# IAE V2500-A1

- Type: Engine model (FAA registry)
- Registry code: 34602
- Manufacturer (registry): IAE
- Model: V2500-A1
- Engine type: Turbo-fan
- Power: 24,800 lb thrust
- Data sheet: [TCDS E31NE](https://openairdocs.org/tcds/E31NE) (OpenAirDocs)
- Holder: International Aero Engines AG (IAE)
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/iae-v2500-a1

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2021-05-18](https://openairdocs.org/ad/2021-05-18): Turbine Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 8 more. Effective Apr 29, 2021
- [AD 2021-01-03](https://openairdocs.org/ad/2021-01-03): Turbine Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 8 more. Effective Jan 21, 2021
- [AD 2020-09-03](https://openairdocs.org/ad/2020-09-03): Turbine Engine Compressor Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 8 more. Effective May 29, 2020
- [AD 2016-19-05](https://openairdocs.org/ad/2016-19-05): High-pressure turbine (HPT) seal · International Aero Engines V2500-A1. Effective Oct 27, 2016
- [AD 2015-10-04](https://openairdocs.org/ad/2015-10-04): HPC stage 3 to 8 drum · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jul 1, 2015
- [AD 2011-25-08](https://openairdocs.org/ad/2011-25-08): High- pressure turbine (HPT) case burn-through events · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jan 17, 2012
- [AD 2010-06-18](https://openairdocs.org/ad/2010-06-18): Vortex reducers · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Apr 22, 2010
- [AD 2009-22-06](https://openairdocs.org/ad/2009-22-06): HPC stage 9-12 disc assembly · International Aero Engines V2500-A1, V2527E-A5, V2528-D5 and 1 more. Effective Nov 30, 2009
- [AD 2008-14-15](https://openairdocs.org/ad/2008-14-15): No. 4 bearing oil system components · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Aug 20, 2008
- [AD 2007-21-05](https://openairdocs.org/ad/2007-21-05): Monitoring of N2 vibration on all IAE V2500 series engines · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Nov 15, 2007
- [AD 2004-12-08](https://openairdocs.org/ad/2004-12-08): Airworthiness Limitations Section (ALS) · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jul 23, 2004
- [AD 99-25-03](https://openairdocs.org/ad/99-25-03): High Pressure Turbine Disks · International Aero Engines V2500-A1. Effective Jan 7, 2000
- [AD 99-13-01](https://openairdocs.org/ad/99-13-01): High Pressure Turbine (HPT) Stage 1 Inner Rotating Airseal (TOBI ID seal) · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 4 more. Effective Jun 25, 1999
- [AD 98-21-01](https://openairdocs.org/ad/98-21-01): Fan Blade · International Aero Engines V2500-A1. Effective Oct 21, 1998

Historical (superseded or no longer in force):

- [AD 2019-06-06](https://openairdocs.org/ad/2019-06-06) (historical): Turbine Engine Combustion Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Apr 12, 2019
- [AD 2012-09-09](https://openairdocs.org/ad/2012-09-09) (historical): High-pressure compressor (HPC) stage 3 to 8 drums · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jun 27, 2012
- [AD 2010-20-07](https://openairdocs.org/ad/2010-20-07) (historical): Initial and repetitive on-wing ultrasonic inspections · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Nov 1, 2010
- [AD 2000-12-05](https://openairdocs.org/ad/2000-12-05) (historical): Critical Life-Limited Parts · International Aero Engines V2500-A1, V2500-A5 Series (all) and V2500-D5 Series (all). Effective Aug 11, 2000
- [AD 99-08-11](https://openairdocs.org/ad/99-08-11) (historical): International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective May 13, 1999
- [AD 99-05-05](https://openairdocs.org/ad/99-05-05) (historical): High Pressure Turbine (HPT) Stage 1 and Stage 2 Disks · International Aero Engines V2500-A1. Effective Apr 30, 1999

## Information bulletins (advisory) (1)

- [SAIB 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## Registered aircraft

None registered with this engine model now.

