# IAE V2528-D5

- Type: Engine model (FAA registry)
- Registry code: 34609
- Manufacturer (registry): IAE
- Model: V2528-D5
- Engine type: Turbo-fan
- Power: 28,000 lb thrust
- Data sheet: [TCDS E40NE](https://openairdocs.org/tcds/E40NE) (OpenAirDocs)
- Holder: International Aero Engines AG (IAE)
- Installed in: 2 registered aircraft
- Page: https://openairdocs.org/engine/iae-v2528-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 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 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 (2)

- [N931TB](https://openairdocs.org/aircraft/N931TB): [Boeing Company](https://openairdocs.org/faa-owner/BOEING%20COMPANY), [Renton, WA](https://openairdocs.org/faa-place/WA/Renton), built 1998, S/N 53532
- [N963DN](https://openairdocs.org/aircraft/N963DN): [Boeing Company](https://openairdocs.org/faa-owner/BOEING%20COMPANY), [Renton, WA](https://openairdocs.org/faa-place/WA/Renton), built 1999, S/N 53533

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (2)

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.

- [Incident 20150325004379I](https://openairdocs.org/incident/20150325004379I), Mar 25, 2015: Mcdonnell Douglas MD-90-30 (N949DN), Denver, CO, Minor damage. On 03/25/2015 at approximately 1000 hrs MDT, N949DN a mcdonald Douglas MD-90-30 had just started to be deiced by swiss port. The deice truck rolled into the…
- [Incident 20130624012709I](https://openairdocs.org/incident/20130624012709I), Jun 24, 2013: Boeing MD-90-30 (N963DN), Washington, DC, Minor damage. Delta airlines flight 1763, an MD-90, N963DN, departing Ronald Reagan Washington national airport (kdca) to minneapolis-st. paul international airport (kmsp),…

