IAE V2522-A5

Service difficulty reports · 3,465

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.

SDR UALA2010051001580Connector · burnedGALLEY G4 CB'S R41 AND R42 FOUND TRIPPED ON ELEC CONTROL UNIT 9002ML4. WILL NOT RESET. FOUND CONNECTOR 9005ML4 BURNED. REF AWM25-33-22 PG.1 CONNECTOR 9005ML4 AND PLUG 9005ML4A SHORTED CAUSING BOTH BREAKERS 900 8ML4 & 9009ML4 TO POP.FOUND NO FAULT WITH HARNESSMay 10, 2010 · N833UA · Airbus A319131 · Equipment/Furnishings WiringSDR UALA2010050601537Rod End · excess playLEFT ELEVATOR BLUE SERVO CONTROL EXCESSIVE PLAY CHECK IS 10MM AND OUT OF LIMITS. REPLACED LEFT I/B BLUE ELEV PCU ROD END. REPLACED LEFT I/B BLUE ELEV PCU ROD END. INSPECTED ROD END, FOUND SECURED AND SAFETIED REF METHOD NR 1.May 6, 2010 · N846UA · Airbus A319131 · Elevator Control SystemSDR UALA2010050601538Rod End · excess playLEFT ELEVATOR GREEN SERVO CONTROL EXCESSIVE PLAY CHECK IS 7MM OUT OF LIMITS. REPLACED LEFT O/B GREEN ELEV SERVO ROD END REF AMM. INSP'D ROD END FOUND SECURED AND SAFETIED, REF METHOD NR 1.May 6, 2010 · N846UA · Airbus A319131 · Elevator Control SystemSDR UALA2010050601539Rod End · faultyRT ELEVATOR YELLOW SERVO CONTROL EXCESSIVE PLAY CHECK IS 7MM AND OUT OF LIMITS. REPLACED RT OB YELLOW ELEV SERVO ROD END REF AMM. INSP RUDDER SERVO, FOUND ROD END SECURED AND SAFETIED REF METHOD NR 1.May 6, 2010 · N846UA · Airbus A319131 · Elevator Control SystemSDR UALA2010050601540Rod End · excess playRIGHT ELEVATOR SERVO CONTROL EXCESSIVE PLAY CHECK IS 7MM AND OUT OF LIMITS. REPLACED RIGHT I/B BLUE ELEV SERVO ROD END REF AMM. INSP SERVO ROD END FOUND SECURED AND SAFETIED REF METHOD NR 1.May 6, 2010 · N846UA · Airbus A319131 · Elevator Control SystemSDR UALA2010050601541Computer · faultyEFCS1 GROUND REPORT FAULTED SEC1 OR INPUT OF SPBK CONTROL TRANSDUCER UNIT 7CE. RECEIVED BAD UNIT FROM STOCK. INSTALLED ORIG UNIT. REPLACED SEC 1 & TESTED IAW MM, NO MESSAGES ARE PRESENT AND NO FAULTS OCCURRED DURING TEST, ALSO COMPLETED SUCCESSFUL AFS TEST IMay 6, 2010 · N846UA · Airbus A319131 · Flight Management Computing Hardware SystemSDR UALA2010050601542Computer · wrong partWHILE TROUBLESHOOTING LOG 2 FOUND FAULTY PART IN SEC 2 POS. REPLACED AND TESTED SEC 2 PER MM, ALL PARTS OF TEST PASS WITH NO FAULTS NOTED.May 6, 2010 · N846UA · Airbus A319131 · Elevator Control SystemSDR UALA2010050601548Smoke Detector · faultyECAM DISPLAYS SMOKE LAV + CRG DET FAULT. REPLACED SDCU PER MM. RESET CIDS AND SYSTEM TESTS NORMAL.May 6, 2010 · N802UA · Airbus A319131 · Smoke DetectionSDR UALA2010050501516Transmitter · faultedAFTER ENG 1 START, GOT ENG 1 REVERSER