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 UALA2010111504203Oven · contaminatedFWD GALLEY OVEN INOP. CREW REPORTED SMOKE COMING FROM THE FWD OVEN. CB'S WERE PULLED AND THE SMOKE DISSIPATED. PER FLT ATTENDANT SMOKE CAME FROM INSIDE THE OVEN. CB'S WERE PULLED AND THE SMOKE DISSIPATED. PER FLT ATTENDANT SMOKE CAME FROM INSIDE THE OVEN. SDR UALA2010111504205Light · odorCAPTS MAP LIGHT EMITTED ELECTRICAL SMOKE ODOR BEFORE BURNING OUT. CHECKED CB Z5: NOT TRIPPED (ASM 33 -12-00), PERFORMED GENERAL VISUAL INSPECTION OF MAP LIGHT, NO HAZARDS EVIDENT. REPLACED LIGHT ASSY, CHECKS OK NOW.SDR UALA2010111204195Fire Loop · faultyFOUND FIRE LOOP IN LEFT WHEEL WELL MAKING CONTACT WITH SHIELDING AND BURNED. REPLACED SECTION OF APU BLEED AIR DUCTING IN LEFT WHEEL WELL.SDR UALA2010111004179Flap Track · dentedDENT IN RT OB FLAP TRAILING EDGE. APPROX 1. 5 FT IB OF OB FLAP TRACK FIRING. MEASURES APPROX 1.5IN BY 2IN. .0 85 IN. IN DEPTH. REPAIRED PER GNMM 1-0-1-24.SDR UALA2010110904160Grounding Strap · looseELECTRIC SHOCK FELT IN GALLEY WHEN ELEC PWR IS TRANSFERRED. ENTIRE GALLEY HAS BEEN HAS BEEN ELECTRICALLY DEACTIVATED. NO SHOCK NOTICED WHEN TRANSFERRING POWER. NEED TO CHECK THE GALLEY ELECTRICAL BONDING AND GROUNDING. FOUND POOR ELECTRICAL BONDING BETWEEN GSDR UALA2010110904162Lamp · failedEMERGENCY LIGHT TEST FAILS EXT LOADS EMER R. RELAMPED, OP CHECKED GOOD.SDR UALA2010110904168Actuator · seizedFLAPS JAMMED ON EXTENSION TO FULL. WORKED NORMAL AFTER CYCLING. FOUND TORQUE LIMITER ON LT WING NR 1 FLAP ROTARY ACTUATOR. RESET LIMITER, DID NOT TRIP AFTER FLAP TEST. CALLS OUT TO REPLACE NR 1 ROTARY ACTUATOR AS A PRECAUTION. REPLACED LEFT WING NR 1 ROTASDR UALA2010110304086Windshield · faultyLEFT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. ANTI ICE. WINDSHIELD FOUND FAULTY. WINDSHIELD REPLACED. OKAY FOR SERVICE.SDR UALA2010110104063Battery Pack · dischargedACCOMPLISHED CIDS TEST RT EMERGENCY POWER SUPPLY UNIT BATTERY FAILED. REPLACED BATTERY WITH NEW CHARGED BATTERY. OPS CHECK GOOD CIDS TEST PASSED.SDR UALA2010110304084Cover · damagedAFT F/A STATION EMERGENCY LIGHT SWITCH COVER DAMAGED. APPLIED INTERIM REPAIR TO LIGHT SWITCH COVER. SWITCH AND COVER STILL USEABLE.SDR UALA2010110304072Oxygen Mask · unwanted deployONE OXYGEN MASK DEPLOYED IN COACH. ROW 12ABC IS THE LOCATION. STOWED MASK. SEATS DEFERRED REF MEL 3521A. O2 DOOR HAD TO BE INTERIM REPAIRED CLOSED WITH APPROVED TAPE. ADJUSTED DOOR LATCH ASSY, FOUND LOOSE AND SHIFTED. SECURED LATCH ASSY. REPACKED MASKS AND CLSDR UALA2010110304087Actuator · malfunctionedROW 10 LEFT SIDE SEATS SEEM TO ENCROACH INTO EMERGENCY EXIT DOOR PATH. SEAT 10A RECLINES INTO THE OVERWING HATCH AREA. ADJUSTED HYDROULOCK ON RECLINE ACTUATOR. SEAT 10A DOES NOT RECLINE INTO EMERGENCY EXIT DOOR HATCH AREA.SDR UALA2010110104042Coffeemaker · odorBURNED PLASTIC ODOR EMANATING FROM COFFEE POTS IN REAR GALLEY. M41 