IAE V2527-A5
Service difficulty reports · 8,009
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA2014022190412Wire · damagedNR 2 PYLON ELEC CONDUIT CONVOLUTED TUBING FOR FIREX BOTTLES WIRING WAS DETERIORATED & WIRING DAMAGED. REPLACED CONVOLUTED TUBING & DAMAGED WIRING 2621-0002 TO CONNECTOR 6WEZA & BOTH WIRES TO 5WEZA. RANG OUT WIRES & ACP CHECK OF FIREX SYS, OPERATIONS CHECKED SDR CALA2014021790384Computer · faultyGPWS TERRAIN FAULT LIGHT. RESET FMGC 1, ACCOMPLISHED AFS TEST IAW AMM22-96-00, FAULT CLEARED.SDR CALA2014021790387Stringer · corrodedSTRINGER 41R, FRAME 58 - 64 HAS CORROSION. REPLACED STRINGER IAW SRM 51-42-11 ON TIMCO NR 39450.SDR CALA2014021790389Rub Strip · unsecureNR 2 ENG HAS A 2 INCH PIECE OF PLASTIC SEAL HANGING FROM BOTTOM. LCL MAINT REPORTED THAT ENG 2 THRUST REVERSER LATCH ACCESS DOOR HAS TEFLON RUB STRIP HANGING. COMPLIED WITH AMM MT78-016, TRIMMED OFF LOOSE SECTION, RUB STRIP MUST BE REPLACED AT NEXT AK IAW MTSDR YENA20140216036Bolt · missingBOTTOM STARBOARD ENGINE PANEL WAS FOUND ON RUNWAY. FURTHER INSPECTION REVEALED BOLT MISSING AT NR 2 ENGINE TURBINE COOLING (TCA) TUBE REAR FLANGE. INSTALLED AND SAFETIED BOLT AT TCA TUBE REAR FLANGE, IPC 75-23-49-81A, ITEM 100, IAW 75-23-49-00. NOTE: THIS MSDR CALA2014021790383Thrust Reverser · damagedSEALS INSTALLED THRUST REVERSE COWL, NR 2 ENG INBD UPPER THRUST REVERSER COWL, TO LOWER PYLON TORN. METAL FLAPPING AGAINST PYLON PANEL PER PASSENGER OBSERVATION. LE OF FILLET IS DAMAGED BEYOND REPAIR & WILL NEED TO BE REPLACED.SDR CALA2014021790386Sill · corrodedCORROSION PRESENT AT L2 DOOR SILL FWD GIRT BAR ATTACH POINT FRAME 66. R & R L2 DOOR SILL PN D534800420601 IAW A320 SRM 51-42-11 PG 7, PARA 5 & 6 & PG 25 PARA 7.SDR CALA2014021390371Sill · corrodedR1 DOOR SILL BENEATH FWD & AFT GIRT BAR ATTACH FITTINGS HAS BEEN REPAIRED IAW SRM 53-11-14 FIG 208 WITH FOUR EACH BUSHINGS & REPAIR WASHERS DUE TO CORROSION.SDR CALA2014021390372Sill · corrodedL1 DOOR SILL BENEATH AFT GIRT BAR ATTACH FITTING HAS BEEN REPAIRED IAW SRM 53-11-14 FIG 208 WITH TWO EACH BUSHINGS & REPAIR WASHERS DUE TO CORROSION.SDR CALA2014021290363Structure · gougedREPAIRED MED R1 FWD GIRT BAR FITTING AREA GOUGE IN TWO PLACES IAW SRM 53-11-14 FIG 108. ACP HFEC IAW NTM'S 51-10-01 PB 6 & 51-10-04 PB 4, NO DISCREPANCIES. FABRICATED & INSTALLED TWO EACH REPAIR WASHERS FWD INBD & OTBD HOLES IAW SRM 53-11-14 FIG 108.SDR CALA2014021090337Fitting · corrodedREPAIRED L1 DOOR SILL FWD GIRT BAR FITTING FWD OTBD HOLE CORROSION IAW SRM 53-11-14 FIG 108. ACP HFEC ROTARY SCAN ON