IAE V2527E-A5

Service difficulty reports · 75

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 = 'V2527EA5'
  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.

SDR SOKF20130828012Solenoid Valve · malfunctionedNR 2 ENGINE EGT OVER LIMIT DURING CLIMB, THRUST EGT EXCEEDED LIMITS. EGT WENT CLOSE TO 670 CELSIUS DEGREES FOR 10 SECONDS THEN REDUCED TO LOWER EGT. R & R HPC 10 STAGE SOLENOID VALVE IAW AMM 75-32-53. PERFORMED FUNCTIONAL TEST IAW AMM 75-32-53-700-010A ANDAug 26, 2013 · N680TA · Airbus A320233 · Compressor Bleed ValveSDR RJEF2013020768701Tachometer · defectiveON ARRIVAL OF AIRCRAFT FLIGHT TAI-396 TO MGA FROM SAL, THE PILOT REPORTED AUTO BRAKE SYSTEM FAILURE, THE AIRCRAFT WAS DECLARED AOG. PER TSM 32-42-00, FOUND TACHOMETER NR 3 INOPERATIVE. REPLACED AND PERFORMED OPERATIONAL TEST AS PER AMM 32-42-00 WITH NO DUPLIFeb 7, 2013 · N687TA · Airbus A320233 · Landing Gear Brake SystemSDR SOKF20130207001Warning System · activatedECAM WARNING ENGINE 1 AND ENGINE 2 EPR MODE FAULT NI DEGRADED MODE. ENTER AS DD ITEM MEL REFERENCE 73-20-04 CATEGORY C.Feb 7, 2013 · N683TA · Airbus A320233 · Engine Pressure Ratio (EPR)SDR RJEF2013010768201Cover · missingAT THE ARRIVAL OF THE AIRCRAFT AS FLIGHT TAI-9951 FROM SAP TO SAL, IT WAS FOUND THAT COVER 622WB ON PANEL 622AB ON RIGHT WING WAS MISSING. THE AIRCRAFT WAS INSPECTED AND NO OTHER DAMAGE WAS FOUND. AS PER AIRBUS REPAIR APPROVAL REF:70571449/003/2013 AND ENGINDec 31, 2012 · N682TA · Airbus A320233 · Wing, Plate/SkinSDR RJEF2012081004Proximity Sensor · defectiveAFTER TAKEOFF OF THE AIRCRAFT AS FLIGHT TAI-561 FROM SFO TO SAL, THE PILOT IN COMMAND REPORTED A L/G SHOCK ABSORBER FAULT, FUEL AUTO FEED FAULT AND LOSS OF AUTO PILOT; CONSEQUENTLY, THE AIRCRAFT WAS RETURNED TO SFO AIRPORT FOR MAINTENANCE. AFTER LANDING OF THAug 7, 2012 · N687TA · Airbus A320233 · Landing Gear Position and WarningSDR USAA2012011800017Warning System · malfunctionedON TAKEOFF ROLL AT 65 KNOTS, ECAM CHIME WITH ENGINE 2 COMPRESSOR FAULT ON UPPER ECAM. MAINTENANCE PERFORMED TROUBLESHOOTING PER TROUBLESHOOTING MANUAL 75-30-00-810-84601 AND POWER ASSURANCE TEST PER AIRBUS MAINTENANCE MANUAL 71-00-00-710-013. NO FAULTS FOUNDJan 13, 2012 · N602AW · Airbus A320232 · Engine Indicating SystemSDR MU1Z2011020200003Frame · dentedFUSELAGE DENT BETWEEN FR 6 AND FR 7 APROX 6.5" DOWN RT SIDE STRINGER. DEPTH 1.57MM A= 21.97MM.Mar 14, 2011 · N498TA · Airbus A320233 · Fuselage Main, FrameSDR 2005UALA00667Epsu · malfunctionedEMERGENCY EXIT PATHWAY LIGHTS WILL NOT EXTINGUISH. REPLACED EMERGENCY POWER SUPPLIES 112WL2, 111WL2 AND 110WL2. OPS CHECK GOOD.Jul 15, 2005 · N402UA · Airbus A320232 · Emergency LightingSDR SOKF20041118Engine · fodDURING LANDING, CAPTAIN REPORTED (FOD ON ENGINE NR 2, NO ABNORMAL INDICATION DURING TAXI). MAINT PERFORMED INSPECTION OF ENGINE NR 2 IAW MM AND FOUND SOME DAMAGES LOCATED ON ATTRITION LININGS AT 5 OCLOCK, ACOUSTIC PANEL AT 4:30, (ENGINE, FROM THE FRONT), SOMENov 18, 2004 · N465TA · Airbus A320233 · Engine (Turbine/Turboprop)SDR SOKF2341AAElement · contaminatedDURING TAKEOFF RUN, ENGINE NR 2 DID NOT SPOOL UP BEFORE 80 KNOTS. AIRCRAFT RETURNED TO GATE. TECHS PERFORMED ANALYSIS IAW TSM AND AMM., REPLACED MAIN ELEMENT OF FUEL FILTER IAW AMM 73-1242, INSPECTED VSV MECHANISM IAW 73-32-42. CLEANED P 4.9, P2/T2 TUBES SYJun 10, 2004 · N482TA · Airbus A320233 · Aircraft Fuel Filter/StrainerSDR 2004F00269Fmu · erraticDURING TAKEOFF, AN ECAM WARNING MESSAGE, ENGINE NR 2 OVERSPEED PROTECTION FAULT CAME ON, AT LOW SPEED. WHEN MOVING TRUST LEVERS TO FLX MCT POSITION ENGINE NR 1 RESPONDED NORMAL, WHILE ENGINE NR 2 REMAINED AT LOW POWER. THE PLANE YAW TO THE RT AND THE TAKEOFFMay 24, 2004 · N991LR · Airbus A320233 · Fuel Controlling SystemSDR RJEF598HAControl Unit · looseDURING CRUISE, AC DIVERTED, PILOT REPORT OF MOD STRUCTURAL VIBRATION. ON GROUND, TECH FOUND THE FWD SEAL AT RT NLG OUT OF POSITION, IT WAS ADJUSTED IAW AMM. DAMAGED SEAL ON PANEL 191 AB LOOSE, INSTALLED SPEED TAPE IAW TSM. INSP OF RUDDER SERVO CONTROLS, HINMay 11, 2004 · N472TA · Airbus A319132 · Rudder Control SystemSDR RYN2004F00001Engine · malfunctionedON TAKEOFF, THERE WAS A LOUD BANG AND ECAM WARNING INDICATED EGT OVERTEMP ON NR 2 ENGINE. ECAM PROCEDURES FOLLOWED AND EMERGENCY DECLARED. AIRCAFT RETURNED, AND LANDED WITHOUT INCIDENT.Feb 21, 2004 · N951LF · Engine (Turbine/Turboprop)SDR 2004F00289Transducer · malfunctionedFLT LR622 - DURING CRUISE, BOTH ENGINES BLEED SYSTEMS FAULT ECAM WARNING CAME ON. BOTH BLEED SYSTEMS WENT TO CLOSED POSITION AND THE AIRCRAFT RETURNED TO SAL STATION. AFTER LANDING, INSPECTION WAS PERFORMED TO THE BLEED SYSTEM AND REPLACED ENGINE NR 1 TRANSDJan 23, 2004 · N462TA · Airbus A320233 · Pneumatic Distribution SystemSDR 2004F00003Engine · fireDURING ENGINE NR 2 TESTS AFTER THE ENGINE FIRE, IAW NORMAL PROCEDURE BOTH ENGINE FIRE EXTINGUISHING BOTTLES WERE USED AND SOME OTHER CHEMICAL EXTINGUISHERS WERE USED ON ENGINE NR 2. THE ENGINE WAS REPLACED AND SENT TO A REPAIR STATION FOR REPAIRS. ENGINE WASDec 1, 2003 · N455TA · Airbus A320233 · Engine (Turbine/Turboprop)SDR 2004F00025Compressor · stalledHAV - FLT 130 - DURING TAKEOFF FLIGHT CU130, HAV-MEX, AN ENGINE STALL OCCURRED ON ENGINE NR 2. TAKEOFF PROCEDURE WAS ABORTED, AIRCRAFT RETURNED TO GATE. AT THE PRESENT AIRCRAFT REMAINS ON GROUND FOR MAINTENANCE. (M)Nov 13, 2003 · Airbus A320233 · Engine (Turbine/Turboprop)SDR RYN2004F00002Floor Support · corrodedA (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 34 AND STRINGERS 34R TO 34L IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 34 FROM STRINGER 34R TO 34L IN FORWARD PIT.Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR RYN2004F00003Floor Support · corrodedAT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 31 TO 33 AT STRINGER 34R IN FORWARD CARGO COMPARTMENT. FABRICATED NEW FLOORBOARD SUPPORT. TREATED, PRIMED, TOP COATED AND INSTALLED FLOORBOARD SUPPORT FROM FRAME 31 TO 33 AT STRINGER 34R.Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR RYN2004F00004Floor Support · corrodedA (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 28 TO 31 AT STRINGER 34R.Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR RYN2004F00005Floor Support · corrodedAT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 31 TO 34 AT STRINGER 34L IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT FROM FRAME 31 TO 34, STRINGER 34L IN FORWARD PIT.Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR RYN2004F00006Latch · damagedAT (C) CHECK, FOUND GOUGE ON FORWARD LT EMERGENCY EXIT DOOR LOWER AFT FITTING LATCH. REMOVED AND REPLACED FORWARD LT EMERGENCY EXIT DOOR, LOWER AFT LATCH FITTING.Sep 15, 2003 · N951LF · Airbus A320233 · Emergency ExitsSDR 2003F00407Blade · bentDURING CLIMB, TWO COMPRESSOR STALLS AND LOSS OF POWER ON ENGINE NR 1 WERE EXPERIENCED. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT WAS RETURNED TO SAL STATION. ON GROUND TECHNICIANS PERFORMED HPC BOROSCOPE INSPECTION PER AMM 72-00-00. THE 6TH WAS FOUJun 27, 2003 · N464TA · Airbus A320233 · Turbine Engine Compressor SectionSDR 2003F00491Liner · erodedAT C-CHECK FOUND NR 2 ENGINE AIR INTAKE ATTRITION LINING WITH EROSION. REPAIRED ATTRITION LINING IAW EM 72-32-85 PAGE 6, FIGURE 72-32-85-990-016. (M)May 15, 2003 · N951LF · Airbus A320233 · Turbine Engine Air Inlet SectionSDR 2002F00913Engine · bird ingestionSAP - DURING LANDING, ENGINE NR 2 EXPERIENCED A BIRD STRIKE. AFTER LANDING MAINTENANCE PERSONNEL PERFORMED INSPECTION OF THE ENGINE NR 2. AT THE MOMENT, AIRCRAFT REMAINS ON GROUND AT SAP STATION FOR INSPECTION AND MAINTENANCE. (M)Aug 29, 2002 · N462TA · Airbus A320233 · Engine (Turbine/Turboprop)SDR 2002F00042Fmu · malfunctionedSJO - FLT 660 - DURING TAKEOFF CLIMB, ENGINE NR 2 HAVE EGT OVERLIMIT BEFORE 1,000 FEET, THIS CONDITION WAS FOR 13 SECONDS EGT PARAMETER WAS 639'C AND N2 98.2 PERCENT. PERFORMED TROUBLESHOOTING IAW AMM 77-00-810, INSPECTED ENGINE INLET AND EXHAUST, FOUND NO DAJan 6, 2002 · N464TA · Airbus A320233 · Fuel Controlling System
Back to IAE V2527E-A5