## Service difficulty reports (133, newest 50)

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

- [SDR DALA2019051002928](https://openairdocs.org/sdr/DALA2019051002928), May 9, 2019: ENGINE. FAILED. RT. ENGINE FAILED DURING CLIMB AT 5000 MSL. (0) OIL PRESSURE, EGT 980 AND RISING. SHUTDOWN NORMAL. REPLACED NUMBER 2 ENGINE ON LOG 1063040. (LP# 5691956)
- [SDR DALA2019032701928](https://openairdocs.org/sdr/DALA2019032701928), Mar 27, 2019: UNKNOWN. MALFUNCTIONED. CLIMBING OUT AT 250, 9000 FT POP FROM LEFT ENGINE STRONG SHUTTER, EGT AT 715+. FOLLOWED ENGINE FAILURE PROCEDURE. DID NOTICE FF AT 700LBS, EGT HAD DECREASED. SH
- [SDR DALA2018102206190](https://openairdocs.org/sdr/DALA2018102206190), Oct 18, 2018: STARTER. DISINTEGRATED. LEFT ENG DURING START NO N2 ROTATION GROUND CREW REPORTED SPARKS AND FLAMES. COMPLIED WITH MANUAL ABORTED START PROCEDURE PER QRH. FOUND STARTER DISINTEGRATED. 
- [SDR AN0R201810010008](https://openairdocs.org/sdr/AN0R201810010008), Sep 28, 2018: SKIN. DELAMINATED. AREAS OF DAMAGE (DISBONDS) EXIST COMMON TO THE C DUCT BONDED ASSEMBLY FWD AND AFT PERF SKIN AND INBOARD BIFUR FWD AND AFT OUTER SKIN AND OUTBOARD BIFUR FWD AND 
- [SDR DALA2018091405597](https://openairdocs.org/sdr/DALA2018091405597), Sep 12, 2018: GENERATOR. FAILED. ATB, LT VSCF FAILURE IN CRUISE WITH LT GEN OFF AND AC PWR FAULT. UNABLE TO START APU. EPCU FAULTED 'LEFT CONV EU FAIL' WITH LT CHANNEL NBPT AND LT CHANNEL UF TR
- [SDR AN0R201808259007](https://openairdocs.org/sdr/AN0R201808259007), Sep 9, 2018: SKIN. DEBONDED. AREAS OF DISBAND EXIST COMMON TO C-DUCT BONDED ASSY FWD AND AFT PERF SKINS AND FWD AND AFT IB BIFURCATION OUTER SKINS.
- [SDR DALA2018073104784](https://openairdocs.org/sdr/DALA2018073104784), Jul 28, 2018: SKIN. DEPARTED. ON T-OFF ACT INFORMED US A PIECE OF ALUMINUM/METAL PART WAS FOUND ON THE RUNWAY. INSPECTED AND FOUND NR 1 ENG CNA AFT INNER SKIN MISSING. INSTALLED SERVICEABLE 
- [SDR DALA2018062604228](https://openairdocs.org/sdr/DALA2018062604228), Jun 24, 2018: COMPRESSOR. DAMAGED. DIV - TO ICT FOR LEFT ENGINE COMPRESSOR STALL AT FLIGHT LEVEL 260. ASSOCIATED RISING EGT. ENGINE POWER REDUCED TO IDLE, COMPRESSOR STALLS DISCONTINUED. ENGINE W
- [SDR AN0R2018618006](https://openairdocs.org/sdr/AN0R2018618006), Jun 1, 2018: SKIN. DELAMINATED. AREAS OF DEBONDS EXIST COMMON TO THE C DUCT BONDED ASSEMBLY, FWD AND AFT SKIN AND FWD OTBD AND FWD AND AFT INBD BIFURCATION OUTER SKINS AND FWD INNER SKIN.
- [SDR AN0R20180328005](https://openairdocs.org/sdr/AN0R20180328005), Mar 5, 2018: SKIN. DELAMINATED. AREAS OF DEBONDED COMMON TO THE C DUCT BONDED ASSEMBLY, FWD AND AFT SKIN AND INBOARD BIFUR FWD AND AFT OUTER SKIN AND OUTBOARD BIFUR FWD AND AFT OUTER SKIN AND 
- [SDR AN0R20180326004](https://openairdocs.org/sdr/AN0R20180326004), Mar 2, 2018: SKIN. CORRODED. AREAS OF CORROSION, COMMON TO THE C DUCT BONDED ASSEMBLY, INBOARD BIFUR FWD AND AFT OUTER SKIN AND OUTBOARD BIFUR FWD AND AFT OUTER SKIN AND FWD INNER SKIN.
- [SDR AN0R20180228003](https://openairdocs.org/sdr/AN0R20180228003), Jan 2, 2018: SKIN. DELAMINATED. AREAS OF DAMAGE (DISBONDS) EXIST COMMON TO THE C DUCT BONDED ASSEMBLY FWD AND AFT PERF SKIN AND INBOARD BIFUR FWD AND AFT OUTER SKIN AND OUTBOARD BIFUR FWD AND 