HOLE IAW NTM 51-10-01 PB 6, NO INDICATION NOTED.SDR CALA2014021090338Fitting · corrodedREPAIRED L1 DOOR SILL FWD GIRT BAR FITTING TWO EACH AFT HOLES CORROSION IAW SRM 53-11-14 FIG 108. ACP HFEC ROTARY SCAN ON HOLES IAW NTM 51-10-01 PB 6, NO INDICATION NOTED.SDR CALA2014021090339Fitting · corrodedREPAIRED R1 DOOR SILL FWD GIRT BAR FITTING AFT TWO EACH HOLES CORROSION IAW SRM 53-11-14 FIG 108. ACCOMPLISHED HFEC ROTARY SCAN ON HOLES IAW NTM 51-10-01 PB 6, NO INDICATION NOTED.SDR CALA2014021090342Proximity Sensor · faultedREF LOG 1 & 2, LGCIU 2 FAULT. PFR & LGCIU BITE SHOW LT LG EXT PROX SENSOR 23GA LGCIU 5GA FAULT. REPLACED LGCIU 2 & CLEANED CONNECTOR ON SENSOR, NO HELP. REINSTALLED ORIGINAL LGCIU, INSTALLED SENSOR 23GA IAW MM32-31-73-000-001-A & MM32-31-73-400-001-A. PASSSDR CALA2014021090335Stringer · corrodedSTRINGER 41 LT HAS CORROSION BETWEEN FRAME 63 - FRAME 64. R & R STRINGER & ATTACHING PARTS IAW A320 SRM 51-42-11 PAGE 7 & 53-41-13 PAGE 101.SDR CALA2014021090336Stringer · corrodedSTRINGER 42 RT HAS CORROSION BETWEEN FRAME 63 &64. REPLACED STRINGER IAW A320 SRM 51-42-11 PG 24 NR 21308.SDR CALA2014021090340Fairing · unsecureLOUD HUMMING SOUND AROUND ROW 22. INSPECTED SEALS ON BOTH LT & RT SIDE, NO DEFECTS FOUND. TAPED FAIRINGS 191DT & 192DT. CREW ON FLIGHT 330 7 REPORTED NO HUMMING.SDR CALA2014020690299Warning System · activatedAIRCRAFT REJECTED TAKEOFF AT 100 KTS DUE TO AFT CARGO DOOR INDICATION.SDR CALA2014020690305Stringer · corrodedCORROSION ON STRINGER 41R BETWEEN FRAME 58 - 64 HAS NO ALLOWABLE LIMITS IAW SRM 53-41-13, PG 101. REPLACED STRINGER 41R BETWEEN FRAME 58 - 64 IAW SRM 51-42-11, PG 9. CORROSION ON STRINGER 41R BETWEEN FRAME 58 - 64 HAS NO ALLOWABLE LIMITS IAW SRM 53-41-13, PGSDR CALA2014020690306Stringer · corrodedCORROSION FOUND ON STRINGER 43L BETWEEN FRAME 54 - 60 HAS NO ALLOWABLE LIMITS IAW SRM 53-41-13, PG 101. REPLACED STRINGER 43L BETWEEN FRAME 54 - 60 IAW SRM 51-42-11, PG 9.SDR CALA2014020690322Stringer · corrodedCORROSION ON STRINGER 40L BETWEEN FRAME 56 - 64 HAS NO ALLOWABLE LIMITS IAW SRM 53-41-13.SDR CALA2014020690304Plate · wornLT NR 2 ENG PYLON BOTTOM ANTI CHAFE PLATE FOUND WORN AT HMV. PLATE WAS REPAIRED IAW SRM 54-51-12 FIG 202 FOR CONFIG 2 IRR 54-51-12-2-001-00 TB L 202.SDR CALA2014020690307Seat Track · corrodedCORROSION FOUND ON SEAT TRACK AT Y 1292 AT FRAME 20 WAS OUT OF SRM LIMITS. SEAT TRACK REPLACED FROM FRAME 12 - FRAME 24 IAW SRM 51-44-11 & 51-42-11.SDR CALA2014020390282Skin · dentedLT FUSELAGE SKIN DENTED AT FRAME 26 STRINGER 34 - 35. REPAIR DOUBLER