OR M42. DEACTIVATED BOTH AFT GALLEY COFFEEMAKERS (PRECAUTIONARY). REPLACED BOTH COFFEEMAKERS M-41 & M-42. RESET C-B'S & CHECKED AFT GALLEY CONDITION. ALL CHECKS GOOD.SDR UALA2010110204067Skin · dentedRIGHT NR 2 SLAT HAS DENT. BEGAN REMOVING SLAT PER MM. DURING SLAT OPS CHECK, HAD NR 2 SFCC FAULT ONE CAM, COULD NOT RESET, SWAPPED MSG FOLLOWED, BACK TO ORIGINAL POS. REPLACED NR 2 SFCC REF AMM, GDN TEST PASSED, CAT III TEST WILL BE ON SMC13. LARGE DENT IN LE SDR UALA2010110104031Oxygen Mask · failedPILOT'S SIDE O2 MASKS NEED TO BE REINSTALLED. REPLACED MASK ON ACCOUNT IT WAS FAILING TEST.SDR UALA2010110104033Skin · gougedAFT ENTRY DOOR (L2) EXTERIOR SKIN LOWER SECTION AT MID-SPAN GOUGED. MAJOR REPAIR ACCOMPLISHED: EVALUATED DAMAGE FOR CRACK. DENT OUT OF LIMITS. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR.SDR UALA2010110104034Regulator · leakingCREW O2 LOW, (1200). REPLACED OXYGEN PRESSURE REGULATOR & TRANSMITTER. REPLACED DUE TO OXYGEN LEAKING.SDR UALA2010110104023Eec · faultyFADEC OVHT, FLIGHT DIVERTED. NEED TO EXAMINE HCU IAW MM FOR HEAT DAMAGE, CHECK UNDER FAN COWLS, STARTER DUCT, ANTI ICE DUCT, PB LINE FOR LEAKS, EEC MR73411 (PCN 482-9555) MUST BE REPLACED IAW AMM. CKD FOR PNEUMATIC LEAKS IN FAN COWL AREA. NONE FOUND. ALL DUCTSDR UALA2010110104030Transmitter · leakingCREW O2 STILL LEAKING. LOST 60PSI IN 50 MINUTES OF FLIGHT. REPLACED 02 PRESSURE REGULATOR TRANSMITTER, LEAK CKD, NO LEAKS FOUND.SDR UALA2010110104048Bearing · migratedLEFT INBD FLAP CARRIAGE SPHERICAL BUSHING IS MIGRATING OUT OF FITTING. REMOVED ECCENTRIC BUSHING & HARDWEAR. LT NR 1 FLAP TRACK CARRIAGE AFT END STOP PLATE REMOVED. STARTED REMOVING FLAP TRACK ATTACH BOLTS. COMPLETED REMOVAL AND REPLACEMENT OF BEARING.SDR UALA2010110104026Stringer · corrodedCORROSION IN AFT PIT FR 56-57 AT STRINGER 42L. MAJOR REPAIR ACCOMPLISHED: CUT OUT CORRODED STRINGER SECTION. FABRICATED & INSTALLED STRINGER SPLICE REPAIR.SDR UALA2010110104027Stringer · corrodedCORROSION ON STRINGER 30R AT FRAME 65 OUTFLOW VALVE. MAJOR REPAIR ACCOMPLISHED: CORRECT STRINGER LOCATION IS 31R. REMOVED CORRODED STRINGER & FABRICATED & INSTALLED STRINGER SPLICE REPAIR.SDR UALA2010110104028Skin · dentedEXISTING FUSELAGE SKIN REPAIR IS DENTED AT FR23 AND STR 23L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED EXISTING REPAIR & FABRICATED & INSTALLED NEW EXTERNAL DOUBLER REPAIR.SDR UALA2010110104029Oxygen Mask · leakingOXYGEN PRESSURE STILL SLOWLY DECREASING. FOUND O2 MASK LEAKING AT QUICK DISCONNECT FITTING IN 1ST OBSERVER POSITION. REPLACED MASK OPS AND LEAK CHECKED GOOD.SDR UALA2010110104046Feeder Cable · faultyENG 2 GEN FEED CONNECTOR 4000VC PIN AND SOCKET PHASE B 8R002 Y00 BURNED. REMOVED NR2 ENG IDG HARNESS FROM PYLON DISCONNECT DOWN TO IDG. REPLACED BOTH CABLES.SDR UALA2010102803981Oxygen Mask · unwanted deployOXY MASKS DEPLOYED FROM OVERHEAD. REQUIRES DROP TEST BEFORE