- [SDR AN0R20171227016](https://openairdocs.org/sdr/AN0R20171227016), Nov 15, 2017: SKIN. DELAMINATED. AREAS OF DEBONDED DAMAGE COMMON TO THE C DUCT BONDED ASSEMBLY OTBD FWD BIFURCATION OUTER SKIN AND AFT INNER SKIN AND AFT AND FWD OUTER PERF SKINS.
- [SDR AN0R2018130002](https://openairdocs.org/sdr/AN0R2018130002), Nov 8, 2017: SKIN. DEBONDED. AREAS OF DEBONDING EXIST COMMON TO THE C DUCT BONDED ASSEMBLY, FWD AND AFT PERF SKIN AND AFT OTBD AND FWD INBD BIFURCATION OUTER SKIN. THE FWD, MID AND AFT CENT
- [SDR AN0R20181192001](https://openairdocs.org/sdr/AN0R20181192001), Nov 3, 2017: SKIN. CORRODED. AREAS OF DAMAGE (CORROSION) EXIST COMMON TO THE C DUCT BONDED ASSEMBLY INBOARD BIFUR FWD AND AFT OUTER SKIN AND OUTBOARD BIFUR FWD AND AFT OUTER SKIN AND AFT IN
- [SDR AN0R20171129014](https://openairdocs.org/sdr/AN0R20171129014), Oct 24, 2017: SKIN. CORRODED. AREAS OF CORROSION COMMON TO THE C DUCT BONDED ASSEMBLY AFT AND FWD OTBD AND FWD AND AFT INBD BIFURCATION OUTER SKINS AND FWD AND MID INNER SKINS.
- [SDR AN0R20171129015](https://openairdocs.org/sdr/AN0R20171129015), Oct 18, 2017: SKIN. DEBONDED. AREAS OF DEBONDING COMMON TO THE C DUCT BONDED ASSEMBLY FWD INNER SKIN AND DOUBLER AND MID BUMPER DOUBLER.
- [SDR AN0R20171005013](https://openairdocs.org/sdr/AN0R20171005013), Aug 29, 2017: SKIN. DELAMINATED. AREAS OF DEBONDING EXIST COMMON TO THE C DUCT BONDED ASSEMBLY, FWD AND AFT SKIN AND INBOARD BIFUR FWD AND AFT OUTER SKIN AND MID AND AFT INNER SKIN.
- [SDR DALA2017080806125](https://openairdocs.org/sdr/DALA2017080806125), Aug 4, 2017: ENGINE. MAKING METAL. IFSD OF NUMBER ONE ENGINE DUE TO AN OIL STRAINER CLOGGED MESSAGE. AIRCRAFT ARRIVED SAFELY IN SAN. SAN MAINTENANCE FOUND SIGNIFICANT METAL IN MAIN OIL FILTER AND
- [SDR DALA2017080205853](https://openairdocs.org/sdr/DALA2017080205853), Aug 1, 2017: OIL SYSTEM. LEAKING. DIVERTED DUE TO RT ENGINE OIL QUANTITY WENT TO ZERO AND OIL PRESSURE BELOW 60 PSI. FOLLOWED QRH IFSD OF RIGHT ENGINE. MAINTENANCE FOUND RIGHT ACOC LEAKING OIL. 
- [SDR DALA2017080205854](https://openairdocs.org/sdr/DALA2017080205854), Jul 27, 2017: OIL SYSTEM. EMPTY. PERFORMED AN AIR TURN BACK TO DEPARTURE DUE TO A NR 2 ENGINE OIL QUANTITY INDICATION OF ZERO. IFSD IAW QRH DUE TO LOSING OIL QUANTITY AND PRESSURE. ENGINE CHANG
- [SDR AN0R20170929012](https://openairdocs.org/sdr/AN0R20170929012), Jul 21, 2017: SKIN. DELAMINATED. AREAS OF DAMAGE (DISBONDS) EXIST COMMON TO THE C DUCT BONDED ASSEMBLY FWD AND AFT SKINS AND AFT AND FWD AND MID CENTER INNER SKINS.
- [SDR AN0R20170822011](https://openairdocs.org/sdr/AN0R20170822011), Jul 14, 2017: SKIN. DELAMINATED. AREAS OF DAMAGE EXIST COMMON TO THE C DUCT BONDED ASSEMBLY FWD AND AFT SKINS AND AFT AND FWD OTBD AND INBD BIFUR OUTER SKINS AND FWD CENTER INNER SKIN. DAMAGE A
- [SDR AN0R2017809010](https://openairdocs.org/sdr/AN0R2017809010), Jun 15, 2017: SKIN. DELAMINATED. AREAS OF DAMAGE EXIST COMMON TO THE C DUCT BONDED ASSEMBLY FWD AND AFT PERF SKINS AND AFT AND FWD OUTBOARD AND INBOARD BIFUR OUTER SKINS AND FWD CENTER INNER SK
- [SDR AN0R2017728008](https://openairdocs.org/sdr/AN0R2017728008), Jun 7, 2017: SKIN. DELAMINATED. AREAS OF DEBOND DAMAGE EXIST COMMON TO THE C DUCT BONDED ASSEMBLY FWD AND AFT SKIN AND FWD OTBD BIFURCATION OUTER SKIN. DAMAGE ALSO EXISTS TO THE CLOSURES.
