# Service difficulty reports: IAE V2527E-A5

A list on [IAE V2527E-A5](https://openairdocs.org/engine/iae-v2527e-a5.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 75 reports

- [SDR 2026FA0000532](https://openairdocs.org/sdr/2026FA0000532.md): Sleeve · damaged · Jun 22, 2026 · N9HFSM · Airbus A320233 · Engine Thrust Reverser
  > T/R ASSY OUT OF LIMIT WITH ISSUED REPAIRED. T/R ASSY LEADING EDGE SLEEVE OUT OF LIMIT WITH ISSUED REPAIRED CERTIFICATE. AFTER INSTALLATION OF NEW RECEIVED SERVICEABLE T/R HALF ASSY INCREASED CLEARANCE FOUND ON LOWER LEADING EDGE SLEEVE APPROXIMATELY 600 MM (W
- [SDR YENA2024122301578](https://openairdocs.org/sdr/YENA2024122301578.md): Actuator · failed · Dec 21, 2024 · N656JB · Airbus A320232 · Turbine Engine Compressor Section
  > FLT#8523, EWR-RDU. (AIRCRAFT DIVERTED TO JFK) 'DURING CLIMB OUT ENG 2 COMPRESSOR VANE ECAM MSG FOLLOWED BY ENG 2 STALL. BANG/THUD HEARD DURING STALL. ENGINE 2 RECOVERED BEFORE ECAM ACTIONS STARTED; REMOVED AND REPLACED #2 ENG LOW PRESS COMPRESSOR BLEED MASTER
- [SDR YENA2024030600360](https://openairdocs.org/sdr/YENA2024030600360.md): Engine · stalled · Mar 5, 2024 · N794JB · Airbus A320232 · Engine (Turbine/Turboprop)
  > FLT#621, BOS-PBI. (AIRCRAFT DECLARED AN EMERGENCY). '#1 ENGINE, ENGINE STALL ENGINE EGT 765 - SHUT DOWN.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR 2023FA0000030](https://openairdocs.org/sdr/2023FA0000030.md): Blower · faulted · Jan 16, 2023 · N684TA · Airbus A320233 · Air Distribution Fan
  > DURING CLIMB FROM MGA TO MIA THE AIRCRAFT RETURNED TO MGA DUE TO VENT SKIN VALVE FAULT. VENT EXTRACT FAULT. VENT BLOWER FAULT. AT MGA STATION WAS INCLUDED OUTLET SKIN VALVE AS DMI IAW MEL 21-26-04 CAT. C
- [SDR SOKF20211108003](https://openairdocs.org/sdr/SOKF20211108003.md): None · none · Nov 7, 2021 · N493TA · Airbus A320233 · Pitot/Static System
  > DURING TAKE OFF FROM SAL TO LAX THE AIRCRAFT REJECTED THE TAKE OF DUE TO UNRELIABLE SPEED CAPTAIN SIDE FOLLOWING TSM 34-13-00-810-998-B WAS PERFORMED CLEANING OF CAPTAIN, F/O AND STANDBY PITOT PROBE IN ACCORDANCE WIH AMM 34-10-00-170-004-A REV 58 PERFORMED FUN
- [SDR SOKF20211108002](https://openairdocs.org/sdr/SOKF20211108002.md): Control Valve · damaged · Nov 6, 2021 · N496TA · Airbus A320233 · Air Distribution System
  > DURING CLIMB FROM BOG TO SAL THE AIRCRAFT RETURNED TO BOG DUE TO ECAM ADVISORY PRESS VENT SKIN OULET VALVE IN AMBER, CAB PRESS SYST 1 Y 2 RESETED NO SUCCESSFUL. AT BOG STATION PERFORMED TSM TASK CARD 21-26-00-810-819, TASK CARD 21-26-00-810-804, TASK CARD 21-2
