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 CALA2015102094682Stringer · corrodedAFT CARGO, STRINGER 43L IS CORRODED, BETWEEN FRAME 58 - 59. R & R STRINGER 43L IAW SRM 51-42-11.SDR CALA2015102094599Pressure Switch · faultyAPU AUTO SHUTDOWN EN-ROUTE, RESTART NO GOOD. REPLACED OIL PRESS SWITCH & CONFIRMED OIL QTY SERVICED TO FULL.SDR CALA2015102094611Skin · dentedEXTERIOR FUSELAGE DENT, BETWEEN FRAME 71 - 72 & STRINGER 29L - 30L. MEASURED DENT, FOUND TO BE OUT OF SRM LIMITS. FABRICATED & INSTALLED DOUBLER IAW SRM 53-00-11 FIG 204.SDR CALA2015102094612Skin · dentedEXTERIOR FUSELAGE DENT AT FRAME 71, STRINGER 19L. MEASURED DENTS & FOUND TO BE OUT OF SRM LIMITS. FABRICATED & INSTALLED A DOUBLER IAW SRM 53-00-11 FIG 205.SDR AALA201510159011Unknown · malfunctionedCAPTAIN REPORTED THAT ON TAKEOFF THAT NR 1 ENG WAS ABOUT 2 SECONDS BEHIND THE OTHER ENG & THE FLIGHT CREW PERFORMED A LOW SPEED ABORTED TAKEOFF, ABOUT 40 KNOTS. REVIEWED AIRMAN, NO FAULTS RECORDED. PERFORMED A TEST OF THE FADEC IAW AMM 73-22-00 WITH NO ISSUESDR CALA2015102094686Frame · corrodedL2 DOOR SILL HAS CORROSION, FRAME 68 & AT FWD AFT GIRT FITTING ATTACHMENTS, FRAME 66 - 68, STRINGER 22L - 23L. BLENDED CORROSION L2 DOOR SILL, MATERIAL LOSS .008, FRAME 68 .036 FOUND TO BE WITHIN LIMITS SRM 53-41-14 FIG 101. INBD FLANGE & FRAME 66 CORROSION SDR CALA2015101494588Connector · dirtyECAM FAULT SYS ONE, NOSE WHEEL IN FLIGHT. DECLARED EMER, REQUESTED LONGER RUNWAY. ACCOMPLISHED TSM 32-51-00-810-811, CFDS TESTS & CLEANED CONNECTORS AT 6GC, 4GC & 3GC. RESET SYS, TESTED GOOD, NO MOISTURE OR CORROSION FOUND.SDR GTIA2015100901385Engine · stalledNR 2 ENGINE STALLED, OIL PRESSURE DROPPED TO ZERO, OIL FILTER CLOGGED LIGHT CAME ON AND ENGINE WAS SHUTDOWN. FLIGHT DIVERTED. R & R NR 2 ENGINE.SDR CALA2015100594573Splice · crackedLEFT FRAME 20 CROSSBEAM SPLICE AT FLOORBEAM HAS CRACK INDICATION IN 2ND FASTENER HOLE FROM OTBD. REPAIRED LT FRAME 20 CROSSBEAM SPLICE AT FLOORBEAM 2ND HOLE OTBD IAW SRM 51-44-11 & RFT S 6000, NO SRI REQUIRED.SDR CALA2015100594564Skin · damagedSKIN DAMAGE BETWEEN FRAME 68 - 69 AT STRINGER 29L. MAJOR REPAIR. SKIN REPAIRED IAW SRM 53-41-11 FIG 215.SDR CALA2015100594565Apu · malfunctionedPACKS ON WITH APU, CABIN FILLED WITH SMOKE & APU AUTO SHUTDOWN. REPLACED APU IAW AMM 49-11-98-890-001-A.SDR CALA2015092994547Slide · unsecureARMING ISSUE, LEVER DOOR 2R WHEN AIRBORNE LIFTED SLIGHTLY & BACK FLUSH AFTER LANDING. REPLACED DOOR 2R SLIDE DUE TO IT SHIFTING IN BUSTLE & CAUSING ARMING ISSUES. REPLACED IAW MM 25-62-44.SDR CALA2015092594399Slide · defectiveCABIN EMER LIGHT TEST FAILED. REPLACED FWD LT SLIDE, NO HELP. REPLACED RT FWD SLIDE, MSG CLEARED IAW AMM 25-62-44. DOOR ASSIST ACTUATORS REAMED.SDR CALA2015092594401Controller · malfunctionedCAPTAIN PITOT ECAM WARNING WITH SMOKE SMELL IN COCKPIT & CABIN. REPLACED CAPTAINS PROBE HEAT CONTROLLER IAW AMM 30-31-34. OPERATIONS CHECKED GOOD, NORMAL ON HIGH HEAT, NO SMOKE SMELL, CB REMAINS CLOSED.SDR CALA2015092194380Battery · dischargedREFERENCE 2 SERVICE, EMER LIGHTS FAIL TEST. R & R LT FWD EPSU BATTERY, BATTERY ONLY, IAW AMM 33-51-38-000-002A & 33-51-38-400-002A. OPERATIONS CHECKED OK.SDR CALA2015092194381Light · no testREFERENCE 2 SERVICE, EMER LIGHT SYS TEST FAILS. RESET EMER EXIT LIGHT BREAKERS H5, H6 & H7. ACCOMPLISHED EMER EXIT LIGHT TEST IAW 31-51-00-7 10-001. OPERATIONS CHECKED OK.SDR CALA2015092194378Brace · corrodedAT FRAME 66, STRINGER 25 BRACE, FROM FRAME TO STRINGER CORRODED. R & R SECTION OF STRINGER 25R & INSTALLED BETWEEN FRAME 66.5 - 67.5 IAW SRM 53-00-13. ACCOMPLISHED AT LCQ C4.SDR CALA2015091694360Stringer · corrodedFUSELAGE STRUCTURE, BENEATH OUTFLOW VLV, FRAME 66, STRINGER 31R, CORROSION. R & R STRINGER 31R, FROM FRAME 64 - 66 IAW SRM 51-42-11 PGS 25 - 26.SDR CALA2015091694361Beam · crackedLEFT SIDE BOX BEAM, UPPER FLANGE AT FRAME 43, HAS CRACK INDICATION AT AFT HOLE NR 9, FWD & AFT SIDES OF HOLE, 6 O'CLOCK & 12 O'CLOCK, FROM TOP SURFACE OF FLANGE TO A DEPTH OF .230". REPAIRED ON EA 5331-01704 OPS 3 - 12.SDR CALA2015091694362Beam · crackedLEFT SIDE BOX BEAM, UPPER FLANGE AT FRAME 43, HAS CRACK INDICATION AT HOLE NR 10, AFT SIDE OF HOLE, 6 O'CLOCK, FROM TOP SURFACE OF FLANGE TO A DEPTH OF .110". REPAIRED ON EA 5331-01704 OPS 3 - 12.SDR CALA2015091494348Battery · dischargedEMERGENCY LIGHTS FAILED TEST IAW 2 SVC. REPLACED BATTERY IAW AMM 33-5 1-38. TESTED OK.SDR CALA2015091494349Light · inoperativeEMERGENCY LIGHT FAILS TEST, FAULT LT FWD EXTERIOR LIGHTS. TROUBLE SHOT TO DOOR 1L SLIDE PACK. HAS OPEN IN ONE BULB, WILL NEED TO HAVE SLIDE PACK REPLACED.SDR CALA2015091694355Cleat · corrodedAT FRAME 66, STRINGER 28R CLEAT, AFT OF FRAME CORRODED. R & R CLEAT IAW SRM 51-42-11 PG 25 PARAGRAPH 7.SDR CALA2015091694356Stringer · corrodedSTRINGER 26R FWD & AFT OF FRAME 66 HAS CORROSION. R & R STRINGER IAW SRM 51-42-11 PGS 25 - 27.SDR CALA2015091694357Stringer · corrodedAT FRAME 66, STRINGER 32R CORRODED UNDER & BEHIND FRAME. R & R STRINGER 32R AT FRAME 66 IAW SRM 51-42-11 PARA 7.SDR CALA2015091694359Slide · defectiveEMERGENCY LIGHT FAILED TEST, FAULT LT FWD EXT LIGHTS. REPLACED SLIDE PACK DOOR 1 LT IAW AMM 25-62-44. EMER LIGHT TESTED OK.SDR CALA2015091494346Cleat · damagedTWO EACH ENLARGED LOCK FASTENER HOLES ON CLEAT, BY FRAME 65 & STRINGER 31R. R & R CLEAT IAW GPM 07-35-0 & SRM 51-42-11 PARA 6 & 7.SDR AALA201509149009Cover · looseFLIGHT 574 NOTIFIED DISPATCH THAT THEY BEGAN TO LOSE OIL QTY WHILE EN-ROUTE. THEY STATED THAT IT WAS OK TO CONTINUE & RECEIVED NO