# IAE V2527E-A5

- Type: Engine model (FAA registry)
- Registry code: 34605
- Manufacturer (registry): IAE
- Model: V2527E-A5
- Engine type: Turbo-fan
- Power: 24,800 lb thrust
- Data sheet: [TCDS E40NE](https://openairdocs.org/tcds/E40NE) (OpenAirDocs)
- Holder: International Aero Engines AG (IAE)
- Installed in: 27 registered aircraft
- Page: https://openairdocs.org/engine/iae-v2527e-a5

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 2026-17-03](https://openairdocs.org/ad/2026-17-03): Turbine Engine Compressor Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Sep 24, 2026
- [AD 2025-19-13](https://openairdocs.org/ad/2025-19-13): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Oct 29, 2025
- [AD 2025-17-16](https://openairdocs.org/ad/2025-17-16): Turbine Engine Compressor Sections · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Oct 10, 2025
- [AD 2024-11-03](https://openairdocs.org/ad/2024-11-03): Turbine Engine · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Jun 26, 2024
- [AD 2022-02-09](https://openairdocs.org/ad/2022-02-09): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Mar 15, 2022
- [AD 2021-14-19](https://openairdocs.org/ad/2021-14-19): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Aug 5, 2021
- [AD 2021-11-51](https://openairdocs.org/ad/2021-11-51): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2527-A5 and 4 more. Effective Jul 19, 2021
- [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 2020-07-51](https://openairdocs.org/ad/2020-07-51): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 6 more. Effective Apr 28, 2020
- [AD 2019-18-01](https://openairdocs.org/ad/2019-18-01): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2527-A5 and 4 more. Effective Oct 15, 2019
- [AD 2017-14-07](https://openairdocs.org/ad/2017-14-07): Turbine Engine · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Aug 21, 2017
- [AD 2016-25-11](https://openairdocs.org/ad/2016-25-11): No. 3 bearing · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Jan 20, 2017
- [AD 2016-18-10](https://openairdocs.org/ad/2016-18-10): High- pressure turbine (HPT) stage 2 hub · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 6 more. Effective Oct 7, 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 2006-25-01](https://openairdocs.org/ad/2006-25-01): Master magnetic chip detector (MCD) · International Aero Engines V2522-A5, V2524-A5, V2527-A5 and 4 more. Effective Jan 8, 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 2000-22-07](https://openairdocs.org/ad/2000-22-07): High Pressure Turbine (HPT) · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 6 more. Effective Dec 6, 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 99-04-03](https://openairdocs.org/ad/99-04-03): High Pressure Compressor (HPC) Stage 9-12 Drum · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 5 more. Effective Apr 12, 1999

Historical (superseded or no longer in force):

- [AD 2021-11-15](https://openairdocs.org/ad/2021-11-15) (historical): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Jul 13, 2021
- [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 2003-11-23](https://openairdocs.org/ad/2003-11-23) (historical): Master magnetic chip detector (MCD) · International Aero Engines V2522-A5, V2524-A5, V2527-A5 and 3 more. Effective Jun 20, 2003
- [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

## 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 (27)

- [N1523](https://openairdocs.org/aircraft/N1523): [Msn 1523 LLC](https://openairdocs.org/faa-owner/MSN%201523%20LLC), [San Diego, CA](https://openairdocs.org/faa-place/CA/San%20Diego), built 2001, S/N 1523
- [N505VL](https://openairdocs.org/aircraft/N505VL): [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE), [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia), built 2011, S/N 4798
- [N506VL](https://openairdocs.org/aircraft/N506VL): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N 4828
- [N507VL](https://openairdocs.org/aircraft/N507VL): [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2011, S/N 4832
