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 CALA2016082395669Cleat · corrodedCLEAT CORRODED AT FRAME 31 BETWEEN STRINGERS 43L & 43R. INSTALLED A NEW CLEAT IAW SRM 51-42-11.SDR CALA2016082395670Cleat · damagedCLEAT HAS OUT OF ROUND HOLES AT FRAME 67, STRINGERS 23 - 27R. MANUFACTURED A NEW CLEAT IAW DWG D53480076 AND INSTALLED IAW SRM 51-42-11.SDR CALA2016082395671Stringer · corrodedCORROSION ON STRINGER 43L, FRAMES 57 - 58. INSTALLED A NEW STRINGER,SPLICE, & CLEATS IAW SRM 51-42-11.SDR CALA2016082395674Door Sill · corroded2R DOOR SILL FRAME 68 LWR AREA HAS CORROSION FRAME WEB AROUND NUTPLATE. REPAIRED AREA WITH RPR FITTING IAW SRM 53-41-12 TBL 202 PARA 5B & FIG 202. SRI 53-41-12-2-002-00 PARA 3B TBL 205.SDR AALA201608219009Flow Divider · defectiveAIRCRAFT WAS GROUNDED: RAMP REPORTED FLAMES COMING OUT OF ENGINE 1 AFTER SHUTDOWN. REPLACED NR 1 ENGINE FUEL FLOW DIVIDER VALVE IAW TSM 79-00-00-810-829 AND AMM 73-13-000-B-13. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED.SDR AALA201608199004Engine · fireNR 1 ENGINE HAS FLAMES OUT THE TAIL PIPE AFTER SHUTDOWN. MAINTENANCE INSPECTED TURBINE WEEP HOLE AND FOUND IT TO BE DRY IAW AMM 72-50-200-010A.SDR CALA2016082395673Power Supply · failedON FWD FAP HAD MESSAGE FOR EPSU FAIL FWD. ON BATTERY POWER SUPPLY HAD MESSAGE UNIT FAILED. REMOVED AND REPLACED FWD L1 DOOR EMERGENCY LIGHT POWER SUPPLY.SDR CALA2016081895652Acm · seizedAIRCRAFT DIVERED TO DUE TO SMOKE IN THE COCKPIT. CREW REPORTED LOUD NOISE AND HUM. NO DEFECTS WITH ELECTRICAL SYSTEM. FOUND NR 1 PACK SEIZED. R & R THE ACM, AND FILTERS. OPS CHECKED GOOD.SDR CALA2016081595646Shear Tie · corrodedFWD CARGO BAY AT FRAME 30 STRINGERS 41-42R SHEAR TIE IS CORRODED. REPLACED THE SHEAR TIE IAW SRM 51-42-11.SDR CALA2016081595644Skin · puncturedLEFT ELEVATOR UPPER SKIN PANEL HAS A PUNCTURE AND DISBONDED, 56 INCHES FROM INBD, 13.5 INCHES FROM TE, 1.5 INCHES IN DIAMETER. CUTOUT DAMAGE AND REMOVED MOISTURE, AND INSTALLED COMPOSITE REPAIR IAW SRM 55-21-11, PAR 5D.SDR CALA2016081595645Skin · puncturedRIGHT ELEVATOR UPPER SKIN PANEL HAS A PUNCTURE, 28 INCHES FROM INBD, .75 INCHES FROM TE. DAMAGE REMOVED AND INSTALLED WET LAYUP REPAIR IAW SRM55-21-11, PAR 5D. SRI 55-21-11, TABLE 203.SDR CALA2016080995609Circuit Board · malfunctionedNO THREE GREEN LIGHTS WHEN GEAR EXTENDED. ILLUMINATED ON SHORT FINAL CHECKED PFR, NO FAULTS NOTED. LGCIU1 PREVIOUSLY REPLACED. IAW ASM 32-61-01. REPLACED BOTH MLG CONTROL LEVER (6GA) IAW AMM 32-31-11. AND REPLACED 9LP ANNUNCIATOR LIGHT TEST AND INTERFACE BOASDR AALA201608099004Apu · leakingF/A REPORTED A CABIN ODOR