IAE V2527-A5
Service difficulty reports · 8,009
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 CALA2013111893026Reservoir · faultyHYDRAULIC SYSTEMS G, B & Y WILL NOT PRESSURIZE WITH APU. APU WITH BLEED ON IN BOOST MODE WITH PACKS ON OR OFF NO PRESSURIZATION. SYSTEMS PRESSURIZE NORMAL WITH NR 1 ENGINE BLEED. REPLACED RESERVOIR PRESSURIZATION UNIT IAW MM, OPERATIONS CHECKED & LEAK CHECKSDR CALA2013111993053Igniter · faultyAPU FAILED TO START AFTER LANDING. FOUND NO FLAME ON CFDS. REPLACED IGNITER PLUGS IAW AMM 49-41-41. ACCOMPLISHED OPERATION TEST OF APU IAW AMM 49-00-00, TESTED OK.SDR CALA2013111893025Structure · scratchedR2 DOOR SCRATCHED AT BOTTOM EDGE 11 INCHES AFT OF FWD EDGE, 1 1/2 INCHES WIDE BY 1 INCH TALL SCRATCH GOES INTO THE METAL. INSPECTED AREA IAW SRM 52-10-00 PG 104. FOUND WITHIN LIMITS.SDR CALA2013111892983Rod End · shearedL1 DOOR TELESCOPIC ARM ROD SHEARED. REMOVED & INSTALLED NEW ROD END ASSEMBLY ON L1 DOOR IAW MM.SDR CALA2013111893000Actuator · faultyHARD FAULT AUTO FLT RUDDER TRIM 2 FAULT. HISTORY SHOWS FAC 2 & RUDDER TRIM ACTUATOR REPLACED IAW TSM 22-62-00-810-810. REPLACED 7CC2 RELAY, ACCOMPLISHED AFS TEST, ALL PASSED, NO FAULTS NOTED.SDR CALA2013111893003Sliding Window · delaminated2 INCH DIAMETER DELAMINATION BUBBLE CAPTAIN'S SLIDING WINDOW BETWEEN PANES. DELAMINATION LOCATED FWD EDGE OF WINDOW, HALF WAY FROM THE TOP, 2" INCH DIAMETER STARTING FROM THE EDGE. CARRIED FWD IAW AMM 56-12-11, WITHIN LIMITS IAW AMM.SDR CALA2013112093101Check Valve · leakingFUEL DRIPPING FROM RT WING. REPLACED RT WING SURGE TANK DRAIN VLV. AFTER REPLACING WATER DRAIN VLV SURGE TANK STILL FILLING WITH FUEL THROUGH SCAVENGE JET PUMP SUCTION LINE. CHECK VLV AT RIB 22 LEAKING, REPLACED CHECK VLV, CHECKED GOOD.SDR CALA2013111492922Controller · faultyRT WINDOW DISPLAYED ON UPPER ECAM SCREEN, ANTI-ICE. REPLACED RT WHC 2DG2 IAW AMM, OPERATIONS CHECKED OKAY.SDR CALA2013111592952Structure · corrodedAFT CARGO COMPARTMENT FRAME 59-61 STRINGER 38-40 PREVIOUS REPAIR SPLICE DOUBLER & RIVETS HAS CORROSION. REMOVED, FABRICATED & INSTALLED SPLICE IAW SRM 53-00-13, FIG 201, PG 209-210.SDR CALA2013111592953Sill · gougedMED R1 DOOR SILL IS GOUGED AROUND FASTENER HOLES FOR AFT GIRT BAR FITTING. REMOVED CORROSION FROM AREA AT MED R1 DOOR SILL BOLT HOLES IAW SRM 53-11-14 FIG 108. ACCOMPLISHED HFEC ON BLENDED AREA IAW NTM 51-10-08 PB 6, THICKNESS TEST IAW NTM 51-10-04 PB 4 & ABSDR CALA2013111592954Sill · corrodedMED L1 DOOR SILL HAS CORROSION AROUND FWD GIRT BAR FITTING FWD 2 FASTENERS. REMOVED CORROSION FROM