# IAE V2525-D5 - Type: Engine model (FAA registry) - Registry code: 34610 - Manufacturer (registry): IAE - Model: V2525-D5 - Engine type: Turbo-fan - Power: 25,000 lb thrust - Data sheet: [TCDS E40NE](https://openairdocs.org/tcds/E40NE) (OpenAirDocs) - Holder: International Aero Engines AG (IAE) - Installed in: 0 registered aircraft - Page: https://openairdocs.org/engine/iae-v2525-d5 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 2021-05-18](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 2019-16-01](https://openairdocs.org/ad/2019-16-01): Turbine section · International Aero Engines V2525-D5 and V2528-D5. Effective Sep 19, 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 2013-07-10](https://openairdocs.org/ad/2013-07-10): Bearing internal scavenge tube and bearing external scavenge tube · International Aero Engines V2525-D5 and V2528-D5. Effective May 20, 2013 - [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 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 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 99-04-03](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 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 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 (30) As reported by operators and repair stations, by the model named in the report. - [SDR DALA2019042402601](https://openairdocs.org/sdr/DALA2019042402601), Apr 23, 2019: ENGINE. MALFUNCTIONED. CLIMBING THROUGH 11000 FEET FELT STRONG YAW TO LEFT, N1 AND N2 ROLLED BACK, EGT HIGH ALL ON NBR 1 ENG. LOUD BANG. SHUT DOWN ENGINE PER QRH AND RETURNED TO PHL. - [SDR DALA2019022201123](https://openairdocs.org/sdr/DALA2019022201123), Feb 20, 2019: ENGINE. VIBRATION. LEFT ENGINE VIBRATION HIGH, 4.9 INDICATION. VIBRATION RETURNED TO .6 10 MINUTES AFTER THROTTLE RETARDED TO IDLE. C/W GVI OF FAN BLADES. NO DAMAGE. ALSO UT TAP T - [SDR DALA2018090705473](https://openairdocs.org/sdr/DALA2018090705473), Sep 5, 2018: ENGINE. FIRE. ATB, IFSD RIGHT ENGINE SURGE FOLLOWED BY FIRE INDICATION PASSING 14K. RAN QRH, DISCHARGED 2 FIRE BOTTLES INTO RT ENG. FIRE EXTINGUISHED AFTER 3 MINUTES. EGT REA - [SDR DALA2018082005151](https://openairdocs.org/sdr/DALA2018082005151), Aug 18, 2018: ENGINE. FAILED. RIGHT ENGINE COMPRESSOR STALL. RETURNED TO DEPARTURE. RIGHT ENGINE FAILED HPC BORESCOPE. REPLACED THE NR 2 ENGINE IAW AMDS 7100-4637-RH. - [SDR DALA2018031301586](https://openairdocs.org/sdr/DALA2018031301586), Mar 13, 2018: ENGINE. FAILED. AIR TURNBACK DUE TO A NR 1 ENGINE COMPRESSOR STALL AND BLUE FLAMES COMING FROM THE ENGINE AFTER TAKE-OFF, DURING CLIMB AT 2,300 FEET. THE FLIGHT CREW FOLLOWED T - [SDR DALA2016081706066](https://openairdocs.org/sdr/DALA2016081706066), Aug 8, 2016: ENGINE. FAULTED. ON SHORT FINAL, NR 1 EGT GAUGE BEGAN FLASHING AND INDICATED 699. EPR GAUGES DID NOT MATCH. LANDING WAS NORMAL. AFTER SHUTDOWN, EGT=708 WITH LT ENG SYS FAIL MESS - [SDR DALA14033579232](https://openairdocs.org/sdr/DALA14033579232), Jun 