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 UALA2009012600268Lanyard · looseLANYARD LOOSE AT DOOR 1R. SECURED LANYARD.SDR UALA2009012600275Seal · leakingL WING LEAK DISPLAYED. FLIGHT DIVERTED. FOUND L WING BLD DUCT SEALS LEAKING INBOARD ON NR 1 PYLON, REF IPC 36-11-05-11B ITEM 220. REPLACED SEALS, NO LEAKS WITH APU BLEED ON, NO FAULTS, BMC1&2 GND TEST PASSED.SDR UALA2009012600263Mask · faultyCREW REPORT: CAPTS O2 MASK WON'T TEST, CAN'T TRANSMIT ON INT HAND MIC CHECKS OK ON INT. SWAPPED WITH 2ED OBS SEAT AND NOW CAPT WORKS NORMAL.SDR UALA2009012200239Pin · missingCOCKPIT HALON FIRE EXTINGUISHER IS MISSING PIN AND SAFETY SEAL. ALSO IS PAST HYDROSTATIC SERVICE DATE CHECK.SDR UALA2009012300251Control Unit · faultySMOKE LAV CARGO DETECTOR FAULT UPPER ECAM. REPLACED SDCU AND ACCOMPLISHED BITE CHECK. ALL CHECKS NORMAL.SDR UALA2009012200238Actuator · leakingTHE LANDING GEAR LOCK-STAY ACTUATOR ON THE LEFT MAIN GEAR LEAK REF CF371 IS OUT OF LIMITS. REPLACE THE LOCK STAY ACTUATOR DUE TO WEAR.SDR UALA2009011900212Control Unit · failedLGCIU2 REVERSER FAULT. FLIGHT DIVERTED. REPLACED LGCIU 2 AND REINSTALLED FLIGHT CONTROL UNIT AFTER TROUBLESHOOTING.SDR UALA2009011900211Control Unit · failedNR 2 ENGINE REVERSER PRESSURIZED. FLIGHT DIVERTED. REPLACED 4101KS THRUST REV HYD CONTROL UNIT. LEAK AND OPS GOOD. NO MESSAGES.SDR UALA2009031000179Fitting · faultyDOOR 2 LT ESCAPE SLIDE BUSTLE STRAP RETAINING CLIP BROKEN. REPLACED SLIDE ASSY.SDR UALA2009011900186Smoke Detector · false activationCREW REPORT: RECEIVED A FWD LAV SMOKE INDICATION. FLIGHT DIVERTED. CREW REPORT: RECEIVED A FWD LAV SMOKE INDICATION. NO VISIBLE SMOKE PRESENT. ALARM WAS RESET ON CIDS PANEL. FAULT WAS ACTUALLY WITH LAV F, WHICH IS AFT MOST LAV. INSPECTED AREA FOR ANY DISSDR UALA2009011500161Frame · damagedFUSELAGE DOUBLER AT FRAME 23 + 24 BETWEEN STR 20L + 21L HAS DAMAGE. DOCUMENTED MAJOR REPAIR ACCOMPLISHED ON W-U'S M8934Q AND D9656Y.SDR UALA2009011900184Unknown · malfunctionedLOSS OF SOME NAV EQUIPT. FLIGHT DIVERTED. IR 1 SW WAS SHOWING OFF WITH NO ACTION ON SWITCH. SWITCH WAS NOT TURNED OFF BY FLT CREW. IR 1 SWITCH OFF ON ARRIVAL. CHECKED INTEGRITY OF SWITCH. FOUND TO BE POSITIVE WITH GOOD DETENT IN NAV POSITION. CHECKED FUSDR UALA2009011300147Slide · unserviceableDURING INTERIOR INSP, FOUND L1 DOOR SLIDE TO BE OUT OF LIMITS. REMOVED 1L SLIDE AND PINED PLACED IN SHOP. PUT ATTACHING HARDWARE BACK INTO ATTACHING HOLES IN ORDER NOT TO LOOSE THE BOLTS. GIRT BAR IS STILL ATTACHED TO SLIDE. INSTALLED LAST BOLT INTO THE SLIDESDR UALA2009011400158Smoke Warning · false indicationAVIONICS SMOKE ECAM. FLIGHT DIVERTED. FLT ATTENDS REPORTED TO FLT CREW LOTS OF CONDENSATION IN THE ACFT. HOWEVER NO SMOKE WAS REPORTED. NO FAULTS REPORTED ON PREVIOUS LEGS RPT OR POST FLT REPORT. ACCOMPLISHED VISUAL INSPECTION OF E&E AND PAX CABIN WITH NOSDR YENA20090114003Sense Line · leakingNOTICEABLE PRONOUNCED REDUCTION IN PWR ON NR2 ENGINE FOR 1 SEC ON CLIMBOUT THROUGH 12000 FT EPR NR1 1.295 EPR2 1.15O THEN STABILIZED. NO ASSC ECAMS. REPEAT ON A PREVIOUS WRITE UP. FOUND FLIGHT DATA FAULT CODE EPRINI AT 12360 FT FLIGHT PHASE 6. CHECKED P5 LINE SDR UALA2009011200127Bleed Valve · failedAPU