- [SDR SOKF20210608001](https://openairdocs.org/sdr/SOKF20210608001.md): Pitot Head · obstructed · Jun 6, 2021 · N684TA · Airbus A320233 · Pitot/Static System
  > DURING TAKE OFF FROM MIA TO SAL THE TAKE OFF WAS REJECTED DUE TO AIRSPEED DISCREPANCY BETWEEN CAP PFD AND FO PFD DURING TAKE OFF ROLL. IN ACCORDANCE WITH TSM TASK 34-13-00-810-998-B PERFORMED INSPECTION IAW AMM 34-11-15-200-001. PERFORMED FLUSHING OF THE PRIN
- [SDR YENA2020082500433](https://openairdocs.org/sdr/YENA2020082500433.md): Seal · leaking · Aug 21, 2020 · N656JB · Airbus A320232 · Turbine Engine Oil System
  > FLT 206, BNA-BOS. LEVEL 1 ODOR EVENT SEE CABIN ODOR FOR DETAILS; TROUBLE SHOT PER TSM 71-00-00-810-801-A, FOUND DE-OILER CARBON SEAL LEAKING. R & R DE-OILER CARBON SEAL REF AMM 72-61-49. LEAK CHECK GOOD. COULD NOT SMELL ANYTHING IN COCKPIT OR CABIN. A/C OK FOR
- [SDR SOKF2020030600000](https://openairdocs.org/sdr/SOKF2020030600000.md): Pump · damaged · Mar 4, 2020 · N493TA · Airbus A320233 · Hydraulic Pump (Electric/Engine), Main
  > DDURING FLIGHT FROM SAL TO SFO THE AIRCRAFT DIVERTED TO MEX DUE TO PILOT REPORT BLUE PUMP OVERHEAT AND BLUE HYDRAULIC SYSTEM WAS LOST AND ECAM WARNING MESSAGE CAME ON, THEN WHEN THE FAULT LIGHT WENT OFF THE BLUE HYD SYSTEM WAS RECOVERED, IN ACCORDANCE WITH TS
- [SDR SOKF2020030200000](https://openairdocs.org/sdr/SOKF2020030200000.md): Unknown · malfunctioned · Feb 27, 2020 · N495TA · Airbus A320233 · Pneumatic Distribution System
  > AFTER TO FROM BOG TO LIM THE AIRCRAFT RETURNED TO BOG DUE TO ECAM WARNING MESSAGE AIR ENG 1 + 2 BLEED FAULT. IN ACCORDANCE WITH AMM 36-11-52 PB 401 PRV WAS REPLACED IN LH ENGINE S/N V10892, IN ACCORDANCE WITH AMM TASK 36-11-52-790-001-A LEAK TEST OF BLEED PRE
- [SDR 5TTY20190417 0001](https://openairdocs.org/sdr/5TTY20190417%200001.md): Regulator · malfunctioned · Apr 13, 2019 · N685TA · Airbus A320233 · Compressor Bleed Valve
  > DURING CRUISE PHASE OF FLIGHT, THE AIRCRAFT WAS TURNED BACK DUE TO THE LH ENGINE AIR BLEED FAULT. THE AIRCRAFT LANDED WITH NO INCIDENT NOR WEIGHT EXCEEDANCE. AT MAINTENANCE, THE BLEED PRESSURE REGULATOR VALVE AND ITS SOLENOID ON LH ENGINE WERE REPLACED PER TR
- [SDR RJEF20190320001](https://openairdocs.org/sdr/RJEF20190320001.md): Transceiver · unserviceable · Mar 19, 2019 · N490TA · Airbus A320233 · Weather Radar System
  > DURING FLIGHT TPU146 (LIM-MED) THE AIRCRAFT HAD FAILURE OF RADAR SYSTEM AND RETURNED TO LIM FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED: "RADAR INOP, GW 61500 KG, NO OVERWEIGHT LANDING", MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS IN ACC