FAULT. IAW SAM S-DOWN ENG, ACCOMPLISHED REVERSER TEST USING FADEC 1A, SYS DETECTED A REVERSER FAULT, CFDS SHOWS CHECK NR 4 BEARING SCAV PRESSURE TRANSMITTER NR 1 CIRCUIT 40 05 EN & REV SL SENS CHB-HC-EEC1, FOUND N40 CB May 5, 2010 · N847UA · Airbus A319131 · Engine Thrust ReverserSDR UALA2010050601531Apu · malfunctionedSTRONG ODOR THROUGHOUT PLANE WITH APU BLEED AND PACKS ON. APU BILLOWING SMOKE. CABIN HAS SMOKEY OILY ODOR. REPLACED APU PER MM. OPS CHECK GOOD.May 5, 2010 · N803UA · Airbus A319131 · APU Core EngineSDR UALA2010050601536Computer · faultySPOILER ELEVATOR COMPUTER (SEC) 3 INOP - F-CTL. COMPLY WITH MEL 2794E, PULLED AND COLLARED C-B SEC 3 FLT CONTROL. REF MT27-011 FOR INTERCHANGEABILITY INFO. REPLACED 33 SEC COMPUTER PER MM. CHECKS OKAY.May 4, 2010 · N846UA · Airbus A319131 · Elevator Control SystemSDR UALA2010050301477Servo · out of toleranceAIRFRAME VIBES. GOES AWAY WITH ROLL INPUTS. VIBRATION REPORT CHECKLIST COMPLETE. FLIGHT CRE W REPORT STATES, SLOWING TO 300 KIAS AT FL280 IN CLIMB, ALL VIBES WENT AWAY. DEFINITELY SPEED RELATED, MEDIUM FREQUENCY FELT LIKE ELEVATOR OR AILERON FLUTTER, BUT INTEMay 3, 2010 · N809UA · Airbus A319131 · Aileron Control SystemSDR UALA2010042901439Power Supply · failedDURING CIDS TEST OF EMERGENCY LIGHT SYS, MESSAGE EXT LOADS EMERGENCY R 33-51-38 CAME UP. REPLACED RT EMERGENCY SUPPLY UNIT. CIDS TEST OK.Apr 28, 2010 · N829UA · Airbus A319131 · Emergency LightingSDR UALA2010042701406Power Supply · faultyLT OVERWING EXIT ECAM AND OVERWING INTERMITTENT. SUSPECT THE WARNING LIGHT PANEL. PANEL NO HELP. CONTINUING TO T/S. ADJUSTED LT OW EXIT DOOR PROXIMITY SENSOR. SLAVED NEW SENSOR, NO HELP. POWER SUPPLY BELOW DOOR WON'T TEST. LT OVERWING EMERGENCY LIGHT POWER SApr 27, 2010 · N813UA · Airbus A319131 · Door Warning SystemSDR UALA2010042701394Slide · partial deployLT OVERWING SLIDE OUT OF CONTAINER PARTIALLY DEPLOYED. DETERMINED THAT SLIDE RAFT PARTIAL DEPLOYMENT WAS DUE TO AMT INSERTING SAFETY PIN WITH THE INFLATION RESERVOIR VALVE REGULATOR PIN HOLE MISS-ALIGNED. A SERVICEABLE SLIDE RAFT WAS PROCURED AND WAS INSTALLApr 26, 2010 · N814UA · Airbus A319131 · Escape SlideSDR UALA2010042301358Cover · damagedF/O O2 MASK RUBBER CONNECTION COVER TORN. REPLACED F/O'S O2 MASK, OP CHECKS NORMAL.Apr 23, 2010 · N815UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2010041901293Computer · faultedSUBSTANTIAL YAW TO RT ON ROTATION. SUSPECT TIRE OR UNCOMMANDED RUDDER INPUT. REPLACED ELAC 1. OP CK'D GROUND SCAN AND MSG FOR ELAC 1 DID NOT APPEAR.Apr 19, 2010 · N806UA · Airbus A319131 · Flight Control SystemSDR UALA2010041901290Terminal · shortedDURING O2 MASK DROP AT C4 VISIT ROWS 6, 8, 13, 15ABC-11 BC-17,19, 21, 23DEF AND LT FWD ATTENDANT DID NOT DROP AND BREAKERS HA 5,6 POPPED. REPAIRED AND OPS CHECKED THE SHORED TERMINAL AT TERMINAL BLOCK 7201VT, AFT CABIN, BLOCK 13 PIN WIRED-1346. OPS CHECKED GApr 17, 2010 · N826UA · Airbus A319131 · Oxygen System WiringSDR UALA2010041901294Frame · dentedDENT IN FUSELAGE RT SIDE FWD OF FRAME 8. CTR OF DENT IS 10 INCHES FROM FIXED WINDOW CUTOUT. EDDY CURRENT SHOWS NO CRACKS. DENT WITHIN LIMITS. MAJOR REPAIR ACCOMPLISHED: REMOVED LOCATED AND DRILLED DOUBLER REPAIR. FABRICATED DOUBLER IAW SRM. OK TO INSTALApr 17, 2010 · N814UA · Airbus A319131 · Fuselage Main, FrameSDR UALA2010041901282Unknown · odorACRID ODOR IN FWD GALLEY, FLIGHT DIVERTED. ACCOMPLISHED THOROUGH VISUAL CHECK OF GALLEY COMPARTMENTS. AVIONICS COMPARTMENT, AVIONICS COOLING SYS AND CABIN. ONLY FOUND DRY ICE CONTAINER BAGS OPENED AND TORN, THERE WERE NO DEFECTS IN ANY SYS WHICH INCLUDED THEApr 16, 2010 · N852UA · Airbus A319131 · Air Distribution SystemSDR UALA2010041401264Slide · inoperativeRT OVERWING SLIDE BAD FROM STOCK, OLD UNIT ALSO BAD. REPLACED WITH SERVICEABLE RT OFF WING SLIDE IAW AMM.Apr 14, 2010 · N853UA · Airbus A319131 · Escape SlideSDR UALA2010041201218Lens · looseRED EMERGENCY EXIT LIGHT AT DOOR 1L IS LOOSE. INTERIM REPAIR MADE WITH TAPE (USED TAP2538-5-0300). TAPE USED TO SECURE LENS IS CLEAR. ENTIRE LENS COVER VISIBLE. LIGHT TEST OK. REPLACED RED EMERGENCY LIGHT LENS AT DOOR 1L. OPS OK.Apr 10, 2010 · N807UA · Airbus A319131 · Emergency LightingSDR UALA2010040701161Smoke Detector · faultyLAV N CRG DET FAULTAND SCDU INOP HISTORY. TROUBLESHOOT REF MT26-002. ATTEMPT TO ID SPECIFIC SMOKE DETECTOR(S) FOR REPLACEMENT OR INOP SDCU CHANNEL. IF NO FAULTS ARE FOUND OR SPECIFIC ITEM(S) CAN NOT BE IDENTIFIED, REPLACE ALL LAV, CARGO SMOKE DETECTORS AND SDApr 7, 2010 · N844UA · Airbus A319131 · Smoke DetectionSDR UALA2010040601157Smoke Detector · faultyLAVATORY DET FAULT DISPLAYED ON UPPER ECAM SCREEN. LAV SMOKE DETECTOR FAULT ECAM. ACCOMPANYING CIDS CAUTION LIGHTS ILLUMINATED. ACCOMPLISH CHRONIC REVIEW. CIDS PANEL SHOWING LAV A 1WQ SMOKE DETECTION FAIL. LAV DEFERRED INOPERATIVE. REPLACED SMOKE DETECTOApr 5, 2010 · N844UA · Airbus A319131 · Smoke DetectionSDR UALA2010040501111Seal · leakingAIR LEAK NOISE CAPTAIN'S FRONT W-SHIELD. 