- [N508VL](https://openairdocs.org/aircraft/N508VL): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2011, S/N 4950
- [N509VL](https://openairdocs.org/aircraft/N509VL): [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE), [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia), built 2012, S/N 5062
- [N510VL](https://openairdocs.org/aircraft/N510VL): [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2012, S/N 5207
- [N511VL](https://openairdocs.org/aircraft/N511VL): [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2012, S/N 5212
- [N512VL](https://openairdocs.org/aircraft/N512VL): [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE), [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia), built 2012, S/N 5308
- [N513VL](https://openairdocs.org/aircraft/N513VL): [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE), [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia), built 2012, S/N 5322
- [N514VL](https://openairdocs.org/aircraft/N514VL): [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE), [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia), built 2012, S/N 5337
- [N515VL](https://openairdocs.org/aircraft/N515VL): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2012, S/N 5391
- [N518VL](https://openairdocs.org/aircraft/N518VL): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2013, S/N 5488
- [N519VL](https://openairdocs.org/aircraft/N519VL): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2013, S/N 5510
- [N520VL](https://openairdocs.org/aircraft/N520VL): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2013, S/N 5595
- [N521VL](https://openairdocs.org/aircraft/N521VL): [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2013, S/N 5651
- [N522VL](https://openairdocs.org/aircraft/N522VL): [Bank Of Utah Owner Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20OWNER%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2013, S/N 5776
- [N523VL](https://openairdocs.org/aircraft/N523VL): [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2014, S/N 6014
- [N524VL](https://openairdocs.org/aircraft/N524VL): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2014, S/N 6161
- [N525VL](https://openairdocs.org/aircraft/N525VL): [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2014, S/N 6332
- [N526VL](https://openairdocs.org/aircraft/N526VL): [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE), [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia), built 2015, S/N 6470
- [N527VL](https://openairdocs.org/aircraft/N527VL): [Wilmington Trust Na Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20NA%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2015, S/N 6705
- [N608NK](https://openairdocs.org/aircraft/N608NK): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2011, S/N 4902
- [N656JB](https://openairdocs.org/aircraft/N656JB): [Jetblue Airways Corp](https://openairdocs.org/faa-owner/JETBLUE%20AIRWAYS%20CORP), [Long Island City, NY](https://openairdocs.org/faa-place/NY/Long%20Island%20City), built 2007, S/N 3091
- [N659JB](https://openairdocs.org/aircraft/N659JB): [Jetblue Airways Corp](https://openairdocs.org/faa-owner/JETBLUE%20AIRWAYS%20CORP), [Long Island City, NY](https://openairdocs.org/faa-place/NY/Long%20Island%20City), built 2007, S/N 3190
- [N766JB](https://openairdocs.org/aircraft/N766JB): [Jetblue Airways Corp](https://openairdocs.org/faa-owner/JETBLUE%20AIRWAYS%20CORP), [Long Island City, NY](https://openairdocs.org/faa-place/NY/Long%20Island%20City), built 2008, S/N 3724
- [N794JB](https://openairdocs.org/aircraft/N794JB): [Jetblue Airways Corp](https://openairdocs.org/faa-owner/JETBLUE%20AIRWAYS%20CORP), [Long Island City, NY](https://openairdocs.org/faa-place/NY/Long%20Island%20City), built 2011, S/N 4904

## NTSB investigations (5)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA26WA177](https://openairdocs.org/ntsb/DCA26WA177), Apr 4, 2026: Airbus A320-232 (N794JB), Punta Cana, Dominican Republic, no damage
- [NTSB DCA23WA291](https://openairdocs.org/ntsb/DCA23WA291), May 11, 2023: Airbus A320-233 (N518VL), Monterrey, Mexico, incident, minor damage
