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.

SDR CALA2013102892419Valve · inoperativeRT WING TANK REFUEL VLV INOPERATIVE.Oct 27, 2013 · N492UA · Airbus A320232 · Fuel StorageSDR CALA2013102892421Actuator · malfunctionedENG 1 COMPRESSOR VANE ECAM ON TAKEOFF ROLL, ABORTED TAKEOFF AT LOW SPEED. R & R VSV ACTUATOR ON NR 1 ENGINE AS IAW AMM 75-32-41-000-010-A & AMM IAW 75-32-41-400-010-A.Oct 27, 2013 · N454UA · Airbus A320232 · Compressor Bleed ControlSDR CALA2013102892422Eec · failedFADEC B FAULT DISPLAYED ON UPPER ECAM SCREEN. ENG 1 WITH ECAM WARNING & FAILURE MESSAGE FROM POST FLIGHT REPORT. UNABLE TO ACCESS ENG 1 FADEC B VIA CFDS, CYCLED FOLLOWING CB'S NO HELP A04, R41, F01 & Q07. ECAM REAPPEARS AS SOON AS MASTER SW IS TURNED ON. ROct 27, 2013 · N464UA · Airbus A320232 · Fuel Control/Turbine EnginesSDR CALA2013102892439Servo · faultyFLTC AIL SERVO FAULT COMES ON WITH GEN 1 OUT WITH GEN 2 ONLINE. RT BLUE AIL SERVO IS DEACTIVATED IAW MEL 2714M. GROUND SCAN REPORT RT BLUE AIL MODE VLV 3 3CE4. REPLACED AIL SERVO BLUE SYSTEM.Oct 27, 2013 · N456UA · Airbus A320232 · Aileron Control SystemSDR CALA2013102992458Sleeve · looseNR 1 ENG OTBD REVERSER SLEEVE INNER LINING 3 FOOT BY 4 FOOT SECTION OF WIRE MESH LINING LOOSE. IAW ECRA 7830-02698 SLEEVE MUST BE REPLACED WITHIN 25 HOURS OR BY PTT 66626, USING PART 115- 9105 & MUST BE CHECKED ONCE PER DAY. ** DL1694 CREATED TO MONITOR **Oct 27, 2013 · N404UA · Airbus A320232 · Engine Thrust ReverserSDR CALA2013102992475Seal · tornLT AILERON INBD UPPER & LOWER EDGE TO WING SEAL TORN. NEED PCN 110-2815 INBD & 110-2816 OTBD RJF. AILERON INBD UPPER & LOWER SEALS REMOVED. REPLACED UPPER & LOWER INBD AILERON SEAL ON LT AILERON. OKAYED FOR SERVICE.Oct 27, 2013 · N498UA · Airbus A320232 · AileronsSDR CALA2013103192545Shelf · damagedSHARP METAL EDGE ON AFT GALLEY SHELF. REPAIRED DAMAGE.Oct 27, 2013 · N470UA · Airbus A320232 · Buffet/GalleysSDR CALA2013110792705Slide · out of toleranceDOOR 1L SLIDE RAFT REMOVED IAW AMM FOR JOB CARD CHANGED SLIDE RAFT IAW MM, MR OFF MR25114-035. ON, MR25120-022 OFF.Oct 27, 2013 · N473UA · Airbus A320232 · Escape SlideSDR CALA2013102992457Line · leakingHYD FLUID COMING DRAIN HOLE FWD OF RADAR ALT IN FRONT OF MAIN GEAR. FLUID COMING FROM BROKEN LINE, WHICH WAS REPAIRED, CLEANED UP LEAKING HYD FLUID.Oct 27, 2013 · N466UA · Airbus A320232 · Hydraulic System, MainSDR CALA2013102892415Threshold · corrodedCORROSION L2 DOOR THRESHOLD INBD OF AFT GIRT BAR LOCK. BLENDED CORROSION ON L2 DOOR THRESHOLD INBD OF AFT GIRT BAR LOCK FRAME 68 STRINGER 23L OUT OF LIMITS IAW SRM 53-41-14. REMOVED, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-41-14.Oct 