IAE V2522-A5
Service difficulty reports · 3,464
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 = 'V2522A5' 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 = 'V2522A5' 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 CALA2013110892759Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN, F CTL. ELAC 2 FAULT HAPPEN WHEN AUTOPILOT ENGAGED RESETS WITH AP OFF BUT FAULTS AGAIN W AP PROG TEXT. ACCOMPLISHED CHRONIC REVIEW. R & R ELAC 2 COMPUTER IAW AMM 27-93-34-400-001 OPERATIONS CHECKED GOOD. UNABLE TSDR CALA2013110892761Liner · looseNR 2 ENG INBD TR INNER LINER. ACCOMPLISH INSPECTION OR RECHECK REQUIRED. WHEN COMPLETE, SIGN OFF THIS MF ITEM ONLY, DO NOT SIGN OFF. NR 2 ENG INBD TR INNER LINER HAS WIRE MESH COMING LOOSE. APPLIED SPEED TO TR INNER SLEEVE 9 TO 6 O'CLOCK POSITION.SDR CALA2013110892763Jumper · installedEMERGENCY LIGHT CHECK TEST FAILS, FAULT CODE, EPSU EXIT LOAD FWD LT ATA 33-51-38. SUSPECT MED 1L SLIDE NEEDS REPLACEMENT. INSTALLED NEW EPSU 565-6758, NO HELP. MED SLIDE PCN 649-9130. INSTALLED JUMPER AT DOOR 1L SLIDE IAW MT33-001 & TEST PASSED.SDR CALA2013111292877Wire · failedEMERGENCY LIGHT CHECK TEST FAILED. INSTALLED JUMPER AT DOOR 1L SLIDE IAW MT33-001 & TEST PASSED. REPLACED SLIDE IAW AMM 25 62-44-400 FOR NR 1L MED. OPS CHECKED GOOD.SDR CALA2013110892760Control Panel · failedUNABLE TO DESELECT VHF 2 AUDIO ON FIRST OFFICER`S SIDE. R & R FIRST OFFICER`S AUDIO CONTROL PANEL.SDR CALA2013110792704Battery · faultyEMERGENCY LIGHT TEST SHOWS 'EPSU BATTERY EMER L' PER 2SVC. REPLACED BATTERY IAW AMM, TESTED NORMAL.SDR CALA2013110792728Tail Cone · crackedCRACK ON TOP OF RT ENG TAIL CONE. CRACK MEASURES 3.75" & RUNS LENGTHWISE ADJACENT TO PREVIOUS WELD. ACCEPTABLE AS IS WITHOUT REPAIR IAW V2500 SRM 54-40.SDR CALA2013110892762Relay · faultyENG 1 REV ISOLATION FAULT ECAM ON LANDING ROLLOUT AFTER THROTTLE WAS BACK TO FWD IDLE. HAD ECAM MSG "ENG 1 REV ISOL FAULT" 77-11-00 WITH CFDS MSG "TR SOV-HCU-EEC1" 78-37-00. TROUBLE SHOT IAW TSM 78-37-00-810-809-A 13, PER STEP 4A2 PG. 2. REPLACED THRUST RESDR CALA2013110692700Proximity Sensor · dirtyDOOR 2R SHOWING DISARMED WITH HANDLE IN ARMED & FLASHING RED CABIN PRESSURE LIGHT. CLEANED DOOR 2R PROX SENSOR & CHECKED DOOR OPERATION OF CABIN OVERPRESSURE WARNING SYS IAW MT52-008 & ALL INDICATIONS NORMAL.SDR CALA2013111492914Linkage · excess playNOSE GEAR TARGET 24 GA LINKAGE HAS EXCESSIVE PLAY CAUSING TARGET POSITION TO BE OUT OF RANGE. REMOVED TARGET LINKAGE & SUPPORT, REPLACED LINK & SUPPORT ASSEMBLY FULL GEAR SWING, NORMAL OPERATION.SDR CALA2013110592668Support · defectiveGEAR NOT UP LOCKED DISPLAYED ON UPPER ECAM SCREEN. GEAR DID NOT COME UP 1ST ATTEMPT. NOT JUST AN INDICATION PROBLEM, RECYCLED + UP 2ND TIME. ACCOMPLISH CHRONIC REVIEW. CFDS FAULTING 24GA TGT POSITION IAW TSM 32-31-00-810-842 -A, 24GA PCN 