AREA AT MED L1 DOOR SILL FASTENERS IAW SRM 53-11-14 FIG 108. ACCOMPLISHED HFEC ON BLENDED AREA IAW NTM 51-10-08 PB 6, THICKNESS TEST IAW NTM 51-10-04 PB 4 & ABSDR CALA2013111592960Light · defectiveRT WING NAV 2 POSITION LIGHT BLINKING BLUE INDICATOR NEOL. REPLACED LAMP ASSEMBLY 565-1601 NR 2 POSITION RT.SDR CALA2013111592961Bolt · looseREFUELING POINT RT WING LEAKS AROUND AIRCRAFT SEAL WHEN REFUELING. TORQUED COUPLING BOLTS IAW MT28- 0 05, NO LEAKS.SDR CALA2013111592963Centering Cam · out of adjustAIRCRAFT PULLING TO THE RT DURING TAXI. NULL FEEDBACK SENSORS 3GC & 4GC IAW AMM 32-51-00- 820-002-A02. ADJUSTMENT OF NWS ZERO POSITION, NLG CENTERING CAMS WILL REQUIRE JACKING OF NOSE. REQUIRED 18 UNITS OF TRIM OR MORE THAN HALF PEDAL DEFLECTION TO TRACK STSDR CALA2013111592964Switch · malfunctionedIAW SMC06 BLUE SYSTEM CHECK FAIL PER A-CHECK JOB CARD 4-2025 STEP 23D ITEM E4. CHECKED POWER TO SOL VLV GOOD ANOTHER VLV ON ORDER. VERIFIED SOL VLV BAD, PART COMING FROM DEN OSTF U2694. REPLACED HYD LEAK MAINTENANCE SWITCH IAW AWD29-19-01 PG 11, GND OPERATISDR CALA2013111492927Blade · nickedNR 1 ENGINE HAS A BLADE NICKED. PERFORM BORE SCOPE INSPECTION IAW AMM 72-00-00-200-017 & HPC IAW SECTION 5 OF MT72-021. ACCOMPLISHED BORE SCOPE INSPECTION IAW AMM 72-00-00-200-017 & MT72-021 WITH NO LIMITING DEFECTS NOTED.SDR CALA2013111492917Stringer · corrodedAFT CARGO COMPARTMENT FRAME 56-57, STRINGER42L HAS SURFACE CORROSION. STRINGER 42L FRAME 56-57 CORROSION IS OUT OF LIMITS. R & R STRINGER 42L & SIX EACH SHEAR TIES FRAME 53-60 IAW SRM 51-42-11. WORKED ON TIMCO NR 23259.SDR CALA2013111492921Transfer Valve · faultyLT OUTER TANK HAS 280 LB WON’T HOLD FUEL WITH VLV INDICATING CLOSE. CONFIRMED FUEL MIGRATION ON LT OUTER TANK TO INNER CELL WITH TRANSFER VLVS CLOSED. WHILE FUELING, OUTER TANK NEVER FILLED TO MAX QUANTITY & WAS OBSERVED ON ECAM DECREASING & INNER INCREASINGSDR CALA2013111492923Connector · dirtyRT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN, ANTI-ICE. CLEANED & RESET CONNECTOR ON WHC 2. OPERATIONS CHECKED GOOD.SDR CALA2013111492924Control Unit · faultyNOSE WHEEL STEERING PULLING RT & REQUIRES RUDDER TRIM TO TRACK STRAIGHT. STRAIGHT TRACKING REQUIRED RUDDER TRIM UNITS LT OR RT TO BE SET. FULL LT RUDDER REQUIRED TO KEEP NOSE STRAIGHT IAW TOMC, REPLACED BSCU IAW A320 AMM, BITE CHECKED GOOD. LAND TEST 3 PASSSDR CALA2013111492925Skin Panel · delaminatedBELLY PANEL 191BB LE OF PANEL DELAMINATING. ACCOMPLISH INSPECTION OR RECHECK REQUIRED. WHEN COMPLETE, SIGN OFF THIS MF ITEM ONLY. INTERIM REPAIR MADE