# Service difficulty reports: IAE V2525-D5

A list on [IAE V2525-D5](https://openairdocs.org/engine/iae-v2525-d5.md).

Newest first. General aviation reporting is voluntary.

- [SDR DALA2019042402601](https://openairdocs.org/sdr/DALA2019042402601.md): Engine · malfunctioned · Apr 23, 2019 · N910DN · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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. REMOVED AND REPLACED ENGINE.
- [SDR DALA2019022201123](https://openairdocs.org/sdr/DALA2019022201123.md): Engine · vibration · Feb 20, 2019 · N931DN · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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 TEST OF FAN BLADES PERMD90AMM 71-00-00 984139. C/W T/S PER FIM 71-00 AND PERF ENGINE RUN AND VIBRATIO
- [SDR DALA2018090705473](https://openairdocs.org/sdr/DALA2018090705473.md): Engine · fire · Sep 5, 2018 · N915DN · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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 REACHED 1100 EGT. ENGINE REPLACED.
- [SDR DALA2018082005151](https://openairdocs.org/sdr/DALA2018082005151.md): Engine · failed · Aug 18, 2018 · N950DN · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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.md): Engine · failed · Mar 13, 2018 · N929DN · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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 THE QRH AND SHUT DOWN THE ENGINE AND RETURNED TO DEPARTURE. EGT EXCEEDANCE OF 730 DEG C. AN OVERWEIGH
- [SDR DALA2016081706066](https://openairdocs.org/sdr/DALA2016081706066.md): Engine · faulted · Aug 8, 2016 · N935DN · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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 MESSAGE. POST FLIGHT INSPECTION, NR 1 ENGINE HAS SMOKE RISING FROM COWL. MAINTENANCE OPENED COWLS A
- [SDR DALA14033579232](https://openairdocs.org/sdr/DALA14033579232.md): Oil System · leaking · Jun 3, 2014 · N932DN · Doug MD9030 · Turbine Engine Oil System
  > 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 ENGINE. ENGINE CHANGE REQUIRED DUE TO ENGINE OPERATION WITH NO OIL PRESSURE FOR 3 MINUTES.
- [SDR DALA1116249217](https://openairdocs.org/sdr/DALA1116249217.md): Coffeemaker · odor · Mar 8, 2011 · N917DN · Doug MD9030 · Buffet/Galleys
  > 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 GALLEY OVEN AND COFFEEMAKERS BUT NO SMOKE OR ODOR WAS NOTED. SOME SPILLED/BURNED COFFEE WAS FOUND ON
- [SDR DLM90080035](https://openairdocs.org/sdr/DLM90080035.md): Skin · corroded · Jan 10, 2008 · N910DN · Doug MD9030 · Fuselage Main, Plate/Skin
  > RT FUSELAGE BENEATH LOWER FILLET FAIRING RUBSTRIP STATION 788 TO 883 HAS EVIDENCE OF CORROSION. NEED RUB STRIPS AND SEALANT REMOVED FOR FURTHER EVALUATION. COMPLIED WITH DELTA ERA 460416-14 ISSUED 06JAN08.
- [SDR UIAA010208001](https://openairdocs.org/sdr/UIAA010208001.md): Actuator · malfunctioned · Jan 2, 2008 · N17921 · Doug MD9030 · Compressor Bleed Governor
  > 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 POWER ASSURANCE TEST AND CONDITION CHECK NORMAL.
- [SDR DLM90070861](https://openairdocs.org/sdr/DLM90070861.md): Flange · cracked · Jun 28, 2007 · N906DA · Doug MD9030 · Engine Thrust Reverser
  > 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, 4000-0103, OPN 7004AD CARD 986.
- [SDR DLM90070863](https://openairdocs.org/sdr/DLM90070863.md): Shear Tie · cracked · Jun 28, 2007 · N906DA · Doug MD9030 · Passenger/Crew Doors
  > 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.md): Skin · gouged · Jun 26, 2007 · N906DA · Doug MD9030 · Wing, Plate/Skin
  > 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.md): Cusp Web · corroded · Jun 25, 2007 · N906DA · Doug MD9030 · Fuselage Miscellaneous Structure
  > 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 AND 51-30-05
- [SDR DLM90070865](https://openairdocs.org/sdr/DLM90070865.md): Cusp Web · corroded · Jun 25, 2007 · N906DA · Doug MD9030 · Fuselage Miscellaneous Structure
  > 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, AND 51-30-05.
- [SDR DLM90060666](https://openairdocs.org/sdr/DLM90060666.md): Starter · overheated · Aug 17, 2006 · N905DA · Doug MD9030 · APU Start/Ignition System