- [NTSB ENG20WA037](https://openairdocs.org/ntsb/ENG20WA037), Jun 16, 2020: Airbus A320 (N526VL), Tijuana, Mexico, incident, no damage
- [NTSB ENG14IA028](https://openairdocs.org/ntsb/ENG14IA028), Sep 18, 2014: Airbus A320 232 (N656JB), Long Beach, CA, incident, minor damage. Probable cause: The probable cause of the engine failure and subsequent undercowl engine fire was due to the fatigue fracture of a high pressure turbine stage 2 disk blade retaining lug that released two blades…
- [NTSB DCA11WA099](https://openairdocs.org/ntsb/DCA11WA099), Sep 19, 2011: Airbus A320 (N493TA), Cusco, Peru, incident, no damage

## FAA accident and incident reports (5)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20260403003209A](https://openairdocs.org/incident/20260403003209A), Apr 3, 2026: Airbus A320-232 (N794JB), Punta Cana, No damage. The aircraft was descending from 8,000 to 3,000 feet on approach to Punta Cana international airport (mdpc) when it encountered unexpected, brief moderate…
- [Incident 20251203017349I](https://openairdocs.org/incident/20251203017349I), Dec 3, 2025: Airbus A320-232 (N656JB), Newark, NJ, Minor damage. On December 3, 2025 (2200L), jetblue flight 390 was in the final phase of flight on final approach to Newark Liberty international airport. At approximately…
- [Incident 20250618007919I](https://openairdocs.org/incident/20250618007919I), Jun 18, 2025: Airbus A320-232 (N794JB), San Juan, PR, Minor damage. On June 18,2025, at 2030 local, [privacy data omitted] an Airbus A-320 [privacy data omitted] departed Luis Munoz Marin International Airport (sju) for orlando…
- [Incident 20191022024209I](https://openairdocs.org/incident/20191022024209I), Oct 22, 2019: Airbus A320-233 (N499TA), Los Angeles, CA, Minor damage. On October 22, 2019 at lax, a hawaiian B-787 was taxing along taxiway c in front of [privacy data omitted] en route to lax-gua. At the time that the B-787…
- [Incident 20140918016799I](https://openairdocs.org/incident/20140918016799I), Sep 18, 2014: Airbus A320-232 (N656JB), Long Beach, CA, Minor damage. September 18, 2014, at approximately 0930 pacific standard time , N656JB, an Airbus A320-232 (msn 3091) operating as flt# 1416 from Long Beach, CA (lgb) to…

## Service difficulty reports (75, newest 50)

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

- [SDR 2026FA0000532](https://openairdocs.org/sdr/2026FA0000532), Jun 22, 2026: SLEEVE. DAMAGED. T/R ASSY OUT OF LIMIT WITH ISSUED REPAIRED. T/R ASSY LEADING EDGE SLEEVE OUT OF LIMIT WITH ISSUED REPAIRED CERTIFICATE. AFTER INSTALLATION OF NEW RECEIVED SERVI
- [SDR YENA2024122301578](https://openairdocs.org/sdr/YENA2024122301578), Dec 21, 2024: ACTUATOR. FAILED. FLT#8523, EWR-RDU. (AIRCRAFT DIVERTED TO JFK) 'DURING CLIMB OUT ENG 2 COMPRESSOR VANE ECAM MSG FOLLOWED BY ENG 2 STALL. BANG/THUD HEARD DURING STALL. ENGINE 2 R
- [SDR YENA2024030600360](https://openairdocs.org/sdr/YENA2024030600360), Mar 5, 2024: ENGINE. STALLED. FLT#621, BOS-PBI. (AIRCRAFT DECLARED AN EMERGENCY). '#1 ENGINE, ENGINE STALL ENGINE EGT 765 - SHUT DOWN.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR 2023FA0000030](https://openairdocs.org/sdr/2023FA0000030), Jan 16, 2023: BLOWER. FAULTED. DURING CLIMB FROM MGA TO MIA THE AIRCRAFT RETURNED TO MGA DUE TO VENT SKIN VALVE FAULT. VENT EXTRACT FAULT. VENT BLOWER FAULT. AT MGA STATION WAS INCLUDED OUTLE
- [SDR SOKF20211108003](https://openairdocs.org/sdr/SOKF20211108003), Nov 7, 2021: NONE. NONE. DURING TAKE OFF FROM SAL TO LAX THE AIRCRAFT REJECTED THE TAKE OF DUE TO UNRELIABLE SPEED CAPTAIN SIDE FOLLOWING TSM 34-13-00-810-998-B WAS PERFORMED CLEANING O
- [SDR SOKF20211108002](https://openairdocs.org/sdr/SOKF20211108002), Nov 6, 2021: CONTROL VALVE. DAMAGED. DURING CLIMB FROM BOG TO SAL THE AIRCRAFT RETURNED TO BOG DUE TO ECAM ADVISORY PRESS VENT SKIN OULET VALVE IN AMBER, CAB PRESS SYST 1 Y 2 RESETED NO SUCCESSFUL.