1 O'CLOCK POSITION DOES NOT SEEM TO BE AC. SOURCE NOT KNOWN. DE-BRIEFED CREW-AIR NOISE POSSIBLY COMING FROM BENEATH PANEL IMMEDIATELY AFT OF WINDSHIELD. CREW REPORTED NOISE CAME & WENT TWICE & THEY DO NOT FEEL IT IS ANApr 3, 2010 · N845UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2010040201098Oxygen Mask · leakingFO'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). REPLACED MASK. OPS NORMAL.Apr 1, 2010 · N838UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2010040201099Rectifier · arcedTR1 CONNECTOR 1PU1 HAS ELECTRICAL ARCING DAMAGE. ON TAXI IN LOUD NOISE HEARD BEHIND F/O AND CAPTAIN SAW SMOKE BY JUMPSEAT. HAPPENED WHEN APU STARTED. AREA ABOVE TR1 SHOWS EVIDENCE OF SOOT & SMOKE CONTAMINATION. CLEANED CONTAMINATION OF WIRING COMPONENTS REF AApr 1, 2010 · N804UA · Airbus A319131 · Starter-GeneratorSDR UALA2010033101086Window Frame · damaged3 EACH LIGHTNING STRIKES ON LT FWD FUSELAGE BELOW CAPT'S FIXED NR 1 AND SLIDING WINDOW AT BS 2540, SUB ZONE 210. INSTALLED 3 EA CHERRY MAX RIVETS WET. PERFORMED HFEC ON EXISTING FASTNER HOLES. NO DEFECTS NOTED.Mar 31, 2010 · N837UA · Airbus A319131 · Fuselage Main, StructureSDR UALA2010033101087Structure · damaged20 EACH LIGHTNING STRIKES ON LT FWD FUSELAGE AFT OF BS 3500, FRAME 1, SUB ZONE 120. BURNISHED BURN AREAS. REMOVED BURNED RIVETS. REPLACED RIVETS AND LOCK FASTENERS WET PRIMED AND PAINTED AREA. HAD HFEC DONE ON HOLES. NO DEFECTS NOTED.Mar 31, 2010 · N837UA · Airbus A319131 · Fuselage Main, StructureSDR UALA2010033101074Microphone · inoperativeFO'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED FO'S OXYGEN MASK AND NR 2 AUDIO CONTROL PANEL.Mar 30, 2010 · N834UA · Airbus A319131 · Audio Integrating SystemSDR UALA2010032901039Spring · brokenDOOR 1L DOOR ASSIST BOTTLE TRIGGER SPRING IS BROKEN. REPLACED DOOR 1 LEFT ASSIST BOTTLE.Mar 28, 2010 · N825UA · Airbus A319131 · Passenger/Crew DoorsSDR UALA2010032501002Smoke Detector · false indicationLAVATORY DET FAULT DISPLAYED ON UPPER ECAM SCREEN. - SMOKE. SMOKE ON GND FAULTS SHOW SMOKE DET LAV A (1WQ). REPLACED 1WQ FWD LAV SMOKE DETECTOR, CKS GOOD.Mar 24, 2010 · N823UA · Airbus A319131 · Smoke DetectionSDR UALA2010032200943Servo Control · faultyLT AILERON ISSUE, FLIGHT DIVERTED. AILERON JERK HAPPENED WITH A-P ON, AP WASN'T DISENGAGED AND DID NOT KICK OFF. SPOILERS DIDN’T DEPLOY OR MOVE TO CAUSE ANY ROLL. AILERON FLOATED UNTIL AN INPUT WAS MADE THEN AILERON JERKED INTO COMMANDED POSITION. UNCOMMANMar 21, 2010 · N811UA · Airbus A319131 · Aileron Control SystemSDR UALA2010032200939Unknown · faultyREF CARGO PIT FIRE BOTTLE WRITE-UP, FOUND 26VDC ON FWD SQUIB CONNECTOR WITH T19 CB PULLED. REPLACED SDCU PRECAUTIONARY, NO HELP. RANG OUT OVERHEAD PNL, WIRING FROM PNL TO SQUIBS AND PANEL TO SDCU. FOUND 26VDC ON PINS R AND S OF 2400VC A. PULLING SDCU CB'S Mar 21, 2010 · N801UA · Airbus