  > 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. REPLACED APU START RELAY. APU OPS CHECKS NORMAL. STARTER LEAK CHECK GOOD. NO FAULTS.
- [SDR DLM90050808](https://openairdocs.org/sdr/DLM90050808.md): Starter · unserviceable · Dec 20, 2005 · N904DA · Doug MD9030 · APU Start/Ignition System
  > 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 EXTINGUISHING AGENT WAS NEEDED. REPLACED STARTER, CLUTCH, AND START RELAY.
- [SDR UIA0505](https://openairdocs.org/sdr/UIA0505.md): Engine · failed · Jun 12, 2005 · N17918 · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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 MATERIAL MISSING AND BEND WITH DENTS. STAGE 5-12 BLADES BURN. THIS CASE COULD BE IOD IAW AMM 71-00-10.
- [SDR UIA0502](https://openairdocs.org/sdr/UIA0502.md): Switch · jammed · Feb 2, 2005 · N17919 · Doug MD9030 · VHF Communications System
  > 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 SYSTEM FAILURE. IAW AMM23-51-07 REPLACED RT CONTROL COLUMN PTT SW AND OPERATIOAL TEST SYSTEM BACK,
- [SDR UIA9216](https://openairdocs.org/sdr/UIA9216.md): Bearing · making metal · Aug 5, 2003 · N17926 · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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 FOUND ON MASTER MCD AND NR 1, 2, 3 BEARING COMPARTMENT DAMAGE. THE AIRCRAFT REPLACED THE NR 1 E
- [SDR UIAFAA9201](https://openairdocs.org/sdr/UIAFAA9201.md): Scavenge Pump · broken · Feb 8, 2003 · N17916 · Doug MD9030 · Turbine Engine Oil System
  > 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 CLAIMED THAT SERIOUS DAMAGE WAS FOUND ON VSCF GEN INCLUDING; EXTRUSION OF 3 ELECTRIC PLUGS BACKSHE
- [SDR DLM90020837](https://openairdocs.org/sdr/DLM90020837.md): Engine · power loss · Jul 19, 2002 · N907DA · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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.md): Bearing · damaged · Feb 28, 2002 · N17921 · Doug MD9030 · Turbine Engine Accessory Drive
  > 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. REPLACED NR 2 ENGINE IAE WOULD VERIFY THE ROOT CAUSE OF THE BEARING DAMAGE OF ENGINE GEAR BOX.
- [SDR 2001UIA007](https://openairdocs.org/sdr/2001UIA007.md): Compressor · damaged · Nov 6, 2001 · N17923 · Doug MD9030 · Turbine Engine Compressor Section
  > 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 SERVICEABLE ENG IAW AMM71-00-10, AND IAW AMM 71-02-10 ENG RUN-UP CHECK NORMAL.
- [SDR DLM90992290](https://openairdocs.org/sdr/DLM90992290.md): Wire · shorted · Oct 18, 1999 · N903DA · Doug MD9030 · Instrument System Wiring
  > 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 DISENGAGED. FOUND WIRE 4 INCH AFT OF DISCONNECT P1-8066 GOING TO P1-8078 T2 CHANNEL A SHORTED TO ENG
- [SDR DLM90990538](https://openairdocs.org/sdr/DLM90990538.md): Engine · failed · Mar 12, 1999 · N906DA · Doug MD9030 · Engine (Turbine/Turboprop)
  > LEFT ENGINE FAILURE WHEN T/O POWER APPLIED. REPLACED ENGINE.
- [SDR ORJA98314](https://openairdocs.org/sdr/ORJA98314.md): Eec · malfunctioned · Dec 16, 1998 · N902RA · Doug MD9030 · Fuel Control/Turbine Engines
  > 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). TAKEOFF WAS DISCONTINUED. REMOVED AND REPLACED NR 2 ENGINE EEC IAW MM 73. PERFORMED OPERATION
- [SDR ORJA9865](https://openairdocs.org/sdr/ORJA9865.md): Engine · overtemp · Mar 17, 1998 · N902RA · Doug MD9030 · Engine (Turbine/Turboprop)
  > 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 LOWER NR 1 ENGINE C-DUCTS, INSPECTED ENGINE EXTERIOR FOR OVERTEMP DAMAGE, TAIL EXHAUST SECTION FOR
- [SDR DLM90970232](https://openairdocs.org/sdr/DLM90970232.md): Inlet · dirty · Feb 6, 1997 · N905DA · Doug MD9030 · APU Cowling/Containment
  > 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.md): Eec · failed · Mar 14, 1996 · N903DA · Doug DC863 · Fuel Control/Turbine Engines
  > 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. REPLACED LEFT ENGINE EEC PER MM. PERFORMED ENGINE FAULT, DISPLAY SYSTEM CHECK AND OPERATIONAL/IDL

## 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 = 'V2525D5'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/iae-v2525-d5/reports

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