3, 2014: OIL SYSTEM. LEAKING. PERFORMED AN IN FLIGHT SHUTDOWN AND AN AIR TURN BACK DUE TO LT ENGINE OIL QUANTITY LOSS WITH OIL QTY INDICATION AT ZERO. MAINTENANCE FOUND OIL IN COWLING AND ON - [SDR DALA1116249217](https://openairdocs.org/sdr/DALA1116249217), Mar 8, 2011: COFFEEMAKER. ODOR. F/A REPORTED ELECTRICAL ODOR IN FIRST CLASS GALLEY. FLIGHT CREW PERFORMED QRH, PULLED THE GALLEY POWER SWITCH OFF, AND THE ODOR DISSIPATED. MX OPERATED FWD GALL - [SDR DLM90080035](https://openairdocs.org/sdr/DLM90080035), Jan 10, 2008: SKIN. CORRODED. RT FUSELAGE BENEATH LOWER FILLET FAIRING RUBSTRIP STATION 788 TO 883 HAS EVIDENCE OF CORROSION. NEED RUB STRIPS AND SEALANT REMOVED FOR FURTHER EVALUATION. COMP - [SDR UIAA010208001](https://openairdocs.org/sdr/UIAA010208001), Jan 2, 2008: ACTUATOR. MALFUNCTIONED. DURING TAXI,THE (R ENG SYS FAIL) MSG SHOW ON EOAP. BITE RT ENGINE EEC FND (VSV ACT/HC/EEC2) CLM MSG. IAW AMM 75-31-01 REPLACED R ENG VSV ACTUATOR. PERFORM R ENG - [SDR DLM90070861](https://openairdocs.org/sdr/DLM90070861), Jun 28, 2007: FLANGE. CRACKED. NR 2 ENGINE AFT LOWER INBOARD SECTION OF THRUST REVERSER V SEAL FLANGE HAS 16 INCH CRACK. REPLACED ENGINE. INSTALLATION TO BE COMPLIED WITH ON 1002751, 4000-010 - [SDR DLM90070863](https://openairdocs.org/sdr/DLM90070863), Jun 28, 2007: SHEAR TIE. CRACKED. L1 DOOR SHEAR TIE BEHIND DOOR INNER HANDLE IS CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW MD-90 SRM 51-30-02, 51-10-05 AND 51-30-05. - [SDR DLM90070862](https://openairdocs.org/sdr/DLM90070862), Jun 26, 2007: SKIN. GOUGED. LT WING FIXED L/E JUST I/B OF SLAT TRACK NR 9 SKIN IS GOUGED REPAIRED LT WING L/E IAW MD-90 SRM 57-20-01 FIG 11 VOL I. - [SDR DLM90070864](https://openairdocs.org/sdr/DLM90070864), Jun 25, 2007: CUSP WEB. CORRODED. RIGHT CUSP WEB STA 579-598 CORRODED OUT OF LIMITS. REMOVED DAMAGED CUSP WEB AND REPLACED WITH A SERVICEABLE WEB IAW THE MD 90 SRM 51-30-02, 51-30-01, 51-10-05 A - [SDR DLM90070865](https://openairdocs.org/sdr/DLM90070865), Jun 25, 2007: CUSP WEB. CORRODED. RIGHT CUSP WEB STA 503-579 CORRODED OUT OF LIMITS. REMOVED DAMAGED CUSP WEB AND REPLACED WITH A SERVICEABLE WEB IAW THE MD90 SRM 51-30-02, 51-30-01, 51-10-05, A - [SDR DLM90060666](https://openairdocs.org/sdr/DLM90060666), Aug 17, 2006: STARTER. OVERHEATED. APU AUTO SHUTDOWN ON TAXI OUT, ACS FAULT ON OAP, AND STRONG ELECTRICAL SMELL IN CABIN. INSTALLED NEW STARTER PER M/M. INSPECTED APU COMP. NO PROBLEMS NOTED. REP - [SDR DLM90050808](https://openairdocs.org/sdr/DLM90050808), Dec 20, 2005: STARTER. UNSERVICEABLE. ON APU START, APU FAULT DISPLAYED AND SMOKE COMING FROM TAIL COMPT. ON FURTHER INSP, SAW VISIBLE FLAME COMING FROM APU STARTER. FLAME WENT OUT AND NO EXTINGUISH - [SDR UIA0505](https://openairdocs.org/sdr/UIA0505), Jun 12, 2005: ENGINE. FAILED. RT ENGINE IN FLIGHT SHUTDOWN (IFSD) CAUSED BY SURGE MESSAGE SHOW ON EOAP, THEN FOLLOW EGT RAPID INCREASE. AFTER LANDING CHECK FOUND