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 CALA2013112693264Rivet · shearedPYLON BLOWOUT PANEL HAS POPPED NR 1 ENG OTBD SIDE. PERFORMED FIM TASK INSPECTION IAW TSM 36-14-00-810-801A. SHEAR RIVETS ON DOOR BROKEN, NO OTHER PROBLEMS FOUND, NO HISTORY. INSTALLED ROBBED DOOR FROM HANGAR AIRCRAFT.SDR CALA2013112593215Director · faultySLIDE AT DOOR 2R INDICATES ARMED FROM FLIGHT DECK. FLIGHT ATTENDANT REPORTS SLIDE DISARMED. REPLACED CIDS DIRECTOR 1. CABIN INTERCOM, CIDS DIRECTOR BITE TESTED GOOD, SMOKE DETECTOR FUNCTION TESTED GOOD, OPERATIONS 2R DOOR THRU ARM, DISARMED POSITIONS, INDICSDR CALA2013112593229Stringer · corrodedAFT PIT STRINGER 40R WAS FOUND CORRODED BETWEEN FRAME 60 & 61. REPLACED STRINGER FROM FRAME 58 - 61, SPLICE IS AT FRAME 60 - 6. WORK ACCOMPLISHED IAW SRM 53-00-13 PARA 4A, TBL 201, FIG 201 & SRM 51-44-11.SDR CALA2013112593230Structure · dentedIAW INBD CF9010. FUSELAGE DENT BETWEEN FRAME 12 - 13 JUST BELOW FLOOR LINE IS OUT OF LIMITS ON LT SIDE. INSTALLED DOUBLER REPAIR IAW SRM 53-00-11 FIG 240 PRINCIPLE NR 2.SDR CALA2013112593236Life Vest · missingNEED FOUR SINGLE CHAMBER DEMO LIFE VEST. REPLACED THREE DOUBLE CHAMBER DEMO LIFE VEST. ONE DOUBLE CHAMBER DEMO LIFE VEST NEED TO BE REPLACED. INSTALLED MISSING LIFE VEST.SDR CALA2013112593240Actuator · faultyFLIGHT CONTROL ELAC 2 PITCH FAULT CAME ON IMMEDIATELY AFTER TAKEOFF. TESTED IAW MM & ALL TESTED GOOD.SDR CALA2013112593243Sensor · faultyLG SYS DISAGREE. REPLACED 18GA NLG DOWN SENSOR, LGCIU 1 & 2 TESTED OK.SDR CALA2013112593245Sealant · damagedAMBIENT NOISE LEVEL TOO HIGH APPEARS TO EMANATE FROM RT WINDSHIELD LOWER QUADRANT. FOR SEALANT IAW MT 56-005, PCN 841-0098. ACCOMPLISHED APPLICATION OF SEALANT IN AREA AS DESCRIBED IN SMC01 SEQ 5272007 FOR DETAILED CORRECTIVE ACTION.SDR CALA2013112693278Structure · nickedNR 2 PYLON FWD MOUNT STRUT BOTTOM SURFACE, NICKS AROUND FASTENER HOLES. MAX DEPTH OF DAMAGE IS .0025" & WITHIN SRM 54-51-8 FIG 105 SHEET 1 LIMIT. DAMAGE WAS BLENDED & VERIFIED CRACK FREE VIA NTM 51-60-00.SDR CALA2013112593212Lever · bindingIN FLIGHT ONLY FLAPS DIFFICULT TO RETRACT PAST 1 & TO EXTEND PAST 1 FLAP LEVER. FOUND FLAP HANDLE MECH BINDING. REPLACED FLAP & SLAT CONTROL LEVER, FLAP LEVER OPERATION NORMAL.SDR CALA2013112593213Sensor · faultyCABIN TEMP ALL AREAS DIFFICULT TO COOL. R & R FLIGHT DECK TEMP SENSOR. TSM21-63-00-810-821-A & AMM21-63-17- 400-001-A OPERATIONS CHECKED NORMAL.SDR CALA2013112593214Tape · looseANTI EROSION TAPE IS COMING OFF IN 4 PLACES