INSTALLED IAW SRM 53-00-11 FIG 240, SRI 53-00-11-2-017-00 TBL 223.SDR CALA2014013190271Warning System · activatedECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN, APU. CYCLED CB'S L41 & L42. TRIED SECOND START ATTEMPT, APU DID NOT START. NO FLAME AT START ATTEMPT. LISTEN FOR CLICKING SOUND. IF CLICKING HEARD SUSPECT FUEL, IF NO CLICKING HEARD CHECK IGNSDR CALA2014012990264Warning System · false activationVENT AVIONICS SYS FAULT. RESET BREAKERS D05 D06 Y1 7 FAULT CLEARED.SDR CALA2014012890250Attach Bolt · corrodedNLG LEG ASSEMBLY DOOR LONG ATTACH BOLT CORRODED. NEW BOLT COMES FROM THE VENDER TEMP INSTALLED IN GEAR LEG.SDR CALA2014012990263Unknown · malfunctionedDUAL LGCIU FAILURE 1 & 2, GEAR COULD NOT BE EXTENDED WITH GEAR HANDLE, TRIED SEVERAL TIMES, USED ALT METHOD TO EXTEND GEAR. JACKED AIRCRAFT & PERFORMED NUMEROUS GEAR RETRACTION & EXTENSIONS. OPERATIONS CHECKED GOOD, ALL FLIGHT DECK INDICATIONS NORMAL & CORRESDR CALA2014012890256Warning System · activatedON LANDING AT 1000 FEET WE GOT AMBER REV FAULT THEN CAP PITOT ANTI-ICE FAULT THEN LG DISAGREE. CFDS SHOWS LT LG EXT PROX SENSOR 23GA TARGET POSITION.SDR CALA2014012890258Computer · faultedELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN.SDR CALA2014012490219Stringer · corrodedAFT CARGO COMPARTMENT STRINGER 41R, BETWEEN FRAME 58 - 64 IS CORRODED BEYOND LIMITS IAW SRM 53-41-13 PG 201. REPLACED STRINGER 41R, BETWEEN FRAME 58 - 64 IAW SRM 53-41-13 PG 201.SDR CALA2014012890255Warning System · activatedCREW REPORTS NR 1 SHOWED FADEC A FAULT & OVER SPEED PROTECT FAULT. CYCLED CB A04 & R41 FOR FADEC, ATTEMPTED RESTART & GOT ENG 1 EPR MODE FAULT WITH AMBER XX ON FUEL FLOW & EPR.SDR CALA2014012890257Epr System · faultedEPR MODE FAULT ENG 1 REFER TO TSM CHAPTER 77 ECAM & UAL A320 MEL CARD 73 120. ENG 1 EPR MODE FAULT DURING CLB. BOTH ENGS PUT INTO N1 MODE IAW CHECKLIST. NOTE ACFT HEALTH MONITORING ALSO SHOWS P2T2 SENS-HC -EEC1.SDR CALA2014012290214Stringer · corrodedAFT CARGO COMPARTMENT FUSELAGE STRINGER 43L, FRAME 56 -57 HAS CORROSION. REPLACED STRINGER 43L BETWEEN FRAME 56 - 57 IAW SRM 51-42-11, PG 7.SDR CALA2014012490230Engine · shutdownNR 2 ENG ACCELERATED THRUST IDLE AT 60 PERCENT N 1 SHUT ENG DOWN.SDR CALA2014012090184Apu · shutdownECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN, APU. TAXI IN APU SHUT DOWN HIGH EGT. ACCOMPLISHED NORMAL APU START. FUNCTION WITH ELECTRICAL & PNEUMATIC LOADS OPERATION NORMAL.SDR CALA2014012090185Sill · corrodedR2 DOOR SILL HAS CORROSION UNDER GIRT BAR FITTINGS. AFTER CLEANUP SILL FOUND