IAE V2528-D5

Service difficulty reports · 133

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2019051002928Engine · failedRT. 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)May 9, 2019 · N952DN · Doug MD9030 · Engine (Turbine/Turboprop)SDR DALA2019032701928Unknown · malfunctionedCLIMBING 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 Mar 27, 2019 · N914DN · Doug MD9030 · Engine (Turbine/Turboprop)SDR DALA2018102206190Starter · disintegratedLEFT 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 SOct 18, 2018 · N952DN · Doug MD9030 · Engine StarterSDR AN0R201810010008Skin · delaminatedAREAS 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.Sep 28, 2018 · Doug MD9030 · Engine Thrust ReverserSDR DALA2018091405597Generator · failedATB, 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 DSep 12, 2018 · N945DN · Doug MD9030 · AC Generator-AlternatorSDR AN0R201808259007Skin · debondedAREAS OF DISBAND EXIST COMMON TO C-DUCT BONDED ASSY FWD AND AFT PERF SKINS AND FWD AND AFT IB BIFURCATION OUTER SKINS.Sep 9, 2018 · Doug MD9030 · Nacelle/Pylon, Plate/SkinSDR DALA2018073104784Skin · departedON 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.Jul 28, 2018 · N951DN · Doug MD9030 · Engine Thrust ReverserSDR DALA2018062604228Compressor · damagedDIV - 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.Jun 24, 2018 · N947DN · Doug MD9030 · Turbine Engine Compressor SectionSDR AN0R2018618006Skin · delaminatedAREAS 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.Jun 1, 2018 · Doug MD9030 · Engine Thrust ReverserSDR AN0R20180328005Skin · delaminatedAREAS 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.Mar 5, 2018 · Doug MD9030 · Nacelle/Pylon, Plate/SkinSDR AN0R20180326004Skin · corrodedAREAS 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.Mar 2, 2018 · Doug MD9030 · Nacelle/Pylon, Plate/SkinSDR AN0R20180228003Skin · delaminatedAREAS 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.Jan 2, 2018 · Doug MD9030 · Engine Thrust ReverserSDR AN0R20171227016Skin · delaminatedAREAS 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.Nov 15, 2017 · Doug MD9030 · Engine Thrust ReverserSDR AN0R2018130002Skin · debondedAREAS 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.Nov 8, 2017 · Doug MD9030 · Engine Thrust ReverserSDR AN0R20181192001Skin · corrodedAREAS 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.Nov 3, 2017 · Doug MD9030 · Engine Thrust ReverserSDR AN0R20171129014Skin · corrodedAREAS 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.Oct 24, 2017 · Doug MD9030 · Nacelle/Pylon, Plate/SkinSDR AN0R20171129015Skin · debondedAREAS OF DEBONDING COMMON TO THE C DUCT BONDED ASSEMBLY FWD INNER SKIN AND DOUBLER AND MID BUMPER DOUBLER.Oct 18, 2017 · Doug MD9030 · Nacelle/Pylon, Plate/SkinSDR AN0R20171005013Skin · delaminatedAREAS 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.Aug 29, 2017 · Doug MD9030 · Nacelle/Pylon, Plate/SkinSDR DALA2017080806125Engine · making metalIFSD 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.Aug 4, 2017 · N964DN · Doug MD9030 · Engine (Turbine/Turboprop)SDR DALA2017080205853Oil System · leakingDIVERTED 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 Aug 1, 2017 · N960DN · Doug MD9030 · Turbine Engine Oil SystemSDR DALA2017080205854Oil System · emptyPERFORMED 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.Jul 27, 2017 · N922DX · Doug MD9030 · Turbine Engine Oil SystemSDR AN0R20170929012Skin · delaminatedAREAS OF DAMAGE (DISBONDS) EXIST COMMON TO THE C DUCT BONDED ASSEMBLY FWD AND AFT SKINS AND AFT AND FWD AND MID CENTER INNER SKINS.Jul 21, 2017 · Doug MD9030 · Nacelle/Pylon, Plate/SkinSDR AN0R20170822011Skin · delaminatedAREAS 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.Jul 14, 2017 · Doug MD9030 · Engine Thrust ReverserSDR AN0R2017809010Skin · delaminatedAREAS 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.Jun 15, 2017 · Doug MD9030 · Engine Thrust ReverserSDR AN0R2017728008Skin · delaminatedAREAS 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.Jun 7, 2017 · Doug MD9030 · Engine Thrust ReverserSDR AN0R20170626007Skin · delaminatedAREAS DEBONDED, COMMON TO THE C DUCT BONDED ASSEMBLY, FWD SKIN AND FWD INNER SKIN AND DOUBLER. DAMAGE