THROUGH OUT ENTIRE CABIN ON ENTERING THE ACFT AT THE GATE. AIRCRAFT WAS GROUNDED. MAINTENANCE HAS DETERMINED THE APU IS THE SOURCE OF THE ODOR. MAINTENANCE REPLACED APU IAW JOB CARD 26L31049005 AND ACCOMPLISHED SATISFACTORY OPS CHECSDR CALA2016081295641Light · no testEMERGENCY LIGHT TEST FAILED. RESET CIDS 1 & 2, LIGHT TESTED OK.SDR CALA2016081295642Battery Pack · no testEMERGENCY LIGHT FAILED OPS TEST, EPSU BATTERY. RESET EPSU BATTERY, OPS TESTED OKSDR CALA2016081295643Battery Pack · inoperativeAFT LEFT EMERGENCY POWER SUPPLY BATTERY FAULT LIGHT ILLUMINATED. R & R THE BATTERY PACK IAW AMM , TESTED OKSDR AALA201608089030Solenoid Valve · faultyAIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED AT START OF TAKEOFF ROLL, RT ENGINE ACCELERATED NORMAL, LT ENGINE HUNG AT ABOUT 1.1 EPR AND NEVER ACCELERATED. THE FLIGHT CREW ABORTED THE TAKEOFF AROUND 40 KNOTS AND RETURNED TO THE GATE. MAINTENANCE PERFORMED TSMSDR CALA2016080495606Pump · failedGREEN HYDRAULIC RESERVOIR OVERHEAT ILLUMINATED FOLLOWED BY LOSS OF HYDRAULIC FLUID PRESSURE. REMOVED AND REPLACED THE NR 1 ENGINE HYD PUMP, GROUND TESTED, & LEAK CHECKED SATISFACTORYSDR YENA20160802678Solenoid Valve · failedAIR TURN BACK. CREW REPORTED RECEIVING THE FOLLOWING ECAM MESSAGE, ENGINE 1 EGT OVERLIMIT, DURING TAKEOFF CLIMB. EGT WAS AT APPROXIMATELY 660 DEGREES FOR 2 MINUTES. FOUND FAULTY 10TH STAGE BLEED VALVE. R & R 10TH STAGE BLEED VALVE AND 10TH STAGE HPC SOLENOISDR YENA20160802679Bleed Valve · failedAIR TURN BACK. CREW REPORTED RECEIVING THE FOLLOWING ECAM MESSAGE, ENGINE 1 EGT OVERLIMIT, DURING TAKEOFF CLIMB, EGT WAS AT APPROXIMATELY 660 DEGREES FOR 2 MINUTES. FOUND FAULTY 10TH STAGE BLEED VALVE. R & R 10TH STAGE BLEED VALVE AND 10TH STAGE HPC SOLENOIDSDR CALA2016080295603Pump · failedDURING CRUISE, LOSS OF GREEN HYDRAULIC SYSTEM. LOW PRESSURE PUMP OVERHEAT. R & R THE NR 1 ENGINE HYD PUMP, GROUND RUN, NO LEAKS NOTED. SERVICED TO FULL. NOT OVERHEAT INDICATIONSSDR YENA20160801680Engine · failedEMERGENCY DECLARED, AIR RETURN TO DEPARTURE. CREW PERFORMED A RETURN TO FIELD AFTER ENGINE 2 EXPERIENCED POSSIBLE COMPRESSOR STALL. REPORTED SEVERAL AUDIBLE STALLS ON TAKEOFF FOLLOWED BY VIBRATION AND BURNED RUBBER/METALLIC ODOR IN THE CABIN. ACFT LANDING WASSDR CALA2016072895587Landing Gear · malfunctionedLANDING GEAR INDICATION RIGHT MAIN NOT DOWN AND LOCKED. GO AROUND AFTER WHILE DOWNLOCK OK. GROUND SCAN OF BOTH LGCIUS AND ALSO TESTS OF LGCIU. NO FAULTS DETECTED. BITE CHECKED WITH MCDU TO ENSURE GEAR NOT DOWN FOR LANDING WARNING OPERATIVE TEST OK.SDR GTIA2016072401521Seal · leakingFUMES COMING