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 UALA2012052702994Switch · out of positionFLIGHT ATTENDANTS REPORTED EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN ARM POSITION. MOVED NO SMOKING SIGN SWITCH FROM AUTO TO ON, EXIT SIGNS WENT OUT.SDR UALA2012052702952Controller · malfunctionedCOCKPIT TEMP IS NOT CONTROLLABLE. REPLACED PACK TEMP CONTROLLER, OPS CHECKED OKAY.SDR UALA2012052903024Sleeve · groovedNOSE GEAR HAS EXCESS VIBRATION ABOVE 100KTS AND THROUGH RETRACTION. VIBRATION FELT THROUGH FIRST CLASS. NR 1 VIBRATION FWD NOSE WHEEL DOORS DUE TO WORN HINGE BUSHING. REMOVED BOTH L-R ROTATING ROD ASSY IAW, REF AMM. NEED TO REINSTALL NEW ASSY LEFT AND RIGHSDR UALA2012052502924Warning Light · illuminatedFIRE LOOP "A" FAULT DISPLAYED ON UPPER ECAM SCREEN, NR 2 ENGINE.SDR UALA2012052702949Windshield · faultyRIGHT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN, ANTI ICE. RT WINDSHIELD SENSOR ON CFDS. COMPLIED WITH MAINTENANCE TIP 30-003 .WHC2 TESTS OK. JUMPER INSTALLED ON RT WINDSHIELD SENSOR. REPLACED FIRST OFFICERS WINDSHIELD REF AMM. WINDOW HEAT OP CHECKED NORSDR UALA2012052502923Seal · wornAIRFRAME VIBRATION, FL200 UP TO FL340, MORE NOTICEABLE IN CLIMB THAN LEVEL FLT. ACCOMPLISHED TSM CHART 05-50-00 PB201 AND INFORMATION FROM VIBRATION SURVEY SUGGESTS BELLY FAIRING SOURCE OF VIBRATION. TAPED BELLY FAIRING SEALS REF MT53-004. FOUND SEAL WORN ONSDR UALA2012052402907Computer · faultyFIRST OFFICERS AIRSPEED INOPERATIVE. ALL CHECKS GOOD FROM ADR2 TO 1510VT TO 1851VT NO DEFECTS FOUND. REPLACED ELAC 1 PER AMM, OPS CHECKED NORMAL.SDR UALA2012052302894Windshield · defectiveL WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. ANTI ICE, REPLACED CAPTAINS WINDSHIELD. REPLACED WINDOW HEAT CONTROLLER 2DG1, COMPLETED OPERATIONAL TEST OF THE WINDSHIELD ANTI-ICING AND DEFOGGING. OPS CHECKS GOOD.SDR UALA2012052302884Packing · damagedFLIGHT RECEIVED GREEN HYD RES LOW QUANTITY ECAM. FOUND GREEN SYSTEM HP MANIFOLD CHECK VALVE PACKING DAMAGED, REPLACED. SERVICED GREEN HYD SYSTEM. MANIFOLD LEAK CHECKED GOOD.SDR UALA2012052302885Computer · faultyELAC 1 PITCH FAULT ECAM AND ALT DISC OF 500 FT BTWN CAPTAIN AND FIRST OFFICERS ALT. RTFL. ALTITUDE DISCREPANCY OF 500' BTWN CAPT & F-O ALTIMETER. POSSIBLE PCN :482-9080. IDT REQUIRED. RMV'D & RPLC'D 19FP 2 AIR DATA MODULE, OPS CHECKED GOOD. ELAC 1 PITCH FAULSDR 2012FA0000374Blade · crackedENGINE UNDERGOING MX. DURING ROUTINE NDT INSPECTION, A CRACK WAS DETECTED IN THE DOVETAIL AT THE