ALSO EXISTS TO THE CLOSURES.May 9, 2017 · Doug MD9030 · Engine Thrust ReverserSDR AN0R2017629008Skin · delaminatedAREAS 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.May 4, 2017 · Doug MD9030 · Nacelle/Pylon, Longeron/StringerSDR DALA2017040502841Pump · failedLEFT 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.Apr 5, 2017 · N917DN · Doug MD9030 · Hydraulic Pump (Electric/Engine), MainSDR AN0R2017323005Skin · delaminatedAREAS 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.Feb 24, 2017 · Doug MD9030 · Engine Thrust ReverserSDR DALA2017020801054Oil Cooler · leakingNR 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)Feb 2, 2017 · N932DN · Doug MD9030 · Turbine Engine Oil SystemSDR AN0R2017403006Skin · delaminatedAREAS 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.Jan 18, 2017 · Doug MD9030 · Nacelle/Pylon, Plate/SkinSDR DALA2017011800449Hydraulic System · pressure lossAFTER 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 FLJan 13, 2017 · N948DN · Doug MD9030 · Hydraulic System, MainSDR DALA2016041803161Turbine Case · crackedLEFT ENGINE AFT VIBRATOR ISOLATOR THERMAL OVERHEATING FROM CRACK IN TURBINE CASE. R & R AFT VIBRATIONS ISOLATOR IAW MM.Apr 16, 2016 · N957DN · Doug MD9030 · Engine (Turbine/Turboprop)SDR Z3EY2016040100155Hub · damagedTHIS 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 Mar 15, 2016 · Turbine Engine Combustion SectionSDR DALA2016022401386Oil System · leakingUPON 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 Feb 21, 2016 · N911DA · Doug MD9030 · Turbine Engine Oil SystemSDR DALA2016010500033Pump · inoperativeON 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 Dec 30, 2015 · N925DN · Doug MD9030 · Hydraulic Pump (Electric/Engine), MainSDR Z3EY2015FA0000551Bolt · missingDURING 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. COct 13, 2015 · Engine (Turbine/Turboprop)SDR DALA2015100806005Engine · making metalACFT 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.Oct 3, 2015 · N959DN · Doug MD9030 · Engine (Turbine/Turboprop)SDR DALA2015072904745Structure · leakingDIVERTED 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 IJul 27, 2015 · N952DN · Doug MD9030 · Turbine Engine Oil SystemSDR DALA2015062103894Nose Cowl · damagedRIGHT ENGINE NOSE COWL DAMAGED BY FOD EVENT. R & R NOSE COWL IAW AMM. PERFORMED ANTI-ICE CHECK.Jun 20, 2015 · N959DN · Doug MD9030 · Turbine Engine Air Inlet SectionSDR DALA2015062203896Blade · damagedNR 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.Jun 20, 2015 · N959DN · Doug MD9030 · Turbine Engine Compressor SectionSDR DALA2014111006013Structure · dentedFOUND BIRD STRIKE DENT AT LT ENGINE NOSE COWL. INSPECTED DENT, FOUND OUT OF LIMITS. R & R LEFT ENGINE NOSE COWL IAW AMM.Nov 8, 2014 · N926DH · Doug MD9030 · Engine Air Intake SystemSDR DALA14020599205Compressor · stalledPERFORMED 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.Mar 28, 2014 · N905DA · Doug MD9030 · Turbine Engine Compressor SectionSDR DALA1102429202Acoustic Liner · departedFLIGHT 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. UJan 9, 2011 · N902DA · Doug MD9030 · Engine Thrust ReverserSDR DALA1053439206Skin · dentedFUSELAGE 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.Dec 27, 2010 · N906DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA1033869207Duct · delaminatedRT 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.Nov 21, 2010 · N907DA · Doug MD9030 · Engine Thrust ReverserSDR 2010FA0001251Turbine 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 HUBS AT THIS FACILITY AND MFG EXPECTS TO BE PRESENTING INFO REGARDING POSSIBLE CAUSES BY EARLY DEC,Nov 19, 2010 · Turbine SectionSDR DALA1034259202Skin · crackedA CRACK WAS FOUND ON THE 5911432-81 SKIN PANEL AT STA 1475 BETWEEN LONGERON 2 LT AND 3 LT SKIN IS 2024-T3 (DLM90103296)Nov 15, 2010 · N902DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA1034289202Skin · crackedA 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.Nov 5, 2010 · N902DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA1034299202Skin · crackedA 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.Nov 5, 2010 · N902DA · Doug MD9030 · Fuselage Main, Plate/Skin
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