FROM PACKS ON GROUND WITH APU BLEED ON. T/S PER TSM 05-50-00-810-831-A, TSM 49-00-00-810-921-A AND TSM 71-00-00-810-801-A. NO OIL LEAKAGE FOUND ON APU & DUCTING, FOUND NR 1 ENGINE DEOILER LEAKING. R/R DEOILER SEAL IAW AMM 72-60-30. LEAK CK GOOD. RSDR CALA2016072295574Power Supply · inoperativeEMERGENCY LIGHTS TEST FAILED ,(UNIT 12WL) FAULTING. REPLACED POWER SUPPLY UNIT 12WL, OPS CHECKED GOOD PER AMM 33-51-38-400-002-ASDR CALA2016072195571Control Valve · failedLEVEL CRUISE FLIGHT AT FL360, HYD RESERVOIR LOW LEVEL ECAM DISPLAYED. SECURED THE HYD SYSTEM, DECLARED EMERGENCY AND DIVERTED. R & R THE NR 2 THRUST REVERSER HYDRAULIC CONTROL VALVE AND ENGINE HYDRAULIC PUMP. CHANGED CASE DRAIN FILTER WITH NO DEBRI NOTEDSDR CALA2016072295577Fitting · leakingGREEN SYS HYD LOSS DURING CLIMB, QTY TO ZERO, NO PRESSURE, EMERGENCY DECLARED FOUND HYDRAULIC FITTING LEAKING AT GREEN ACCUMULATOR DDP POSITION, R & R ACCUMULATOR, LEAK CHECKED OKSDR CALA2016071895566Bracket · damagedISP BRACKET ON LEFT SIDE BETWEEN FRAMES 28 AND 29 HAS A MISDRILLED HOLE, 13" AFT OF FRAME 28. STRINGER 22 - 23L. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-00-13 FIG 202 (SHEET 2) PG 227. T.SDR CALA2016071895565Oxygen Mask · unwanted deployPASSENGER OXYGEN MASK DROPPED AT SEAT 36 ABC. INSPECTION OXYGEN CONTAINER ASSEMBLY AND REPACKED THE MASKSSDR CALA2016071195559Pin · damagedENGINE THRUST LEVER DISAGREE ECAM DISPLAYED. REPLACED PINS ON J1 CONNECTOR. PIGGY BACK WIRES J7 AT EEC TO FIREWALL CONNECTOR 407VC1.SDR CALA2016070895524Power Supply · inoperativeEMERGENCY LIGHTS INOPERATIVE AT ROWS 11, 12, 20 A ND 21. REPLACED THE POWER SUPPLY UNIT 12WL IAW AMM 33-51-39 PG 401, OPS CHECKED NORMAL.SDR CALA2016070895525Hydraulic System · low pressure100KT ABORTED TAKEOFF DUE TO B SYS LOW PRESSURE ECAM WARNING AT FLT PHASE 3. DRAINED BLUE HYD SYS, SERVICED BLUE SYS. RAN FOR 20 MIN AND REPORTED NO LEAKS WITH PRESSURE & QTY GOODSDR CALA2016070195498Skin · crackedFUSELAGE BUTT JOINT AREA AT FRAME 35 STINGER 30L CRACKED. REPAIRED IAW ECRA 5330-05742 REV- PART 1.SDR CALA2016070895503Keelbeam · damagedWHILE ACCOMPLISHING FCD 5330-05575 REV.B, THE L11 HOLE THROUGH THE KEEL BEAM SIDE WALL STRUCTURAL LAYERS WAS FOUND DAMAGED. REPAIRED IAW ECRA 5330-05745.SDR CALA2016070895504Stringer · corrodedSTRINGER 41L CORRODED IN AFT CARGO BETWEEN FRAMES 52 AND 53. REMOVED CORROSION AND REPAIRED THE STRINGER IAW SRM 53-00-13 PARA 4B FIG 202 SHEET 5.SDR CALA2016070195502Pump · leakingGREEN RESERVOIR LOW LEVEL TO NEAR ZERO DISPLAYED ON ECAM. FOUND NR 1 HYDRAULIC PUMP LEAKING, REPLACED PUMP, OPS GOODSDR