TOP OF THE BEDDING AREA AND ACROSS THE FRONT FACE. ALSO NOTED WAS FRETTING DAMAGE ADJACENT TO THE CRACK. THE ITEM HAS BEEN REMOVED FROM SERVICE.SDR UALA2012052102845Ballast · odorBURNING SMELL FROM AFT GALLEY W- COFFEE AND CHILLERS ON. FOUND AFT FA PANEL LOCKED UP, CYCLED POWER AND FAULT CLEARED. REPLACED BOTH AFT OVERHEAD LIGHTS ASSEMBLIES & BALLAST AND RELAMPED. GROUND CHECKED OKAY.SDR UALA2012052102846Door · leakingAFT OVERWING EMERGENCY EXIT WINDOW AT ROW 21 ON THE RIGHT SIDE IS LEAKING WATER. PRESSURIZED ACFT TO 3 LBS NO LEAKS NOTED CLEANED AREA OF WATER. NO OTHER LEAKS NOTED AT THIS TIME, FLASH RAIN STORM AT TIME OF LEAK.SDR UALA2012052202871Fan · failedSMOKE SMELL IN COCKPIT. DIVERTED. REMOVED & REPLACED EXTRACT AVIONICS FAN, OPS CHECKED GOOD.SDR UALA2012052202876Connector · unsecureRED EMERGENCY EXIT ROW LIGHT ON SEAT 11C INOPERATIVE. FOUND CONNECTOR LOOSE AT UNDER SEAT BOX. SECURED CONNECTOR AND WIRES. OPS CHECKED GOOD.SDR UALA2012052202880Warning Light · false activationNOSE WHEEL STEERING DISCONNECT AMBER MSG DISPLAYED AFTER GEAR RETRACTION. NO FAULTS RECORDED FOR PAST TEN FLT LEGS PER TSM 32-51-00-810-833-A PARA 4.A.(1)(B). NO MAINT ACTION TAKEN.SDR UALA2012052102849Stringer · corrodedSTRINGER 11 LEFT AT FR 59-60 HAS CORROSION, AFT CARGO BAY. INSTALLED NEW STRINGER PER SRM 51-44-11, AND 51-42-11.SDR UALA2012052102848Stringer · corrodedFWD CARGO BAY, STRINGER 40R, BETWEEN FR 29 AND FR 30 CORRODED. CUTOUT DAMAGED STRINGER SECTION AND INSTALLED NEW SECTION AND SPLICE REPAIR PER SRM 51-41-11 AND SRM 53-00-13.SDR UALA2012052102850Stringer · corrodedAFT CARGO BAY STRINGER 38 RIGHT HAS CORROSION BETWEEN FR 59 AND 60. CUTOUT DAMAGED STRINGER SECTION AND SLICED IN NEW SECTION PER SRM 53-00-13.SDR UALA2012052102851Stringer · corrodedAFT CARGO BAY STRINGER 40 RIGHT CORRODED BETWEEN STR 63 AN D 64. CUT OUT DAMAGED STRINGER SECTION AND INSTALLED NEW SECTION AND SPLICE REPAIR PER 53-00-13.SDR UALA2012052102847Stringer · corrodedHEAVY CORROSION ON STRINGER 31 RIGHT BELOW OUTFLOW VALVE FR 65 - FR66. INSTALLED NEW STRINGER. MAJOR REPAIR.SDR UALA2012051802838Controller · malfunctionedHAD CABIN PRESSURIZATION FAULT DESCENDED TO 10,000 FT, OUTFLOW VLV FULL OPEN, MASK DID NOT DEPLOY. REPLACED BOTH CABIN PRESS CONTROLLERS AND PERFORMED ALL TESTS AS REQUIRED PER MM AND 05-53-00. NO FAULTS NOTED A-C OKAY FOR SERVICE.SDR UALA2012052202877Outflow Valve · malfunctionedCABIN PRESSURIZATION FAULT, DESCENDED TO 10,000 FT, OUTFLOW VALVE FULL OPEN, MASK