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (306, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2026FA0000291](https://openairdocs.org/sdr/2026FA0000291), Apr 24, 2026: CASE. UNSERVICEABLE. IBERIA MAINTENANCE HAS RECEIVED A NOTIFICATION FROM AN EXTERNAL REPAIR STATION (FAA DLAY225D LUFTHANSA TECHNIK AG (“LHT”) TO INFORM OF AN OCCURRENCE STATING THA
- [SDR 2025FA0000822](https://openairdocs.org/sdr/2025FA0000822), Dec 12, 2025: UNKNOWN. UNKNOWN. THE PARTS RECORDED UNDER EASA FORM 1 TRACKING NR 44543 AND 44538 HAVE BEEN DETECTED AS SUSPICIOUS. DISCREPANCY ON MISSING SIGNATURE, (SECTION 14B), APPROVAL/CER
- [SDR CALA2024083000519](https://openairdocs.org/sdr/CALA2024083000519), Aug 28, 2024: ENGINE. UNKNOWN. 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
- [SDR CALA2022112803241](https://openairdocs.org/sdr/CALA2022112803241), Nov 28, 2022: MODULE. DAMAGED. *EMERGENCY DECLARED* BIRDSTRIKE ENG 2 ENGINE #2 SN V10989 HAD BIRDSTRIKE ON TAKEOFF. ONLY PARAMETERS CHANGE WAS VIBRATION. ENGINE WAS NOT SHUTDOWN, BROUGHT BACK
- [SDR CALA2022112503227](https://openairdocs.org/sdr/CALA2022112503227), Nov 25, 2022: DRAIN LINE. DAMAGED. 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), Nov 21, 2022: HARNESS. FAILED. 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 TAK
- [SDR CALA2022103102993](https://openairdocs.org/sdr/CALA2022103102993), Oct 30, 2022: ACTUATOR. FAULT MESSAGE. 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 EN
- [SDR CALA2021100601806](https://openairdocs.org/sdr/CALA2021100601806), Oct 6, 2021: ENGINE. NONE. 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 PERF
- [SDR YENA2020121700606](https://openairdocs.org/sdr/YENA2020121700606), Dec 13, 2020: ENGINE. VIBRATION. 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. FE
- [SDR AALA202011149001](https://openairdocs.org/sdr/AALA202011149001), Nov 13, 2020: BEAM. CRACKED. 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), Nov 13, 2020: BEAM. CRACKED. 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), Nov 13, 2020: BEAM. CRACKED. 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), Dec 3, 2019: ACTUATOR. FAULTY. 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 PERFORME
- [SDR YENA2019120280685](https://openairdocs.org/sdr/YENA2019120280685), Nov 28, 2019: RELAY. FAILED. 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), Jul 21, 2016: SEAL. LEAKING. 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, D
- [SDR GTIA2016070101497](https://openairdocs.org/sdr/GTIA2016070101497), Jul 1, 2016: PACKING. LEAKING. 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 BLEED
- [SDR USAA2014080400012](https://openairdocs.org/sdr/USAA2014080400012), Aug 1, 2014: DOOR. LOOSE. 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 77-30-0
- [SDR IU5R2014032800001](https://openairdocs.org/sdr/IU5R2014032800001), Mar 21, 2014: FUEL NOZZLE. CRACKED. 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, S
- [SDR USAA2013121600018](https://openairdocs.org/sdr/USAA2013121600018), Dec 14, 2013: UNKNOWN. ODOR. FLT 657, VERY STRONG ODOR IN CABIN MAKING FLIGHT ATTENDANT ILL WITH RESPIRATORY IRRITATION. COMPLIED WITH JOB CARD 26L00021001 TROUBLE SHOT CABIN AIR QUALITY. F
- [SDR USAA2013121600015](https://openairdocs.org/sdr/USAA2013121600015), Dec 13, 2013: ACTUATOR. INOPERATIVE. 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. 
- [SDR USAA2013121300011](https://openairdocs.org/sdr/USAA2013121300011), Dec 12, 2013: VANE. FAULTED. NUMBER 1 ENG COMPUTER VANE FAULT. VSV LUBE & FORCE CHECK PERFORMED IAW JOB CARD 26T40075001. ADDITIONAL TROUBLESHOOTING BEING ACCOMPLISHED IAW A320 TSM TASK 75-
- [SDR USAA2013022200001](https://openairdocs.org/sdr/USAA2013022200001), Feb 21, 2013: ENGINE. VIBRATION. 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 FE
- [SDR USAA2012022800009](https://openairdocs.org/sdr/USAA2012022800009), Feb 26, 2012: SOLENOID VALVE. FAULTY. 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 TAK
- [SDR USAA2012011700023](https://openairdocs.org/sdr/USAA2012011700023), Jan 12, 2012: PUMP. FAILED. 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 ACTIVA
- [SDR USAA2012011000022](https://openairdocs.org/sdr/USAA2012011000022), Jan 8, 2012: ACTUATOR. FAILED. 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 
- [SDR USAA2012061900022](https://openairdocs.org/sdr/USAA2012061900022), Jan 8, 2012: ACTUATOR. FAILED. 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 
- [SDR USAA2012010400021](https://openairdocs.org/sdr/USAA2012010400021), Jan 1, 2012: TRANSDUCER. FAILED. 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 COMPRESS