IAW MT-53-002 & SRM 51-77-13 APPLIED SPEED TAPE. PERMANENT REPAIR TO BE MADE WITHIN 300 FLIGHT HRS. ACCOSDR CALA2013111492926Bolt · looseBOLT HANGING DOWN ON PACK COVER JUST FWD OF RAT.SDR CALA2013111492928Fastener · missingFASTENER MISSING PANEL 575KB, UNDER LE LT WING NEAR TIP. REPLACED FASTENER.SDR CALA2013111492929Solenoid Valve · faultyIAW A CHECK JOB CARD 4-2025. ITEM 23 RUDDER HYD ACT OPERATION CHECKED STEP E4. WHEN THE LEAK MEASURE B IS SELECTED THE B INDICATION ON ECAM STAYS GREEN & DOES NOT TURN AMBER. REPLACED SOLENOID VLV PCN 644-0070 IAW MM.SDR CALA2013111592962Connector · brokenRT WS HT COMP 2DG2 AFT CONNECTOR 2DG2 B BACKSHELL BROKEN.SDR CALA2013111392884Proximity Sensor · faultyLGCIU 1 FAULT ON UPPER ECAM LGCIU BITE FAULTS '32-31-73 L LG EXT PROX SENSOR 21GA LGCIU1 5GA1'. REPLACED LGCIU-1, NO HELP. HUNG NEW SENSOR 21GA ALL FAULTS CLEARED FOR LOG003-007. NEEDS NEW SENSOR. MRDATA TAKEN FOR NEW LGCIU-1. REPLACED L LG EXT PROX SENSOSDR CALA2013111392885Tube · leakingFLUID LEAK ON LT MLG. REPLACED TUBE ASSEMBLY, LEAK CHECKED GOOD.SDR CALA2013111392889Power Supply · failedESPU EMERGENCY FWD LT FAILED ON TEST. INSTALLED NEW ESPU FWD LT POSITION IAW AMM, TEST PASSED.SDR CALA2013111292835Mount · looseCREW REPORT ON ARRIVAL AFT FLIGHT ATTENDANT`S JUMP SEAT LOOSE AT WALL. REPLACED AFT FLIGHT ATTENDANT`S JUMP SEAT MOUNT WALL. JUMP SEAT SECURE.SDR CALA2013111292837Cover · missingDISK COVER FOR BOLT OTBD CTR FLAP PYLON MISSING NEAR R4 MAG FUEL LEVEL.SDR CALA2013111292838Sensor · faultyLGCIU 1 FAULT, FLIGHT DIVERTED. PFR SHOWS 27GA DOOR SENSOR FAULT. REPLACED SENSOR MM32-31-73-400-001-A. OPERATIONS CHECKED NORMAL.SDR CALA2013111292876Cradle · defectiveAFT HALON EXTINGUISHER CRADLE STRAP WILL NOT FASTEN CLOSED. REPLACED CRADLE.SDR CALA2013111392886Fastener · missingFASTENER NEEDS TIGHTENING JUST FWD OF THE NR 2 PACK EXHAUST. REPLACED MISSING FASTENER.SDR CALA2013111292855Fire Bottle · unserviceableFWD AFT LAVATORY FIRE EXTINGUISHER PRESSURE IN RED BAND. R & R FWD AFT LAVATORY FIRE EXTINGUISHER IAW AMM.SDR CALA2013111292836Bearing · migratedDOOR 1L DIFFICULT TO OPEN AS REPORTED BY CUSTOMER SERVICE AFTER AIRCRAFT ARRIVAL. VERIFIED CONDITION EXISTS & FOUND UPPER DOOR HINGE UPPER BEARING ASYMMETRICALLY MIGRATED OUT. INNER SIDE APPROXIMATELY 1-8TH INCH & INBD SIDE APPROXIMATELY 1-4 INCH. REPLACEDSDR CALA2013111292854Table · bindsFIRST OFFICER'S FLIGHT DECK TABLE IS BINDING. NEEDS ADJUSTMENT WHEN IN THE FULL OPEN SETTING, IT WOBBLES UP & DOWN. REPLACED ROLL PIN, OPERATIONS CHECKED GOOD.SDR