ECAM MSGS RELATED. ON APPROACH, THE CREW ASKED FOR NO UNDUE DELAYS DUE TO OIL QTY BEING LOW. ATC DECLARED AN EMER FOR THE FLIGHSDR CALA2015091194292Light · failedEMERGENCY LIGHT TEST FAILED IAW NR 2 SVC. EPSU BATTERY EMER LT. OPERATIONS TESTED IAW AMM 33-51-0 0-710-001-A.SDR CALA2015091194295Relay · faultyCREW REPORT ENG 1 N1 IS OPERATING IN THE UNRATED MODE, IAD EFS AMT'S. REPLACED RELAY BOX IAW AMM 71-51-49 401. ACCOMPLISHED 2 EACH AUTO STARTS, EPR INDICATION NORMAL, PFR'S CLEAN, ALSO ACCOMPLISHED CAT III CHECK IAW AMM 22-97-00.SDR CALA2015091194289Beam · crackedLEFT SIDE BOX BEAM UPPER FLANGE AT FRAME 43 HAS CRACK INDICATION AT HOLE NR 9 AT 11 O`CLOCK POSITION. CRACK IS INSIDE AREA A. HOLE DIAMETER START AT .248 AT LOWER SURFACE OF BOX BEAM UPPER FLANGE TO .252 AT UPPER SURFACE OF PRESS PLATE FITTING. REPAIRED IAWSDR CALA2015091194293Skin · saturatedRIGHT ELEV UPPER SKIN PANEL HAS TRAPPED WATER INDICATION IN 3 LOCATIONS, 133" FROM INBD END, 16" FROM TE 2" DIAMETER, NEXT 131" FROM INBD END, 10" FROM TE 2" X 3"DIAMETER, NEXT 117" FROM INBD END, 12" FROM TE .250" DIAMETER, CARRIED FROM 12 13 14. CUT OUT TSDR CALA2015091094285Regulator Valve · faultyAFTER TAKEOFF CREW LOST BOTH ENG BLEEDS & CROSS BLEED VLV, STARTED APU FOR BLEED, DIVERTED. ACCOMPLISHED BMC BITE CHECKS OK. ACCOMPLISH FAULT CHECK OF CROSS BLEED VLV POSITION CONTROL OK. REPLACED PRESS REGULATOR VLV. OPERATIONS CHECKED GOOD.SDR CALA2015090394267Smoke Detector · false activationSMOKE DET FAULT ECAM. CYCLED ACFT POWER, NO MSG DISPLAYED. ACCOMPLISHED CFDS SMOKE DETECTOR TEST, NO FAULTS. SYS CHECKED OK.SDR CALA2015083194262Unknown · odorCREW REPORTED THAT ONE PAX AT ROW 29 SMELLED SMOKE, WHICH THEN DISSIPATED. AFTER REVIEW OF SMOKE ODOR QUESTIONNAIRE, AN INSPECTION WAS ACCOMPLISHED WITH ALL CABIN SYSTEMS POWERED & GALLEY CHILLERS ON. NO SMELL OR SMOKE NOTED. ACFT BACK TO NORMAL CONFIGURATISDR AALA201509049010Thrust Reverser · defectiveFLIGHT 647 DEPARTED & AT 15000 FT THEY GOT AN ENG ONE OVER SPEED FAULT & THE ENG BEGAN OSCILLATING ON ITS OWN. THE ENG WAS BROUGHT BACK TO IDLE & THE ACFT RETURNED FOR MX. AN EMER WAS DECLARED & THE ACFT LANDED WITHOUT INCIDENT. REPLACED THE NR 1 ENG RT TRSDR AALA201509049011Solenoid Valve · defectiveFLIGHT 647 DEPARTED & AT 15000 FT THEY GOT AN ENG 1 OVER SPEED FAULT & THE ENG BEGAN OSCILLATING ON ITS OWN. THE ENG WAS BROUGHT BACK TO IDLE & THE ACFT RETURNED FOR MX. AN EMER WAS DECLARED & THE ACFT LANDED WITHOUT INCIDENT. REPLACED THE NR 1 ENG RT TRANSSDR AALA201509049012Bleed Valve · defectiveFLIGHT 647 DEPARTED & AT 15000 FT THEY GOT AN ENG 1 OVER SPEED FAULT & THE ENG BEGAN OSCILLATING ON ITS OWN. THE ENG WAS BROUGHT BACK TO IDLE & THE ACFT RETURNED FOR MX. AN EMER WAS DECLARED & THE ACFT LANDED