IAE V2527-A5

Service difficulty reports · 8,007

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 = 'V2527A5'
  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 AALA201705249005Engine · stalledDURING CLIMB PASSING ABOUT 7500 FT, THE NR 2 ENGINE EXHIBITED APPARENT COMPRESSOR STALL AND OVERHEATT. THE ENGINE WAS SHUTDOWN IAW QRH. DIVERTED. REMOVED AND REPLCED THE NR 2 ENGINE IAW JOB CARD 26L40071004. OPS & LEAK CHECKED NORMAL. AIRCRAFT WAS GROUNDED.May 23, 2017 · N809AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR YENA201705200390Engine · overservicedFA'S REPORTED A TOXIC, DIRTY SOCK ODOR ON GROUND, IN FLIGHT, AND DURING DESCENT FOR THE THREE LEGS FLOWN. MX FOUND THE NR 2 ENGINE OVERSERVICED BY 2 QUARTS. MX BROUGHT TO CORRECT LEVEL. R & R THE RT OZONE FILTER, LEAK CHECKED GOOD IAW 21-51-00. ACCOMPLISHEMay 20, 2017 · N607JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR YENA201705170376Engine · failedRETURN TO FIELD. TOXIC FUMES IN THE COCKPIT. R & R THE NR 1 ENGINE IAW AMM 71-00-20-000-040, AND 71-00-20-400-040.May 17, 2017 · N653JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR YENA201705170377Engine · failedCAPTAIN REPORTED AN ODOR IN THE COCKPIT AFTER TAKEOFF. THE ODOR DISSIPATED AND THEN REAPPEARED DURING DESCENT. NR 1 ENGINE REMOVED AND REPLACED. OPS CHECK NORMAL IAW 36-10-00.May 17, 2017 · N590JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR YENA201705160379Engine · odorPILOTS DETECTED A DIRTY SOCK ODOR WHILE PASSING THROUGH 7500 - 5000 FT DURING DESCENT. ODOR SEEMED STRONGEST IN THE COCKPIT. NR 1 ENGINE CHANGE ACCOMPLISHED IAW W/O 847556. R & R THE OZONE FILTERS 1 & 2. NO LEAKS NOTED IAW MM 21-51-41. ACCOMPLISHED A PACMay 16, 2017 · N641JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR YENA201704280318Engine · failedFROM CLIMB TO CRUISE, ALTITUDE FL 350, THERE WAS CONTINUOUS ENG OIL SCENT IN THE COCKPIT FROM THE BLEED AIR SUPPLY SYSTEMS. THE NR 1 ENGINE WAS R & R, ALL OP CHECKS NORMAL.Apr 28, 2017 · N523JB · Airbus A320232 · Engine Cowling SystemSDR YENA201704270316Filter · contaminatedODOR OF OIL IN THE FLIGHT DECK DURING CLIMBOUT. NO INDICATION OF ODOR IN CABIN . BLEEDS ON, ODOR RETURNED AT 340 IN CLOUDS WITH NORMAL CRUISE POWER SETTINGS, IN DECENT OUT OF 5500 AT IDLE POWER. ACCOMPLISHED THE NR 1 ENGING BORESCOPE INSPECTION OF THE LPC Apr 27, 2017 · N519JB · Airbus A320232 · Air Distribution SystemSDR YENA201704270317Filter · contaminatedODOR OF OIL IN FLIGHT DECK DURING CLIMBOUT. NO INDICATION OF ODOR IN CABIN . TAKEOFF BLEEDS ON, ODOR RETURNED AT 340 IN CLOUDS WITH NORMAL CRUISE POWER SETTINGS, IN DECENT OUT OF 5500 AT IDLE POWER, ACCOMPLISHED A NR 1 ENGINE BORESCOPE INSPECTION OF THE LApr 27, 2017 · N519JB · Airbus A320232 · Air Distribution SystemSDR YENA201704250309Engine · odorTURBINE OIL / DIRTY SOCK ODOR DURING CLIMB 7-12000 FT. INCREASED WHEN ENTERING THIN CLOUD LAYER. DURATION 3-4 MINUTES. FA REPORTED SLIGHTLY STRONGER IN FRONT. HI / LO FLOW NO CHANGE. DFDR EVENT BUTTON PUSHED. NR 1 ENGINE AND LT & RT OZONE FILTERS REPLACApr 25, 2017 · N507JT · Airbus A320232 · Engine (Turbine/Turboprop)SDR YENA201704250315Engine · leakingAN ODOR IN THE CABIN. BOROSCOPE CHECK FOUND INTERNAL OIL LEAKAGE. R & R NR 1 ENGINE IAW AMM 71-00-20.Apr 25, 2017 · N804JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR YENA201704250310Filter · odorTURBINE OIL / DIRTY SOCK ODOR DURING CLIMB 7-12000 FT. INCREASED WHEN ENTERING THIN CLOUD LAYER. DURATION 3-4 MINUTES. FA REPORTED SLIGHTLY STRONGER IN FRONT. HI / LO FLOW NO CHANGE. DFDR EVENT BUTTON PUSHED. NR 1 ENGINE AND LT & RT OZONE FILTERS REPLACApr 25, 2017 · N507JT · Airbus A320232 · Air Distribution SystemSDR YENA201704170290Engine · contaminatedDURING CLIMB, EXPERIENCED A STRONG ODOR. ALSO DURING DESCENT. DONNED OXYGEN MASKS DUE TO THE EYES BURNING. PERFORMED CLEANING OF THE NR 1 & 2 ENGINES IAW AMM 72-00-00-100-010. OZONE CONVERTERS LT & RT REPLACED. DECONTAMINATION OF ECS ALSO PERFORMED. Apr 17, 2017 · N804JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR AALA201704069018Thermocouple · faultyAIRCRAFT WAS GROUNDED. ON DESCENT ENGINE 1 IDLE AT 41 % FF 1200 ENGINE 2 IDLE 28 % FF 700. REMOVED & REPLACED NR 1 ENGINE FUEL TEMP SENSOR.Apr 5, 2017 · N661AW · Airbus A320232 · Engine Fuel Indicating SystemSDR YENA201704040249Engine · leakingDURING DESCENT AND CLIMB,STRONG ODOR, INDICATING OIL IN THE AIR CON DUCT. R & R THE NR 1 ENGINE . ALL CHECKED GOOD AND NO ODOR.Apr 4, 2017 · N809JB · Airbus A320232 · Turbine Engine Oil SystemSDR GTIA2017031501833Cap Seal · damagedSWEATY SOCK SMELL ON DESCENT AT 5000'. COCKPIT/FWD CABIN HAD THE SMELL. PACK 1 ISOLATED THE SMELL PER OPS BULLETIN PROCEDURE. PER TSM 71-00-00 FOUND ENG NR 1 BLIND CAP SEAL LEAKING. R&R IAW AMM 72-51-41. LEAK CHECK GOOD. DECONTAMINATION OF ENVIRONMENTAL SYSTEMMar 15, 2017 · N621NK · Airbus A320232 · Turbine SectionSDR GTIA2017031201813Seal · leakingDURING DESCENT, IDLE THRUST OUT OF 9000 FT, A DIRTY SOCK OR MUSTY ODOR MOSTLY IN CABIN AND AFT CABIN. FOUND AN OIL LEAK AT THE NR 1 ENGINE DEOILER SEAL. REPLACED THE NR 1 AND 2 ENGINES DEOILER SEALS.Mar 12, 2017 · N621NK · Airbus A320232 · Turbine Engine Oil SystemSDR CALA2017010500010Engine · overtempCREW REPORTS ON APPROACH ENG 2 SPIKED TO 890 DEGREES. SHUTDOWN ENGINE PER QRH. PULLED THROTTLE BACK, EGT STAYED AT 890. COMMENCE ENGINE SHUTDOWN PER QRH REMOVED AND RPL THE FWD AND AFT EGT HARNESS AND 4 EACH THERMOCOUPLE EGT PROBES REF AMM-TASK 77-21-43-00-010Jan 5, 2017 · N423UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR GTIA2017010401732Seal · leakingDURING INITIAL CLIMB, FLIGHT ATTENDANT REPORTED FOUL SMELL IN AFT GALLEY. CLOSED PACK 2 AND CROSSBLEED. ODOR CAME BACK DURING CRUISE, PERFORMED AIR PACK 1 + 2 FAULT PROCEDURE, DECLARED EMERGENCY AND LANDED. ACCOMPLISHED TSM 05-50-00-810-831. FOUND NR 2 ENG DEOJan 4, 2017 · N622NK · Airbus A320232 · Turbine Engine Oil SystemSDR CALA2017010496075Door Sill · corrodedCORROSION ON LT DOOR SILL AFT CORNER FITTING AT L2 DOOR. REMOVED & REPLACED IAW SRM 51-42-11.Dec 23, 2016 · N403UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2017010496071Shear Tie · corrodedFWD CARGO BAY AT FRAME 32 BETWEEN STRINGERS 42-43R SHEAR TIE HAS CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11.Dec 22, 2016 · N407UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017010496072Shear Tie · corrodedSHEAR TIE AT FRAME 31, BETWEEN STRINGERS 41-42L HAS CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11.Dec 22, 2016 · N407UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017010496073Shear Tie · corrodedFWD CARGO BAY AT FRAME 30, BETWEEN STRINGERS 42-43R SHEAR TIE HAS CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11.Dec 22, 2016 · N407UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017010496074Stringer · corrodedEVIDENCE OF CORROSION ON STRINGER 43R , BETWEEN FRAMES 32 AND 33. REMOVED & REPLACED THE STRINGER IAW SRM 51-42-11.Dec 22, 2016 · N407UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2017010496067Shear Tie · corrodedFWD CARGO BAY SHEAR TIE AT FRAME 31 BETWEEN STRINGERS 42-43R HAS CORROSION. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-44-11Dec 19, 2016 · N407UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017010496068Shear Tie · corrodedFWD CARGO BAY FRAME 32 BETWEEN STRINGERS 41-42R SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-44-11.Dec 19, 2016 · N407UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017010496069Shear Tie · corrodedFWD CARGO BAY SHEAR TIE AT FRAME 31 BETWEEN STRINGERS 42 AND 43R HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-44-11.Dec 19, 2016 · N407UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017010496070Stringer · corrodedFWD CARGO BAY STRINGER 41R HAS CORROSION BETWEEN FRAMES 32 AND 33. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11.Dec 19, 2016 · N407UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2017010496063Shear Tie · corrodedFWD CARGO SHEAR TIE CORRODED AT FRAME 31, BETWEEN STRINGERS 40 - 41R. THE SHEAR TIE WAS REPLACED IAW SRM 51 -42-11. MAJOR REPAIR.Dec 18, 2016 · N407UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017010496064Shear Tie · corrodedFWD CARGO BAY SHEAR TIE CORRODED AT FRAME 31, BETWEEN STRINGERS 41 - 42R. THE SHEAR TIE WAS REPLACED IAW SRM 51 -42-11. MAJOR REPAIRDec 18, 2016 · N407UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017010496065Stringer · corrodedFWD CARGO BAY STRINGER 41R CORRODED BETWEEN FRAMES 32 AND 33. THE STRINGER SECTION WAS REPLACED IAW SRM 51-42-11. MAJOR REPAIRDec 18, 2016 · N407UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2017010496061Stringer · corrodedAFT CARGO BAY, FRAMES 59-60, STRINGER 43L IS CORRODED. REMOVED AND REPLACED IAW SRM 51-42-11.Dec 17, 2016 · N403UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2017010496062Stringer · corrodedAFT CARGO FRAMES 56-57, STRINGER 44R IS CORRODED. REPAIRED THE STRINGER IAW SRM 53-00-13 FIG 202.Dec 17, 2016 · N403UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016121696044Skin · dentedDENT 5 FEET FWD OF L1 DOOR. FOUND TO BE FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11 PAR 4.6. REPAIRED IAW SRM 53-00-11 FIG 240.Dec 15, 2016 · N403UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016121696037Shear Tie · corrodedAFT CARGO BAY FRAME 59 STRINGERS 44-43R SHEAR TIE IS CORRODED REMOVED & REPLACED THE SHEAR TIE IAW SRM 51- 42-11Dec 14, 2016 · N403UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016121696038Stringer · corrodedAFT CARGO BAY FRAMES 58-59 STRINGER 41R IS CORRODED REMOVED & REPLACED THE STRINGER IAW SRM 51-72-11.Dec 14, 2016 · N403UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016121696039Fitting · corrodedFITTING CORRODED ON BACK SIDE ATTACHED TO FRAME 70, Y-1162. REMOVED AND REPLACED THE FITTING.Dec 14, 2016 · N407UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016121696040Stringer Splice · corrodedFORWARD CARGO STRINGER SPLICE 43L CORRODED JUST FORWARD OF FRAME 31. REMOVED & REPLACED THE STRINGER SPLICE IAW SRM 51-42-11.Dec 14, 2016 · N403UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016121696041Stringer