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 CALA2013110892739Servo · malfunctionedSPOILER SERVO CNTL NR 1 RT, THERE HAVE BEEN REPEAT GRIPES & RESETS FOR FLT CONTROL SPOILER FAULTS AFTER ENG START. CFDS REPORTING FAULT "RT SPOILER 1 POS X-DUCER, 31CE2." AT NEXT MX OPPORTUNITY, REPLACE THE RT GRN NR 1 SPOILER SERVO-CONTROL, PCN 644-9561 IAW Nov 6, 2013 · N465UA · Airbus A320232 · Drag Control SystemSDR CALA2013110692691Acoustic Liner · deterioratedACOUSTIC PANEL REPAIR ENG 2 HAS DETERIORATION. PLACED NR 2 ENG ATTRITION LINER AT 8 O'CLOCK POSITION ON CF873, NO LOOSE MATERIAL & GRC LAYER NOT PUNCTURED, IAW MT 72-017.Nov 5, 2013 · N414UA · Airbus A320232 · Turbine Engine Air Inlet SectionSDR CALA2013110692695Starter · faultySPARKS OBSERVED ON START OF ENG 2, REPLACED STARTER.Nov 5, 2013 · N478UA · Airbus A320232 · Engine StarterSDR CALA2013110692701Dome Nut · defectiveSCREW STICKING OUT ON BELLY OF PLANE BY AC INLET. PANEL 192KB & ONLY ONE FASTENER IS ISSUE, NOT NEAR LE OR CORNER. REPLACED DOME NUT & FASTENER.Nov 5, 2013 · N446UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013110792720Acoustic Liner · damagedACOUSTIC LINER NEEDS TO BE REEXAMINED FOR INTEGRITY. MORE DAMAGE NOTED AT 1 O'CLOCK POSITION. PREVIOUS REPAIRS AT 2:00 POSITION & 7:00 POSITION. NR 2 ENG INLET ATTRITION GRC LAYER REQUIRE PERM REPAIR IAW A320 MT 72-017. DAMAGE LESS THAN 20 PERCENT, PLACED Nov 5, 2013 · N414UA · Airbus A320232 · Turbine Engine Air Inlet SectionSDR CALA2013110892738Actuator · faultyRUDDER TRIM 2 ECAM MESSAGE. ADJUSTED RUDDER TRIM ACTUATOR IAW AMM 27-22-00-820-001A, & ECRA 2722-01008. INSTALLATION OF RUDDER TRIM ACTUATOR IAW 27-22-51-400-001A. RUDDER TRIM & RUDDER HYD NORMAL, LEAK CHECKED OK, NO DEFECTS NOTED. ALL RIG PINS REMOVED, NONov 5, 2013 · N457UA · Airbus A320232 · Rudder Tab Control SystemSDR CALA2013110892740Controller · faultyBUILDING HISTORY OF "HOT AIR FAULT" ECAM WARNINGS. RECENT LEG FAULTED "NO ZONE CTL DATA" AT FLT PHASE 4. REPLACE ZONE CONTROLLER, PCN 565-9207, IAW AMM 21-63-34.Nov 5, 2013 · N483UA · Airbus A320232 · Cabin Temperature ControllerSDR CALA2013110592647Control Lever · faultyLANDING GEAR HANDLE IS DIFFICULT TO OPERATE TO THE UP POSITION WHEN RETRACTING. REPLACED LANDING GEAR CONTROL LEVER, OPERATIONS CHECKED GOOD.Nov 4, 2013 · N496UA · Airbus A320232 · Landing Gear SelectorSDR CALA2013110592669Stringer · corrodedFWD CARGO FUSELAGE STRINGER HAS SPOTS OF CORROSION BETWEEN FRAME 28 - 29, STRINGER 43R. REMOVED & INSTALLED NEW STRINGER AT FRAME 28 - 29, STRINGER 43R IAW SRM 51-42-11, PG 7 & SRM 53-00-13,FIG 201.Nov 4, 2013 · N435UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2013110592671Rivet · missingENG 1 EXHAUST TAIL CONE LOWER FIXED VERTICAL FAIRING INBD SIDE MISSING ONE RIVET. REPLACED FASTENER WITH CR3524-5 FASTENER IAW MT 78-001.STEP O.2.Nov 4, 2013 · N477UA · Airbus A320232 · Engine Collector/Tailpipe/NozzleSDR CALA2013110692694Display · faultyFIRST OFFICER`S NAV DISPLAY GOES BLANK. REPLACED FIRST OFFICER`S CRT DISPLAY AMM 31-63-22.Nov 4, 2013 · N420UA · Airbus A320232 · Central DisplaySDR CALA2013110592645Sleeve · delaminatedNR 1 ENGINE REVERSER SLEEVE SCREEN DELAMINATE INOPERATIVE. NR 1 ENG REVERSER DEFER IAW MEL. TAKE PICTURES OF DAMAGE OF DELAMINATE & UPDATE ON RVI SITE & UPDATE WITH PARTS NEEDED & IPC IAW. SLEEVE NEEDED PER