BLEED FAULT. RTFL. REPLACED NR1 ENG HP BLEED VALVE. ALL CKS NORMAL AFTER HP VALVE REPLACEMENT.SDR UALA2009010900097Director · faultyEMERGENCY EXIT LIGHTS AND NO SMOKING-FASTEN SEAT BELT SIGN LIGHTS THROUGHOUT CABIN WILL NOT EXTINGUISH. EMERG EXIT LIGHTS WILL NOT EXTINGUISH. TROUBLESHOT TO A CIDS DIRECTOR. REPLACED THE CIDS DIRECTOR.SDR UALA2009010900087Slide · faultyEMERG LIGHT CK MESSAGE EXT LOADS FWD LT SLIDE LIGHTS INOP. REPLACED DOOR 1L SLIDE. EMERGENCY LIGHT CHECK PASSED.SDR UALA2009010500042Structure · damagedCOVERED RAMP TUG STRUCK ACFT LT SIDE, FWD OF LT WING BODY TO WING FAIRING, LR EDGE, 7IN GASH. ACCOMPLISHED FLUSH REPAIR.SDR UALA2009010500060Smoke Detector · damagedAFT PIT SMOKE DETECTOR DAMAGED. R&R FWD DETECTOR.SDR UALA2008123007049Stringer · damagedSTRINGER 38 LT BETWEEN FRAMES 32 & 31 HAS IMPACT DAMAGE. MFG NEW CLEAT. HFEC REVEALED NO CRACKS AT THIS TIME. ACCOMPLISHED STRINGER REPAIRS TO 37L AND 38L.SDR UALA2008122907034Smoke Detector · false activationAVIONICS MSG RCV'D. SUSPECT HUMIDITY SET OFF THE ALARM. MSG WAS NOT PRESENT WHEN MECH ARRIVED. PERFORMED AEVC TEST AND SDCU TEST AND TESTED OK. CHECKED AVIONICS BAYS FOR SMOKE AND NONE FOUND. NO BURNING ODOR EITHER.SDR UALA2008123007051Skin · dentedDOOR 2L HAS DENT 16.0" AFT OF FWD EDGE AND 13.5" FROM BOTTOM. EVALUATED DENT & FOUND OUT OF LIMITS. CUT OUT DAMAGE. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR. RESTORED THE PROTECTIVE COATING.SDR UALA2008122407000Slide · low pressureTHE 1L SLIDE PRESSURE LOW. COLD SOAKED DOOR WAS OPEN FOR OVER 1 HR. OP PER MM 25-62-00 PG 603 (NOTE A).SDR UALA2008122607006Fire Warning · malfunctionedFIRE LOOP-B FAULT DISPLAYED ON UPPER ECAM SCREEN - ENG 2. CREW COMMENTS: ECAM APPEARS INTERMITTENTLY PERFORMED CFDS BITE CK OF FDU. TEST OK. PERFORMED FIRE TEST. TESTS OK. NO MESSAGES.SDR UALA2008122406984Wire · brokenSEAT MOUNTED EMERGENCY LIGHTS AT ROW 10 AND 11 LEFT HAVE BROKEN WIRES. LIGHTS ARE OVERWING EXIT-NOT DEFERRABLE. REPLACED UNDER SEAT CABLE P/N 565-2099 ON BOTH ROWS REF IPC 33-51-09, ALL EMERGENCY LIGHTS ALL ROWS OPS NORMAL.SDR UALA2008122406985Light · inoperativeSEAT 18 EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT ON SEAT ROW END CAP AT POSITION 18C, OPS NORMAL.SDR UALA2008122406991Support · corrodedR2 DOOR SILL HAS CORROSION AT AFT GIRT SUPPORT BLOCK. MAJOR REPAIR. INSTALLED REPAIR ANGLE.SDR UALA2008122406992Sill · corrodedL2 DOOR SILL HAS CORROSION AT AFT GIRT FITTING. MAJOR REPAIR. INSTALLED ANGLE REPAIR.SDR UALA2008122206955Battery · faultyEPSU BATTERY EMERGENCY RIGHT FAULT DISPLAYED AFTER EMERGENCY LIGHT TEST. REPLACED BATTERY.SDR UALA2008121206861Power Supply · failedFWD LT ESPU FAILED TEST. REPLACED FWD LT EPSU. OPS CHECK NORMAL.SDR UALA2008120906801Wire · pinchedBOTH OVERWING EXIT LIGHTS WILL NOT ILLUMINATE AND RT EPSU FAILED BITE TEST. FOUND EMERGENCY LIGHT WIRE PINCH UNDER SEAT TRACK ROW 10 LEFT. REMOVED WIRE AND REPAIRED DAMAGE WIRE, OPERATIONAL CHECKS OF LEFT AND RIGHT OVERWING LIGHTS CHECKS OK, ALSO NO FURTHER SDR UALA2008120906802Beam · corrodedBEAM 200 HAS SEVERAL PLACES CORRODED. MAJOR REPAIR ACCOMPLISHED. CONNECTED NEW BEAM 200 TO NEW BEAM 205. INSTALLED BEAM 200 IN