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 2000UALA00465Display · failedELECTRIC BURNING SMELL IN COCKPIT. *S/D* THE CONTROL DISPLAY UNIT (CDU) WAS REPLACED WITH NO EVIDENCE OF CONTINUED BURNING ODOR IN AFFECTED AREA. THE REMOVED CDU WAS INSPECTED AND TESTED WHICH IDENTIFIED A LOOSE LOCKING INSIDE THE CHASSIS ASSEMBLY, BUT NO SDR 2000UALA00434Power Supply · failedEMERGENCY LIGHTS FAIL TEST FROM PROGRAMMING AND TEST PANEL (PTP). REPLACED RIGHT EMERGENCY POWER SUPPLY.SDR 2000UALA00440Light · inoperativeEMERGENCY ESCAPE LIGHTS AT ROWS 15, 16, 17, 21, 22, 23 NOT OPERATING DURING EMERGENCY LIGHT TEST.SDR 2000UALA00394A/C Pack · cloggedCOULD NOT CONTROL CABIN AND COCKPIT TEMPERATURE. *S/D* REPLACED NR 1 PACK REHEATER. OPERATIONAL AND LEAK CHECK NORMAL.SDR 2000UALA00395Bottle · dischargedAFT MAIN ENTRY DOOR ASSIST BOTTLE INDICATES LOW PRESSURE.SDR 2000UALA00386Light · inoperativeESCAPE PATH SEAT LIGHTING AT 8C LAMP INOPERATIVE. RELAMPED.SDR 2000UALA00379Lever · restrictedLANDING GEAR LEVER HARD TO RAISE. *S/D* REPLACED LANDING GEAR LEVER ASSEMBLY. PERFORMED FUNCTIONAL TEST INCLUDING EXTENSION AND RETRACTION OF MAIN LANDING GEAR AND NOSE LANDING GEAR. PERFORMED CENTRALIZED FAULT DISPLAY SYSTEM LANDING GEAR CONTROL INTERFACESDR 2000UALA00368Warning System · activatedABORTED TAKEOFF AT 100 KNOTS DUE TO FLIGHT MANAGEMENT SYSTEM AND POSITION DISAGREEMENT MESSAGE ON ELECTRONIC CENTRALIZED AIRCRAFT MONITORING SYSTEM. *S/D* NO ACTION TAKEN BY MAINTENANCE. THIS IS A KNOWN ANOMALY AND CREW INSTRUCTIONS FOR HANDLING THIS POSITISDR 2000UALA00400Slide · tornSLIDE/RAFT MR25612-032, MANUFACTURERS PART NUMBER D30665-105, SERIAL NUMBER A5824, MANUFACTURE DATE 12/93, DEVELOPED A SEAM TEAR OF OVER 3 FEET IN LENGTH. THE TEAR WAS IN THE LOWER TUBE ON THE MID SPAN CROSSOVER TUBE RIGHT HAND SIDE. THIS TEAR HAPPENED DURINSDR 2000UALA00364Acm · leakingUNABLE TO COOL THE CABIN. *S/D* THE AIR CYCLE MACHINE AND VARIOUS PACK BLEED DUCT SEALS WERE LEAKING CAUSING POOR PERFORMANCE OF THE LEFT HAND AIR CONDITIONING PACK. THE AIR CYCLE MACHINE (10HM1) WAS CHANGED ALONG WITH THE FLOW CONTROL VALVE (11HB).SDR 2000UALA00357Warning System · activatedFLIGHT CONTROL CLASS II MAINTENANCE MESSAGE DISPLAYED ON LOWER ELECTRONIC CENTRALIZED AIRCRAFT MONITORING UNIT. *S/D* ALIGNED AIR DATA INERTIAL REFERENCE UNITS (ADIRU). NO MESSAGE WAS THEN SHOWN.SDR 2000UALA00351Unknown · odorCREW REPORTED PASSENGERS COMPLAINED OF BURNING SMELL IN CABIN. *S/D* MAINTENANCE INVESTIGATED AND COULD NOT ISOLATE BURNING SMELL IN ROWS 10-13. NO FURTHER OCCURRENCES WERE NOTED. NO COMPONENTS WERE REPLACED.SDR 2000UALA00339Blade · failedNR 2 ENGINE FAILED IN FLIGHT. MAX EXHAUST GAS TEMPERATURE EXCEEDED. *S/D* THE IFSD WAS CAUSED BY A FAILURE OF A HIGH PRESSURE COMPRESSOR (HPC) 4TH STAGE (C4) BLADE. THE ROOT CAUSE OF THE BLADE FAILURE WAS HIGHER-THAN-NORMAL HIGH CYCLE FATIGUE STRESS CAUSEDSDR 2000UALA00310Switch · failedAFTER PUSH, BEFORE TAXI, GOT ECAM HYDRAULIC GREEN SYSTEM LOW PRESSURE. SYSTEM PRESSURE SHOWS 3000 PSI. QUANITITY NORMAL. NOSEWHEEL STEERING INOPERATIVE. *S/D* REPLACED GREEN SYSTEM FLIGHT CONTROL PRESSURE SWITCH, ITEM 1151GN.SDR 2000UALA00311Control Box · malfunctionedELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE DISPLAYED FOR SMOKE IN LAVATORY AND CARGO DETECTION FAULT. *S/D* REPLACED SMOKE DETECTION CONTROL UNIT REFERENCING MAINTENANCE MANUAL 26-17-34-000-001 AND MAINTENANCE MANUAL 26-17-34-400-001. OPERATIONAL TESDR 2000UALA00301Outflow Valve · fluctuatesPASSING THROUGH 18,000 FEET, LARGE FLUCTUATIONS IN CABIN VERTICAL SPEED (SYS 1). *S/D* REPLACED OUTFLOW VALVE AND BOTH PRESSURE CONTROLLERS.SDR 2000UALA00303Fan · failedSTRONG ODOR THROUGHOUT CABIN IN DESCENT THRU 4000 FT. *S/D* FOUND AVIONICS BLOWER 20HQ TO BE MAKING EXCESSIVE NOISE. REMOVED AND REPLACED FAN. OPERATIONAL CHECK GOOD.SDR 2000UALA00290Switch · leakingCREW REPORTS A LOSS OF ALL GREEN HYDRAULIC FLUID. *S/D* FOUND HYDRAULIC PRESSURE SWITCH LEAKING. REMOVED AND REPLACED SWITCH.SDR 2000UALA00291Heater · failedCREW REPORTS SMOKE DETECTOR ALARM SOUNDING CONTINUOUSLY WITH NO ELECTRONIC CENTRALIZED AIRCRAFT MONITORING SMOKE WARNING. *S/D* REPLACED HOT WATER HEATER.SDR 2000UALA00293Connector · dirtyCREW REPORTS WEATHER RADAR WILL NOT PAINT VISIBLE PRECIPITATION. *S/D* FOUND A FAULT ON THE RADAR RT UNIT. PULLED UNIT AND FOUND DUST ON RACK CONNECTOR. CLEANED RACK CONNECTOR AND THEN REINSTALLED UNIT. PERFORMED GROUND OPERATIONAL CHECK AND VERIFIED SYSTSDR 2000UALA00286Idg · failedAT 80 KNOTS ON T/O ROLL ECAM IDG2 LO OIL PRESS. ABORTED THE TAKEOFF PRIOR TO 100 KTS AND COMPLETED ECAM PROCEDURE DISCONNECTING IDG. *S/D* REMOVED AND REPLACED ENGINE 2 INTEGRATED DRIVE GENERATOR PER AMM 24-21-51-401.SDR 2000UALA00275Unknown · odorSTRONG SULFUR ODOR IN CABIN, SOME PASSENGER NAUSEA. UNABLE TO FIND OUT THROUGH FF WHAT IS ACTUALLY ON AIRCRAFT. NO HAZMAT LISTED IN DCLR/DPWM. HOWEVER, CAPTAIN HAS HAZMAT FORM FOR DRY ICE TO CHILL MEDICAL SPECIMENS. ODOR SUBSIDING ON RETURN TO LAX WITH CABISDR 2000UALA00266Tube · will not testAFT DOOR SLIDE/RAFT LOWER TUBE FAILED PROOF PRESSURE TEST. *S/D* FOUND THE LOWER TUBE TO HAVE A SEAM FAILURE AT THE TOP END CROSSOVER TUBE. SENT UNIT TO VENDOR FOR REPAIR.SDR 2000UALA00264Indicator · malfunctionedERRONEOUS AIRSPEED INDICATIONS ON APPROACH. AT 1500 AGL CAPT AS INDICATED 180 STBY INDICATED 180 KTS F/O INDICATED 170 KTS. AT 500 FT AGL CAPT IND 158 KTS STBY 160 KTS F/O 140 KTS. AT 100 FT AGL CAPT 140 KTS STBY 140 KTS F/O 118 KTS. *S/D* RESET SYSTEM. SDR 2000UALA00257Door · leakingACFT EN ROUTE TO ORD, ECAM FWD CARGO DOOR, PRESSURIZATION FLUX. PATCH WITH SAM. FLT CONTINUED TO ORD AT 10 THOUSAND FT.SDR 2000UALA00250Power Supply · inoperativeEMERGENCY LIGHT TEST FAULT (BAT AFT LT) 33-51-38. *S/D* REPLACED POWER SUPPLY UNIT AND BATTERY IN AFT LEFT POSITION.SDR 