SEVERAL STAGE 4 BLADES MATER - [SDR UIA0502](https://openairdocs.org/sdr/UIA0502), Feb 2, 2005: SWITCH. JAMMED. IN FLT RADIO COMMUNICATION FAILURE (VHF NR 1 AND NR 2). AC AIR TURN BACK. MAINTENANCE CHECK FOUND RT CONTROL COLUMN PTT SW FUNCTION NO T GOOD. CAUSED RADIO SYST - [SDR UIA9216](https://openairdocs.org/sdr/UIA9216), Aug 5, 2003: BEARING. MAKING METAL. IN FLT, LT ENG OIL STRAINER CLOG MESSAGE SHOW ON EOAP AND OIL PRESSURE DROP TO (0) FAST, FLT CREW SHUTDOWN THE ENG MANUALLY, A/C DIVERTED ON BKI. METAL CHIP WAS - [SDR UIAFAA9201](https://openairdocs.org/sdr/UIAFAA9201), Feb 8, 2003: SCAVENGE PUMP. BROKEN. RT GEN OFF SHOW ON EOAP DURING THE FIGHT FROM MACAU TO SHANGHAI, AFTER LANDING LINE MAINTENANCE PERSONNEL REPORTED RT GEN BEARING FAIL WAS SHOWN ON EPCU AND HE - [SDR DLM90020837](https://openairdocs.org/sdr/DLM90020837), Jul 19, 2002: ENGINE. POWER LOSS. LEFT ENGINE POWER ROLLED BACK AND EGT 625. CREW FOLLOWED POM AND SHUT ENGINE DOWN. REPLACED NR 1 ENG PER M/M. - [SDR UIA02001](https://openairdocs.org/sdr/UIA02001), Feb 28, 2002: BEARING. DAMAGED. FLT 6182 FROM KNH TO TSA, PILOT REPORT R AC POWER FAULT SHOW ON EOAP AFTER LANDING MECHANIC CHECK FOUND BEARING DAMAGE OF ENGINE GEAR BOX, IAW AMM71-00-00. REPL - [SDR 2001UIA007](https://openairdocs.org/sdr/2001UIA007), Nov 6, 2001: COMPRESSOR. DAMAGED. IN FLIGHT, LT ENG SURGE, EGT HIGH TO 660 C, MAIN IDLE TO LAND (IDLE N2:68.5 EGT:426 N1:33 EPR:0.9). THE ENG PFM BSI FOUND STAGE 6 HPC DAMAGE. REPLACED SERVICEAB - [SDR DLM90992290](https://openairdocs.org/sdr/DLM90992290), Oct 18, 1999: WIRE. SHORTED. PASSING 28,000 STATUS LT AND RT ENG SYSTEM FAIL MESSAGE CAME ON. ENG WENT INTO N1 DEFAULT MODE. EPR AND EPR LIMIT INDICATIONS WENT AWAY AND AUTO THROTTLES DISEN - [SDR DLM90990538](https://openairdocs.org/sdr/DLM90990538), Mar 12, 1999: ENGINE. FAILED. LEFT ENGINE FAILURE WHEN T/O POWER APPLIED. REPLACED ENGINE. - [SDR ORJA98314](https://openairdocs.org/sdr/ORJA98314), Dec 16, 1998: EEC. MALFUNCTIONED. IN SJC - AT 40-50 KNOTS ON TAKEOFF ROLL AUTO THROTTLES ON, ENGINES SPOOLING UP AT 1.35 EPR ON LEFT AND RIGHT. RIGHT ENGINE THEN STARTED TO SPOOL DOWN (ROLL BACK - [SDR ORJA9865](https://openairdocs.org/sdr/ORJA9865), Mar 17, 1998: ENGINE. OVERTEMP. ON TAKEOFF ROLL, BELOW 20 KTS, ENGINES JUST SPOOLED, LEFT ENGINE EGT REACHED 663 DEGREES PEAK, AFTER FUEL LEVER SHUT OFF AND TAKEOFF REJECTED. OPENED UPPER AND - [SDR DLM90970232](https://openairdocs.org/sdr/DLM90970232), Feb 6, 1997: INLET. DIRTY. SULFUR SMELL IN CABIN. DIVERTED TO ONT. OIL FOUND IN APU INLET. DEFERRED APU INOP. FLIGHT CONT'D TO SLC. CLEANED APU INLET, PERFORMED BURN-OUT, NO ODORS. - [SDR DLM90960584](https://openairdocs.org/sdr/DLM90960584), Mar 14, 1996: EEC. FAILED. ON TAKEOFF ROLL AFTER ADVANCING THROTTLES, THE LEFT ENGINE SURGE LIGHT CAME ON WITH THE LEFT ENGINE IGNITION LIGHT. BOTH LIGHTS CAME ON AND OFF, 3 TIMES TOTAL. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.