- [SDR RJEF20190107001](https://openairdocs.org/sdr/RJEF20190107001.md): Unknown · malfunctioned · Jan 3, 2019 · N494TA · Airbus A320233 · Fuel Controlling System
  > DURING TAKE OFF PROCESS OF FLIGHT TP823 FROM LIM TO CUZ ENGINE 1 ACCELERATED LESSER IN COMPARISON WITH ENGINE 2, THE TAKE OFF WAS ABORTED AND RETURNED TO THE GATE FOR MAINTENANCE. THE PILOT REPORTED: "DURING ROLLING TAKE OFF ENG 1 DELAY ACCELERATION IN RELATIO
- [SDR 5TTY2018110500001](https://openairdocs.org/sdr/5TTY2018110500001.md): Hydraulic System · overserviced · Dec 4, 2018 · N499TA · Airbus A320233 · Hydraulic System, Auxiliary
  > DURING ENGINE START, PRIOR TO THE DEPARTURE OF THE AIRCRAFT FLIGHT AV503, PILOT REPORTED LOW PRESSURE ON BLUE HYDRAULIC SYSTEM; CONSEQUENTLY, THE AIRCRAFT WAS RETURNED TO BLOCK. AT MAINTENANCE, AND PER TSM 29-12-00-860-053-C, THE BLUE HYD. SYSTEM WAS FOUND
- [SDR YENA2018121014838](https://openairdocs.org/sdr/YENA2018121014838.md): Pump · failed · Nov 14, 2018 · N659JB · Airbus A320232 · Turbine Engine Oil System
  > FT # 1735, BOS-MSP. DIVERTED TO BUF. #2 ENG LO OIL PRESS NO SECONDARIES; REMOVED + REPLACED #2 ENG OIL PRESSURE PUMP ASSY PER AMM 79-21-41 LEAK/OPS GOOD ALSO FOUND REAGS CLOGGING STRAINER REMOVED AND INSP OIL TANK FOR OTHER RAGS- NO DEFECT FOUND.
- [SDR SOKF20181116009](https://openairdocs.org/sdr/SOKF20181116009.md): Gps · faulted · Nov 12, 2018 · N683TA · Airbus A320233 · Global Positioning System
  > DURING FLIGHT FROM LIM TO CUZ THE AIRCRAFT RETURN TO LIM DUE TO ECAM WARNING MESSAGE NAV GPS 1 FAULTGPS 1. AT LIM STATION TRANSFERRED TO DMI PAGE 06571 ITEM 2 IAW MEL 34-58-01 CAT C AND RNP-AR OPERATION PROHIBITED. THE AIRCRAFT RETURN TO NORMAL OPERATION.
- [SDR SOKF20181019008](https://openairdocs.org/sdr/SOKF20181019008.md): Anti-Ice Valve · damaged · Oct 15, 2018 · N496TA · Airbus A320233 · Airfoil Anti/De-ice System
  > DURING FLIGHT FROM AQP TO CUZ THE AIRCRAFT DEVERTED TO LIM DUE TO ECAM WARNING WING ANTI-ICE FAULT AND BAD WEATHER AT CUZ STATION. AT LIM STATION PERFORMED TSM 30-11-00-810-803-A, REMOVED AND REPLACED OF WING ANTI ICE CONTROL VALVE PERFORMED IAW AMM 30-11-51-0
- [SDR SOKF2018100210006](https://openairdocs.org/sdr/SOKF2018100210006.md): Fmc · damaged · Sep 28, 2018 · N493TA · Airbus A320233 · Auto Throttle System
  > DURING TO FROM LIM TO JUL THE, TO WAS REJECTED DUE ECAM WARNING A/T OFF. REMOVED AND REPLACED FMGC IAW AMM 22-83-34-000-001-A AND AMM 22-83-34-400-001-A OP TEST AFS IAW AMM 22-96-00-710-001 TEST SATISFACTORY. THE AIRCRAFT RETURN TO NORMAL OPERATION.