26, 2013 · N484UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013102992459Screw · missingTWO SCREWS MISSING ON PANEL 192KB RT UNDERSIDE OF FUSELAGE. REINSTALLED TWO EACH SCREWS ON PANEL 192KB, OK TO CONTINUE.Oct 26, 2013 · N482UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013102992460Hydraulic Line · leakingEVIDENCE OF FLUID LEAK FROM VICINITY OF HYD SERVICE PANEL TO TAIL OF AIRCRAFT. BOTH LINES TO BRAKE VLV ON WW CEILING CENTERLINE LEAKING. TIGHTENED BOTH LINES NO LEAKS NOTED.Oct 26, 2013 · N492UA · Airbus A320232 · Hydraulic System, MainSDR CALA2013102992461Threshold · damagedAFT BAG PIT THRESHOLD DAMAGED. REPLACED SILL PLATE IAW ECRA 5322-01050 PERMANENT REPAIR.Oct 26, 2013 · N493UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013103092510Hydraulic Line · leakingBELOW FWD CARGO PIT'S J-S DRIVE MOTOR, BILGE AREA, FOUND "DOOR CLOSE PRESS" HYD LINE FOAMING & DRIPPING AT SUPPORT CLAMP, YELLOW SYS. PERFORMED RYNLOCK REPAIR ON THE HYD LINE IAW GPM 1-0-13-028 & AMM 20-23-11-300-007A. INSTALLED REPAIRED HYD LINE, LEAK CHECKOct 26, 2013 · N466UA · Airbus A320232 · Hydraulic System, MainSDR CALA2013102892401Windshield · damagedCAPTAIN'S WINDSHIELD VISIBILITY IS IMPAIRED. EVIDENCE OF ARCING. CRACKED AREA IS DISCOLORED & APPEARS TO BE LOCATED ON THE MIDDLE PANE. FAR LOWER LT CORNER OF WINDSHIELD APPEARS TO BE CRACKING AT THE OUTER PANE. WILL REQUIRE REPLACEMENT IAW AMM. REPLACED COct 25, 2013 · N409UA · Airbus A320232 · Flight Compartment WindowsSDR CALA2013102892438Thrust Reverser · damagedNR 1 ENG MATERIAL STICKING OUT TOP EXTERIOR AT REVERSER SLEEVE. NR 1 ENG RT C DUCT BULL NOSE SEAL DAMAGED. REMOVED SEAL & DEACTIVATED REVERSER IAW MEL SUSPECT PCN 222-1067 IPC 78-32-76-82A NR 40.Oct 25, 2013 · N425UA · Airbus A320232 · Engine Thrust ReverserSDR CALA2013102492353Control Panel · faultyAFT GALLEY EQUIP CONTROL PANEL ABNORMALLY WARM & UNABLE TO CONTROL. FLIGHT DIVERTEDOct 24, 2013 · N442UA · Airbus A320232 · Buffet/GalleysSDR CALA2013102592392Structure · damagedFABRICATE & INSTALLED REPAIR DOUBLER AT FR 74-75 STRINGER 26L.Oct 24, 2013 · N433UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013102892403Life Vest · faultyFLIGHT ATTENDANT SAYS SHE NEEDS A SINGLE CHAMBER LIFE VEST DEMO. REPLACED LIFE VEST AS NEEDED.Oct 24, 2013 · N455UA · Airbus A320232 · Life JacketSDR CALA2013102892404Bolt · shearedNR 2 ENG FUEL FILTER COVER PLATE HAS ONE SHEARED BOLT, PLATE & ADAPTER RING ARE REMOVED, WAITING ON PARTS FROM SFO. IAW ECRA 7900-01318 REPLACED D BOLT PCN 645-0007 & INSTALLED ADAPTOR RING IAW ECRA. CONTINUED WITH INSTALLATION OF FILTER CAP INSTALLATION IAWOct 24, 2013 · N454UA · Airbus A320232 · Engine Fuel DistributionSDR CALA2013102892405Thrust Reverser · delaminatedNR 1 ENG INBD THRUST REVERSER SLEEVE REMOVED. IAW AMM 78-32-46 FOR CF595 DUE TO EXCESS PREVIOUS REPAIRS & NEWLY DELAMINATED AREAS. REMOVED NR 1 INBD REVERSER IAW MM 78-32-03. NEW REVERSER INSTALLED UP TO STEP E (2) PG 7.3 FWD BOLTS TORQUED AFT SLEEVE INSTALOct 24, 2013 · N425UA · Airbus A320232 · Engine Thrust ReverserSDR CALA2013102392303Structure · damagedTOP OF RT ENG PYLON THERE IS A CREASE BENT PORTION.Oct 23, 2013 · N490UA · Airbus A320232 · Nacelle/Pylon Miscellaneous StructureSDR CALA2013102492339Structure · dentedSIX MINOR DENTS AT FR 59 TO FR 60 BETWEEN STRINGER 38R TO STRINGER 41R. DEEPEST DENT IS .OO5" WITHIN LIMITS IAW SRM 53-41- 11 PG115. ACCOMPLISHED HFEC IAW NTM 51-10-08 NO CRACKS NOTED.Oct 23, 2013 · N433UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013102492340Skin · damagedRT WING FUEL TANK ACCESS LANDING AT 640KB HAS FIVE DAMAGED HOLES. ONE WITHIN SRM57-21-11 LIMIT, FOUR WERE REPAIRED IAW ECRA5720-02453 & REO-L01417 REV IR ON TIMCO NR 33599.Oct 23, 2013 · N433UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2013102492342Skin · damagedLT WING FUEL TANK ACCESS LANDINGS AT 540KB & 540LB HAVE ONE EACH DAMAGED FASTENER HOLE AT EACH PANEL LOCATION. HOLES WERE REPAIRED IAW ECRA5720-02452 & REO-L01416 REV IR ON NR 33651 & 33649 IAW ECRA5720-02452.Oct 23, 2013 · N433UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2013102492351Sensor · faultyREPLACED THE FLSCU2 CFDS CONTINUES TO REPORT FAULT MESSAGE "FUEL LEVEL SENSING RT OUT TEMPERATURE SENSOR 30QJ2." TEMPERATURE SENSOR HAS BEEN REPLACED. PLACED FLSCU2 IAW ABOVE.Oct 23, 2013 · N457UA · Airbus A320232 · Fuel Temperature IndicatorSDR CALA2013102592385Control Panel · faultyAFT GALLEY EQUIPMENT CONTROL PANEL FAULTY, FLT DIVERTED. NO SMOKE OR ELECTRICAL SMELL ASSOCIATED WITH WARM PANEL. ACCOMPLISHED CHECK OF CM IAW MM25 -35-00-710-013A, RAN CHILLER IAW MM25-34-00-710-001A, OPERATED LIGHTING & HOT PLATE. MONITORED PANEL NO INDICOct 23, 2013 · N442UA · Airbus A320232 · Buffet/GalleysSDR CALA2013102892400Landing Gear · out of limitsMOMENTARY LG UNLOCKED ECAM AFTER GEAR EXTENSION FOR 10 SEC WHICH CLEARED ITSELF. FOUND LT MAIN GEAR & RT MAIN GEAR OUT OF LIMITS IAW MM 12-12-32-611-010-A. LT UPPER CHAMBER APPROXIMATELY 1150PSI, LOWER CHAMBER 1100, H DIMENSION 5 INCHES. RT GEAR UPPER CHAMBOct 23, 2013 · N421UA · Airbus A320232 · Main Landing GearSDR CALA2013102892402Fastener · missingTHREE MISSING FASTENERS ON PANEL LT FUSELAGE JUST 3FT AFT OF LT WING TE. REPLACED MISSING FASTENERS.Oct 23, 2013 · N498UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013102292243Latch · brokenSEAT 25 DEF OXYGEN MASK BOX LATCH BROKEN. SEATS NOT USABLE. REPLACED LATCH, INSPECTED MASK & CANISTER IAW AMM 35-21-00-601. STOWED MASKS & PERFORMED DROP TESTS OF AIRCRAFT MASK SYSTEM IAW AMMOct 22, 2013 · N425UA · Airbus A320232 · Passenger Oxygen SystemSDR CALA2013102392288Stringer · corrodedAFT PIT, STRINGER 41R, FRAME 57-59 CORRODED. R & R STRINGER 41R FROM FRAME 58 -64 IAW SRM 51-42-11, PG 7.Oct 22, 2013 · N433UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2013102392296Fan · inoperativeLEFT CABIN RECIRCULATION FAN INOPERATIVE.Oct 22, 2013 · N438UA · Airbus A320232 · Air Distribution FanSDR CALA2013102392298Clamp · brokenCLAMP ON FIRST CLASS OXYGEN BOTTLE BROKEN.Oct 22, 2013 · N474UA · Airbus A320232 · Portable Oxygen SystemSDR CALA2013102392299Start Valve · defectiveSTART FAULT DISPLAYED ON UPPER ECAM SCREEN, HUNG START, ENG 1. START VLV NEVER DID OPEN, TRIED THREE START ATTEMPTS. REPLACED PNEUMATIC START VLV IAW AMM-80-13-51. OPERATIONS CHECKED GOOD.Oct 22, 2013 · N489UA · Airbus A320232 · Engine Start Valves/ControlsSDR CALA2013102392300Connector · dirtyLGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN LG. CLEANED PLUGS ON LT MLG DOOR UP LOCK SENSORS 27GA & 29GA. RESET LGCIU1 CB RAN BITE ON LGCIU1 USING MCDU IAW MM 32-69-00-740-001-A, NO FAULTS FOUND. ECAM STATUS IS NORMAL.Oct 22, 2013 · N401UA · Airbus A320232 · Landing Gear System WiringSDR CALA2013102392301Oxygen Mask · malfunctionedCAPTS O2 MASK STUCK IN EMERGENCY CONT FLOW, UNABLE TO SHUT OFF UNTIL RESTOWED. R & R CAPTAIN'S O2 MASK IAW AMM. TESTED IAW AMM.Oct 22, 2013 · N427UA · Airbus A320232 · Crew Oxygen SystemSDR CALA2013102392302Nose Cowl · damagedNR 1 ENGINE NOSE COWL HAS A 1 INCH DIAMETER HOLE IN ABRADABLE LINER AT THE 6 OCLOCK POSITION 1ST STAGE FAN LINER. IAW MAINT TIP 2717, PARTS 841-0591 ADH3002-48 ADHESIVEOct 22, 2013 · N427UA · Airbus A320232 · Engine Cowling SystemSDR CALA2013102392305Oxygen Mask · faultyFIRST OFFICERS O2 MASK DOES NO INFLATE ON TOP LT SIDE. SWAPPED WITH 1ST OBSERVERS.Oct 22, 2013 · N448UA · Airbus A320232 · Crew Oxygen SystemSDR CALA2013102392287Stringer · corrodedAFT CARGO BAY STRINGER 43L CORRODED FROM FRAME 54 TO 60. R & R STRINGER IAW SRM 51-72-11, PG 1.Oct 22, 2013 · N433UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2013102192200Unknown · malfunctionedAPU WILL NOT PICKUP ELECTRICS WHEN COMING OFF EXTERNAL POWER.Oct 21, 2013 · N465UA · Airbus A320232 · AC Generation SystemSDR CALA2013102192229Valve · faultyUNUSUAL CYCLING SOUND FLOOR OF AFT GALLEY. PLACED AFT CARGO EXTRACTION FAN ON MEL IAW 2128F, PULLED & COLLARED CIRCUIT BREAKER