IAE V2527-A5
Service difficulty reports · 8,011
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 AWXA200501579Sill · corrodedDURING C6 CHECK DISCOVERED CORROSION ON BULK FUSELAGE DOOR SILL AROUND 5 NUT PLATE HOLES OVER STR. 38R, Y-670 AND BETWEEN FR 60+1 INCH AND FR 62. MAINTENANCE REWORKED THE DAMAGED ARE AND WAS FOUND OUT OF LIMITS IAW SRM 53-41-49 PAGE 103, FIG 101. CUT OUT DAMSDR 2005UALA01350Beam · corrodedCORROSION OUTBOARD BEAM FWD OF R2 DOOR BETWEEN FR66 & FR65. REPLACED DOOR R2 SILL PER SRM 51-42-00-004.SDR 2005UALA01337Sensor · dirtyRETURN TO FIELD DUE TO CARGO DOOR INDICATION. CLEANED SENSOR. OPERATED DOOR SEVERAL TIMES WITH NO FAULTS.SDR 2005UALA01338Engine · bird ingestionMULTIPLE BIRD STRIKES ON CLIMBOUT, LITE SMOKE ODOR THROUGHOUT CABIN. AIRFRAME AND NR 2 ENG DAMAGED. AMBER ALERT DECLARED AND RETURNED TO FIELD. BIRD STRIKE CAUSED THE RTF. DAMAGED FAN BLADES WERE REPLACED AND THE LPC AND HPC WERE BORESCOPE INSPECTED AND FOSDR 2005UALA01301Engine · surgesRETURNED TO FIELD AFTER THE NR 1 ENGINE SURGED. ECM SHOWS NO RECORD OF A SURGE/STALL. EEC/FADEC RECORDED NO STALL MESSAGE. FMU WAS REPLACED FOR N1 OVER SPEED AND CHANNEL B FAULT. FMU TEST SHOWS NO FAULT FOUND. CAUSE OF SURGE CAN NOT BE DETERMINED.SDR 2005UALA01311Battery · faultyCABIN EMERGENCY LIGHTS TEST, EPSU BATTERY EMERGENCY LIGHT FAULT. REPLACED EPSU BATTERYSDR 2005UALA01287Bottle · dischargedDOOR 1R ESCAPE SLIDE BOTTLE INDICATION OUT OF GREEN BAND. THE SLIDE (MR25611-1055) HAD BEEN REMOVED FROM ACFT 4622 WITH A WRITE-UP STATING THAT BOTTLE PRESS NEEDLE WAS IN "RED BAND". HOWEVER, THE SHOP INSPECTION REVEALED THAT THE BOTTLE WAS IN THE "GREENSDR 2005UALA01284Ram Air Turb · no testRAT TEST FAILED AS PER EQ3073. GREEN GOV LIGHT WILL NOT ILLUMINATE DURING TEST. REPLACED RAT GRD CHK MODULE IAW MM, DID NOT HELP. REPLACED RAT PER 29-22-51, NEEDS OPS CHK & LEAK CHK TO BE COMPLETED. INSPECTED INSTALLATION.SDR 2005UALA01286Power Supply · no testFWD LEFT EMERGENCY POWER SUPPLY UNIT FAILED TEST DURING EMERGENCY LIGHT TEST. PSU REPLACED.SDR 2005UALA01266Battery · faultyEMERGENCY LIGHT TEST FAULTS "EPSU BATTERY EMER R". SUPPLEMENTAL DATA UPDATE REPLACED EPSU 12WL BATTERY.SDR 2005UALA01255Skin · damagedFUSELAGE WAS DAMAGED BETWEEN FR73 & FR74 AND STR 41R TO 41L DURING AIRCRAFT JACKING, SKIN AND 6 EACH SHEAR TIES WERE BENT. *S/D* REPLACED 6 EA SHEAR TIES BETWEEN STR 41R & 41, 3EA ON FR73 AND FR74 REF SRM 51-42-11. INSTALLED 2EA TRIPLER REPAIRS PER SRM 53-0SDR 2005UALA01259Skin · dentedBIRD STRIKE ON APPROACH LOWER FWD SECTION OF ACFT. *S/D* FABRICATED SKIN REPAIR AND INSTALLED PER SRM 53-00-11.SDR 2005UALA01260Skin · dentedFOUND DENT IN FUSELAGE SKIN ON WALKAROUND 62.5 INCHES FWD OF DOOR 2L. *S/D* INSTALLED DOUBLER REPAIR PER SRM 53-41-11.SDR 2005UALA01261Skin · dentedFOUND DENT IN FUSELAGE AFT OF DOOR 2L, 27 INCHES PAST DOOR & 4.75 INCHES ABOVE DOOR SILL. DENT IS 1.5 INCH WIDE & 1.75 INCH LONG BY .062 DEEP. LOCATED 9 INCHES PAST FR69 & 1 INCH BELOW STR 24. * S/D* ACCOMPLISHED HFEC TO BOTH EXTERNAL AND INTERNAL AREA OF SDR 2005UALA01228Battery · malfunctionedEPSU COMM FWD LT MESSAGE DURING EMERGENCY BATTERY SYS TEST. REPLACED