A319131 · Extinguishing SystemSDR UALA2010031900925Solenoid · malfunctionedO2 LOW PRESSURE DISPLAYED. REPLACED O2 PSI REGULATOR AND CREW O2 SWITCH, ALL NO HELP. REPLACED LP OXYGEN SUPPLY VALVE SOLENOID 3HT IAW MM. CHECKS GOODMar 19, 2010 · N815UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2010031500867Slat · dentedDENT REPORTED IN RT WING FIRST SLAT FROM FUSELAGE, 23 INCHES FROM INBOARD EDGE OF SLAT. MAJOR REPAIR ACCOMPLISHED. DENT IS 4 X4 INCHES AND .350 INCH DEEP AT THE CENTER, NO CRACKS OR SHARP EDGES NOTED. CUT OUT DAMAGE, NDT AREA FOR DAMAGE REMOVAL. MANUFACTURMar 12, 2010 · N823UA · Airbus A319131 · Leading Edge DevicesSDR UALA2010031100830Battery · failedLEFT EMERGENCY LIGHTS BATTERY FAILED TEST. REPLACED BATTERY, OP'S CHECKS GOOD.Mar 11, 2010 · N840UA · Airbus A319131 · Emergency LightingSDR UALA2010031200839Cartridge · defectiveWATER LEAK, RTFL. LEAK COMING FROM SINK FAUCET IN FLIGHT. SHUT OFF WATER TO SINK AND TURNED OFF WATER HEATER. RPLC'D FAUCET. NEED TO RDF BECAUSE COULD NOT GET WATER TO FLOW OUT OF FAUCET. REPLACED CARTRIDGE AND TURNED ON BOTH WATER VALVES, OPS CKS GOOD.Mar 11, 2010 · N807UA · Airbus A319131 · Potable Water SystemSDR UALA2010030900811Door · faultyCABIN-SEAT ROW 21L O2 MASKS - DOOR DID NOT OPEN DURING TEST. FROM BASE W-U R7210M. SUPPLEMENTAL DATA UPDATE REPLACED DOOR, TEST STOP AND REINSTALLED ACTUATOR. OPS CHECKED GOOD AT SFOMB WRITEUP R7210MMar 9, 2010 · N823UA · Airbus A319131 · Passenger Oxygen SystemSDR UALA2010030900812Container · no testCABIN-SEAT ROW 24R O2 MASKS - DOOR DID NOT OPEN DURING TEST. REPLACED O2 MASK CONTAINER.Mar 9, 2010 · N823UA · Airbus A319131 · Passenger Oxygen SystemSDR UALA2010030500777Oil System · leakingSMOKE IN CABIN, FLIGHT DIVERTED. APU AUTO SHUT DOWN: CHECKING OIL QTY AND INLET, AND APU COMPT. FOR LEAKS. APPROX 4 QUARTS OF OIL ADDED. STARTED APU, VAST QUANTITY OF SMOKE FROM TAIL PIPE. ODOR CAUSED BY APU OIL LOSS. APU DEFERRED INOP. PACK BURNOUT ACCOMPLISMar 5, 2010 · N819UA · Airbus A319131 · APU Oil SystemSDR UALA2010030100738Unknown · unknownFLAPPING NOISE FROM DOOR 2R AREA, RTFL. CHECKED ALL AREAS ON RT SIDE OF ACFT INCLUDING EE BAY ON BOTH SIDES. CHECKED ALL DOOR SEALS, CARGO COMPT. FWD AND AFT, FWD NOSE GEAR DOORS, AND ALL ACCESS PANEL DOORS. NO PROBLEMS FOUND. CONTACTED OPBLM ABOUT ACTION TMar 1, 2010 · N814UA · Airbus A319131 · Fuselage Structure (General)SDR UALA2010030200747Seal · leakingRT WING LEAK, RTFL. FOUND DUCT LEAKING JUST INBD OF RT-PYLON UNDER WING PANEL 621EB, BLOWING INTO MUFF-INSULATION. REMOVED RT UNDER WING PANELS 621EB, 621CB & R-PYLON TOP PNL 621BT. SECURED