TOMC, ON ORDER IAW OSTF V4807. PARTS 115-9104 MRNov 3, 2013 · N437UA · Airbus A320232 · Engine Thrust ReverserSDR CALA2013110592648Relay · failedFLT CTL SEC 1 FAULT ECAM RAN CHECK LIST WOULD NOT RESET. LND DIST REQ LESS THAN 4000 FT. REPLACED RELAY 41CE1, RERACKED SEC1 & OPERATIONS CHECKED IAW MM. TESTED NORMAL, NO FURTHER FAULTS, OPERATIONS NORMAL.Nov 3, 2013 · N486UA · Airbus A320232 · Flight Control SystemSDR CALA2013110592649Control Cable · brokenFIRST OFFICER`S RUDDER PEDALS WILL NOT LOCK IN POSITION. FOUND CABLE BROKEN FROM RUDDER PEDAL ADJUSTER MECHANISM. REPLACED CABLE IAW AMM, OPERATIONS CHECKED GOOD.Nov 3, 2013 · N466UA · Airbus A320232 · Rudder Control SystemSDR CALA2013110592652Gauge · obstructedSLIDE GAUGE AT DOOR 2R IS UNREADABLE BECAUSE INSPECTION STICKER COVERS IT. REPOSITIONED VIEWER IAW MM 25-62-44, SLIDE GAUGE READABLE BY OTBD CREW.Nov 3, 2013 · N438UA · Airbus A320232 · Escape SlideSDR CALA2013110592653Computer · faultyFQI CH1 FAULT. REPLACED FQIC & OPERATIONS CHECKED OK IAW AMM.Nov 3, 2013 · N459UA · Airbus A320232 · Fuel Quantity IndicatorSDR CALA2013110592655Valve · faultedECAM HOT BRAKES, RT BRAKES AT 480 & DRAGGING. BOTH NR 3 & NR 4 BRAKES WERE SMOKING & DRAGGING DURING TAXI. REPLACED DUAL ALTERNATE BRAKE DISTRIBUTION VALVE IAW MM & REPLACED ALTERNATE BRAKE SERVO VALVE MANIFOLD IAW MM. BLEED BOTH ALTERNATE & NORMAL BRAKE SYNov 3, 2013 · N432UA · Airbus A320232 · Landing Gear Brake SystemSDR CALA2013110592672Connector · damagedDURING STARTING OF ENG NR 2, UPPER ECAM DISPLAYS "ENG 2 EPR MODE FAULT" & "N 1 DEGRADED MODE". EEC CONNECTOR 4000KS-J2 DAMAGED, REPLACED CONNECTOR. SEE SEQ 3632010.Nov 2, 2013 · N455UA · Airbus A320232 · Engine Fuel System WiringSDR CALA2013110892734Thrust Reverser · damagedON WALK AROUND CREW FOUND MATERIAL LOOSE & PEELING ON NR 1 ENG INBD REVERSER HALF AS VIEWED FROM THE REAR OF THE ENGINE. REPAIRED IAW ECRA 7830-02701.Nov 2, 2013 · N437UA · Airbus A320232 · Engine Thrust ReverserSDR CALA2013110592651Lens · missingVIEWPORT FOR SLIDE PRESSURE GAUGE MISSING AT DOOR 1L. ACCOMPLISHED TEMPORARY REPAIR WITH CLEAR MYLAR TAPE. VIEWPORT LENS PCN 110-3639. REPLACED VIEW PORT LENS AS REQUIRED.Nov 1, 2013 · N476UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2013110492583Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. CONFIRMED NR 2 ELAC COMPUTER IS BAD. SWAPPED BOX INTO THE NR 1 ELAC POSITION & MEL NR 1 ELAC SYSTEM INOPERATIVE. ACFT DOWNGRADED TO CAT 1. SN OF NR 1 ELAC IS 1039, SN OF NR 2 ELAC IS 5084. ALL DDPG IAW DF0980.Nov 1, 2013 · N479UA · Airbus A320232 · Flight Control SystemSDR CALA2013110692692Computer · failedCAP MAP NOT AVAILABLE ON ND. REPLACED FMGC 1 IAW AMM 22-83-34, OPS CHECKED GOOD. LAND TEST IAW AMM22-97-710 TEST PASSED.Nov 1, 2013 · N479UA · Airbus A320232 · Autopilot SystemSDR CALA2013110192552Stringer Splice · corrodedFWD CARGO FUSELAGE FR 30-31, STRINGER 41, STRINGER SPLICE HAS CORROSION. REPLACED FACTORY SPLICE IN FWD CARGO COMPARTMENT FR 30-31, STRINGER 41 IAW SRM 53-42-11, PG 7.Oct 31, 2013 · N435UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2013110192554Transceiver · faultyIAW LOG 1, TROUBLESHOOT WX RADAR TILT PROBLEM. PERFORMED ANTENNA CONTROL TEST IAW AMM 34.41.00.730.001.A & DURING THE TEST THE ANTENNA DID NOT TURN IN ELEVATION (+10, -10) PAGE 8 OF 10. REPLACED WX TRANSCEIVER, ON