ACFT.SDR UALA2008120906800Slide · disconnectedFWD RT CABIN DOOR SLIDE PACK ASSY CONNECTOR BETWEEN CABLE LOOP ASSY AND COVER RELEASE CABLE WAS FOUND DISCONNECTED. SLIDE REPLACED DUE TO CRACKED MOUNTING LUG.SDR UALA2008121006837Plate · corrodedONE EA FLOORBOARD CONNECTOR PLATE CORRODED AT FRAME 68. MAJOR REPAIR ACCOMPLISHED. REPLACED PLATE AT FRAME 68.SDR UALA2008121006838Beam · corrodedBEAM 205 HAS 1EA HOLE CORRODED. MAJOR REPAIR ACCOMPLISHED. CONNECTED NEW BEAM 205 TO NEW BEAM 200 AND INSTALLED GALLEY HOLD DOWN NUTS IN RETAINERS. INSTALLED BEAM 205.SDR UALA2008120906796Connector · disconnectedAFT RT CABIN DOOR SLIDE ASSY CONNECTOR BETWEEN CABLE LOOP ASSY AND COVER RELEASE CABLE WAS FOUND DISCONNECTED. CABLE LOOP ASSY AND COVER RELEASE CABLE CONNECTED.SDR UALA2008120906799Connector · disconnectedLT AFT CABIN DOOR SLIDE CONNECTOR BETWEEN CABLE LOOP ASSY AND COVER RELEASE CABLE WAS FOUND DISCONNECTED. CABLE LOOP ASSY & COVER RELEASE CABLE CONNECTED.SDR UALA2008120806770Fan Blade · damagedBIRD INJESTION NR 2 ENGINE. RTFL. CREW REPORTS 4EA FAN BLADES FOUND DAMAGED UPON ARRIVAL. INSPECTION COMPLETED, BLADES REPLACED.SDR UALA2008120806788Oxygen Mask · no testF/O O2 MASK WILL NOT TEST. REMOVED & REPLACED FIRST OFFICER'S O2 MASK STOWAGE BOX. LEAK CHECKED O2 LINE. LEAK CHECK OKAY. CREW O2 BOTTLE VALVE OPEN & SAFETIED MASK AND BOX. OPS CHECK OKAY.SDR UALA2008120806778Shear Plate · corrodedAFT RT SIDE TRIANGULAR SHEAR PLATE HAS CORROSION AT FASTENER HOLES. REMOVED 4EA LOCK FASTENERS AT SHEAR PLATE AND BEAM 205. REMOVED PLATE, DRILLED NEW PLATE, NEEDS INSTALL. INSTALLED 5 EA LOCK AND BLIND FASTENERS. COMPLETED INSTALLATION OF FRAME AND SHEAR SDR UALA2008120506768Proximity Sensor · dirtyL-G SYS DISAGREE ECAM. RTFL. RECURRED ON NEXT FLT OUT. PROX SENSOR S24GA AND 25GA, DIRTY. CLEANED -OK.SDR UALA2008120406755Frame · corrodedAFT TRIANGLE SHEAR PLATE ATTACH FRAME TO FUSELAGE CORRODED. REMOVED FRAME, DRILLED NEW FRAME NEEDS INSTALL. FRAME AND PLATE REPLACED COMPLETE. INSPECTED INSTALLATION AFT RT TRIANGLE TO FUSELAGE SHEAR PLATE SUPPORT FRAME.SDR UALA2008120306737Sill · corrodedDOOR 2R SILL PLATE HAS CORROSION IN SEVERAL PLACES. REMOVED SILL PLATE. REPLACED DOOR 2R SILL.SDR UALA2008120306738Floorbeam · corrodedBEAM 165 HAS 2EA HOLE CORRODED. REMOVED BEAM 165 AND TRANSFERRED BRACKETS TO NEW BEAM. JOINED BEAM BS 200 TO 165. INSTALLED BEAM 165 IN ACFT.SDR UALA2008120306734Beam · damagedBEAM 210 NEEDS REPLACED. STARTED REMOVAL OF BEAM. INSTALLED NEW BEAM.SDR UALA2008120306736Beam · corrodedBEAM 95 HAS CORROSION. INSTALLED NEW BEAM.SDR UALA2008120106689Fcu · faultyAUTOPILOT ISSUES. FLIGHT DIVERTED. AUTO FLT 'FCU 1+2 FAULT' DISPLAYED ON UPPER ECAM SCREEN. CYCLED CB B5 AND M21 AND FCU CHANNEL 1 RECOVERED BUT FCU CHANNEL 2 REMAINED INOP. REPLACED FCU.SDR UALA2008120106683Skin · damagedAFT LOWER FUSELAGE FR70 TO FR72 HAS TAIL STRIKE DAMAGE TO EXTERNAL SKIN BETWEEN STR 42R TO STR 41L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED & INSTALLED EXTERNAL DOUBLER.SDR UALA2008120106685Shear Plate · crackedSHEAR PLATE AFT OF DOOR 2R LOCATED BETWEEN FRAMES 68 AND 69 CRACKED. REPLACED TRAY.
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