- [SDR AN0R20170626007](https://openairdocs.org/sdr/AN0R20170626007), May 9, 2017: SKIN. DELAMINATED. AREAS DEBONDED, COMMON TO THE C DUCT BONDED ASSEMBLY, FWD SKIN AND FWD INNER SKIN AND DOUBLER. DAMAGE ALSO EXISTS TO THE CLOSURES.
- [SDR AN0R2017629008](https://openairdocs.org/sdr/AN0R2017629008), May 4, 2017: SKIN. DELAMINATED. AREAS OF DAMAGE EXIST COMMON TO THE C DUCT BONDED ASSEMBLY, FWD AND AFT SKIN, INBOARD AND OUTBOARD SIDEWALL FWD AND AFT OUTER SKINS AND MID CENTER INNER SKIN. D
- [SDR DALA2017040502841](https://openairdocs.org/sdr/DALA2017040502841), Apr 5, 2017: PUMP. FAILED. LEFT HYDRAULIC TEMP HIGH DURING CRUISE. TURNED ON TRANSFER PUMP PRESSURE WENT TO ZERO. LEFT ENGINE HYDRAULIC PUMP ON. PRESSURE IS ZERO. REMOVED AND REPLACED THE
- [SDR AN0R2017323005](https://openairdocs.org/sdr/AN0R2017323005), Feb 24, 2017: SKIN. DELAMINATED. AREAS OF DAMAGE (DISBONDS CORROSION) EXIST COMMON TO THE C DUCT BONDED ASSEMBLY INBOARD SIDEWALL FWD AND AFT OUTER SKINS AND OUTBOARD SIDEWALL FWD OUTER SKIN.
- [SDR DALA2017020801054](https://openairdocs.org/sdr/DALA2017020801054), Feb 2, 2017: OIL COOLER. LEAKING. NR 2 ENGINE OIL QUANTITY LOW. DECREASED TO 0 ON ARRIVAL. TEMPERATURE AND PRESSURE NORMAL. FOUND OIL COOLER LEAKING. REMOVED AND REPLACED #2 FUEL/OIL COOLER PER 
- [SDR AN0R2017403006](https://openairdocs.org/sdr/AN0R2017403006), Jan 18, 2017: SKIN. DELAMINATED. AREAS OF DAMAGE EXIST COMMON TO THE C DUCT BONDED ASSEMBLY, FWD AND AFT SKIN AND FWD INBOARD OUTER SIDEWALL SKIN. THE FWD CENTER INNER SKIN. THE MID CENTER INNE
- [SDR DALA2017011800449](https://openairdocs.org/sdr/DALA2017011800449), Jan 13, 2017: HYDRAULIC SYSTEM. PRESSURE LOSS. AFTER TAKE-OFF. RIGHT HYDRAULIC PRESSURE 0. QUANTITY WAS NORMAL. AN ALTERNATE GEAR EXTENSION WAS PERFORMED DUE TO THE RIGHT HYDRAULIC PRESSURE LOSS. EMERGENCY D
- [SDR DALA2016041803161](https://openairdocs.org/sdr/DALA2016041803161), Apr 16, 2016: TURBINE CASE. CRACKED. LEFT ENGINE AFT VIBRATOR ISOLATOR THERMAL OVERHEATING FROM CRACK IN TURBINE CASE. R & R AFT VIBRATIONS ISOLATOR IAW MM.
- [SDR Z3EY2016040100155](https://openairdocs.org/sdr/Z3EY2016040100155), Mar 15, 2016: HUB. DAMAGED. THIS ENGINE IS UNDERGOING MAINTENANCE. DURING ENGINE TEARDOWN THE T2 HUB COULD NOT BE REMOVED FROM THE T1 HUB DUE TO SEVERE DISTORTION OF THE T2 HUB SNOUT. SUSP
- [SDR DALA2016022401386](https://openairdocs.org/sdr/DALA2016022401386), Feb 21, 2016: OIL SYSTEM. LEAKING. UPON ENGINE SHUTDOWN, GROUND CREW REPORTED EXCESSIVE SMOKE COMING FROM NR 1 ENGINE TAIL PIPE. MAINTENANCE TROUBLESHOT. FOUND TURBINE EXHAUST BLADES WET WITH OIL
- [SDR DALA2016010500033](https://openairdocs.org/sdr/DALA2016010500033), Dec 30, 2015: PUMP. INOPERATIVE. ON APPROACH, WHEN LANDING GEAR LEVER WAS SELECTED DOWN, THERE WAS A 4 TO 5 SECOND DELAY IN EXTENSION. THE RT HYDRAULICS INDICATED ZERO THEN PRESSURIZATION RECOV
- [SDR Z3EY2015FA0000551](https://openairdocs.org/sdr/Z3EY2015FA0000551), Oct 13, 2015: BOLT. MISSING. DURING INDUCTION INSPECTION, IT WAS NOTED THE FRONT VSVA CRANKSHAFT HOUSING SUPPORT BRACKET WAS MISSING ONE MOUNTING BOLT AND THE BRACKET WAS HANGING DOWN BY 2-
