# Service difficulty reports: IAE V2528-D5

A list on [IAE V2528-D5](https://openairdocs.org/engine/iae-v2528-d5.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 133 reports

- [SDR DALA2019051002928](https://openairdocs.org/sdr/DALA2019051002928.md): Engine · failed · May 9, 2019 · N952DN · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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.md): Unknown · malfunctioned · Mar 27, 2019 · N914DN · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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. SHUTDOWN LEFT ENGINE, MOTOR WINDMILLED FOR 20 MINUTES NO OIL PRESSURE ISSUES ON OAP, OR LIGHTS ON OIL
- [SDR DALA2018102206190](https://openairdocs.org/sdr/DALA2018102206190.md): Starter · disintegrated · Oct 18, 2018 · N952DN · Doug MD9030 · Engine Starter
  > LEFT ENG DURING START NO N2 ROTATION GROUND CREW REPORTED SPARKS AND FLAMES. COMPLIED WITH MANUAL ABORTED START PROCEDURE PER QRH. FOUND STARTER DISINTEGRATED. NO VISIBLE DAMAGE TO ENGINE CASE OR COWLING. R/R LEFT ENGINE STARTER IAW AMM 80-11-01-401. STARTER S
- [SDR AN0R201810010008](https://openairdocs.org/sdr/AN0R201810010008.md): Skin · delaminated · Sep 28, 2018 · Doug MD9030 · Engine Thrust Reverser
  > 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 AFT OUTER SKIN AND FWD INNER SKIN.
- [SDR DALA2018091405597](https://openairdocs.org/sdr/DALA2018091405597.md): Generator · failed · Sep 12, 2018 · N945DN · Doug MD9030 · AC Generator-Alternator
  > 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 TRIP. VERIFIED LT GEN NO VOLTS/FREQS. REPLACED LT VSCF GEN. INSPECTED LT ENG GEN CONTROL HARNESS, NO D
- [SDR AN0R201808259007](https://openairdocs.org/sdr/AN0R201808259007.md): Skin · debonded · Sep 9, 2018 · Doug MD9030 · Nacelle/Pylon, Plate/Skin
  > 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.md): Skin · departed · Jul 28, 2018 · N951DN · Doug MD9030 · Engine Thrust Reverser
  > 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 COMMON NOZZLE ASSEMBLY. ENGINE CLOSED AND T/R OPS CK GOOD. A/C OK FOR SVC.
- [SDR DALA2018062604228](https://openairdocs.org/sdr/DALA2018062604228.md): Compressor · damaged · Jun 24, 2018 · N947DN · Doug MD9030 · Turbine Engine Compressor Section
  > DIV - TO ICT FOR LEFT ENGINE COMPRESSOR STALL AT FLIGHT LEVEL 260. ASSOCIATED RISING EGT. ENGINE POWER REDUCED TO IDLE, COMPRESSOR STALLS DISCONTINUED. ENGINE WAS NOT SHUT DOWN. FLIGHT DIVERTED TO ICT. BORESCOPED ENGINE FOUND 3RD, 5TH AND 6TH STAGE HPC DAMAGE.
- [SDR AN0R2018618006](https://openairdocs.org/sdr/AN0R2018618006.md): Skin · delaminated · Jun 1, 2018 · Doug MD9030 · Engine Thrust Reverser
  > 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.md): Skin · delaminated · Mar 5, 2018 · Doug MD9030 · Nacelle/Pylon, Plate/Skin
  > 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 FWD INNER SKIN.
- [SDR AN0R20180326004](https://openairdocs.org/sdr/AN0R20180326004.md): Skin · corroded · Mar 2, 2018 · Doug MD9030 · Nacelle/Pylon, Plate/Skin
  > 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.md): Skin · delaminated · Jan 2, 2018 · Doug MD9030 · Engine Thrust Reverser
  > 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 AFT OUTER SKIN AND MID AND FWD INNER SKIN.
- [SDR AN0R20171227016](https://openairdocs.org/sdr/AN0R20171227016.md): Skin · delaminated · Nov 15, 2017 · Doug MD9030 · Engine Thrust Reverser
  > 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.md): Skin · debonded · Nov 8, 2017 · Doug MD9030 · Engine Thrust Reverser
  > 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 CENTER INNER SKINS ARE ALSO DAMAGED.
- [SDR AN0R20181192001](https://openairdocs.org/sdr/AN0R20181192001.md): Skin · corroded · Nov 3, 2017 · Doug MD9030 · Engine Thrust Reverser
  > 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 INNER SKIN.