- [SDR SOKF20180927005](https://openairdocs.org/sdr/SOKF20180927005.md): Autothrottle Sys · malfunctioned · Sep 23, 2018 · N493TA · Airbus A320233 · Auto Throttle System
  > DURING TO FROM LIM TO CUZ THE TO WAS REJECTED DUE TO A/THR INOP AND DURING T/O PWR CLB DO NOT SHOW INDICATION THRUST MODE AND FLEX TOGA. AUTO FLIGHT AUTO THRUST OFF DURING TAKE OFF ROLL. AT LIM STATION LAND CAT 3 CAPABILITY TEST PERFORMED IAW AMM 22-97-00-710-
- [SDR RJEF20180410002](https://openairdocs.org/sdr/RJEF20180410002.md): Egt Indication · illuminated · Apr 8, 2018 · N490TA · Airbus A320233 · Engine Temperature Indicating System
  > DURING ENGINE START, THE PILOT REPORTED THE NR 1 ENGINE EGT OVERLIMIT, DURING THE NR 1 ENGINE START, EGT INDICATION WENT TO MAX DISPLAYED EGT ON THE NEEDLE AND DIGITAL 818°C, NR 1 ENGINE MASTER WAS SET TO OFF, THEN THE NR 1 ENGINE INDICATIONS DISPLAY XX, TH
- [SDR SOKF20180304002](https://openairdocs.org/sdr/SOKF20180304002.md): Actuator · damaged · Mar 1, 2018 · N683TA · Airbus A320233 · Compressor Bleed Valve
  > DURING TO FROM LIM TO AQP THE TO WAS REJECTED DUE TO ECAM MSG ENG 2 COMPRESSOR VANE. AT LIM STATION PERFORMED TSM 75-30-00-810-853-A REMOVED AND REPLACED OF THE VSV ACTUATOR AS PER AMM 75-32-41-000-010-A A01 AND AMM 75-32-41-400-010-A01 PERFORMED IDLE LEAK CHE
- [SDR RJEF20180219001](https://openairdocs.org/sdr/RJEF20180219001.md): Actuator · malfunctioned · Feb 16, 2018 · N498TA · Airbus A320233 · Engine Thrust Reverser
  > DURING CLIMB, HAD A WARNING MESSAGE OF THE NR 2 THRUST REVERSE UNLOCKED, RETURNED TO DEPARTURE. UNEVENTFUL LANDING. PERFORMED FAULT ANALISYS IAW TSM 78-30-00-810-844-A, REPLACED THE HCU, REPLACED THE NON-LOCKING ACTUATORS FOR THE NR 2 THRUST REVERSER IA
- [SDR 5TTY2018012900001](https://openairdocs.org/sdr/5TTY2018012900001.md): Controller · faulted · Jan 29, 2018 · N499TA · Airbus A320233 · Cabin Pressure Controller
  > AFTER T/O, THE AIRCRAFT WAS TURNED BACK TO DEPARTURE BASE DUE TO PRESSURE SYS 1 FAILURE AND UNABLE TO CONTROL PRESSURIZATION AFTER SWITCHING TO SYS 2. LANDING IN MANUAL MODE WITH NO INCIDENTS. FUEL AUTO FEED FAULT WAS REPORTED. PRESSURIZATION SYSTEM 1 FAILU
- [SDR RJEF20180110001](https://openairdocs.org/sdr/RJEF20180110001.md): Engine · malfunctioned · Jan 9, 2018 · N687TA · Airbus A320233 · Engine (Turbine/Turboprop)
  > DURING FLIGHT, THE NR 1 ENGINE HAD A STALL CONDITION AND EGT OVERLIMIT, DUE THAT SITUATION THE AIRCRAFT DIVERTED. UNEVENTFUL LANDING. CARRIED OUT THE CORRESPONDING FAILURE ANALYSIS. FOLLOWED THE INSTRUCTIONS OF TSM 71-00-00-810-808-A, PERFORMED BORESCOPE
- [SDR RJEF20171110001](https://openairdocs.org/sdr/RJEF20171110001.md): Outflow Valve · malfunctioned · Nov 8, 2017 · N492TA · Airbus A320233 · Pressure Regulator/Outflow Valve