- [SDR SOKF20210608001](https://openairdocs.org/sdr/SOKF20210608001), Jun 6, 2021: PITOT HEAD. OBSTRUCTED. DURING TAKE OFF FROM MIA TO SAL THE TAKE OFF WAS REJECTED DUE TO AIRSPEED DISCREPANCY BETWEEN CAP PFD AND FO PFD DURING TAKE OFF ROLL. IN ACCORDANCE WITH TSM TA
- [SDR YENA2020082500433](https://openairdocs.org/sdr/YENA2020082500433), Aug 21, 2020: SEAL. LEAKING. FLT 206, BNA-BOS. LEVEL 1 ODOR EVENT SEE CABIN ODOR FOR DETAILS; TROUBLE SHOT PER TSM 71-00-00-810-801-A, FOUND DE-OILER CARBON SEAL LEAKING. R & R DE-OILER CAR
- [SDR SOKF2020030600000](https://openairdocs.org/sdr/SOKF2020030600000), Mar 4, 2020: PUMP. DAMAGED. DDURING FLIGHT FROM SAL TO SFO THE AIRCRAFT DIVERTED TO MEX DUE TO PILOT REPORT BLUE PUMP OVERHEAT AND BLUE HYDRAULIC SYSTEM WAS LOST AND ECAM WARNING MESSAGE C
- [SDR SOKF2020030200000](https://openairdocs.org/sdr/SOKF2020030200000), Feb 27, 2020: UNKNOWN. MALFUNCTIONED. AFTER TO FROM BOG TO LIM THE AIRCRAFT RETURNED TO BOG DUE TO ECAM WARNING MESSAGE AIR ENG 1 + 2 BLEED FAULT. IN ACCORDANCE WITH AMM 36-11-52 PB 401 PRV WAS REPL
- [SDR 5TTY20190417 0001](https://openairdocs.org/sdr/5TTY20190417%200001), Apr 13, 2019: REGULATOR. MALFUNCTIONED. DURING CRUISE PHASE OF FLIGHT, THE AIRCRAFT WAS TURNED BACK DUE TO THE LH ENGINE AIR BLEED FAULT. THE AIRCRAFT LANDED WITH NO INCIDENT NOR WEIGHT EXCEEDANCE. AT
- [SDR RJEF20190320001](https://openairdocs.org/sdr/RJEF20190320001), Mar 19, 2019: TRANSCEIVER. UNSERVICEABLE. DURING FLIGHT TPU146 (LIM-MED) THE AIRCRAFT HAD FAILURE OF RADAR SYSTEM AND RETURNED TO LIM FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED: "RA
- [SDR RJEF20190107001](https://openairdocs.org/sdr/RJEF20190107001), Jan 3, 2019: UNKNOWN. MALFUNCTIONED. DURING TAKE OFF PROCESS OF FLIGHT TP823 FROM LIM TO CUZ ENGINE 1 ACCELERATED LESSER IN COMPARISON WITH ENGINE 2, THE TAKE OFF WAS ABORTED AND RETURNED TO THE GA
- [SDR 5TTY2018110500001](https://openairdocs.org/sdr/5TTY2018110500001), Dec 4, 2018: HYDRAULIC SYSTEM. OVERSERVICED. DURING ENGINE START, PRIOR TO THE DEPARTURE OF THE AIRCRAFT FLIGHT AV503, PILOT REPORTED LOW PRESSURE ON BLUE HYDRAULIC SYSTEM; CONSEQUENTLY, THE AIRCRAFT WAS R
- [SDR YENA2018121014838](https://openairdocs.org/sdr/YENA2018121014838), Nov 14, 2018: PUMP. FAILED. FT # 1735, BOS-MSP. DIVERTED TO BUF. #2 ENG LO OIL PRESS NO SECONDARIES; REMOVED + REPLACED #2 ENG OIL PRESSURE PUMP ASSY PER AMM 79-21-41 LEAK/OPS GOOD ALSO FO