- [SDR AN0R20171129014](https://openairdocs.org/sdr/AN0R20171129014.md): Skin · corroded · Oct 24, 2017 · Doug MD9030 · Nacelle/Pylon, Plate/Skin
  > 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.md): Skin · debonded · Oct 18, 2017 · Doug MD9030 · Nacelle/Pylon, Plate/Skin
  > 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.md): Skin · delaminated · Aug 29, 2017 · Doug MD9030 · Nacelle/Pylon, Plate/Skin
  > 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.md): Engine · making metal · Aug 4, 2017 · N964DN · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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 ON CHIP DETECTORS, REPLACED LEFT ENGINE. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2017080205853](https://openairdocs.org/sdr/DALA2017080205853.md): Oil System · leaking · Aug 1, 2017 · N960DN · Doug MD9030 · Turbine Engine Oil System
  > 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. REMOVED AND REPLACED ACOC IAW MM. FUNCTIONAL CHECKED GOOD, NO CONTAMINATION. SERVICED. AIRCRAFT
- [SDR DALA2017080205854](https://openairdocs.org/sdr/DALA2017080205854.md): Oil System · empty · Jul 27, 2017 · N922DX · Doug MD9030 · Turbine Engine Oil System
  > 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 CHANGED.
- [SDR AN0R20170929012](https://openairdocs.org/sdr/AN0R20170929012.md): Skin · delaminated · Jul 21, 2017 · Doug MD9030 · Nacelle/Pylon, Plate/Skin
  > 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.md): Skin · delaminated · Jul 14, 2017 · Doug MD9030 · Engine Thrust Reverser
  > 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 ALSO EXISTS TO THE CLOSURES.
- [SDR AN0R2017809010](https://openairdocs.org/sdr/AN0R2017809010.md): Skin · delaminated · Jun 15, 2017 · Doug MD9030 · Engine Thrust Reverser
  > 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 SKIN.DAMAGE ALSO EXISTS TO THE CLOSURES.
- [SDR AN0R2017728008](https://openairdocs.org/sdr/AN0R2017728008.md): Skin · delaminated · Jun 7, 2017 · Doug MD9030 · Engine Thrust Reverser
  > 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.md): Skin · delaminated · May 9, 2017 · Doug MD9030 · Engine Thrust Reverser
  > 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.md): Skin · delaminated · May 4, 2017 · Doug MD9030 · Nacelle/Pylon, Longeron/Stringer
  > 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. DAMAGE ALSO EXISTS TO THE CLOSURE.
- [SDR DALA2017040502841](https://openairdocs.org/sdr/DALA2017040502841.md): Pump · failed · Apr 5, 2017 · N917DN · Doug MD9030 · Hydraulic Pump (Electric/Engine), Main
  > 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 NR 1 ENGINE DRIVEN PUMP IAW MM. OPERATIONS CHECKED GOOD.
- [SDR AN0R2017323005](https://openairdocs.org/sdr/AN0R2017323005.md): Skin · delaminated · Feb 24, 2017 · Doug MD9030 · Engine Thrust Reverser
  > 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.md): Oil Cooler · leaking · Feb 2, 2017 · N932DN · Doug MD9030 · Turbine Engine Oil System
  > 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 MM. LEAK AND OPERATION CHECK GOOD. (LP# 8680580)
- [SDR AN0R2017403006](https://openairdocs.org/sdr/AN0R2017403006.md): Skin · delaminated · Jan 18, 2017 · Doug MD9030 · Nacelle/Pylon, Plate/Skin
  > 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 INNER SKIN. THE FWD INBD INNER SIDEWALL SKIN.
- [SDR DALA2017011800449](https://openairdocs.org/sdr/DALA2017011800449.md): Hydraulic System · pressure loss · Jan 13, 2017 · N948DN · Doug MD9030 · Hydraulic System, Main
  > AFTER TAKE-OFF. RIGHT HYDRAULIC PRESSURE 0. QUANTITY WAS NORMAL. AN ALTERNATE GEAR EXTENSION WAS PERFORMED DUE TO THE RIGHT HYDRAULIC PRESSURE LOSS. EMERGENCY DECLARED AND RETURNED TO DEPARTURE. MAINTENANCE REPLACED RIGHT EDP, HYDRAULIC SYSTEM FILTERS AND FL
- [SDR DALA2016041803161](https://openairdocs.org/sdr/DALA2016041803161.md): Turbine Case · cracked · Apr 16, 2016 · N957DN · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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.md): Hub · damaged · Mar 15, 2016 · Turbine Engine Combustion Section
  > 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. SUSPECTED OIL LEAK FROM THE NR 4 BEARING AREA WHICH HAS ALLOWED OIL TO ACCUMULATE IN THE HPT, STAGE 1
- [SDR DALA2016022401386](https://openairdocs.org/sdr/DALA2016022401386.md): Oil System · leaking · Feb 21, 2016 · N911DA · Doug MD9030 · Turbine Engine Oil System
  > UPON ENGINE SHUTDOWN, GROUND CREW REPORTED EXCESSIVE SMOKE COMING FROM NR 1 ENGINE TAIL PIPE. MAINTENANCE TROUBLESHOT. FOUND TURBINE EXHAUST BLADES WET WITH OIL. OIL BEGINNING TO POOL. IAW PROPULSION ENGINEERING CHANGE NR 1 OIL QUANTITY TRANSMITTER AND NR
- [SDR DALA2016010500033](https://openairdocs.org/sdr/DALA2016010500033.md): Pump · inoperative · Dec 30, 2015 · N925DN · Doug MD9030 · Hydraulic Pump (Electric/Engine), Main
  > 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 RECOVERED AND THE GEAR EXTENDED. MAINTENANCE BLED HYDRAULICS, CHECKED FOR PROPER SERVICE LEVEL. R & R
- [SDR Z3EY2015FA0000551](https://openairdocs.org/sdr/Z3EY2015FA0000551.md): Bolt · missing · Oct 13, 2015 · Engine (Turbine/Turboprop)
  > 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 2-3MM. THE CUSTOMER CONFIRMS THAT THEY HAVE NO RECORD OF MAINTENANCE BEING PERFORMED IN THIS AREA. C
- [SDR DALA2015100806005](https://openairdocs.org/sdr/DALA2015100806005.md): Engine · making metal · Oct 3, 2015 · N959DN · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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 TAILPIPE AND HAVE REPLACED THE NR 2 ENGINE.