RT WING LOWER L/E PANELS AND TOP PANEL. SEALED TOP PANEL. REPLACED 2Mar 1, 2010 · N811UA · Airbus A319131 · Pneumatic Distribution SystemSDR UALA2010030200748Smoke Detector · faultyLAVATORY DET FAULT DISPLAYED ON UPPER ECAM SCREEN. - CHECK P.F.R. CYCLE CB'S C6 AND T18 FOR 20 SECONDS. MX COMPLIED WITH STEPS IN MEL 267 1H. DOOR PLACARDED INOP AND WASTE BIN DOOR TAPED OVER. PERFORMED RESET IN EWR, NO HELP. SDCU TEST FAULTING LAV "A" SMOKEMar 1, 2010 · N811UA · Airbus A319131 · Smoke DetectionSDR UALA2010030100716Wire · damagedCB CARGO DOOR ON PANEL 122VU IS POPPED. SMOKE COMING FROM FWD CARGO DOOR OPEN-CLOSE SWITCH AREA. SWITCH ON AOG Y5092. AOG FOR SWITCH IS G3529. FOUND BROKEN WIRE TO FWD CARGO PIT OPEN LOCKED LIGHT. CHANGE LIGHT AND REPAIR WIRE TO LIGHT.OPS CHECKED GOOD.Feb 27, 2010 · N847UA · Airbus A319131 · Door System WiringSDR UALA2010022400678Plate · dentedFWD CARGO DOOR THRESHOLD PLATE HAS A DENT APPROX 1-8 INCH LONG BY 1-8 INCH IN DEPTH. DENT IS APPROX 28.5 INCH FROM LEADING EDGE OF DOOR CUTOUT. DAMAGE IS A PREVIOUS REPAIR THAT WAS ADDRESSED ON 27APR 09. REF SEQ 6282008.Feb 23, 2010 · N841UA · Airbus A319131 · Cargo/Baggage DoorsSDR UALA2010022300675Control Panel · malfunctionedEMERGENCY EXIT LIGHTS ILLUMINATE IN THE CABIN WITH THE EMERGENCY EXIT LIGHT SWITCH IN THE OFF POSITION ON THE OVERHEAD PANEL 25VU WHEN AC POWER IS REMOVED FROM THE AIRCRAFT. REPLACED 126RH PANEL (AFT ATTENDANT). BITE AND EMERGENCY LIGHT CHECKS OKAY.Feb 22, 2010 · N822UA · Airbus A319131 · Emergency LightingSDR UALA2010021900631Computer · failedCREW HAD NUMEROUS ECAM MSGS, FLIGHT DIVERTED. REPLACED NR 1 FLIGHT WARNING COMPUTER AND ALSO THE NR 1 SYS DATA ACQUISITION CONCENTRATOR. ALSO ACCOMPLISHED CAT III CHK IAW AMM. ALL OK AND SATISFACTORY.Feb 19, 2010 · N812UA · Airbus A319131 · Flight Management Computing Hardware SystemSDR UALA2010021800622Hook And Loop · detachedALL LAVS - O2 MASK COMPTS - HOOK AND LOOP DETACHED FROM FABRIC, WHICH PUSHES MASKS OUT WHEN DOOR OPENS, MASKS DID NOT DROP IN 'D' LAV. FROM BASE W-U J7589B. REATTACHED HOOK AND LOOP TO FABRIC, MASK REPACK ON OV-JIC 4R3590091.Feb 18, 2010 · N822UA · Airbus A319131 · Passenger Oxygen SystemSDR UALA2010021800615Hook And Loop · detachedLAV A O2 CONTAINER: HEAT SHIELD HOOK AND LOOP DISBONDED FROM HEAT SHIELD. VELCRO IS WRAPPED AROUND AND GLUED TO ONE OF THE MASK BAGS AND ATTACHED TO MATING HOOK AND LOOP STRIP. MASK WOULD NOT HAVE DROPPED IN EMERGENCY. REPLACED LAV 'A' O2 BOX AND INSTALLED Feb 17, 2010 · N811UA · Airbus A319131 · Passenger Oxygen System
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