DID NOT DEPLOY.SDR UALA2012051802839Module · faultedFIRST OFFICER LOST AIRSPEED INDICATIONS. FLT ABORTED. FIRST OFFICER LOST AIRSPEED INDICATIONS W- NUMEROUS ECAMS. FOUND ON POST FLT RPT ADM 19FP8 FAULT AND NR 3 ADIRU FAULT, REPLACED AMD PER AMM AND NR 3 ADIRU PER AMM. ACCOMPLISHED FULL RANGE TEST PER AMM, SDR UALA2012051802836Knob · looseFIRST OFFICER BRIGHTNESS CONTROL KNOB FOR THE MAP LIGHT FALLS OFF. REPLACED. REPLACED MAP LIGHT ASSY.SDR UALA2012051802837Sensor · malfunctionedNLG STEERING FAULT DISPLAYED ON UPPER ECAM SCREEN. REMOVDE AND REPLACED NOSE WHEEL STEERING FEED BACK SENSOR 4GC, IAW MM, OPS CHECKED OK.SDR UALA2012051802815Stringer · corrodedAFT CARGO BAY STRINGER 39R CORRODED AT FR 62. REMOVED DAMAGED SECTION OF STRINGER 39R AT FR 62 AND INSTALLED STR REPAIR PER SRM 53-00-13. MAJOR REPAIR.SDR UALA2012051802816Stringer · corrodedFWD CARGO, STRINGER 41R BETWEEN FR 31 AND FR 34 HAS CORROSION. CUTOUT DAMAGED STRINGER SECTION AND INSTALLED STRINGER SPLICE REPAIR PER SRM 53-00-15. MAJOR REPAIR.SDR UALA2012052102852Controller · faultedUPPER ECAM DISPLAYING AIR PACK 1 REGULATOR FAULT PACK CONTROL TEMP INOPERATIVE. REPLACED NR 1 A/C PACK TEMP CONTROLLER 7HH PER MM 21-61-34. OPS CHECKED NORMAL.SDR UALA2012051602800Brake Sys · malfunctionedLEFT BRAKE PEDDLE MASTER CYLINDER IS BY PASSING WITH BRAKES OFF. LEFT IND SHOWS 1000LBS. REPLACED LEFT LOW PRESSURE BRAKE PEDDLE MASTER CYLINDER. NO HELP STILL SHOWS 1000 PSI ON TRIPLE INDICATOR WITH BRAKE OFF.SDR UALA2012051802808O-Ring · leakingUNION LEAKING AT NOSE GEAR DOOR GROUND BYPASS VALVE. REPLACED O-RING SEAL PER AMM, NO FURTHER LEAKS NOTED.SDR UALA2012051602778Selector Valve · failedPER ACFT POST FLT REPORT LGCIU2 05GA2 - LANDING GEAR DOORS SELECTOR VALVE 41GA IS FAILING. REPLACED MLG DOOR 41GA SELECTOR VALVE PER MM.SDR UALA2012060103040Attach Fitting · wornNR 2 PYLON TO ENGINE LT AND RT SIDE MOUNT FITTING WEAR WAS BLENDED REF ECRA:5451-01086. PERFORMED HFEC INSPECTION WITH NO DEFECTS FOUND.SDR UALA2012111906649Mount Fitting · wornNR 2 PYLON TO ENGINE LT AND RT SIDE MOUNT FITTING WEAR WAS BLENDED REF ECRA:5451-01086. PERFORMED HFEC INSPECTION WITH NO DEFECTS FOUND.SDR UALA2012051502763Brake Assy · overtempDIVERTED TO DEPARTURE, DUE TO HOT BRAKES.SDR UALA2012051602777Actuator · faultedSELECTED PACK FLOW TO HIGH AND RT PACK COMPRESSOR OUTPUT TEMP WENT TO 230 AND AMBER. FOUND PACK 2 RAM AIR OUT ACTUATOR FAILED AND REPLACED ACT PER MM 21-61-52. RAN TEST AGAIN AND PASSED. NO MESSAGES.SDR