ON VERTICAL TAIL. TRIMMED LOOSE EROSION TAPE IAW MT 55-003.SDR CALA2013112293190Unknown · malfunctionedAFT CARGO PIT HOT AIR VALVE WILL NOT OPEN, EVEN WHEN TEMP SELECTED FULL HOT.SDR CALA2013112293191Valve · faultyENG 2 FUEL HEAT SYSTEM FUEL RETURN VLV OPEN ECAM AFTER ENG START. CYCLED FADEC EIU CB A5 & Q40. FAULT RETURNED WHEN ENG RESTARTED. IAW TSM TASK 73-00-00-810-810-B FOR CORRECTIVE ACTION. R & R FUEL DIVERTER & RETURN VLV IAW AMM, OPERATIONS OK NO FAULTS NOTESDR CALA2013112293192Strap · missingNEED LIFE VEST REINSTALLED 31D, STRAP IS MISSING. MEL COMPLIED WITH SEAT IS UNUSABLE. INSTALLED NEW LIFE VEST WITH STRAP. SEALED LIFE VEST COMPARTMENT AT SEAT 31D.SDR CALA2013112593205Connector · overheatedDURING OPEN UP FOR PTU MODIFICATION FOUND CONNECTOR 221 6VC & 2216VCA OVERHEATED, AT PIN 45 WIRE NR 2821-001 YELLOW. R & R CONNECTOR 2216VC & 2216VCA IAW AMM 28-21-51-400-001-A. OPERATIONS CHECKED OKAY.SDR CALA2013112593239Fire Loop · warning messageAPU FIRE LOOP 'B' FAULT. RAN APU FIRE LOOP SELF TEST, NO FAULTS NOTED. DUE TO PREVIOUS HISTORY REPLACEMENT OF APU FIRE LOOP B REQUIRED REPLACED 'B' LOOP PER AMM, OPS CHECKED OKAY.SDR CALA2013112293193Computer · faultyFLIGHT CONTROL ELEV SERVO FAULT DURING FLIGHT CONTROL CHECK ON TAXI OUT. REPLACED ELAC 2 IAW AMM 27-93-34 ACP CAT III TEST FULL AUTO LAND CAPABLE.SDR CALA2013112093099Trim Switch · faultyUPPER MESSAGE "AUTO FLT RUD TRIM 2 FAULT" DISPLAYED. IAW ORD-TECH SUPPORT REPLACED FAC NR 1 & FAC NR 2 FROM ACFT 4712 IAW MM22-66-34. REPLACED RUDDER TRIM RESET SWITCH 8CC IAW MM22-62-12. ACCOMPLISHED OPERATIONAL TEST OF THE AFS IAW MM22-96-00 & LAND CAT IISDR CALA2013112093100Striker · faultyCOCKPIT DOOR 'FAULT' LIGHT & DOOR CONTROLLER 'MID STRIKE' LIGHT IS ON. REPLACED MID STRIKER & TESTED IAW MM 52-51-12-400, ALL NORMAL.SDR CALA2013112093122Seal · tornSMALL DOOR ON LT NLG HAS SEAL TORN & DISTORTED. MADE INTERIM REPAIR IAW ECRA.SDR CALA2013112093126Handset · defectiveAFT CABIN HANDSET INOPERATIVE. CAN TRANSMIT, BUT NOT RECEIVE. TROUBLE SHOT & FOUND AFT ATTENDANTS HANDSET BAD, MFG ST3100-23-10, PCN 582-0042, PARTS 582-0042 & ST3100-23-10U3 HANDSET.SDR CALA2013112193155Connector · dirtyLGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. LG CLEANED CONNECTOR ON NOSE GEAR PROX SENSOR 24GA & ACCOMPLISHED LGCIU 1 TEST, ALL OKAY.SDR CALA2013112193157Reservoir · overservicedBLUE RESERVOIR LOW AIR PRESS DISPLAYED ON UPPER ECAM SCREEN. HYD BLUE SYS HYD RESERVOIR OVER SERVICED. DRAINED & REPLACED YELLOW HYD SYS