S22, AFT CARGO VENT & HTG FAN AS PRECAUTIONARY. IAW GMM 05-30-05, COMPLIED WITH MX PROCEDURES, OK TO CONTINUE. R & R AFT CARGO COOct 21, 2013 · N478UA · Airbus A320232 · Air Distribution SystemSDR CALA2013102292244Transducer · faultyIAW EQ3055 ABILITY OF SEC 1 TO ACHIEVE PITCH CONT FAIL TO RETURN TO 0.0 + OR -0.3 IT IS AT 0.5 IAW AMM27-9 6-00-710-018-A STEP 32 PAGE 37. REPLACED SEC1 F1CE1 IAW AMM-2794-34-000-0001-A & AMM-27-34-400-0001-A, WITH NO HELP. REINSTALLED OLD UNIT. REPLACED NROct 21, 2013 · N417UA · Airbus A320232 · Stabilizer Control SystemSDR CALA2013102392297Cowling · out of adjustNR 1 ENG COWL IS NOT FLUSH JUST AHEAD OF FWD COWL LATCH UNDERSIDE. ADJUSTED COWL & FOUND COWL WITHIN LIMITS.Oct 21, 2013 · N483UA · Airbus A320232 · Engine Cowling SystemSDR CALA2013102192231Engine · malfunctionedDURING ENGINE START, NR 1 ENGINE WENT TO RED LINE AT 715 DEGREES FOR 5 SECONDS ON RESTART. ENGINE STARTED TO STABLIZE & THEN RACED TO RED LINE, SHUTDOWN ENGINE. CHECKED, NO DEFECTS NOTED. STARTED ENGINE FOR FOURTH TIME & ALLOWED ENGINE TO STABILIZE. ENGIOct 21, 2013 · N440UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2013102192199Door Seal · leakingFLIGHT ATTENDANT REPORTS PRESSURE LEAK AT DOOR 2L. PRESSURIZED A-C FOUND AFT LOWER CORNER LEAKS & SMALL LEAK AT FWD LOWER CORNER, HAS HISTORY. REPLACED DOOR SEAL IAW MM.Oct 20, 2013 · N401UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2013102192223Sill · corrodedCORROSION ON CABIN L2 DOOR THRESHOLD DOOR SILL AT FRAME 66 - 68. REPAIRED CABIN L2 DOOR THRESHOLD DOOR SILL FRAME 66-68 IAW SRM 53-41-14, FIG 201, PRINCIPLE 5.Oct 20, 2013 · N485UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013102192228Fdu · faultyAPU FIRE DET WILL NOT TEST. IAW MEL, REPLACED APU FDU, TESTED OKAY.Oct 20, 2013 · N412UA · Airbus A320232 · Fire DetectionSDR CALA2013102192230Warning System · activatedPFR SHOWS "FLP LT PROX SNSR 2 39CV OR LGCIU 2" PREVIOUSLY BOTH PARTS ARE REPLACED.Oct 20, 2013 · N404UA · Airbus A320232 · Central WarningSDR CALA2013102192198Control Valve · faultyPACK 1 & 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. BOTH VLV POSITION INDICATIONS AMBER. - AIR. RT PACK PLACED UNDER MEL LT PACK FUNCTIONED OK. REPLACED FLOW CONTROL VLV IAW AMM, SYSTEM OPERATIONS & LEAKS CHECKED GOOD.Oct 19, 2013 · N474UA · Airbus A320232 · Cabin Cooling SystemSDR CALA2013102192205Frame · dentedDENT AT FRAME 15 LT SIDE OF FUSELAGE APPROXIMATELY STRINGER 20. MEASURED DENT & FOUND OUT OF LIMITS, INSTALLED REPAIR DOUBLER IAW SRM 53-00-11, FIG 240.Oct 19, 2013 · N416UA · Airbus A320232 · Fuselage Main, Frame
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