CALA2013111292856Inverter · faultyIAW EQ3333 STATIC INVERTER DOES NOT TEST. REPLACED STATIC INVERTER, OPERATIONS NORMAL, TESTED NORMAL.SDR CALA2013110892764O-Ring · leakingENG 1 FUEL LEAK. REPLACED O-RINGS ON FUEL MANIFOLD TUBE ASSEMBLY. PERFORMED A LOW POWER ENG RUN ON NR 1 ENG, NO LEAKS NOTED.SDR CALA2013111292857Sill · corrodedR2 DOOR SILL CORRODED ON OTBD FLANGE AT FR 68. REPAIR ACCOMPLISHED IAW SRM53-41-14 TABLE 202, FIG 201, REPAIR PRINCIPAL 5. CAT A REPAIR NO SRI REQUIRED IAW TABLE 202.SDR CALA2013111292858Start Valve · faultyENG 1 START VLV DID NOT OPEN AT ENG START. REPLACED START VLV IAW AMM 80-13-49-400-010-B13. OPERATIONS NORMAL.SDR CALA2013110792707Valve · faultyBRAKES DRAGGING DURING TAXI, APPEARS TO BE RIGHT SIDE. HI TEMP RT .38 PERCENT THRUST REQUIRED TO TAXI. SYSTEM PRESSURE WAS BLEEDING THRU GREEN SYSTEM TO YELLOW THRU THE AUTO SELECTOR VLV. REPLACED VLV & AIRCRAFT CHECKED NORMAL.SDR CALA2013110792719Unknown · faultyLT MLG UNSAFE SUSPECT PRIORITY VLV AT PTU. REPLACED PRIORITY VLV ASSEMBLY IAW AMM 29-11-33-000-001-A, NO HELP. LT MLG STILL SLOW TO FULL DOWN & LOCK.SDR CALA2013110792723Rivet · missingTHREE RIVETS MISSING ENG 2 TAIL CONE LOWER VERTICAL SUPPORT UPPER FLARED SHEET METAL 2 ON LT, 1 ON RT. RIVETS MISSING AT 6 O’CLOCK POSITION LOWER STRUT FAIRING WILL REQUIRE RECHECK.SDR CALA2013110892736Indication Sys · activated"FUL DIV RET VLV-HC-EEC1" FAULT CODE "SPVFO"SDR CALA2013110892741Structure · dentedDENT IN LT LOWER AFT CARGO DOOR. DENT IS 3 IN. AFT EDGE 3 IN FROM BOTTOM, DENT IS 1IN X .5IN DEEP .004. VISUALLY INSPECTED NO CRACKS FOUND. OK TO CONTINUE.SDR CALA2013110692693Light · intermittentLT LG LIGHT IS INTERMITTENT. IND ON ECAM OPERATIONS NORMAL.SDR CALA2013110792706Gauge · brokenCREW O2 SHOWS 1090 PSI, O2 BOTTLE PRESSURE GAUGE BROKEN. REPLACED O2 BOTTLE IAW AMM 35-11-41-000-001-A & AMM 35 -11-41-400-001-A. PERFORMED OPERATIONAL TEST OF CREW OXYGEN DISTRIBUTION IAW AMM 35-12-00-700-001-A, OK CHECKED GOOD, NO LEAKS NOTED.SDR CALA2013110792721Computer · malfunctionedRT WINDSHIELD HEAT ECAM DISPLAY. REPLACE WINDOW HEAT COMPUTER NR 2, PCN 565-9018 IAW AMM. REPLACED WINDOW HEAT CONTROLLER, CHECKED GOOD.SDR CALA2013110792722Solenoid · faultySLAT SYS 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F -CTL REPLACED THE EXTEND SOLENOID ON 25CV POWER CONTROL UNIT REF AMM. PERFORMED OPS CHECKS PER AMM 27-84-00-710. NO DEFECTS OR LEAKS NOTED. SYSTEM CHECKS OKSDR CALA2013110892735Indication Sys · activatedGEAR UNSAFE INDICATION.
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