RESERVOIR DRAIN VALVE, ON ACCOUNT OF STUCK OPEN WHEN DRAINING SYSTEM DUE TO OVER SERVICE.SDR CALA2013112193158Motor · inoperativeCAPTAIN`S WINDSHIELD WIPER INOPERATIVE. WIPER MOTOR PCN 565-9005 AMM 30-45-51. SWITCH PCN 565-0615, TSM 30-45-00-810-801. ADJUSTED CAPTAIN`S WIPER BLADE, CYCLED SEVERAL TIMES & OPERATIONS CHECKED NORMAL IAW AMM.SDR CALA2013112093098Indication Sys · malfunctionedBLUE HYD SYS SD DISP SHOWS GREEN PSI DOWN STREAM OF PUMP WITH PUMP OFF.SDR CALA2013112093119Retainer Seal · missingPASSENGER SEAT OVERHEAD 02 MASK FELL AT 34DEF. PANEL HANGING DOWN, O2 CONTAINER ASSEMBLY LOOSE DUE TO APPROXIMATE 1 FT OF RETAINING SEAL MISSING. CONTAINER TRACK & J HOOK INTACT & CONTAINER SECURE. INTERIM REPAIR WITH TAPE IAW ECRA 2525-01548. SEATS 32DEF SDR CALA2013112093120Battery · faultyBATTERY 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED BATTERY 1 & BCL 1 IAW AMM, GND TESTED OKAY.SDR CALA2013112093128Connector · brokenRT WS HT COMPARTMENT 2DG2 AFT CONNECTOR 2DG2 B BACKSHELL BROKEN.SDR CALA2013112093129Lens · missingDOOR 1R ARM DISARM SIGHT PLATE LENS MISSING. VISUAL INSPECTION OF AREA, APPLIED ONE LAYER OF CLEAR TAPE. FUNCTIONAL CHECK OF ARM DISARM, WITH NO INTERFERENCE & PROPER FUNCTION.SDR CALA2013112193156Amu · faultyTHE FWD & AFT FLIGHT ATTENDANT INTERPHONE HAS HIGH STATIC & WHEN THE FWD FLIGHT ATTENDANT TRIES TO TRANSMIT THE TRANSMISSION SHORTS TO THE PA SYSTEM. SWAPPING HANDSETS BETWEEN THE FWD & AFT CABIN, NO HELP. RESETTING THE AMU IS NO HELP. REPLACED AMU, BOTH HASDR CALA2013111892984Angle · damagedON PREFLIGHT WALK AROUND FIRST OFFICER NOTICED STRAP HANGING OFF LT AILERON. REPLACED T CHORD & L ANGLE.SDR CALA2013111993065Seal · missingFWD HALON FIRE EXTINGUISHER SEAL MISSING. REPLACED SEAL.SDR CALA2013111993066Hose · leakingFLUID DRIPPING UNDER NR 2 ENG. REPLACED NR 2 ENG INBD THRUST REVERSER CROSSOVER HOSE IAW AMM. PERFORMED OPERATIONAL TEST OF THE THRUST REVERSER IAW AMM 78-31-00- 710-041-A13. NO LEAKS & OPERATIONS CHECKED NORMAL.SDR CALA2013111993067Sensor · out of adjustACCOMPLISHED GAP CHECK OF SENSOR 23GA. FOUND GAP TOO LARGE, INSTALLED 0.03 2 IN SHIM.SDR CALA2013112093102Fitting · crackedDOOR 2L HAS 4 INCH CRACK AT LOWER AFT INTERNAL FRAME CORNER FITTING.SDR CALA2013112093127Relay · failedAUTO FLT RUDDER TRIM 1 FAULT. REPLACED THE RELAY 7CC IAW FIM 22-62-00, SYSTEM CHECKED OK. CAT III TESTED OK IAW MM 22-9 7-00, AIRCRAFT IS FULL AUTO LAND CAPABLE.SDR CALA2013111892982Hydraulic Line · leakingG RESERVOIR LOW LEVEL