565-1759. REPLACEDSDR CALA2013110592685Unknown · odorELECTRICAL BURNING SMELL ROW 30 & AFT. INSPECTED AC IN & NEAR ROW 30 & AFT. CHECKED GALLEY OVEN, COFFEE MAKERS, CABIN LIGHTING, & PAX ENTERTAINMENT SYSTEM RAN APU WITH BOTH PACKS IAW TSM 24-00-00-810-823A. NO FAULTS NOTED.SDR CALA2013110592686Actuator · leakingDRIPPING OIL UNDER NR 1 ENG. NR 1 ENG THRUST REVERSER OTBD ENG COWL OPENING ACTUATOR LEAKING. APPEARS CASE IS CRACKED ON OTBD END AT BASE OF ATTACH POINT. REQUIRES ACTUATOR PCN 644-010 5 IAW IPC 78-36-51-80A NR 70. PLACED ON DF IAW MEL 2522EZ.SDR CALA2013110692697Receptacle · shortedLGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN L G, CAME ON DURING CLIMB. CFDS ATA 323171 LGCIU1 05GA1 ID LGCIU TSM32-31-00-810-802-A O5GA1 565-9032. LGCUI 1 FAULTED 20GA PROX SENSOR. IAW ASM 32-31-03, CHECKED WIRING FROM LGCIU 1 BENCH PLUG TO 20GA PROX SENSOSDR CALA2013110892758Thrust Reverser · damagedNR 1 ENG REVERSER, INBOARD C DUCT, SEAL BETWEEN THE TRANSLATING SLEEVE & THE LOWER BIFURCATION FOUND PARTLY DELAMINATED. FIBERGLASS OUTER SECTION HAS SEPARATED FROM THE RED INNER CORE, OUTER SECTION IS GONE. INNER SECTION IS STILL ATTACHED TO THE REVERSER & SDR CALA2013110192570Power Supply · failedCABIN EMERGENCY LIGHT SYSTEM FAILED SELF-TEST. REPLACED LT OVERWING EXIT EPSU & BATTERY IAW MM, EMERGENCY LIGHT TESTED, NOW PASSES.SDR CALA2013110492634Display · faultyCAPTAIN`S PFD BLANK. REPLACED CAPTAIN`S PFD & TESTED OK IAW AMM.SDR CALA2013102992486Unknown · odorHEAVY MUSTY, ACRID & MOLDY SMELL FROM AC SYSTEM IN LOW & HIGH FLOW.SDR CALA2013103092529Switch · damagedWX RADAR SWITCH DAMAGED. REPLACED PANEL GRD CHECKED GOOD BY LAXMM.SDR CALA2013110192569Warning System · activatedBCL 1 FAULT DISPLAYED ON UPPER ECAM SCREEN, ELECTRICAL. CAME ON 15 MIN AFTER PUSH BACK ITEM ROLLED FORWARD. CFDS REPORTS ELECTRICAL BCL 1 FAULT & PREVIOUS REPORT HIT FUSE 4PB11 PCN 562-3969 & FOLLOW TSM 24-38-00-810-807. R & R BATTERY SHUNT 3PB1 IAW AMM 2SDR CALA2013103092530Contactor · failedBEFORE PUSHBACK BCL 1 FAULT. REPLACED CONTACTOR IAW MM 24-38-55-000-001-A. MESSAGE CLEARED, BCL CFDS TEST PASSED.SDR CALA2013102992452Liner · damagedNR 1 ENG FAN CASE ATTRITION LINER HAS A HOLE & CRACK AT THE 6 O'CLOCK POSITION. DAMAGE AREA MEASURES APPROXIMATELY 3" X 3" & IS LESS THAN 20% OF THE PANEL. REPAIRED NR 1 ENG FAN CASE ATTRITION LINER IAW MT 72-017.SDR CALA2013102992485Tube · leakingAPU OIL TUBE LEAKING 5 DROPS PER MINUTE. ITEM 60 IS THE TUBE THAT IS LEAKING. REPLACED TUBE IAW IPC 49-21- 04-51A. LEAK CHECKED GOOD, CLEANED EFFECTED AREAS IN APU COMPARTMENT.SDR CALA2013102992502Outflow Valve · faultyFLT DIVERTED, DURING TAKEOFF AT 110 KNOTS RECEIVED VENT SKIN VLV FAULT MESSAGE, FOLLOWED BY UNABLE TO PRESSURIZE AIRCRAFT DURING CLIMB, DIVERTED TO LAX. REPLACED THE SKIN AIR OUTLET VLV IAW AMM & THE SKIN AIR INLET