2000UALA00239Skin · damagedTAIL OF AIRCRAFT STRUCK UPON FLARE AND LANDING AT SNA. SIX FOOT LONG SCRAPE ON BOTTOM OF AIRCRAFT FUSELAGE WITH NUMEROUS BREAKS IN SKIN LOCATED IN AREA AFT OF DRAIN MAST. *S/D* EXCESSIVE FLARE DURING LANDING. ISSUED EVA MOC1-8111 TO INSTALL TEMPORARY REPAISDR 2000UALA00232Selector Valve · leakingYELLOW SYSTEM LO QTY IN FLIGHT. TURNED OFF PUMP PER ECAM. *S/D* FOUND LEAK AT AUTO BRAKE SELECTOR. REPLACED PACKING. SERVICED YELLOW SYSTEM TO FULL.SDR 2000UALA00225Power Supply · failedEMERGENCY LIGHT TEST FAULT, EPSU COMM AFT L 33-51-38. *S/D* REPLACED AFT LEFT EMERGENCY POWER SUPPLY UNIT (P/N 3214-54-10), (S/N 1576).SDR 2000UALA00207Outflow Valve · malfunctionedCABIN PRESSURE SYSTEM ONE AUTO MODE FAILED AT FL180. CABIN VERTICAL SPEED PEGGED AT 1000 FPM UP. CABIN PRESS AT 2500 FT. MANUAL MODE WORKED OK. *S/D* REPLACED OUTFLOW VALVE (FIN 10HL, MR21301).SDR 2000UALA00140Power Supply · failedEMERGENCY EXIT LIGHTS FAIL TEST WITH MESSAGE EPSU COM AFT. *S/D* REPLACED POWER SUPPLY PCN 565-0038.SDR 2000UALA00156Power Supply · failedEMERGENCY LIGHT POWER SUPPLYS AT DOOR 1L AND OVERWING FAIL SELF TEST. *S/D* REPLACED POWER SUPPLIES AT DOOR 1L AND LEFT OVERWING POSITIONS.SDR 2000UALA00193Switch · looseCREW REPORTED LOW QUANTITY WITH GREEN HYDRAULIC SYSTEM. CREW, SAMC, DISPATCH AGREED TO DIVERT TO ORD. AMBER ALERT DECLARED, EQUIPMENT REQUESTED TO MEET AIRCRAFT IN ORD. *S/D* FOUND NR 1 ENGINE HYDRAULIC PRESSURE SWITCH BACKED OUT AND THE O-RING DISPLACED. SDR AWXA0000244Engine · vibrationNR 2 ENGINE VIBRATION WAS 5.3 ON T/O. PERFORMED FAN TRIM BALANCE IAW CARD F5M71303 AND GROUND CARD F5M71306. VIBRATION LEVELS LESS THAN 1 UNIT. CURRENT HISTORY: A/C HAD VIBRATION 2.6-2.9 MILS ON 14 MAR 00 WITHIN LIMITS. RECOMMENDATION: MONITOR.SDR 2000UALA00176Coffeemaker · smokeF/A REPORTS ACRID SMOKE SMELL IN AFT GALLEY. STRONGEST AROUND EYEBALL VENT. *S/D* FOUND ELECTRICAL SMELL COMING FROM RIGHT AFT COFFEEMAKER. REPLACED COFFEEMAKER (P/N:3510 0032 01U2). OPERATIONAL CHECK NORMAL.SDR 20000420AP001Cowling · damagedJFK - FLT 570 - DURING TAXIING GATE, ENG NR 2 INTAKE COWL BARREL AND RT ENG FAN COWL RE HIT BY A BELT LOADER. STAYED AT JFK FOR MX. PERFORMED INSPECTION THE FOLLOWING DAMAGE WAS FOUND: TWO CRACKS ON THE EXTERIOR LOWER SKIN OF THE ENG INTAKE COWL BARREL, AFT SDR 2000UALA00155Switch · leakingGREEN HYD RES LO LVL ECAM-GRAVITY GEAR EXTENSION. *S/D* FOUND RESERVOIR TANK FULL. REPLACED GREEN HYD RESERVOIR QUANTITY INDICATOR AND GREEN HYD RESERVOIR LOW LEVEL SWITCH. ALL INDICATIONS NORMAL, NO MSGS.SDR 2000UALA00138B-Nut · looseRETURN TO SFO DUE TO LOSING OIL IN NR 1 ENGINE. *S/D* FOUND FUEL COOLED OIL COOLER (FCOC) OUTLET LINE LEAKING AT FITTING (REF A320 IPC 79-21-09-80 /ITEMS 110 & 120). TIGHTENED ONE HALF TURN. REPLACED SCAVENGE OIL FILTER AND CHECKED MAGNETIC CHIP DETECTOR. SDR 2000UALA00133Computer · malfunctionedCOULD NOT PRESSURIZE CABIN AFTER TAKEOFF. SHORTLY