- [SDR DALA2015072904745](https://openairdocs.org/sdr/DALA2015072904745.md): Structure · leaking · Jul 27, 2015 · N952DN · Doug MD9030 · Turbine Engine Oil System
  > 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. SHORTLY AFTER ENGINE GENERATOR FAILURE, APU WAS STARTED. F/A REPORTED A SMOKE OIL FUME ODOR I
- [SDR DALA2015062103894](https://openairdocs.org/sdr/DALA2015062103894.md): Nose Cowl · damaged · Jun 20, 2015 · N959DN · Doug MD9030 · Turbine Engine Air Inlet Section
  > 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.md): Blade · damaged · Jun 20, 2015 · N959DN · Doug MD9030 · Turbine Engine Compressor Section
  > 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.md): Structure · dented · Nov 8, 2014 · N926DH · Doug MD9030 · Engine Air Intake System
  > 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.md): Compressor · stalled · Mar 28, 2014 · N905DA · Doug MD9030 · Turbine Engine Compressor Section
  > 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 STILL STALLING. R & R NR 2 ENGINE.
- [SDR DALA1102429202](https://openairdocs.org/sdr/DALA1102429202.md): Acoustic Liner · departed · Jan 9, 2011 · N902DA · Doug MD9030 · Engine Thrust Reverser
  > 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 ACFT WAS THE LAST TO DEPART. MX FOUND ACOUSTIC MATERIAL MISSING ON THE NR1 ENGINE THRUST REVERSER. U
- [SDR DALA1053439206](https://openairdocs.org/sdr/DALA1053439206.md): Skin · dented · Dec 27, 2010 · N906DA · Doug MD9030 · Fuselage Main, Plate/Skin
  > 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. DENT WAS CUT-OUT AND REPAIRED IAW ERA 488513-14. NON ROUTINE NR1.
- [SDR DALA1033869207](https://openairdocs.org/sdr/DALA1033869207.md): Duct · delaminated · Nov 21, 2010 · N907DA · Doug MD9030 · Engine Thrust Reverser
  > 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. 7TH STAGE BLEED VALVE SOLENOID WAS REPLACED. LOWER COWL/ T/R ASSY WAS ALSO REPLACED.
- [SDR 2010FA0001251](https://openairdocs.org/sdr/2010FA0001251.md): Turbine Blades · corroded · Nov 19, 2010 · Turbine Section
  > (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 HUBS AT THIS FACILITY AND MFG EXPECTS TO BE PRESENTING INFO REGARDING POSSIBLE CAUSES BY EARLY DEC,
- [SDR DALA1034259202](https://openairdocs.org/sdr/DALA1034259202.md): Skin · cracked · Nov 15, 2010 · N902DA · Doug MD9030 · Fuselage Main, Plate/Skin
  > 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.md): Skin · cracked · Nov 5, 2010 · N902DA · Doug MD9030 · Fuselage Main, Plate/Skin
  > 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-OUTS.
- [SDR DALA1034299202](https://openairdocs.org/sdr/DALA1034299202.md): Skin · cracked · Nov 5, 2010 · N902DA · Doug MD9030 · Fuselage Main, Plate/Skin
  > 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. A NEW SECTION OF LONGERON WAS FABRICATED AND A SPLICE MADE IAW ERA.

Next page: https://openairdocs.org/engine/iae-v2528-d5/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 = 'V2528D5'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/iae-v2528-d5/reports

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