SEATS CAN BE OCCUPIED. RESET O-2 DOOR. PERFORMED OPS CK IAW AMM. OPS CHECKED GOOD.SDR UALA2010102803983Unknown · odorAVIONICS SMOKE ECAM, RTFL. REVIEWED CFDS: NO FAULT MESSAGES. PERFORMED AEVC TEST: NO FAILURES. SDCU TEST HAS NO FAULTS. INSPECTED - SNIFFED E & E AREA: NO EVIDENCE OF SMOKE. VENT EXHAUST FAN HAS NO SMOKE ODOR. --WET WOOD BOXES IN FWD CARGO HAVE A WOODEN ODOR,SDR UALA2010102803982Unknown · odorFAS REPORTED SLIGHT BURNING ELECTRICAL ODOR THAT LASTED FOR 5 MINS AND DISSIPATED. BURNING ODOR WENT AWAY WHEN F/A'S TURNED OFF GALLEY & CHILLERS. OPERATED AFT GALLEY EQUIPMENT AND CHECKED POST FLT REPORT FOR CIDS SYS FAULTS. RAN ALL AFT GALLEY EQUIPMENT: COUSDR UALA2010102803995Wire Harness · brokenLAST 3 ROWS HAVE EMERGENCY ESCAPE LIGHT FAULTS. ISOLATED FAULT TO EPSU PACK 11WL. CIDS RESET AND CONNECTOR PLUG REMOVAL, NO HELP-INTERNAL FAULT. FLOOR PATH MARKING LIGHTS ARE INOP. REPLACE EPSU 11WL (LEFT OVERWING EMERGENCY EXIT). SLAVED IN NEW EPSU AT 11WLSDR UALA2010102803996Window · delaminatedF/O RT REAR WINDOW DELAMINATED ON LWR EDG-APPEARS MILKY LIKE AN ELEC ARC MARK. REPLACED F/O RT REAR WINDOW.SDR UALA2010102803997Oxygen Mask · unwanted deployO2 MASKS DROPPED AT ROW 16A. REINSTALLED DROPPED MASK. OPS CHECKS GOOD.SDR UALA2010102803979Oxygen System · unwanted deployCREW REPORTS O2 MASKS AT 7ABC DROPPED ON LANDING. DEFERRED. DOOR WILL NOT STAY LATCHED CLOSED. NEEDS NEW O2 BOX ASSY. SEATS 7ABC ARE PLACARDED, DO NOT OCCUPY. CONTAINER, FOAM PAD, 4EA MASK ON ORDER 2 LASMM (SEE STATION STA SH PAGE). IF O2 GENERATOR NEEDED, UNSDR USAA2010102692408Fire · detectedFLT 498 - DEN - POSSIBLE FIRE / TORCHING NEAR NUMBER 2 ENGINE REPORTED BY PASSENGER. CREW REPORTED ALL ENGINE PARAMETERS WERE NORMAL. MAINTENANCE INSPECTED AND PERFORMED ENGINE RUN WITH NO FAULTS OR LEAKS FOUND.SDR UALA2010102503956Cap · crackedRT FORESTAY UPPER BEARING CAP ASSY CRACKED IN LOWER AFT CORNER. REPLACED RT FORESTAY UPPER BEARING CAP ASSY.SDR UALA2010102503957Cap · crackedLEFT UPPER FORESTAY BEARING CAP IS CRACKED IN UPPER AFT CORNER. REPLACED LT UPPER FORESTAY BEARING CAP ASSY.SDR UALA2010102503943Bolt · shearedCABIN FLOOR EXPANSION JOINT C-46, RT BOLT IS SHEARED. ALL 6 BOLTS REPLACED AND AREA INSPECTED IAW MM.SDR UALA2010101903872Duct · damagedALIGNMENT PIN IS BROKEN ON THE DUCT AT THE INBOARD CONNECTION FOR THE RT WING ANTI ICE VALVE. DUCT FOUND OUT OF TOLERANCE. REPLACED RT WING ANTI ICE VALVE DUCT. ALL OKAY.SDR UALA2010101903869Hook · out of adjustDOOR 2 RT - INTERIOR HANDLE CAN BE MOVED TO THE CLOSED POSITION WITH DOOR STILL OPEN. SUSPECT HANDLE INTERLOCK MECHANISM NOT FUNCTIONING AS DESIGNED. REMOVED UPPER DOOR LINING. FOUND THE HOOKS HAVE SLIPPED ON THEIR ADJUSTMENT SERRATIONS. (THEY ARE MOUNTED OSDR UALA2010101803852Wire Harness · openFOUND NR1 SLIDING WINDOW SENSORS OUT OF TOLERANCE. ACCOMPLISHED T-S PER TSM 30-42-00-810-809. SLAVED IN WHC-1 