  > AFTER TAKEOFF, THE PILOT REPORTED THE CABIN PRESSURE SYSTEM 1 & 2 FAULTED. NR 1 ENGINE COMPRESSOR VANE DUE TO THAT SITUATION THE AIRCRAFT RETURNED TO DEPARTURE FOR MAINTENANCE. MAINTENANCE PERFORMED FAULT ANALYSIS IAW TSM 21-31-00-810-807-A, REPLACED TH
- [SDR RJEF20171012001](https://openairdocs.org/sdr/RJEF20171012001.md): Thermocouple · faulty · Oct 11, 2017 · N687TA · Airbus A320233 · Engine EGT/TIT Indicating System
  > DURING THE NR 1 ENGINE START, EGT ROSE TO 780°C, INDICATION ON RED. DUE TO THAT SITUATION THE AIRCRAFT RETURNED TO THE GATE FOR MAINTENANCE. MAINTENANCE PERFORMED FAULT ANALYSIS IAW TSM 77-20-00-810-801-B, INSPECTED THE NR 1 ENGINE THERMOCOUPLES, AND FOUN
- [SDR RJEF20171005002](https://openairdocs.org/sdr/RJEF20171005002.md): Indication Sys · malfunctioned · Oct 2, 2017 · N687TA · Airbus A320233 · Engine EGT/TIT Indicating System
  > DURING TAXI, THE PILOT REPORTED THE NR 1 ENGINE EGT EXCEEDED DURING TAXI TO 720°C, THEN THE TEMPERATURE DROPS TO -10°C, AFTER THAT INDICATION STABILIZED, THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PERFORMED FAULT ANALYSIS IAW TSM 77-00-00-810-934-A, INSP
- [SDR SOKF20170818008](https://openairdocs.org/sdr/SOKF20170818008.md): Filter · contaminated · Aug 16, 2017 · N493TA · Airbus A320233 · Aircraft Fuel Filter/Strainer
  > DURING MAJOR CHECK, PERFORMED TASK CARD 731000-11-1, FOUND FUEL FILTER CONTAMINATED. FUEL FILTER ELEMENT WERE EVALUATED IAW AMM 73-12-42-210-061-A PARAGRAPH A ITEM (2)REV.40 01. LT AND RT ENGINE FUEL FILTERS ELEMENT WERE REPLACED. LT FUEL COOLED OIL COOLER
- [SDR YENA201704300320](https://openairdocs.org/sdr/YENA201704300320.md): Engine · failed · Apr 30, 2017 · N794JB · Airbus A320232 · Engine (Turbine/Turboprop)
  > AT TOP OF DESCENT, THERE WAS A BURNED MATERIAL ODOR IN THE COCKPIT. SOON DISSAPATED, AT 2200 MSL ON APPROACH A VERY STRONG DIRTY SOCK ODOR PERMEATED THE FLIGHT DECK & DID NOT GO AWAY UNTIL ENGINE SHUTDOWN. R & R THE NR 1 ENGINE.
- [SDR SOKF20170307003](https://openairdocs.org/sdr/SOKF20170307003.md): Valve · failed · Mar 4, 2017 · N683TA · Airbus A320233 · Cabin Pressure Control System
  > AFTER TAKE OFF, THE AIRCRAFT RETURN TO DEPARTURE, DUE THE FAILURE OF THE VENT SKIN VALVE, ABOUT 5, 000 FT. FOLLOWED THE ECAM PROCEDURE AND THE LIMIT UP TO 10,000 FT. PERFORMED PROCEDURES IAW TSM 21-26-00-810-804-A AND FOUND THE VENT SKIN VALVE FAULTY. REMO
- [SDR RJEF20170117001](https://openairdocs.org/sdr/RJEF20170117001.md): Adiru · malfunctioned · Jan 15, 2017 · N499TA · Airbus A320233 · Integrated Flight System
  > DURING TAKEOFF PROCESS OF FLIGHT TA567 FROM JFK TO SAL, THE AIRCRAFT SHOWED FAILURE OF AIRSPEED AND ATL INDICATIONS, DUE THAT SITUATION THE TAKEOFF WAS ABORTED AND RETURNED TO THE GATE FOR MAINTENANCE. THE PILOT REPORTED "DURING T.O. ROLL, AIRSPEED AND ALT IND