- [SDR USAA2011090600025](https://openairdocs.org/sdr/USAA2011090600025), Sep 2, 2011: PRESSURE SWITCH. DEFECTIVE. CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM ON DESCENT INTO PDX. CONDUCTED GRAVITY EXTENSION OF LANDING GEAR AND DECLARED AN EMERGENCY; PASSENGERS WERE NOT INS
- [SDR USAA2011090600028](https://openairdocs.org/sdr/USAA2011090600028), Sep 2, 2011: PUMP. DEFECTIVE. CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM ON DESCENT INTO PDX. CONDUCTED GRAVITY EXTENSION OF LANDING GEAR AND DECLARED AN EMERGENCY; PASSENGERS WERE NOT INS
- [SDR EE4Y20110382](https://openairdocs.org/sdr/EE4Y20110382), Jun 18, 2011: STRAP. WORN. 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 GUIDE
- [SDR EE4Y20110384](https://openairdocs.org/sdr/EE4Y20110384), Jun 18, 2011: FITTING. CRACKED. ENGINE NR 1, PYLON AFT FIXED FAIRING, LOWER FWD SUPPORT FITTING WITH CRACK. MAJOR REPAIR IAW SRM.
- [SDR USAA2011032591231](https://openairdocs.org/sdr/USAA2011032591231), Mar 22, 2011: COMPRESSOR BLADE. DAMAGED. 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. PASSENGE
- [SDR USAA2011031491044](https://openairdocs.org/sdr/USAA2011031491044), Mar 10, 2011: ACTUATOR. STALLED. 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. MA
- [SDR USAA2010092392080](https://openairdocs.org/sdr/USAA2010092392080), Sep 22, 2010: LANYARD. FRAYED. L2 DOOR SLIDE YELLOW COVER TIE CORDS FRAYED IN SVERAL SPOTS. REPLACED L2 DOOR SLIDE.
- [SDR USAA2009090892391](https://openairdocs.org/sdr/USAA2009090892391), Sep 6, 2009: FILTER. CONTAMINATED. 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 ADVI
- [SDR USAA2009090892404](https://openairdocs.org/sdr/USAA2009090892404), Sep 6, 2009: FILTER. CONTAMINATED. 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 ADVI
- [SDR USAA2009090892405](https://openairdocs.org/sdr/USAA2009090892405), Sep 6, 2009: FILTER. CONTAMINATED. 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 ADVI
- [SDR USAA2009081892154](https://openairdocs.org/sdr/USAA2009081892154), Aug 17, 2009: ENGINE. BIRD INGESTION. FLT 407 PHX-ATL - DIVERSION / BURNING SMELL - DIVERTED INTO MEMPHIS DUE TO STRONG BURNING PLASTIC SMELL IN CABIN THROUGHOUT CLIMB AND INTO CRUISE. MAINTENANCE F
- [SDR USAA2009062491571](https://openairdocs.org/sdr/USAA2009062491571), Jun 24, 2009: BOTTLE. LOW. 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), Jun 21, 2009: UNKNOWN. UNKNOWN. 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
- [SDR USAA2009042891000](https://openairdocs.org/sdr/USAA2009042891000), Apr 23, 2009: BLADE. SEPARATED. FLT 500 YYC-PHX - COMPRESSOR STALLS - NR 2 ENGINE EXPERIENCED TWO RAPID COMPRESSOR STALLS CLIMBING THROUGH FL340 IN SMOOTH AIR, VCM. TEMPORARILY LOST POWER. ENG
- [SDR USAA2009030290477](https://openairdocs.org/sdr/USAA2009030290477), Feb 28, 2009: BLADE. FAILED. 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 S
- [SDR GTIA0900006](https://openairdocs.org/sdr/GTIA0900006), Jan 8, 2009: FLOORBEAM. CORRODED. FR68 - FR70 FLOORBEAM CORRODED AT Y765.
- [SDR USAA920080920](https://openairdocs.org/sdr/USAA920080920), Apr 27, 2008: BLEED VALVE. INOPERATIVE. 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 
- [SDR USAA920071255](https://openairdocs.org/sdr/USAA920071255), Dec 1, 2007: METERING UNIT. FAULTY. 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
- [SDR GTIA200700017](https://openairdocs.org/sdr/GTIA200700017), Jul 15, 2007: POWER SUPPLY. NO TEST. 14WL EMERGENCY LIGHTING SYSTEM POWER SUPPLY UNIT FAILED TEST. REPLACED SAME.
- [SDR AWXA200700720](https://openairdocs.org/sdr/AWXA200700720), Jun 7, 2007: ENGINE. FLAMED OUT. 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 STAR
- [SDR YENA2007019](https://openairdocs.org/sdr/YENA2007019), Mar 22, 2007: A/C PACK. ODOR. APRX 1645Z, NO VISIBLE SMOKE (BURNING RUBBER SMELL) DURING APPROACH QRH COMPLIED WITH MID CABIN. EMERGENCY DECLARED. SMELL SUBSIDED UPON EXITING TAXIWAY. EVACUA
- [SDR AWXA200700390](https://openairdocs.org/sdr/AWXA200700390), Mar 19, 2007: ENGINE. FIRE. 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
- [SDR AWXA200601837](https://openairdocs.org/sdr/AWXA200601837), Oct 28, 2006: FUEL CONTROL. FAILED. 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 P

All 306: https://openairdocs.org/engine/iae-v2500-a1/reports.md

## STCs that may be installed (OpenAirDocs) (1)

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SE636NE](https://openairdocs.org/stc/SE636NE): Installation of thrust reverser/exhaust system. Rohr Inc

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