WITHOUT INCIDENT. REPLACED THE NR 1 ENG RT TRANSSDR CALA2015082894245Battery Pack · defectiveDURING 2 SERVICE CHECK FOR EMER LIGHTS, HAD EPSU BATTERY AFT L MSG AT DOOR 1L TEST PANEL. REPLACED EMER EXIT LIGHT BATTERY PACK AT AFT LT DOOR & EMER EXIT LIGHT BATTERY ASSEMBLY AT LT OVERWING EXTERIOR. ACCOMPLISHED EMER LIGHT TEST. OPERATIONS CHECKED NORMASDR CALA2015082494241Eec · faultyEN-ROUTE ECAM STATUS MSG REVERSER 2 & ENG 2 THRUST MSG. OPERATIONS OK ON GND. REPLACED NR 2 ENG EEC IAW MM 73-22-34. RAN ENGINE, PFR CLEAN.SDR CALA2015081894225Stringer · corrodedSTRINGER 42L IN AFT CARGO COMPARTMENT IS CORRODED FROM FRAME 57 & 60. REMOVED STRINGER 42L, SPLICES FROM FRAME 57 & 60. INSTALLED NEW STRINGER & SPLICES IAW SRM 53-00-13, TABLE 201.SDR CALA2015081894227Bushing · wornVIBE FELT IN COCKPIT & FWD GALLEY ON CLIMB OUT, FL 27O TO FL 340, 280 KIAS, NO VIBES LVL. REPLACED NLG AFT DOORS BUSHINGS & BOLTS IAW MM 32-22-13-410-001-A.SDR CALA2015081894228Power Supply · inoperativeINTERNAL LOADS EMER L, FAULT MSG WHEN PERFORMING EMER LIGHTS TEST. REPLACED POWER SUPPLY & BATTERY FWD LT IAW AMM 33-51-38-000-001. OPERATIONS CHECKED NORMAL.SDR CALA2015081894224Skin · dentedEXTERNAL FUSELAGE DENTED AT FRAME 29, STRINGER 39L. DENT OUT OF LIMITS, SO DAMAGE CUT OUT & EXTERNAL DOUBLER INSTALLED IAW PER SRM 53-00-11 FIG 239. IAW SRI 53-00-11-2-017-00 PARA 3L FIG 225, REPAIR NEEDS TO BE INSPECTED AT 60,000 CYCLES FROM TIME OF REPAIR SDR CALA2015081494222Oxygen Mask · deployedPASSENGER OXYGEN MASKS FELL AT ROW 23 ABC. REPACK OXYGEN MASKS, ALSO ROW 28 ABC DROPPED & REPACKED. DROP CHECKED AMM 35-23-00-710- 001-A.SDR CALA2015081194196Coffeemaker · malfunctionedFORWARD GALLEY WORK LIGHT, CB TRIPPED G2, ELEC ODOR NOTICED. NOTE FWD GALLEY WORK LIGHT IS DEACTIVATED & COLLARED BLACK. FOUND ELEC ODOR COMING FROM FWD GALLEY COFFEE MAKER. REPLACED COFFEE MAKER, CHECKED OK.SDR CALA2015081194189Slide · activatedDOOR 2L SLIDE INFLATED DURING CLEANING. REMOVED INFLATED SLIDE FROM DOOR 2L IAW AMM 25-62-44-000-011-A.SDR CALA2015081194190Unknown · odorFLIGHT ATTENDANT REPORTED SMELL OF PLASTIC, HOT OR BURNING IN AFT GALLEY. PUT PACK FLOW TO HI & FLIGHT ATTENDANT TURNED OFF WORK LIGHT, SMELL WENT AWAY. IAW AMM 05-51-10-200-801C1 INSPECTED AFT GALLEY AREA, COULD NOT DUPLICATE ODOR. NO FAULTS FOUND, CHECKEDSDR AALA201508119002Compressor · failedRETURN TO FIELD, DURING FLIGHT A COMPRESSOR FAILURE WAS ENCOUNTERED ON THE NR 1 ENGINE. R & R THE NR 1 ENGINE. ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK IAW TASK CARD 26L40071004.SDR CALA2015081194187Structure · dentedDENT AT FRAME 62 - 63, 4" WIDE & 7" LONG. CUT OUT DAMAGE & INSTALLED .071" DOUBLER IAW SRM 53-00-11 PARA 4W FIG 238.
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