Compressor Bleed Valve
  > UPON THRUST REDUCTION TO CLIMB, NR 2 ENGINE HAD TWO COMPRESSOR STALLS BEFORE THRUST LEVER COULD BE MOVED TO IDLE. EGT EXCEEDED LIMITS; ENG 2 FAIL ON ECAM. NR 2 ENGINE WAS SHUTDOWN IAW ECAM ACTIONS, FIRE BOTTLE WAS DISCHARGED AND AIRCRAFT DIVERTED, (EMERGENCY
- [SDR USAA2012061900022](https://openairdocs.org/sdr/USAA2012061900022.md): Actuator · failed · Jan 8, 2012 · N632AW · Airbus A320231 · Compressor Bleed Control
  > UPON THRUST REDUCTION TO CLIMB, NR 2 ENGINE HAD TWO COMPRESSOR STALLS BEFORE THRUST LEVER COULD BE MOVED TO IDLE. EGT EXCEEDED LIMITS; ENG 2 FAIL ON ECAM. NR 2 ENGINE WAS SHUTDOWN IAW ECAM ACTIONS, FIRE BOTTLE WAS DISCHARGED AND AIRCRAFT DIVERTED TO LAX, (EM
- [SDR USAA2012010400021](https://openairdocs.org/sdr/USAA2012010400021.md): Transducer · failed · Jan 1, 2012 · N628AW · Airbus A320231 · Compressor Bleed Control
  > AFTER TAKEOFF PRIOR TO 1000', ENGINE NR 1 SURGED TWICE AND SELF-RECOVERED WITH NORMAL INDICATIONS. ON LANDING ROLLOUT, RECEIVED ECAM MESSAGES FOR ENG 1 COMPRESSOR VANE AND FADEC MX. TWO SUBSEQUENT EVENTS FOR NR 1 ENGINE SURGE ON TAKEOFF ON 1/3/12 AND 1/4/12.
- [SDR USAA2011090600025](https://openairdocs.org/sdr/USAA2011090600025.md): Pressure Switch · defective · Sep 2, 2011 · N622AW · Airbus A320231 · Hydraulic Pressure Relief Valve, Main
  > CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM ON DESCENT INTO PDX. CONDUCTED GRAVITY EXTENSION OF LANDING GEAR AND DECLARED AN EMERGENCY; PASSENGERS WERE NOT INSTRUCTED TO BRACE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP IAW AIRBUS MAINTENAN
- [SDR USAA2011090600028](https://openairdocs.org/sdr/USAA2011090600028.md): Pump · defective · Sep 2, 2011 · N622AW · Airbus A320231 · Hydraulic Pump (Electric/Engine), Main
  > CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM ON DESCENT INTO PDX. CONDUCTED GRAVITY EXTENSION OF LANDING GEAR AND DECLARED AN EMERGENCY; PASSENGERS WERE NOT INSTRUCTED TO BRACE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP IAW AIRBUS MAINTENAN
- [SDR EE4Y20110382](https://openairdocs.org/sdr/EE4Y20110382.md): Strap · worn · Jun 18, 2011 · N506NK · Airbus A319132 · Engine Air Intake System
  > ENGINE NR 2, FAN COWL, AIR INTAKE COWL, CAPPING STRAP UPPER AREA LT AND RT CORNERS WITH WEAR. NOTE: THE CAPPING STRAP WEAR REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.
- [SDR EE4Y20110384](https://openairdocs.org/sdr/EE4Y20110384.md): Fitting · cracked · Jun 18, 2011 · N506NK · Airbus A319132 · Nacelle/Pylon, Attach Fittings
  > ENGINE NR 1, PYLON AFT FIXED FAIRING, LOWER FWD SUPPORT FITTING WITH CRACK. MAJOR REPAIR IAW SRM.
- [SDR USAA2011032591231](https://openairdocs.org/sdr/USAA2011032591231.md): Compressor Blade · damaged · Mar 22, 2011 · N627AW · Airbus A320231 · Turbine Engine Compressor Section
  > FLT 51 - PHX - RTO - ON TAKEOFF ROLL AT ABOUT 110 KNOTS, CREW REPORTED A LOUD BANG AND THE AIRCRAFT VEERED SHARPLY TO THE RIGHT - TAKEOFF WAS REJECTED. PASSENGERS REPORTED SEEING FLAMES COMING OUT OF THE RIGHT ENGINE. MAINTENANCE FOUND NR 2 ENGINE HIGH PRES
- [SDR USAA2011031491044](https://openairdocs.org/sdr/USAA2011031491044.md): Actuator · stalled · Mar 10, 2011 · N622AW · Airbus A320231 · Turbine Engine Compressor Section
  > FLT 88 - CREW REPORTED NR 1 ENGINE COMPRESSOR STALL ON CLIMB WITH MAX EGT 720+ FOR ONE MINUTE. SHUT DOWN ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. THE ROOT CAUSE WAS IDENTIFIED AS THE VSV ACTUATOR WHI
- [SDR USAA2010092392080](https://openairdocs.org/sdr/USAA2010092392080.md): Lanyard · frayed · Sep 22, 2010 · N629AW · Airbus A320231 · Escape Slide
  > L2 DOOR SLIDE YELLOW COVER TIE CORDS FRAYED IN SVERAL SPOTS. REPLACED L2 DOOR SLIDE.