- [SDR SOKF20181116009](https://openairdocs.org/sdr/SOKF20181116009), Nov 12, 2018: GPS. FAULTED. DURING FLIGHT FROM LIM TO CUZ THE AIRCRAFT RETURN TO LIM DUE TO ECAM WARNING MESSAGE NAV GPS 1 FAULTGPS 1. AT LIM STATION TRANSFERRED TO DMI PAGE 06571 ITEM 2 I
- [SDR SOKF20181019008](https://openairdocs.org/sdr/SOKF20181019008), Oct 15, 2018: ANTI-ICE VALVE. DAMAGED. DURING FLIGHT FROM AQP TO CUZ THE AIRCRAFT DEVERTED TO LIM DUE TO ECAM WARNING WING ANTI-ICE FAULT AND BAD WEATHER AT CUZ STATION. AT LIM STATION PERFORMED TSM 
- [SDR SOKF2018100210006](https://openairdocs.org/sdr/SOKF2018100210006), Sep 28, 2018: FMC. DAMAGED. DURING TO FROM LIM TO JUL THE, TO WAS REJECTED DUE ECAM WARNING A/T OFF. REMOVED AND REPLACED FMGC IAW AMM 22-83-34-000-001-A AND AMM 22-83-34-400-001-A OP TEST
- [SDR SOKF20180927005](https://openairdocs.org/sdr/SOKF20180927005), Sep 23, 2018: AUTOTHROTTLE SYS. MALFUNCTIONED. DURING TO FROM LIM TO CUZ THE TO WAS REJECTED DUE TO A/THR INOP AND DURING T/O PWR CLB DO NOT SHOW INDICATION THRUST MODE AND FLEX TOGA. AUTO FLIGHT AUTO THRUST
- [SDR RJEF20180410002](https://openairdocs.org/sdr/RJEF20180410002), Apr 8, 2018: EGT INDICATION. ILLUMINATED. DURING ENGINE START, THE PILOT REPORTED THE NR 1 ENGINE EGT OVERLIMIT, DURING THE NR 1 ENGINE START, EGT INDICATION WENT TO MAX DISPLAYED EGT ON THE NEEDLE AND 
- [SDR SOKF20180304002](https://openairdocs.org/sdr/SOKF20180304002), Mar 1, 2018: ACTUATOR. DAMAGED. DURING TO FROM LIM TO AQP THE TO WAS REJECTED DUE TO ECAM MSG ENG 2 COMPRESSOR VANE. AT LIM STATION PERFORMED TSM 75-30-00-810-853-A REMOVED AND REPLACED OF THE
- [SDR RJEF20180219001](https://openairdocs.org/sdr/RJEF20180219001), Feb 16, 2018: ACTUATOR. MALFUNCTIONED. DURING CLIMB, HAD A WARNING MESSAGE OF THE NR 2 THRUST REVERSE UNLOCKED, RETURNED TO DEPARTURE. UNEVENTFUL LANDING. PERFORMED FAULT ANALISYS IAW TSM 78-30-00-81
- [SDR 5TTY2018012900001](https://openairdocs.org/sdr/5TTY2018012900001), Jan 29, 2018: CONTROLLER. FAULTED. AFTER T/O, THE AIRCRAFT WAS TURNED BACK TO DEPARTURE BASE DUE TO PRESSURE SYS 1 FAILURE AND UNABLE TO CONTROL PRESSURIZATION AFTER SWITCHING TO SYS 2. LANDING I
- [SDR RJEF20180110001](https://openairdocs.org/sdr/RJEF20180110001), Jan 9, 2018: ENGINE. MALFUNCTIONED. DURING FLIGHT, THE NR 1 ENGINE HAD A STALL CONDITION AND EGT OVERLIMIT, DUE THAT SITUATION THE AIRCRAFT DIVERTED. UNEVENTFUL LANDING. CARRIED OUT THE CORRESPOND
- [SDR RJEF20171110001](https://openairdocs.org/sdr/RJEF20171110001), Nov 8, 2017: OUTFLOW VALVE. MALFUNCTIONED. AFTER TAKEOFF, THE PILOT REPORTED THE CABIN PRESSURE SYSTEM 1 & 2 FAULTED. NR 1 ENGINE COMPRESSOR VANE DUE TO THAT SITUATION THE AIRCRAFT RETURNED TO DEPARTURE 