NO HELP, OHMED OUT SENSOR PRIMARY GOOD SPARE DOES NOT BUT NOT IN CIRCUIT SUSPECT WINDOW OR HARNESS PCN 565-2286 IPC 56-12-01-02J. LOB WIRE HARNESS ANSDR UALA2010101903863Liner · crackedNR 2 ENGINE INLET ATTRITION LINER HAS A 3 INCH CRACK AT 6:00 POSITION. MEASURED AND FOUND DAMAGE ATTRITION LINER LOWER OB PANEL TOTAL DAMAGE IS 26.81%. STARTED ATTRITION LINER REPAIR PER MT 72-017. DAMAGE REMOVED AND INSTALLED FILLER MATERIAL AT 14:00. NEEDS SDR UALA2010101803847Light · malfunctionedFOUND OVERHEAD PANEL CB H-7 POPPED, RESET & CB POPPED AGAIN, IT'S EMERGENCY LIGHT BREAKER. REPLACED DOME AND AUX LIGHT ASSY AT LAV 'A', OPS CHECKED OK.SDR UALA2010101803848Controller · damagedANTI-ICE L WINDSHIELD ECAM, FLT DIVERTED. STARTED REMOVAL OF CAPTAIN'S WINDOW. RMV'D INNER TRIM AND UPPER AND LOWER OUTER FRAME, CENTER FRAME STILL SEALED TO AIRCRAFT AND 2 BOLTS SEALED IN. REPLACED CAPTAIN'S WINDSHIELD. LAST LEG REPORT SHOWED LT WINDSHIELDSDR UALA2010101403817Valve · leakingCREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. PSI-1480, 100 PSI LOSS IN 4 HRS. CHECKED CREW O2 FOR LEAKS AND FOUND CAPT BOX TEST RESET VALVE LEAKING. REPLACED CAPT O2 BOX. OP CHECKED AND LEAK CHECKED GOOD.SDR UALA2010101403813Lamp · inoperativeCABIN EMERGENCY LIGHT CHECK IAW NR 3 SERVICE CHECK FAILS. (EXT LOADS EMER R). FOUND RT OVERWING LIGHT POWER SUPPLY 12WL SHOWING EXT FAULT AT ROW 11DEF. RELAMPED RT OVERWING AFT SLIDE LIGHT ASSY. 12WL BITE TEST OK, EMERGENCY LIGHT CK REF 3SVC, OP CKS OK.SDR UALA2010101203797Switch · faultyEMERGENCY LIGHTS TEST FAILS "EPSU UNIT FWD L". REPLACED EPSU AND GOT SAME RESULT, REPLACED BATTERY, NO HELP. REINSTALLED ORG UNITS. IAW TSM BEGAN TO SEARCH FOR SHORTED LIGHTS. FOUND SEAT ROWS 1AB-8ABC ESCAPE PATH LIGHTS INOP. THE EMERG LIGHTS TEST HAS SHOWN RSDR UALA2010101403819Power Supply · out of tolerancePOWER SUPPLY 11WL USED FOR TROUBLESHOOTING. REPLACED EMERGENCY LIGHT POWER SUPPLY 11WL. OP CKS OK.SDR UALA2010101403820Connector · disconnectedEMERGENCY LIGHT CONNECTOR DISCONNECTED AT SIDEWALL NEAR SEAT 7A FOR TROUBLESHOOTING. SECURED CONNECTOR AT SEAT 7A.SDR UALA2010101203799Computer · faultyTRIM AT FL 310 300K IS ROLL 1.4 RWD REPLACED ELAC 1 AND OP CK GOOD. REPLACED FAC 1, OP CHECKED GOOD.SDR UALA2010101203800Floorboard · delaminatedAT ROW 18 THE CABIN FLOOR IS SPONGY AND HAS A DIP IN IT. REMOVED FLOORBOARD 251FF ROW 16 THRU 19. BOARD REPORTED SPONGY AT ROW 18. FOUND FLOORBOARD DELAMINATED. REPLACED FLOORBOARD. FOUND FLOORBOARD SUPPORT BRACKET BROKEN ROW 18. REPLACED SUPPORT BRACKET.SDR UALA2010101103788Mount · crackedFOUND DOOR OPENING HANDLE MOUNT CRACKED LETTING HANDLE INTERFERE WITH AND DAMAGING EXTERIOR SKIN PANEL UPON OPENING DOOR. BRACKET PLATE BROKEN, WILL NEED REMOVAL OF ENTIRE DOOR MECHANISM (HANDLE MECH) TO INSPECT FOR FURTHER DAMAGE. DOOR SKIN PANEL INSIDE AFT P
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