TO BE OUT OF SRM LIMITS. SILL REPLACED IAW SRM 53-42-11. SRM REF FOR REPLACEMENT IS 53-42-11 PGS 7-25.SDR CALA2014012090181Access Panel · damagedRT WING FUEL TANK ACCESS PLATE 640NB HAS DAMAGED HOLE. INSTALLED BUSHING IAW SRM57-21-11 FIG 202 & BRIDGE REPAIR IAW SRM57-21-11 PAGE 213.SDR CALA2014012090182Selector Valve · failedON DESCENT, FLIGHT ATTEMPTED TO LOWER GEAR, BUT RECEIVED 3 RED LIGHTS. FLIGHT EXECUTED A FLY-BY & DECLARED AN EMERGENCY. CREW USED ALTERNATE GEAR EXTENSION PROCEDURES & LOWERED GEAR. FLIGHT LANDED SAFELY. ACCOMPLISHED NON-RII INSPECTION OF AMIS ITEM 5102002SDR CALA2014012090186Oil System · leakingOIL STREAK RUNNING FROM BENEATH DRAIN MAST ON INSIDE SIDE OF LT ENG. RESIDUAL OIL FROM THE COWLING VENT AREA, SMALL AMOUNT. OIL QTY CHECKED AT TANK, TANK IS FULL. REVIEW OF PLENOIL, ENG IS OPERATING AT 0.03 QTS PER HR WELL WITHIN LIMITS. CLEANED AREA, OK TSDR CALA2014012190205Warning System · activatedAUTO FLT YAW DAMPER 2 DISPLAYED ON UPPER ECAM SCREEN.SDR CALA2014012090183Eec · malfunctionedENG 1 FADEC B FAULT ON START. EEC REPLACED IN NR 1 ENG POSITION, OPERATIONS CHECKED OK IAW MM73-22-34 & MM73-22-34-400-010-A13.SDR CALA2014011690165Oxygen Bottle · low pressureO2 READING 900 PSI. ACCOMPLISHED O2 SERVICING IAW MM REF 12-14-35. OPERATIONS CHECKED GOOD. NO LEAKS, AIRCRAFT OK TO CONTINUE.SDR CALA2014011690166Battery · dischargedEMERGENCY LIGHT TEST THRU CIDS FAILED GIVING A 33-51-18 EPSU EMERGENCY BATTERY RT. REPLACED RT MID BATTERY IAW MM 33-51-38, OPERATIONS CHECKED OK.SDR CALA2014011690167Light · inoperativeSEAT ROW 27 ABC, EMERGENCY EXIT LIGHT INOPERATIVE. TERMINATED CONNECTOR AT EMERGENCY EXIT LIGHT SEAT ROW 27 ABC, OPERATIONS CHECKED GOOD.SDR CALA2014011690168Light · inoperativeSEAT ROW 37 ABC, EMERGENCY EXIT LIGHT INOPERATIVE. TERMINATED CONNECTOR EMERGENCY EXIT LIGHT AT SEAT ROW 37 ABC, OPERATIONS CHECKED GOOD.SDR CALA2014011690169Unknown · malfunctionedEMERGENCY LIGHTS TEST FAILED WITH EPSU EMERGENCY LT BATTERY & COMM MESSAGES. ORDERED EPSU BATTERY, TESTED SYS AGAIN & TESTED OK.SDR CALA2014011590153Light · inoperativeSEAT 28C EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT IAW MM 33-51-19, OPERATIONS OK.SDR CALA2014011590154Battery · faultyDURING EMERGENCY LIGHT CHECK ON 2 SERVICE, ESPU BATTERY EMERGENCY LT IS FAULTING. REPLACED EPSU EMERGENCY POWER SUPPLY UNIT BATTERY AT LT MID, OPERATIONS CHECKED OK.SDR CALA2014011490140Oxygen Mask · unsecureO2 MASKS FELL 11 ABC, IAW MT35-003 FOR DROP CHECK WITHIN 3 DAYS.
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