- [SDR RJEF20171012001](https://openairdocs.org/sdr/RJEF20171012001), Oct 11, 2017: THERMOCOUPLE. FAULTY. DURING THE NR 1 ENGINE START, EGT ROSE TO 780°C, INDICATION ON RED. DUE TO THAT SITUATION THE AIRCRAFT RETURNED TO THE GATE FOR MAINTENANCE. MAINTENANCE PERFORM
- [SDR RJEF20171005002](https://openairdocs.org/sdr/RJEF20171005002), Oct 2, 2017: INDICATION SYS. MALFUNCTIONED. DURING TAXI, THE PILOT REPORTED THE NR 1 ENGINE EGT EXCEEDED DURING TAXI TO 720°C, THEN THE TEMPERATURE DROPS TO -10°C, AFTER THAT INDICATION STABILIZED, THE AI
- [SDR SOKF20170818008](https://openairdocs.org/sdr/SOKF20170818008), Aug 16, 2017: FILTER. CONTAMINATED. DURING MAJOR CHECK, PERFORMED TASK CARD 731000-11-1, FOUND FUEL FILTER CONTAMINATED. FUEL FILTER ELEMENT WERE EVALUATED IAW AMM 73-12-42-210-061-A PARAGRAPH A I
- [SDR YENA201704300320](https://openairdocs.org/sdr/YENA201704300320), Apr 30, 2017: ENGINE. FAILED. AT TOP OF DESCENT, THERE WAS A BURNED MATERIAL ODOR IN THE COCKPIT. SOON DISSAPATED, AT 2200 MSL ON APPROACH A VERY STRONG DIRTY SOCK ODOR PERMEATED THE FLIGHT 
- [SDR SOKF20170307003](https://openairdocs.org/sdr/SOKF20170307003), Mar 4, 2017: VALVE. FAILED. AFTER TAKE OFF, THE AIRCRAFT RETURN TO DEPARTURE, DUE THE FAILURE OF THE VENT SKIN VALVE, ABOUT 5, 000 FT. FOLLOWED THE ECAM PROCEDURE AND THE LIMIT UP TO 10,00
- [SDR RJEF20170117001](https://openairdocs.org/sdr/RJEF20170117001), Jan 15, 2017: ADIRU. MALFUNCTIONED. DURING TAKEOFF PROCESS OF FLIGHT TA567 FROM JFK TO SAL, THE AIRCRAFT SHOWED FAILURE OF AIRSPEED AND ATL INDICATIONS, DUE THAT SITUATION THE TAKEOFF WAS ABORTED 
- [SDR 5TTY201609260001](https://openairdocs.org/sdr/5TTY201609260001), Sep 26, 2016: TRANSDUCER. FAILED. DURING FLIGHT, THE AIRCRAFT GENERATED THE FLT CONTROL ELAC 2 FAULT MESSAGE AND DUE TO DEFERRED ELAC 1, THE AIRCRAFT WAS DIVERTED. AFTER AN UNEVENTFULLY LANDING,
- [SDR RJEF20160708001](https://openairdocs.org/sdr/RJEF20160708001), Jul 7, 2016: LEVER. FAULTY. DURING CLIMB OF FLIGHT TP803, THE LANDING GEAR CONTROL LEVER DID NOT MOVE UP, DUE THAT REASON THE AIRCRAFT RETURNED TO DEPARTURE FOR MAINTENANCE. AFTER AN UNEVE
- [SDR RJEF20160422001](https://openairdocs.org/sdr/RJEF20160422001), Apr 19, 2016: SENSOR. FAULTY. DURING LANDING PROCEDURES, THE FLAPS BECAME JAMMED, THE PILOT ASKED FOR THE ACTIVATION OF THE EMERGENCY PROTOCOL AND LANDED WITHOUT INCIDENT IN THAT CONFIGURATI