SOKF20160704004Valve · damagedDURING TAKE OFF FL 803, THE AIRCRAFT REJECTED TAKE OFF DUE NR 2 ENGINE COMPRESOR VANE MAINTENANCE REQUIERED AS PER TSM 75-30-00-810-853-A AND TSM 75-30-00-810-844-A PERFORMED REMOVAL AND REPLACED VSV ACTUATOR (4022KS) IAW AMM 75-32-41-00-010-A AND AMM 75-32-4SDR CALA2016070195491Tire · vibrationNOSE GEAR HAS STRONG VIBRATION ON ROTATION AND RETRACTION :REPLACED BOTH NOSE TIRES IAW AMM 32-41-12-400-001-A.SDR CALA2016070195495Stringer Splice · corrodedFWD CARGO STRINGER 43L SPLICE JUST FWD OF FRAME 31 HAS CORROSION REMOVED THE STRINGER SPLICE AND FOUND DEFECTS AFTER REMOVING CORROSION, RECEIVED NEW STRNGR SPLICE AND INSTALLED IAW SRM 51-42-11.SDR CALA2016070195490Door Sill · corrodedAFT CABIN R2 DOOR SILL CORRODED AT FRAME 68. FOUND OUT OF LIMITS SRM 53-41-14. R & R THE R2 DOOR SILL & ATTACHING PARTS IAW SRM 51-72-11.SDR CALA2016070195494Stringer Splice · corrodedFWD CARGO BAY, STRINGER 41L SPLICE JUST FWD OF FRAME 31 HAS CORROSION REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11.SDR CALA2016081195626Battery Pack · no testEMERGENCY LIGHT TEST FAILED WITH EPSU BATTERY FWD LEFT FAULT. REPLACED EPSU BATTERY, OPS CHECKED NORMAL.SDR CALA2016062895488Cleat · corrodedCLEAT AT FRAME 33, IN FORWARD BETWEEN STR 43R, HAS CORROSION. R & R CLEAT AT FRAME 33, STR 43L IAW SRM 51-42-11.SDR CALA2016081195638Light · malfunctionedRIGHT WING EMERGENCY LIGHT CAME ON DURING LANDING RESET CIDS, LIGHTS CHECKED GOOD.SDR CALA2016081195634Slide · no testCIDS CABIN CHECK, FAULTS LEFT AFT EXT LOADS REPLACED THE LEFT AFT SLIDE PACKSDR CALA2016081195636Power Supply · no testEPSU UNIT FWD LT MESSAGE 10WL DURING TEST. REPLACED FWD LEFT EPSU IAW AMM. OPS CHECKED NORMALSDR CALA2016081195635Module · no testLEFT AFT EMERGENCY LIGHT MODULE FAULT RESET THE MODULE, OPS CHECKED GOODSDR RJEF20160621001Probe · faultyDURING TAKEOFF OF FLIGHT, THE ACFT LOST THE AIR SPEED INDICATION ON CAPTAIN´S SIDE, THE TAKEOFF WAS ABORTED AND RETURNED TO THE GATE FOR MAINTENANCE. NO AIR SPEED INDICATION ON CAP SIDE, RTO, BRAKE TEMPERATURE 420 DEGREES C". MAINTENANCE PERSONNEL PERFORMED SDR CALA2016062295470Cleat · corrodedFRAME CLEAT AT FRAME 67, STR 23R-26R HAS SEVERAL OUT OF ROUND HOLES AT DOOR SILL ATTACH POINT. REMOVED FRAME 67 CLEAT AT STR 23-24R OUTER ROUND HOLES FAB CLEAT IAW SRM 53-41-12.SDR CALA2016062295471Frame · damagedFRAME SECTION AT FRAME 67, STR 23R-30R HAS SEVERAL OUT OF ROUND HOLES AT DOOR SILL ATTACH POINT. REMOVED FRAME SECT AT FRAME 67, OUTER ROUND HOLES NEW FRAME LOCATED DRILLED AND INSTALLED.
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