- [SDR USAA2009090892391](https://openairdocs.org/sdr/USAA2009090892391.md): Filter · contaminated · Sep 6, 2009 · N632AW · Airbus A320231 · Air Distribution System
  > FLT 128 - PHX - CABIN ODOR - NR 1 ENGINE IS PUTTING OILY SMELL IN THE AIRCRAFT - SMELLS LIKE DIRTY SOCKS. IT'S NOT BEING FILTERED OUT AND FLIGHT ATTENDANTS ADVISED SMELL IS REALLY BAD IN BACK OF AIRCRAFT. MAINTENANCE PERFORMED COMPRESSOR WASH AND REPLACED RE
- [SDR USAA2009090892404](https://openairdocs.org/sdr/USAA2009090892404.md): Filter · contaminated · Sep 6, 2009 · N632AW · Airbus A320231 · Air Distribution System
  > FLT 128 - PHX - CABIN ODOR - NR 1 ENGINE IS PUTTING OILY SMELL IN THE AIRCRAFT - SMELLS LIKE DIRTY SOCKS. IT'S NOT BEING FILTERED OUT AND FLIGHT ATTENDANTS ADVISED SMELL IS REALLY BAD IN BACK OF AIRCRAFT. MAINTENANCE PERFORMED COMPRESSOR WASH AND REPLACED RE
- [SDR USAA2009090892405](https://openairdocs.org/sdr/USAA2009090892405.md): Filter · contaminated · Sep 6, 2009 · N632AW · Airbus A320231 · Air Distribution System
  > FLT 128 - PHX - CABIN ODOR - NR 1 ENGINE IS PUTTING OILY SMELL IN THE AIRCRAFT - SMELLS LIKE DIRTY SOCKS. IT'S NOT BEING FILTERED OUT AND FLIGHT ATTENDANTS ADVISED SMELL IS REALLY BAD IN BACK OF AIRCRAFT. MAINTENANCE PERFORMED COMPRESSOR WASH AND REPLACED RE
- [SDR USAA2009081892154](https://openairdocs.org/sdr/USAA2009081892154.md): Engine · bird ingestion · Aug 17, 2009 · N644AW · Airbus A320231 · Turbine Engine Compressor Section
  > FLT 407 PHX-ATL - DIVERSION / BURNING SMELL - DIVERTED INTO MEMPHIS DUE TO STRONG BURNING PLASTIC SMELL IN CABIN THROUGHOUT CLIMB AND INTO CRUISE. MAINTENANCE FOUND EVIDENCE OF BIRD INGESTION IN NR 1 ENGINE ON STAGE 3 HIGH PRESSURE COMPRESSOR. PERFORMED COMP
- [SDR USAA2009062491571](https://openairdocs.org/sdr/USAA2009062491571.md): Bottle · low · Jun 24, 2009 · N632AW · Airbus A320231 · Passenger/Crew Doors
  > EMERGENCY EGRESS SYS - R-2 DOOR ASSIST BOTTLE NEEDS SERVICING. MX SERVICED R-2 DOOR ASSIST BOTTLE IAW MM 52-10-00-614-001. (K)
- [SDR USAA2009062291536](https://openairdocs.org/sdr/USAA2009062291536.md): Unknown · unknown · Jun 21, 2009 · N637AW · Airbus A320231 · Central Warning
  > REJECTED TAKEOFF AT 80 KTS DUE TO THRUST ASYMMETRY - LT INDICATION 1.390 RT 1320 - NO THRUST ASYMMETRY FELT IN LATERAL CONTROL INPUTS, ECAM WARNING. MX REPORTED ALL PARAMETERS NORMAL - NO MESSAGES AND NO SUBSEQUENT ISSUES TO DATE. (K)
- [SDR USAA2009042891000](https://openairdocs.org/sdr/USAA2009042891000.md): Blade · separated · Apr 23, 2009 · N644AW · Airbus A320231 · Turbine Engine Compressor Section
  > FLT 500 YYC-PHX - COMPRESSOR STALLS - NR 2 ENGINE EXPERIENCED TWO RAPID COMPRESSOR STALLS CLIMBING THROUGH FL340 IN SMOOTH AIR, VCM. TEMPORARILY LOST POWER. ENGINE QUICKLY SELF RECOVERED. NO LIMITS EXCEEDED. ENGINE CONTINUED NORMAL POWER THEREAFTER. RAN 3
- [SDR USAA2009030290477](https://openairdocs.org/sdr/USAA2009030290477.md): Blade · failed · Feb 28, 2009 · N644AW · Airbus A320231 · Turbine Engine Compressor Section
  > FLT 180 - WHILE CLIMBING THROUGH 23,000 FT THE FLIGHT CREW FELT 6 TO 12 STRONG JOLTS AND RECEIVED ECAM MESSAGES "NUMBER 1 ENGINE FAIL" THEN "NUMBER ONE ENGINE STALL". THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO MCI FOR MAINTENANCE. COMPLIED WITH (D
- [SDR GTIA0900006](https://openairdocs.org/sdr/GTIA0900006.md): Floorbeam · corroded · Jan 8, 2009 · N508NK · Airbus A319132 · Fuselage Main, Floor Beam
  > FR68 - FR70 FLOORBEAM CORRODED AT Y765.