- [SDR 5TTY201609260001](https://openairdocs.org/sdr/5TTY201609260001.md): Transducer · failed · Sep 26, 2016 · N498TA · Airbus A320233 · Flight Control System
  > DURING FLIGHT, THE AIRCRAFT GENERATED THE FLT CONTROL ELAC 2 FAULT MESSAGE AND DUE TO DEFERRED ELAC 1, THE AIRCRAFT WAS DIVERTED. AFTER AN UNEVENTFULLY LANDING, MAINTENANCE REPLACED THE CAPTAIN`S TRANSDUCER UNIT 4CE1 ON CAPTAIN SIDE STICK IAW TSM 27-93-00-810
- [SDR RJEF20160708001](https://openairdocs.org/sdr/RJEF20160708001.md): Lever · faulty · Jul 7, 2016 · N499TA · Airbus A320233 · Landing Gear Selector
  > DURING CLIMB OF FLIGHT TP803, THE LANDING GEAR CONTROL LEVER DID NOT MOVE UP, DUE THAT REASON THE AIRCRAFT RETURNED TO DEPARTURE FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS IN ACCORDANCE WITH TSM 32-31-00-810-88
- [SDR RJEF20160422001](https://openairdocs.org/sdr/RJEF20160422001.md): Sensor · faulty · Apr 19, 2016 · N687TA · Airbus A320233 · Trailing Flap Position Indicating System
  > DURING LANDING PROCEDURES, THE FLAPS BECAME JAMMED, THE PILOT ASKED FOR THE ACTIVATION OF THE EMERGENCY PROTOCOL AND LANDED WITHOUT INCIDENT IN THAT CONFIGURATION. ONCE THE ACFT ARRIVED TO THE GATE THE PILOT REPORTED: LANDING WITH FLAPS JAMMED BETWEEN 0 AND
- [SDR RJEF20160419001](https://openairdocs.org/sdr/RJEF20160419001.md): Fcu · faulty · Apr 15, 2016 · N687TA · Airbus A320233 · Flight Controller
  > DURING CLIMB OF FLIGHT TA588, THE PILOT REPORTED FCU ALTITUDE UNABLE TO CHANGE ALTITUDES. DUE THAT SITUATION THE ACFT RETURNED. AFTER AN UNEVENTFUL LANDING, ONCE THE ACFT PARKED AT THE GATE, PERFORMED FAULT ANALYSIS IAW TSM 22-81-00-810-801-A. REPLACED THE
- [SDR RJEF201603220001](https://openairdocs.org/sdr/RJEF201603220001.md): Check Valve · failed · Mar 22, 2016 · N498TA · Airbus A320233 · Hydraulic System, Main
  > DURING TAKEOFF, THE PILOT REPORTED OVERHEAT YELLOW HYDRAULIC RESERVOIR ECAM WARNING; HENCE THE ACFT TURN BACK TO AIRPORT. AT LANDING, THE PILOT REPORTED NO OVERWEIGHT LANDING. AFTER AN UNEVENFUL LANDING AND FOLLOWING TSM 29-13-00-810-802-A, IT WAS DETERMINED
- [SDR RJEF20160118001](https://openairdocs.org/sdr/RJEF20160118001.md): Warning System · false activation · Jan 16, 2016 · N498TA · Airbus A320233 · Pitot/Static Anti-Ice System
  > DURING PUSHBACK OF FLIGHT TA561, AT ENG STARTING THE PILOT REPORTED, ECAM WARNING ANTI-ICE FIRST OFFICER & STANDBY PITOT, DUE THAT SITUATION THE ACFT RETURNED TO THE GATE. PERSONNEL PERFORMED FAULT ANALYSIS IAW TSM 30-31-00-810-812-A, TESTED THE FIRST OFFICER
- [SDR RJEF20151105001](https://openairdocs.org/sdr/RJEF20151105001.md): Computer · malfunctioned · Nov 5, 2015 · N492TA · Airbus A320233 · Aileron Control System