- [SDR DALA2015100806005](https://openairdocs.org/sdr/DALA2015100806005), Oct 3, 2015: ENGINE. MAKING METAL. ACFT DIVERTED DUE TO THE NR 2 ENGINE ROLLED BACK TO IDLE DURING CRUISE AT FL 310. DECLARED EMERGENCY AFTER FOLLOWING QRH. MAINTENANCE FOUND METAL IN THE TAILPIP
- [SDR DALA2015072904745](https://openairdocs.org/sdr/DALA2015072904745), Jul 27, 2015: STRUCTURE. LEAKING. DIVERTED DUE TO OIL FUME ODOR IN CABIN. RT GENERATOR OFF AND RT AC POWER FAULT WITH CORRESPONDING LOSS OF AC POWER. RT GENERATOR OVERHEAT STATUS MESSAGE ON EOAP
- [SDR DALA2015062103894](https://openairdocs.org/sdr/DALA2015062103894), Jun 20, 2015: NOSE COWL. DAMAGED. RIGHT ENGINE NOSE COWL DAMAGED BY FOD EVENT. R & R NOSE COWL IAW AMM. PERFORMED ANTI-ICE CHECK.
- [SDR DALA2015062203896](https://openairdocs.org/sdr/DALA2015062203896), Jun 20, 2015: BLADE. DAMAGED. NR 2 ENGINE HAS FOD DAMAGE TO SEVERAL BLADES AND NOSE COWL. R & R 1ST STAGE FAN BLADES IAW AMM. PERFORMED VIBE SURVEY AND FAN BALANCE IAW AMM. CHECKS OK.
- [SDR DALA2014111006013](https://openairdocs.org/sdr/DALA2014111006013), Nov 8, 2014: STRUCTURE. DENTED. FOUND BIRD STRIKE DENT AT LT ENGINE NOSE COWL. INSPECTED DENT, FOUND OUT OF LIMITS. R & R LEFT ENGINE NOSE COWL IAW AMM.
- [SDR DALA14020599205](https://openairdocs.org/sdr/DALA14020599205), Mar 28, 2014: COMPRESSOR. STALLED. PERFORMED AIR TURN BACK DUE TO NR 2 ENGINE COMPRESSOR STALLS ABOVE IDLE DURING CLIMBOUT. EMERGENCY WAS DECLARED. BOROSCOPED ENGINE. R & R SEVERAL PARTS. ENGINE 
- [SDR DALA1102429202](https://openairdocs.org/sdr/DALA1102429202), Jan 9, 2011: ACOUSTIC LINER. DEPARTED. FLIGHT CREW DIVERTED, DUE TO REPORTS OF DEBRIS ON DEPARTURE RUNWAY OUT OF MSP WHICH "MAY HAVE COME OFF OF OUR JET". DEBRIS IDENTIFIED AS ACOUSTICAL LINER AND AC
- [SDR DALA1053439206](https://openairdocs.org/sdr/DALA1053439206), Dec 27, 2010: SKIN. DENTED. FUSELAGE DENTED AT STA 271 BETWEEN LONGERON 30 AND LONGERON 29RT. DENT CAUSED BY MAINT ATTEMPT TO JACK ACFT AT FWD LAV DRAIN HOLE DURING NLG STRUT SERVICING. DE
- [SDR DALA1033869207](https://openairdocs.org/sdr/DALA1033869207), Nov 21, 2010: DUCT. DELAMINATED. RT ENGINE FIRE DET FAULT ON CLIMBOUT. RETURNED TO DEPARTURE, OVERWEIGHT LANDING. LOWER T/R C DUCT WAS FOUND DELAMINATED AND COMING APART IN THE COLD STREAM AREA
- [SDR 2010FA0001251](https://openairdocs.org/sdr/2010FA0001251), Nov 19, 2010: TURBINE BLADES. CORRODED. (Z3EY) THIS ENGINE IS UNDERGOING MX. DURING ROUTINE VISUAL INSP, EXCESSIVE CORROSION WAS DETECTED IN THE FIR TREE ROOTS. THIS ISSUE HAS BEEN DETECTED ON OTHER H
- [SDR DALA1034259202](https://openairdocs.org/sdr/DALA1034259202), Nov 15, 2010: SKIN. CRACKED. A CRACK WAS FOUND ON THE 5911432-81 SKIN PANEL AT STA 1475 BETWEEN LONGERON 2 LT AND 3 LT SKIN IS 2024-T3 (DLM90103296)
- [SDR DALA1034289202](https://openairdocs.org/sdr/DALA1034289202), Nov 5, 2010: SKIN. CRACKED. A CRACK WAS FOUND UNDER THE PREVIOUSLY INSTALLED DOUBLER AT STA 1475 LONGERON 1 AND 2 RT. NEW CRACK WAS TRIMMED OUT AND DOUBLER ENLARGED TO REPAIR BOTH SKIN CUT
- [SDR DALA1034299202](https://openairdocs.org/sdr/DALA1034299202), Nov 5, 2010: SKIN. CRACKED. A CRACK WAS FOUND IN LONGERON 2 LT AT STA 1475. THIS CRACK FOUND DURING INSP OF TAIL AREA, AFTER FINDING FUSELAGE SKIN CRACKS AT STA 1494 BOTH LT AND RT SIDES. 

All 133: https://openairdocs.org/engine/iae-v2528-d5/reports.md

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