- [SDR RJEF20160419001](https://openairdocs.org/sdr/RJEF20160419001), Apr 15, 2016: FCU. FAULTY. DURING CLIMB OF FLIGHT TA588, THE PILOT REPORTED FCU ALTITUDE UNABLE TO CHANGE ALTITUDES. DUE THAT SITUATION THE ACFT RETURNED. AFTER AN UNEVENTFUL LANDING, ONC
- [SDR RJEF201603220001](https://openairdocs.org/sdr/RJEF201603220001), Mar 22, 2016: CHECK VALVE. FAILED. DURING TAKEOFF, THE PILOT REPORTED OVERHEAT YELLOW HYDRAULIC RESERVOIR ECAM WARNING; HENCE THE ACFT TURN BACK TO AIRPORT. AT LANDING, THE PILOT REPORTED NO OVER
- [SDR RJEF20160118001](https://openairdocs.org/sdr/RJEF20160118001), Jan 16, 2016: WARNING SYSTEM. FALSE ACTIVATION. DURING PUSHBACK OF FLIGHT TA561, AT ENG STARTING THE PILOT REPORTED, ECAM WARNING ANTI-ICE FIRST OFFICER & STANDBY PITOT, DUE THAT SITUATION THE ACFT RETURNED T
- [SDR RJEF20151105001](https://openairdocs.org/sdr/RJEF20151105001), Nov 5, 2015: COMPUTER. MALFUNCTIONED. DURING CLIMB, THE PILOT REPORTED FLIGHT CONTROL RT & LT AILERON FAULT, FLIGHT CONTROL ALTN LAW & HENCE THE ACFT WAS RETURNED, LANDING WITH NO INCIDENTS. ONCE ON
- [SDR RJEF20150928001](https://openairdocs.org/sdr/RJEF20150928001), Sep 26, 2015: ACTUATOR. FAULTY. PREVIOUS TO DEPART AS FLIGHT TA561. THE ACFT SHOWED THE FOLLOWING NO DISPATCH FAILURE MSGS. FLIGHT CONTROL RUDDER TRAVEL LIMIT 2 FAULT MSG ON ECAM. FOR THIS FAI
- [SDR RJEF20150613001](https://openairdocs.org/sdr/RJEF20150613001), Jun 13, 2015: CONTROL LEVER. FAULTY. DURING THE DESCENT OF THE ACFT FLIGHT TA-397, THE LG LGCIU 1 & 2 FAULT MSG WAS TRIGGERED ON THE ECAM DISPLAY. THEREFORE, THE ACFT WAS DIVERTED TO ITS ALTERNATE 
- [SDR RJEF20150321001](https://openairdocs.org/sdr/RJEF20150321001), Mar 21, 2015: ACTUATOR. LEAKING. PRIOR TO ITS DEPARTURE, FOUND HYD LEAK FROM THE ENG 1 RT THRUST REVERSER LOCKING ACTUATOR. THE ACFT WAS HELD ON GND FOR THE ACTUATOR REPLACEMENT IAW AMM 78-32-4
- [SDR RJEF20141211001](https://openairdocs.org/sdr/RJEF20141211001), Dec 11, 2014: UNKNOWN. SMOKE. AFTER TAKEOFF, THE PILOT REPORTED SMOKE IN PAX CABIN SO THE ACFT WAS RETURNED TO AIRPORT. AFTER LANDING, THE PILOT REPORTED OVERWEIGHT LANDING 66.6 TONS. IAW TS
- [SDR RJEF20141031001](https://openairdocs.org/sdr/RJEF20141031001), Oct 29, 2014: ENGINE. STALLED. AFTER ARRIVAL, THE PILOT REPORTED A NR 2 ENGINE STALL. PERFORMED ENG 2 FULL TROUBLESHOOTING PROCEDURE DESCRIBED ON TSM 71-00-00-810-809-A WITH NO DISCREPANCIES 
- [SDR YENA20140918200](https://openairdocs.org/sdr/YENA20140918200), Sep 18, 2014: ENGINE. FAILED. AIR RETURN TO DEPARTURE DUE TO ENGINE NR 2 FAILURE AND FIRE CLIMBING THROUGH 8000'. NR 2 ENGINE WAS R & R IAW AMM 71-00-20. ENGINE RUN OK.