VLV IAW AMM 21-26-52-000-001-A. REPLACED THSDR CALA2013103092532Hydraulic Line · leakingFLUID LEAKING FROM LT MAIN WW, 6 DROPS EVERY 5 SECONDS. HYD LINE BETWEEN NR 2 & NR 8 RIB LT WING SEE IPC 29-11-05-03D ITEM 115. REPLACED LINE, LEAK CHECKED OKAY.SDR CALA2013102992469Starter · failedAPU AUTO SHUTDOWN AT GATE, UNABLE TO START. REPLACED APU STARTER MOTOR & STARTER MOTOR CLUTCH, OPERATIONS CHECKED GOOD.SDR CALA2013102992468Transceiver · faultyVHF 1 RECEIVE BUT NO TRANSMIT. R & R NR 1 VHF TRANSCEIVER IAW AMM 23-12-33. OPERATIONS CHECKED NORMAL. OK TO CONTINUESDR CALA2013102892410Computer · inoperativeRT OUTER WING FUEL TEMPERATURE INDICATION INOPERATIVE. REPLACED FQIC.SDR CALA2013102892412Sill · corrodedR2 DOOR SILL CORRODED AT FR 68. RII INSP ACP.SDR CALA2013102892413Rudder · dentedRT SIDE OF RUDDER HAS DENT-DELAMINATION 47" FROM THE BOTTOM & 20.5" FROM THE TE. CUTOUT DENTED & DELAMINATION AREA, REMOVED HONEYCOMB CORE FULL DEPTH, PREPPED, CLEANED, BONDED HONEYCOMB. APPLIED REPAIR & RESTORED FINISH IAW SRM 51-77-11, AIRBUS TD-G2-S2-0055SDR CALA2013102892411Line · leakingOIL ODOR IN CABIN. ON ARRIVAL, NOTICED STREAM OF SMOKE COMING FROM REAR TURBINE SECTION OF APU, FOUND OIL LINE AT 11 O'CLOCK POSITION AFT LEAKING. FWD LOOSE AT FITTING, OIL DRIPPING TO TURBINE CASE. SECURED FITTING, CLEANED EXCESS OIL, RAN APU FOR 30 MINUTSDR CALA2013102592389Cylinder · crackedONE RT MED DAMPER CYLINDER STRIKER ASSEMBLY IS CRACKED AT ATTACH FLANGE. GENERATED C-CHECK WU M7739I. REPLACED CYLINDER ON WU M7739I.SDR CALA2013102892444Wire · damagedENG 2 NO OIL PRESSURE INDICATION. AMBER CROSSES ON ECAM ENG 2. W-D 71-51-05, REPAIRED WIRE ST033W20 IAW GPM 2-0-15, IAW DF208.SDR CALA2013102492358Computer · faultyELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN, CAME UP DURING FLAP RETRACTION FROM 1 TO 0 AFTER TAKEOFF. REPLACED ELAC 2, OPERATIONS TESTED GOOD, AFS TESTED GOOD & AUTO LAND TESTED GOOD.SDR CALA2013102592382Transmitter · faultyREVERSER FAULT DISPLAYED ON UPPER ECAM SCREEN. ENG 2 FOUND OIL PRESS XMTR FAULTING. REPLACED XMTR IAW AMM. OPERATIONS & LEAK CHECKED GOOD NO FAULTS NOTED.SDR CALA2013102292252Screw · missingTWO SCREWS MISSING ON RT SIDE VERTICAL STABILIZER. THREE EACH SCREWS MISSING ON RT SIDE VERTICAL STABILIZER PANEL 323AR. INSTALLED ONE EACH SCREW, REMAINING TWO ARE MISSING RECEPTACLES. REPLACED TWO EACH MISSING FASTENERS AT AFT END OF PANEL 323AR.SDR CALA2013102292273Actuator · faultyPACK 2 RAM AIR FAULTS. DUE TO REPEAT FAULTS ON AHM FOR PACK 2 RAM AIR OUTLET ACTUATOR. R & R THE PACK 2 RAM AIR OUTLET ACTUATOR FIN 29HH IAW AMM 21-61-52 PB401. IAW IPC 21-61-03-13A PCN 565-9028. TEMP CONTROL SYSTEM OPERATIONS CHECKED GOOD.SDR CALA2013102292274Oxygen Mask · scratchedCOCKPIT 4TH OCCUPANT OXYGEN MASK LENS IS SCRATCHED. REPLACED ON WU B9223T.SDR CALA2013102392322Warning System · activatedFUEL HEAT SYSTEM DISPLAYED ON UPPER ECAM SCREEN. FUEL RETURN VLV OPEN. ENG 1 MAINT TEXT IAW TSM 73-00-00-810-809B FADEC FLIGHT DATA SHOWS FAULT CODE SPVFO IN FADEC 1A. FAULT CONFIRMATION REQUIRES HIGH POWER ASSURANCE TEST TO SEE IF THE FAULT IS PRESENT. IASDR CALA2013102392323Spring · distortedRT NLG DOWNLOCK SPRING DISTORTED AT LOWER FITTING. REPLACED SPRING.SDR CALA2013102192235Fdu · faultyAPU WILL SHUT DOWN WHEN DOING A FIRE TEST. DEF IAW MEL 4910B APU CB PULLED & LOCKED. REPLACED APU DIRE DETECTOR UNIT IAW AMM & PERFORMED APU FIRE & OVERHEAT DETECTION SYSTEM IAW AMM, NOW ALL OKAY.SDR CALA2013101892185Pump · overheatedHYD B ELEC PUMP OVERHEATED AT CRUISE. REPLACED BLUE ELEC HYD PUMP IAW AMM, OPERATIONS TESTED NORMAL.SDR CALA2013102192204Wire · brokenLGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. AIRMAN SHOWS CFDS MESSAGE RT LG DOOR CLOSED PROX SNSR 26GA". REPLACE SENSOR 26GA PCN 565-1759 IAW AMM 32-31-73 PB401. TROUBLE SHOT IAW TSM 32-31-00-810-8 19-A FOUND WIRE BROKEN GOING TO PROX SENSOR 26GA CP. REPASDR CALA2013101892181Uplock Sensor · faultedCREW REPORTED LGCIU 1 FAULT. FOUND NLG DOWN LOCK SENSOR 18GA AT FAULT. R & R SENSOR 18GA & LGCIU 1 IAW AMM 32-31-73,32-31-71. ALSO FOUND INTERMITTENT SHORT A ON 1300VC & B ON SENSOR. REMOVED 1300VC & CLEANED OUT CONNECTOR, NO SHORT. WIRES CHECKED GOOD FROSDR CALA2013101892180Concentrator · faultyRT WINDOW DISPLAYED ON UPPER ECAM SCREEN. ANTI ICE REPLACED NR 2 WINDOW HEAT COMPUTER. FAULTS CLEARED & OPERATIONS CHECKED GOOD. WINDOW HEAT COMPUTER NR 2 R & R PART FROM IAD.SDR CALA2013101892183Tire · unbalancedEXTREME VIBRATION FROM NOSE WHEEL AT ROTATION ON TAKEOFF ROLL. WHEELS 110-0010 TWO EACH, ACCOMPLISHED CHECKS OF NLG IAW TSM 32-20-00-810-802-A, TIRE PRESSURES WERE FOUND MISMATCHED, L-240 PSI R-190 PSI BALANCED PRESSURES & COMPLETED CHECKS WITH NO DEFECTS NOTSDR CALA2013102192203Interface Unit · malfunctionedREF LOG 1 FOR THE CLUNKING NOISE & VIBRATION, CREW REPORTS AT THAT TIME BRIEFLY HAD A UNUSUAL ODOR IN THE FLT DECK & ALSO REPORTED SMELLING IN THE CABIN. THE ODOR DISSIPATED QUICKLY. BOTH LGCIUS WERE REPLACED, NO OTHER ACTION NECESSARY IAW MM 05-51-10.SDR CALA2013102292275Oxygen Mask · missingO2 ABOVE 34 DEF MISSING MASK. REPLACED MISSING MASK.SDR CALA2013101792154Warning System · activatedFLT CTL AILERON SERVO FAULT. R G AIL SERVO AMBER ON FLT CTL PAGE. ALSO HAD MOMENTARY FLT CTL ELAC 1 FAULT. RESET, NO HELP. DEFERRED IAW MEL 2714R. R H GREEN AIL SERVO CONNECTOR 33CE2 HAS BEEN DISCONNECTED & STOWED.SDR CALA2013101592081Display · faultyCAPTS LT PFD SCREEN IS BLURRY, EVEN SWITCHING DISPLAY THE LT SCREEN IS FUZZY. R & R LOWER ECAM DU IAW TASK 31-63-22, OPERATIONS CHECKED GOOD. ALSO PERFORMED TASK 2 4-25-00-710-001-A ESS-GEN SWITCHING TESTED GOOD.
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