Splice · corrodedFORWARD CARGO STRINGER SPLICE 41L CORRODED JUST FORWARD OF FRAME 31. REMOVED & REPLACED THE STRINGER SPLICE IAW SRM 51-42-11.Dec 14, 2016 · N403UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016121496032Shear Tie · corrodedFWD CARGO BAY FRAME 32 CLEAT BETWEEN STR.42-43R HAS CORROSION AND ELONGATED. FOUND ELONGATED HOLE ON FWD PIT FRAME 32 CLEAT BETWEEN STR. 42-43R OUT OF LIMITS, REMOVED AND REPLACED CLEAT IAW SRM 51-72-11,51-42-11.Dec 12, 2016 · N403UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016121496033Door Sill · corrodedCORROSION ON L2 DOOR SILL IN NUMEROUS PLACES. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51-42-11, PG.25, SRM 51-72-11, PG.1Dec 12, 2016 · N403UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016121496034Stringer · corrodedFWD CARGO FOUND STRINGER 41L AT AND FWD OF FRAME 31 CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 53-21-13, SRM 51-42-11.Dec 12, 2016 · N403UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016121496026Spar · corrodedLEFT WING OTBD FLAP LEADING EDGE HAS CORROSION ON FWD SPAR FWD FACE AROUND FASTENER HOLE JUST ABOVE FLAP TRACK NR 3 INSIDE PANEL NR 2. REMOVED CORROSION LT WING OTBD SPAR WEB AND FOUND TO BE OUT OF LIMITS, IAW SRM 51-74-00. REMOVED AND REPLACED THE SPAR WEDec 10, 2016 · N405UA · Airbus A320232 · Wing SparSDR CALA2016121496028Support · corrodedAFT CABIN FRAME 70 SUPPORT CORRODED AT STRINGER 23R. FRAME SUPPORT WAS REPLACED IAW SRM 51-42-11Dec 10, 2016 · N407UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2016121496029Strap · corrodedAFT PRESSURE BULKHEAD FWD FACE RIGHT SIDE DOUBLER STRAP CORRODED AT FRAME 70, Y1162. DOUBLER STRAP WAS FABRICATED AND REPLACED IAW SRM51-42-11 AND 53-51-16.Dec 10, 2016 · N407UA · Airbus A320232 · Fuselage Main, BulkheadSDR CALA2016121496030Door Sill · corrodedDOOR 2R SILL CORRODED AT FWD AND AFT ENDS DOOR SILL WAS REPLACED PER SRM 51-72-11 AND SRM 51-42-11.Dec 10, 2016 · N407UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016120996021Door Sill · corrodedR2 DOOR SILL HAS NUMEROUS AREAS OF CORROSION. REMOVED & REPLACED THE DOOR SILL IAW SRM 51-42-11, PG.25 & SRM 51-72-11, PG.1.Dec 9, 2016 · N403UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016120996022Door Frame · corrodedLEFT FWD EMERGENCY HATCH HAS CORROSION ON INNER STRUCTURE FITTING AFT LOWER CORNER. REMOVED CORROSION AT LH FWD EMERGENCY HATCH T SECTION LOWER FRAME. NO ALLOWABLE DAMAGE LIMITS IN SRM. R & R T SECTION, CURVED EDGE FRAME, SEAL RETAINER IAW SRM 51-42-11,PAR.Dec 7, 2016 · N405UA · Airbus A320232 · Emergency ExitsSDR CALA2016120296014Stringer · corrodedAFT CARGO COMPARTMENT FR 58-59 STRINGER 42L CORRODED. REMOVED & REPLACED STR 42 L FROM FR 53 TO FR 60 IAW SRM 53-00-13, SRM 51-42-11.Dec 1, 2016 · N403UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016120296015Stringer · corrodedAFT CARGO AT FR62 STR40R HAS CORROSION. REMOVED AND REPLACED STR4 0 FROM FR58 TO FR64 IAW SRM 51-42-11 PARA 6 AND 7.Dec 1, 2016 · N405UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016120296016Stringer · corrodedAFT CARGO COMPARTMENT FR54-55 STR43L HAS CORROSION. REMOVED AND REPLACED STR43L FROM FR54-60 IAW SRM 51-42-11 PARA 6 AN 7.Dec 1, 2016 · N405UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
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