BATTERY PACK AT DOOR 1 LEFT,SDR 2005UALA01226Light · inoperativeEELS INOPERATIVE.SDR 2005UALA01227Light · burned outONE LIGHT OF THE EMERGENCY LIGHTING PATH IS BURNED OUT ROW 15.SDR 2005UALA01219Generator · malfunctionedF/A REPORTS INTERMITTENT BURNING SMELL AT ROW 15, SMELLS LIKE BURNT RUBBER. CREW SHUT DOWN & SECURED GEN 2. NR 2 ENG IDG PYLON CONNECTOR FOUND WITH EVIDENCE OF FRETTING, ARCING AND BLACK SOCKETS WITH SOME PITTING. NR 2 ENG IDG HARNESS REPLACED.SDR 2005UALA01206Skin · gougedTHREE EACH GOUGES FOUND IN RVSM AREA ON RIGHT SIDE OF AIRCRAFT. DAMAGE IS APPROXIMATELY SIX INCHES FORWARD OF FORWARD CARGO DOOR. BLENDED DAMAGES TO REPAIR, REF. SRM53-11-11 AND SRM 53-00-11.SDR 2005UALA01205Battery Pack · failedEMERGENCY LIGHT TEST FAILS RT EPSU. REPLACED BATTERY PACK AT 12WL.SDR 2005UALA01198Battery · failedEPSU BATTERY FWD LT FAILED EMERGENCY LIGHT TEST. REPLACED EPSU BATTERY.SDR 2005UALA01203Aspirator · unserviceableTWO (2) DAMAGED ASPIRATORS.SDR 2005UALA01183Odor · detectedWHILE DESCENDING THRU 7000 FT, HAD BURNING RUBBER SMELL AND ACRID FUMES IN THE FWD CABIN AREA AND THE COCKPIT. INITIALLY SUSPECTED THERAPUETIC O2 CYCLINDER TO BE REASON FOR BURNING RUBBER SMELL. THERAPUETIC O2 BOTTLE WAS REMOVED. THE PSUS, SIDEWALL PANELS, SDR 2005UALA01184Light · no testWHILE TESTING EMERGENCY LIGHTS FAULTED EXT LOADS FWD L HAD RED FAULT LIGHT EXT LOADS. WHILE PERFORMING THE AIRCRAFT EMERGENCY LIGHT TEST, SYSTEM MESSAGE POINTING TO FAULT IN FWD DOOR SLIDE ASSY. THE SLIDE WAS REPLACED SERVICEABLE ONE AND THE AIRCRAFT SYSTEMSDR 2005UALA01185Light · malfunctionedLEFT FWD EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN, DOOR. REPLACED FWD EMER BATTERY.SDR 2005UALA01186Light · malfunctionedLEFT AFT EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN, DOOR. REPLACED EMERGENCY BATTERY AT LEFT OVERWING POSITION AND LEFT AFT POSITION.SDR 2005UALA01177Blade · wornENGINE 2 STALL DISPLAYED ON UPPER ECAM SCREEN DURING CLIMB OR CRUISE ACCELERATION. ENGINE NOT SHUTDOWN. STALL DISPLAYED ON UPPER ECAM SCREEN AFTER POWER REDUCTION FROM T/O POWER. ENGINE NOT SHUT DOWN. TROUBLESHOOTING BORESCOPE INSPECTION REVEALED OUT-OF-LISDR 2005UALA01182Skin · damagedDOOR 1L HAS SKIN DAMAGE. MAJOR REPAIR OF DOOR SKIN PER SRM 52-10-00 FIGURE 203 WITH INCLUSION OF CORNER PRINCIPLE FROM FIGURE 205.SDR 2005UALA01174Power Supply · inoperativeFWD LEFT POWER SUPPLY UNIT AND BATTERY FOR EMERGENCY LIGHT INOP. REPLACED FWD LEFT POWER SUPPLY UNIT WITH BATTERY.SDR YENA200576Battery Pack · dischargedDURING EMERGENCY LIGHT SYSTEM TEST. EPSU EMER. L DISPLAYED. REMOVED AND REPLACED EPSU (11WL) BATTERY PACK IAW AMM 33-51-38. SYSTEM OPS CHECK GOOD.SDR 2005UALA01175Light · failedCABIN EMERGENCY LIGHT TEST FAILED, INDICATES ON MESSAGE, FWD BATTERY LOW ON THE FIRST TEST. FOLLOWED BY INT LOADS FWD L MESSAGE AFTER FEW MORE TEST. REPLACED EMERGENCY POWER SUPPLY AND BATTERYSDR 2005UALA01142Light · inoperativeSEAT MOUNTED EEL LIGHT INOP AT SEAT 13ABC. REPLACED CABLE ASSY.SDR 2005UALA01143Light · inoperativeEMERGENCY LIGHT AT SEAT ROW 20 ABC INOPERATIVE. REPLACED HARNESS.SDR 2005UALA01127Epsu · will not testEMERGENCY LIGHT TEST FAILED EPSU INT