- [SDR USAA920080920](https://openairdocs.org/sdr/USAA920080920.md): Bleed Valve · inoperative · Apr 27, 2008 · N637AW · Airbus A320231 · Compressor Bleed Valve
  > FLT NR 455 PHX-SLC - ATB - ON CLIMB-OUT AT ABOUT 7500 FT, CREW REPORTED TWO AUDIBLE LOUD BOOMS FROM THE NR 1 ENGINE. NO ECAM WARNINGS CAME UP. REDUCED POWER TO IDLE, ALL PARAMETERS REMAINED NORMAL INCLUDING OIL PRESSURE AND TEMPERATURE. AIRCRAFT RETURNED TO
- [SDR USAA920071255](https://openairdocs.org/sdr/USAA920071255.md): Metering Unit · faulty · Dec 1, 2007 · N637AW · Airbus A320231 · Fuel Control/Turbine Engines
  > FLT NR 9205 - TPA-PHX - IFSD - LEVEL OFF AT 5000' ON APPROACH TO PHX, RIGHT ENG DID NOT RESPOND TO AUTOTHRUST. ENGINE INDICATIONS WERE LESS THAN IDLE. PERFORMED ECAM ACTIONS TO SHUT DOWN NR 2 ENGINE. FUEL CONTROL DID NOT RESPOND TO NR 2 ENG MASTER. PUSHED
- [SDR GTIA200700017](https://openairdocs.org/sdr/GTIA200700017.md): Power Supply · no test · Jul 15, 2007 · N584NK · Airbus A321231 · Emergency Lighting
  > 14WL EMERGENCY LIGHTING SYSTEM POWER SUPPLY UNIT FAILED TEST. REPLACED SAME.
- [SDR AWXA200700720](https://openairdocs.org/sdr/AWXA200700720.md): Engine · flamed out · Jun 7, 2007 · N634AW · Airbus A320231 · Engine (Turbine/Turboprop)
  > EWR - PHX - IFSD - CREW REPORTED HEARING A "BANG" FOLLOWED BY THE NR 1 ENGINE SHUTTING DOWN. CREW INITIATED AN IN-FLIGHT RESTART OF THE NR 1 ENGINE, ENGINE STARTED AND UPON APPLICATION OF POWER ANOTHER BANG WAS HEARD FOLLOWED BY THE NR 1 ENGINE SHUTTING DOWN.
- [SDR YENA2007019](https://openairdocs.org/sdr/YENA2007019.md): A/C Pack · odor · Mar 22, 2007 · N589JB · Airbus A320232 · Cabin Cooling System
  > APRX 1645Z, NO VISIBLE SMOKE (BURNING RUBBER SMELL) DURING APPROACH QRH COMPLIED WITH MID CABIN. EMERGENCY DECLARED. SMELL SUBSIDED UPON EXITING TAXIWAY. EVACUATION WAS DEEMED NOT REQUIRED. PERFORMED TROUBLESHOOTING IAW TSM 24-00-00-810-823 AND TSM 23-39-00-81
- [SDR AWXA200700390](https://openairdocs.org/sdr/AWXA200700390.md): Engine · fire · Mar 19, 2007 · N626AW · Airbus A320231 · Engine (Turbine/Turboprop)
  > LAS - ESD - CREW REPORTED DURING CLIMB THEY HEARD A LOUD BANG FOLLOWED BY A RISING EGT INDICATION ON THE RIGHT ENGINE. THE FLIGHT ATTENDANTS REPORTED SPARKS AND FLAMES COMING FROM THE RIGHT ENGINE. THE ENGINE SHUT DOWN AND THE CREW DISCHARGED THE FIRE BOTTLE
- [SDR AWXA200601837](https://openairdocs.org/sdr/AWXA200601837.md): Fuel Control · failed · Oct 28, 2006 · N622AW · Airbus A320231 · Fuel Controlling System
  > FLIGHT 430: PHL - LAS - DURING CRUISE AT FL340, ECAM MESSAGE. ENGINE NR 1 FUEL CONTROL FAULT APPEARED ON ECAM. NR 1 ENG THRUST HAD RETARDED TO IDLE, ALL OTHER PARAMETERS NORMAL. ECAM MESSAGE ENG FAIL APPEARED AND ENGINE SHUT DOWN. ACCOMPLISHED ENG NR 1 REL

Next page: https://openairdocs.org/engine/iae-v2500-a1/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 engine_model_key = 'V2500A1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/iae-v2500-a1/reports

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