  > DURING CLIMB, THE PILOT REPORTED FLIGHT CONTROL RT & LT AILERON FAULT, FLIGHT CONTROL ALTN LAW & HENCE THE ACFT WAS RETURNED, LANDING WITH NO INCIDENTS. ONCE ON GND THE ACFT, BOTH ELAC 1 & ELAC 2 WERE RESET IAW TSM 27-93-00-810-949-A. PERFORMED OPERATIONAL T
- [SDR RJEF20150928001](https://openairdocs.org/sdr/RJEF20150928001.md): Actuator · faulty · Sep 26, 2015 · N687TA · Airbus A320233 · Rudder Actuator
  > PREVIOUS TO DEPART AS FLIGHT TA561. THE ACFT SHOWED THE FOLLOWING NO DISPATCH FAILURE MSGS. FLIGHT CONTROL RUDDER TRAVEL LIMIT 2 FAULT MSG ON ECAM. FOR THIS FAILURE IT WAS PERFORMED FAULT ANALYSIS IAW TSM 22-61-00-810-804-A BY RESETTING THE FAC 2 & TESTING
- [SDR RJEF20150613001](https://openairdocs.org/sdr/RJEF20150613001.md): Control Lever · faulty · Jun 13, 2015 · N685TA · Airbus A320233 · Landing Gear Selector
  > DURING THE DESCENT OF THE ACFT FLIGHT TA-397, THE LG LGCIU 1 & 2 FAULT MSG WAS TRIGGERED ON THE ECAM DISPLAY. THEREFORE, THE ACFT WAS DIVERTED TO ITS ALTERNATE AIRPORT. THE ACFT LANDED WITH LG`S EXTENDED BY GRAVITY WITH NO INCIDENT & NO ADDITIONAL REPORTS.
- [SDR RJEF20150321001](https://openairdocs.org/sdr/RJEF20150321001.md): Actuator · leaking · Mar 21, 2015 · N499TA · Airbus A320233 · Engine Thrust Reverser
  > PRIOR TO ITS DEPARTURE, FOUND HYD LEAK FROM THE ENG 1 RT THRUST REVERSER LOCKING ACTUATOR. THE ACFT WAS HELD ON GND FOR THE ACTUATOR REPLACEMENT IAW AMM 78-32-43 PB 401 WITH NO LEAK NOR FAULT. THE ACFT WAS RETURNED TO SERVICE ONCE THE MENTIONED CORRECTIVE AC
- [SDR RJEF20141211001](https://openairdocs.org/sdr/RJEF20141211001.md): Unknown · smoke · Dec 11, 2014 · N490TA · Airbus A320233 · Air Distribution System
  > AFTER TAKEOFF, THE PILOT REPORTED SMOKE IN PAX CABIN SO THE ACFT WAS RETURNED TO AIRPORT. AFTER LANDING, THE PILOT REPORTED OVERWEIGHT LANDING 66.6 TONS. IAW TSM 05-50-00-810-831-A & CABIN ODOR OR SMOKE COS REPORTING SHEET, IT WAS FOUND BOTH A/C PACKS AS THE
- [SDR RJEF20141031001](https://openairdocs.org/sdr/RJEF20141031001.md): Engine · stalled · Oct 29, 2014 · N490TA · Airbus A320233 · Engine (Turbine/Turboprop)
  > AFTER ARRIVAL, THE PILOT REPORTED A NR 2 ENGINE STALL. PERFORMED ENG 2 FULL TROUBLESHOOTING PROCEDURE DESCRIBED ON TSM 71-00-00-810-809-A WITH NO DISCREPANCIES FOUND. THE ACFT WAS RETURNED TO SERVICE AFTER A SUCCESSFUL POWER ASSURANCE TEST.
- [SDR YENA20140918200](https://openairdocs.org/sdr/YENA20140918200.md): Engine · failed · Sep 18, 2014 · N656JB · Airbus A320232 · Engine (Turbine/Turboprop)
  > AIR RETURN TO DEPARTURE DUE TO ENGINE NR 2 FAILURE AND FIRE CLIMBING THROUGH 8000'. NR 2 ENGINE WAS R & R IAW AMM 71-00-20. ENGINE RUN OK.