LOAD FWD L. REPLACED THE FWD LEFT EPSU.SDR 2005UALA01125Computer · malfunctionedRETURN TO FIELD DUE TO A FUEL QUANTITY ISSUE. OPERATED BOTH ENGINES TO OBSERVE ENGINE FUEL BURN AND THE POSSIBILITY OF FUEL LEAKS. VISUALLY CHECKED MFLI (MAGNETIC FUEL LEVEL INDICATORS) FOR VERIFICATION OF FUEL QUANTITY INDICATIONS. ALSO, FQIC (FUEL QUANTITSDR 2005UALA01111Display · inoperativeABORTED TAKEOFF AT 142 KNOTS DUE TO CAPTAIN'S PFD BLANKED OUT. HOT BRAKES ECAM WITH ONE BRAKE OVER 600 DEGREES.SDR 2005UALA01092A/C Pack · malfunctionedFLIGHT DIVERTED WITH THE NR 1 PACK TRIPPING AND NR 2 PACK ALREADY DEFERRED. AIRCRAFT LOST NR 1 PACK APPROXIMATELY 20 MINUTES AFTER TAKEOFF. NR 2 PACK PREVIOUSLY DEFERRED. CIRCUIT BREAKERS CYCLED AND PROVIDED NO HELP. REPLACED NR 1 RAI ACTUATOR (MR21603-11 SDR 2005UALA01091Warning Light · illuminatedLANDED UNDER AMBER ALERT DUE TO FLUCTUATING CABIN PRESSURE. CABIN PRESSURE EXCESS CABIN ALTITUDE ON DESCENT. AFTER RAPID DESCENT, THEN GOT CABIN PRESSURE LOW DIFFERENTIAL PRESSURE AND SAFETY VALVE OPEN ECAM MESSAGES. CABIN PRESSURE CHANGES FELT BY CREW & PASSESDR 2005UALA01077Battery · failedEMERGENCY LIGHT BATTERY RT FAILED 3SVC TEST. REPLACED EMERGENCY LIGHT BATTERY.SDR 2005UALA01059Floor Support · corrodedAFT GALLEY CORROSION. FLOORBEAM AND SPLICE ANGLE REPLACED.SDR 2005UALA01046Hose · brokenFOUND BROKEN HOSE.SDR 2005UALA01023B-Nut · leakingYELLOW HYDRAULIC SYSTEM PROBLEM IAD MM FOUND FLUID LEAKING AT BRAKE SHUTOFF VALVE 2579GM LOWER B-NUT FITTING. IAD MM REPLACED PARKING BRAKE SHUTOFF VALVE FIN 2579GM PER MM 32-45-14. NO LEAKS NOTED. SERVICED YELLOW HYD SYSTEM TO FULL.SDR 2005UALA01022Engine · leakingFLIGHT DIVERTED WITH NR 1 ENGINE OIL QUANTITY PROBLEM. DURING FLIGHT, LEFT ENGINE OIL QTY DECREASED TO 1.5 QTS. THE PILOTS DID NOT SHUT DOWN THE ENGINE & KEPT THE ENGINE RUNNING AT IDLE THRUST 62% N1, WITH OIL PRS 120, OIL TEMP 115. NONE OF THE ENGINE PARAMESDR 2005UALA01015Stringer · corrodedCORROSION ON STR 43L BETWEEN FS 57 AND FS 58. BUSINESS DECISION TO REPLACE STRINGER RATHER THAN REPAIR.SDR 2005UALA01037Warning Light · illuminatedUPPER ECAM NR 2 ENGINE STALL DISPLAYED ON TAKEOFF. ECM DATA SHOW STALL OCCURRED IN FLIGHT PHASE 6. MAINTENANCE FOUND MUSCLE LINE LOOSE ON TENTH STAGE HPC BLEED SOLENOID. LEAKING MUSCLE AIR COULD OF LEAD TO SLOW OR FAULTY OPERATION OF TENTH STAGE HPC STABILSDR 2005UALA01004Stringer · corrodedAFT PIT STR 42L HAS CORROSION BETWEEN FS 53 AND FS 54.SDR 2005UALA01005Stringer · corrodedSTR 42L HAS CORROSION BETWEEN FR 55 AND FR 57.SDR 2005UALA01006Switch · malfunctionedALL CABIN EMERGENCY EXIT SIGNS ILLUMINATED WITH SWITCHES SELECTED OFF. AMIS ITEM 8612012, CONTINUATION OF AMIS ITEM 8612010: CYCLED NO SMOKING SWITCH.SDR YENA200567Proximity Sensor · inoperativeON TAKE OFF, AT APPROXIMATELY 1500, AGL GOT ECAM. F/O PERFORMED ECAM ACTION, SHOCK ABSORBER FAULT, THAT CLEARED AND THEN GOT ECAM GEAR NOT LOCKED IN UP POSITION. PERFORMED THAT ECAM WHICH CLEARED ALL PROBLEM WITH NO STATUS MESSAGE. AIRCRAFT LANDED WITHOUT ISDR 2005UALA01000Stringer · corrodedSTRINGER 43L HAS CORROSION BETWEEN FS 54 AND FS 55.
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