AFTER DEPARTURE, VENT AVIONICS SYSTEM FAULT ECAM MESSAGE APPEARED WITH A RUMBLING, EVIDENT ON THE RIGHT SIDE OF THE ACFT. SYSTEM DID NOT CORRECT ITSELF AFTER FOLLOWING ECAM PROCEDURE, STOPPED CLIMB AT 10,000 SDR 2000UALA00134Battery · failedEMERGENCY LIGHT SYS TEST FAIL. MESSAGE: EPSU INT LOAD AFT L. *S/D* REPLACED EPSU AND BATTERY, REF: TASK 33-51-38-000-001.SDR 2000UALA00172Battery · inoperativeEMERGENCY LIGHT TEST FAILS WITH A \COMM AFT L\ DISPLAYED. *S/D* REPLACED EMERGENCY LIGHT BATTERY ABOVE DOOR 2L.SDR 2000UALA00061Pressure Switch · leakingSTRONG ODOR MOSTLY IN AFT CABIN AND ON FLIGHT DECK. FLEW WITH CABIN FANS OFF, HI FLOW, AND NR 1 PACK OFF. BECAME TOLERABLE. *S/D* ISOLATED OIL SMELL TO APU. REPLACED APU REF MM 49-11-98.SDR 2000UALA00052O-Ring · blownLOST YELLOW SYSTEM HYDRAULICS. *S/D* REPLACED PTU MANIFOLD BLOWN O-RING AT THE QUICK DISCONNECT FITTING. ALSO, REPLACED NR 2 ENGINE HYD PUMP AND CASE DRAIN FILTER DUE TO SUBSEQUENT CONTAMINATION. SERVICED HYDRAULICS AND CLEANED UP EFFECTED AREA, OPS AND LESDR 2000UALA00053Flap · out of rigON APPROACH INTO LAX, FLAPS LOCKED UP AT POSITION 1. MADE A NO FLAP LANDING. *S/D* LEFT HAND FLAP SYSTEM REQUIRED RIGGING. SYSTEM WAS RIGGED AND HAS BEEN FUNCTIONAL SINCE.SDR 2000UALA00664Skin · gougedFUSELAGE SKIN GOUGE AT BUTT JOINT FR12. A BLEND OUT OF THE AFFECTED AREA WAS PERFORMED, ALONG WITH HIGH FREQUENCY EDDY CURRENT INSPECTIONS TO INSURE THAT THE AREA IS CRACK FREE, AND REPROTECTION WAS PERFORMED. THIS WAS A MAJOR REPAIR.SDR 2000UALA00667Structure · corrodedCORROSION WAS DETECTED ON THE AFT LOWER CORNER OF THE FORWARD GALLEY DOOR AT FR21. THE AFFECTED AREA WAS BLENDED OUT, A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED, A FLAP PEENING WAS PERFORMED, THE DAMAGED AREA WAS REPROTECTED, AND A CORROSION PREVESDR 2000UALA00022Manifold · leakingON DEPARTURE OUT OF IAD FLT 231 LOST YELLOW HYD SYSTEM. COMPLIED WITH AFM. CPT AND DISPATCH AGREED ON CONTINUING TO SJC. *S/D* FOUND GROUND SERVICE MANIFOLD LEAKING. REPLACED MANIFOLD PER AMM. LEAK CHECKED GOOD.SDR 2000UALA00009Light · will not testEMERGENCY LIGHT TEST FAILED PER A CHECK. *S/D* REPLACED BATTERY POWER SUPPLY PER MM 33-51-38. OPS CHECK NORMAL. CABIN EMERGENCY LIGHTING CHECK PASSED TEST PER ''A'' CHECK PAPERWORK.SDR 99UAL900661Fuel Control · leakingON TAXI OUT AN AMERICAN AIRLINES CREW REPORTED FLAMES FROM THE APU EXHAUST. CREW SHUT DOWN THE APU AND RETURNED TO THE GATE. MM RESTARTED THE APU AND FLAMES RETURNED. FIRE BOTTLE WAS BLOWN AND FIRE DEPARTMENT CALLED TO STANDBY. *S/D* THE CAUSE OF THE FAILSDR 20000420AP005Intake Duct · damagedSAL - FLT 390 - DURING TAKEOFF (SAL-TGU-SAP-MIA) A LARGE BIRD IMPACTED THE ENGINE NR 1, HOWEVER THE ENGINE PARAMETERS REMAINED NORMAL, DUE TO THIS SITUATION THE AIRCRAFT RETURNED TO EL SALVADOR STATION FOR MAINTENANCE. AT EL SALVADOR, MAINTENANCE TECHNICANS P
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