DISPLAYED ON UPPER ECAM SCREEN, HYD. LOSS OF ALL GREEN FLUID. PTU & GREEN HYD PUMP COMMANDED OFF WITHIN 30 SECONDS OF ECAM INSTRUCTIONS. REPLACED LEAKING LINE.SDR CALA2013111893001Headset · inoperativeOBSERVER HEADSET INOPERATIVE, SUSPECT SHORT IN CORD. REPLACED OBSERVER HEADSET.SDR CALA2013111893023Engine · damagedNR 2 ENG FOUND EXIST GUIDE VANE OUTER PLATFORM BASE MATERIAL MISSING 1.5 X 6 INCHES WITH CRACKS EXTENDING INTO VANE SLOTS. THREE EACH PLATFORM CRACKS IN EACH VANE SLOT. IAW AMM 72-32-88-200-010-B13 ITEM 4.9A. ENG WILL NEED TO BE REMOVED FOR REPAIR IAW MT 71-SDR CALA2013111893024Seal · tornL3 WINDOW HAS TORN SEAL OUTSIDE LOWER AFT QUADRANT. HIGH FREQUENCY VIBRATION IN AIRSTREAM. REPAIRED WEATHER SEAL AT LOWER AFT QUADRANT OF WINDOW L3 IAW AMM.SDR CALA2013111993050Screw · missingSCREW MISSING AT FWD PANEL CORNER RT SIDE OF ACFT IMMEDIATELY AFT OF GEAR WELL JUST BELOW WING. REPLACED MISSING SCREW.SDR CALA2013111993051Seal · damaged8 TO 9 INCH CHUNK OF SEAL MISSING BETWEEN LE SLAT & FUSELAGE AT PANEL 192BT FAIRING. NEED SEAL PCN 110-1027 & RETAINER PCN 110-1025.SDR CALA2013111993052Cone · crackedNR 1 ENG EXHAUST CONE CRACKED. IAW MM 78-11-12-200-011-B FOR ALLOWABLE LIMITS. HAS MULTIPLE EXTENDING PASSED PREVIOUS STOP DRILLS HAVE CRACK EXCEEDING 6IN ZONE 1 REJECTING TAIL CONE. REPLACED TAIL CONE IAW MM.SDR CALA2013112093096Computer · faultyDUE TO HISTORY ELAC 2 NEEDS R & R. REPLACED ELAC, OPERATIONS CHECKED NORMAL.SDR CALA2013112093123Skin Panel · delaminatedLE OF BELLY PANEL 191BB DELAMINATING. ACCOMPLISH INSPECTION OR RECHECK REQUIRED BY CF0896. INTERIM REPAIR MADE IAW MT-53-002 & SRM 51-77-13 APPLIED SPEED TAPE. VERIFIED SPEED TAPE SECURED.SDR CALA2013112793306Oxygen Mask · leakingFIRST OFFICER'S OXY HARNESS FAILS TO INFLATE & IS LEAKING. REPLACED MASK TESTED OKSDR CALA2013111892985Sill · corrodedL2 DOOR SILL IS CORRODED FRAME 66, INBD GIRT BAR ATTACHMENT HOLES. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. INSTALLED SILL IAW SRM 51-42-11, PAGE 25.SDR CALA2013111893020Relief Valve · noisyAFT GALLEY MAKING A VERY LOUD CHATTER NOISE APU RUNNING & BLEED ON. DETERMINED TO BE AIR RELIEF VLV BEHIND AFT GALLEY COFFEEMAKER. ACCOMPLISHED BLEED PROCEDURE IAW MT 38-005, NOISE STOPPED.SDR CALA2013111893021Unknown · malfunctionedCARGO HEAT ZONE CONT FAILS TO SEND SIGNAL TO HOT AIR VLV TO OPEN. NO HEAT TO PIT. DEACTIVATED TRIM AIR VLV IAW MEL, POST FLIGHT REPORT FAILURE MESSAGE NO AFT CHC DATA.
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