- [SDR RJEF20140901001](https://openairdocs.org/sdr/RJEF20140901001), Aug 28, 2014: ELEVATOR SYSTEM. VIBRATION. DURING CLIMB, THE PILOT REPORTED STRONG FUSELAGE VIBRATION DURING CLIMB, FLIGHT LEVEL 250, AIS 320 KTS & 0.74M, DIMINISH BY LOWERING AIS 270 KTS. THE ACFT RETUR
- [SDR RJEF20140818012](https://openairdocs.org/sdr/RJEF20140818012), Aug 15, 2014: WIRE HARNESS. FAULTY. DURING TAKEOFF PROCEDURES OF FLIGHT LR625 THE ACFT HAD THE FAILURE MSG ENG 1 SENSOR FAULT & AIR PACK 1 & 2 FAULT. THE TAKEOFF WAS REJECTED & THE ACFT RETURNED T
- [SDR RJEF20140623007](https://openairdocs.org/sdr/RJEF20140623007), Jun 22, 2014: THERMOCOUPLE. FAULTY. WHEN ARRIVING THE PILOT REPORTED THAT ENG 2 HAD ABNORMAL EGT INDICATION AROUND 220°C DIFFERENCE. DUE THAT REASON THE ACFT WAS HELD ON GND FOR MX. PERFORMED A FA
- [SDR RJEF20140527006](https://openairdocs.org/sdr/RJEF20140527006), May 27, 2014: WIRE HARNESS. CUT. PIC REPORTED DURING TAKEOFF BRAKE RELEASE MSG APPEARS THEREFORE, THE TAKEOFF WAS ABORTED. PIC REPORTED THRUST REVERSERS WERE USED BELOW 70 KNOTS. PERFORMED TSM 
- [SDR RJEF20140110002](https://openairdocs.org/sdr/RJEF20140110002), Jan 9, 2014: HANDLE. MALFUNCTIONED. ON ARRIVAL, PILOT REPORTED THAT THE LANDING GEAR LEVER STUCK IN DOWN POSITION UNTIL 1000 FT AFTER TAKEOFF. PERFORMED A FUNCTIONAL TEST OF THE LANDING GEAR, RETR
- [SDR RJEF20140108001](https://openairdocs.org/sdr/RJEF20140108001), Jan 5, 2014: ENGINE. VIBRATION. DURING CLIMB, PILOT REPORTED INTERMITTENT ADVISORY OF NR 1 ENGINE HIGH N1 VIBRATION, REACHED 7.2 UNITS, N2 VIBRATION REACHED 4.2 UNITS. AN OIL ODOR DETECTED. AC

All 75: https://openairdocs.org/engine/iae-v2527e-a5/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 SE1091NE](https://openairdocs.org/stc/SE1091NE): Installation of thrust reverser/exhaust system. Rohr Inc

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