UALA2012051602775Skin · damagedRT FUSELAGE SKIN FR 33 AND STR 23R UNDER FILLET PANEL 192AT EXCESSIVE MATERIAL REMOVED REF SMB WU U9578I. MAJOR REPAIR ACCOMPLISHED PER SRM 53-21-11 FIG.215.SDR UALA2012051602769Warning Light · false activationRECEIVED MASTER WARNING BELL AFTER TAKEOFF WHEN GEAR LEVER RAISED. LOWERED GEAR HANDLE AND GOT TEXT, RAISED GEAR HANDLE AFTER 1 MIN. GEAR RAISED NORMAL. ALMOST LIKE SENSOR STUCK. VERIFIED SECURITY OF GEAR POSITION AND LOCK SENSORS. PERFORMED BITE TEST TO BOSDR UALA2012051602776O-Ring · leakingGROUND CREW REPORTS NR 1 ENGINE LEAKING FLUID WHEN RUNNING. REPLACED O-RINGS AT IDG OIL TO FUEL COOLER PER AMM 24 21 42.SDR UALA2012051102738Support Bracket · corroded1 LT MED EMERGENCY SLIDE DOOR SUPPORT BRACKET ON PACK HAS CORROSION EXFOLIATION. REPLACED SLIDE AND INSTALLED.SDR UALA2012051002695Stringer · corrodedSTRINGER 31R BELOW OUTFLOW VALVE IS CORRODED. REMOVED AND REPLACED STRINGER IAW SRM 51-42-11. MAJOR REPAIR.SDR UALA2012051102736Skin · damagedSKIN DAMAGED BETWEEN FR 68 - 69 AT STRINGER 29L. SKIN REPAIRED IAW SRM.SDR UALA2012051002693Skin · dentedDENT FOUND IN SKIN BELOW DOOR 1L OUT OF LIMITS. INSTALLED DOUBLER REPAIR IAW SRM 53-11-11. MAJOR REPAIR.SDR UALA2012051002694Skin · dentedSKIN DENT OUT OF LIMITS BETWEEN FR 24-25 STR 22L AFT OF MAIN ENTRY DOOR. INSTALLED DOUBLER REPAIR PER SRM 53-11-11 FIG 212. MAJOR REPAIR.SDR UALA2012051002692Web · crackedFWD END OF NR 2 PYLON, INTERNAL WEB IS CRACKED. STOP DRILLED CRACK, REF S RM54-52-12. ACCOMPLISHED WELD REPAIR PER SRM 54-50-00. INSTALLED DOUBLER REPAIR OVER WELD PER SRM 54-52-12 FIG 207, SHEET 2. N-R F1834T.SDR UALA2012051002687Dome Nut · missingRIVET AND BOLT MISSING 3 AND 4TH BRACKET AFT FWD CARGO DOOR LATCH. REPAIRED MISSING DOME NUT PER MT-53-014.SDR UALA2012051002688Fadec · malfunctionedFADEC A FAULT DISPLAYED ON UPPER ECAM SCREEN. RESET FADEC AND EIU. SYSTEM OPS NORMAL.SDR UALA2012051002689Power Supply · no testWHEN TESTING EMERGENCY LIGHTING AFT LT BAT FAULTED. REPLACED POWER SUPPLY AND BATTERY PACK.SDR UALA2012051002696Outflow Valve · failedAVIONICS SKIN VENT FAULT, AFTER FLT ECAM PROCEDURE EXTRACT VALVE WILL NOT CLOSE AND ACFT UNABLE TO PRESSURIZE. REPLACED VALVE 22HQ PER MM 21- 26-53 AND OPS CHECKED GOOD PER MM 21-26-00.SDR UALA2012051002691Bushing · damagedRT WING NR 3 FLAP TRACK HAS EXCESSIVE PLAY AT AFT WING ATTACH POINT. REPLACED AFT SPIGOT PIN AND BUSHING PER CMM 57-51-41.
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