- [SDR RJEF20140901001](https://openairdocs.org/sdr/RJEF20140901001.md): Elevator System · vibration · Aug 28, 2014 · N490TA · Airbus A320233 · Elevator Control System
  > DURING CLIMB, THE PILOT REPORTED STRONG FUSELAGE VIBRATION DURING CLIMB, FLIGHT LEVEL 250, AIS 320 KTS & 0.74M, DIMINISH BY LOWERING AIS 270 KTS. THE ACFT RETURNED FOR MAINTENANCE WHERE LANDED WITHOUT INCONVENIENCE. IAW TSM 05-50-00-810-801-A WAS FOUND PLA
- [SDR RJEF20140818012](https://openairdocs.org/sdr/RJEF20140818012.md): Wire Harness · faulty · Aug 15, 2014 · N682TA · Airbus A320233 · Engine Indicating System Wiring
  > DURING TAKEOFF PROCEDURES OF FLIGHT LR625 THE ACFT HAD THE FAILURE MSG ENG 1 SENSOR FAULT & AIR PACK 1 & 2 FAULT. THE TAKEOFF WAS REJECTED & THE ACFT RETURNED TO THE GATE FOR MX, THE BRAKE TEMP WAS 300°C AT BRAKE 2. THE ACFT WAS HELD ON GND & PERFORMED FAULT
- [SDR RJEF20140623007](https://openairdocs.org/sdr/RJEF20140623007.md): Thermocouple · faulty · Jun 22, 2014 · N490TA · Airbus A320233 · Engine EGT/TIT Indicating System
  > WHEN ARRIVING THE PILOT REPORTED THAT ENG 2 HAD ABNORMAL EGT INDICATION AROUND 220°C DIFFERENCE. DUE THAT REASON THE ACFT WAS HELD ON GND FOR MX. PERFORMED A FAULT ANALYSIS IAW TSM 77-20-00-810-802-B FINDING THAT THE THERMOCOUPLES OF POSITIONS B & C OF ENG 2
- [SDR RJEF20140527006](https://openairdocs.org/sdr/RJEF20140527006.md): Wire Harness · cut · May 27, 2014 · N492TA · Airbus A320233 · Landing Gear System Wiring
  > PIC REPORTED DURING TAKEOFF BRAKE RELEASE MSG APPEARS THEREFORE, THE TAKEOFF WAS ABORTED. PIC REPORTED THRUST REVERSERS WERE USED BELOW 70 KNOTS. PERFORMED TSM TASL 32-32-00810-815-A & FOUND HARNESS 2M MLG RT CUT. THE HARNESS 2M WAS REPLACED IAW AMM 32-11-43
- [SDR RJEF20140110002](https://openairdocs.org/sdr/RJEF20140110002.md): Handle · malfunctioned · Jan 9, 2014 · N490TA · Airbus A320233 · Landing Gear Selector
  > ON ARRIVAL, PILOT REPORTED THAT THE LANDING GEAR LEVER STUCK IN DOWN POSITION UNTIL 1000 FT AFTER TAKEOFF. PERFORMED A FUNCTIONAL TEST OF THE LANDING GEAR, RETRACTION & EXTENSION IAW AMM 32-31-00-720-002 OBTAINING NORMAL RESULTS. R & R LANDING GEAR CONTROL
- [SDR RJEF20140108001](https://openairdocs.org/sdr/RJEF20140108001.md): Engine · vibration · Jan 5, 2014 · N682TA · Airbus A320233 · Engine (Turbine/Turboprop)
  > DURING CLIMB, PILOT REPORTED INTERMITTENT ADVISORY OF NR 1 ENGINE HIGH N1 VIBRATION, REACHED 7.2 UNITS, N2 VIBRATION REACHED 4.2 UNITS. AN OIL ODOR DETECTED. ACFT RETURNED DEPARTURE FOR MAINTENANCE. UNEVENTFUL LANDING. BORESCOPIC INSPECTIONS TO NR 1 ENGI

Next page: https://openairdocs.org/engine/iae-v2527e-a5/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/iae-v2527e-a5/reports

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