MR43123-1054, OFF 1128. WX CONTROL PANEL ONOct 31, 2013 · N498UA · Airbus A320232 · Weather Radar SystemSDR CALA2013110192555Nose Cowl · crackedNR 2 ENG NOSE COWL HAS APPROXIMATELY HALF INCH CRACK AT 8 O'CLOCK POSITION. FOUND CRACK IS IN ZONE J, STOP DRILLED CRACK, MUST REPAIR NO LATER THAN 600 FLIGHT HOURS, 750 FLIGHT CYCLES OR 100 DAYS, CHECK CRACK EVERY FLIGHT TO MAKE SURE CRACK DOES NOT BECOME LAOct 31, 2013 · N417UA · Airbus A320232 · Engine Cowling SystemSDR CALA2013110192556Extinguisher · unserviceableAFT WATER FIRE EXTINGUISHER NOT SEALED. REPLACED FIRE EXTINGUISHER.Oct 31, 2013 · N447UA · Airbus A320232 · Fire Bottle, PortableSDR CALA2013110192557Seal · damagedLEFT WING AILERON INBD BOTTOM SEAL MISSING 5 0R 6 INCHES OF SEALANT. A 3 INCH SECTION OF LOWER BLADE SEAL MISSING, NEEDS A NEW LOWER BLADE SEAL.Oct 31, 2013 · N422UA · Airbus A320232 · AileronsSDR CALA2013110192558Fuse · faultyBCL 2 FAULT DISPLAYED ON UPPER ECAM SCREEN, ELECTRICAL. REPLACED FUSE 4PB2 IAW WD24-38-01. CHECKED NORMAL IAW 24-38-00-710-001.Oct 31, 2013 · N402UA · Airbus A320232 · DC Generating SystemSDR CALA2013110192571Transceiver · faultyWXR INOPERATIVE - NAV. RADAR INTERMITTENTLY DISPLAYS GREEN ARC AT RANDOM RANGES. RESET SAFTER CYCLING PWR SWITCH. REPLACED WXR TRANSCEIVER, HAD XMTR DRVR CAL FAULTS LOGGED IN TRANSCEIVER. IAW AMM 34-41- 33 OPERATIONS CHECKED GOOD.Oct 31, 2013 · N491UA · Airbus A320232 · Weather Radar SystemSDR CALA2013103092533Engine · malfunctionedENG 1 HAVING 2 SEPARATE STALL EVENTS DURING DESCENT AT THROTTLE REDUCTION. AFTER SECOND STALL CREW CONTINUED WITH ENG AT IDLE. ENGINE DID NOT SHUTDOWN AT ANY TIME. TROUBLESHOOT IAW TSM. NR 1 ENG REPLACED IAW MT71-017.Oct 30, 2013 · N426UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2013103192534Microphone · faultyCAPT BOOM MIKE VERY GARBLED, HAND MIKE WORKS OK. REPLACED CAPTS BOOM MIKE.Oct 30, 2013 · N421UA · Airbus A320232 · Audio Integrating SystemSDR CALA2013103192535Rivet · shearedRT SIDE OF NR 2 ENG PYLON HAS DOOR OPEN. FOUND SHEAR RIVETS SHEARED AT AUTOMATIC OPENING MECHANISM. INSTALLED NEW RIVETS IAW MM, ALSO PERFORMED A VISUAL INSPECTION OF BLEED DUCTS. NO DEFECTS NOTED.Oct 30, 2013 · N460UA · Airbus A320232 · Nacelle/Pylon Miscellaneous StructureSDR CALA2013110592646Ignition Lead · defectiveAPU WILL NOT START, HANGS AT 18% N1. REPLACED IGNITION UNIT IAW MM-49-41-38, NO HELP. REPLACED FUEL CONTROL UNIT FOR TROUBLESHOOTING IAW MM, NO HELP. REPLACED IGNITER PLUGS & LOWER IGNITION LEAD IAW MMS. OPERATIONS CHECKED GOOD.Oct 30, 2013 · N491UA · Airbus A320232 · APU Start/Ignition SystemSDR CALA2013103092503Skin Panel · corrodedAFTER REMOVAL OF WASTE TANK, SKIN HAS CORROSION IN AREA OF WASTE DUMP VLV & WASTE TANK. BLENDED CORROSION BETWEEN FRAMES 65 & 66, BETWEEN STRINGER S41R & LAVATORY SERVICE PANEL. ACCOMPLISHED HFEC INSPECTION OF BLENDED AREAS IAW NDT-NTM 51-10-08 PB6, NO DEFECOct 29, 2013 · N424UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013103092511Light · inoperativeNOSE GEAR TAXI LIGHT SYSTEMS INOPERATIVE.Oct 29, 2013 · N472UA · Airbus A320232 · Exterior LightingSDR CALA2013103092512Hydraulic Line · leakingHYD FLUID DRIPPING FROM AFT CARGO PIT CEILING, FWD END RT SIDE. YELLOW & GREEN SYSTEM RESERVOIRS AT REFILL. FOUND YELLOW SYS HYD LINE LEAKING JUST BELOW T FITTING IAW IPC 52-36-04-02C LINE-ITEM 170, PCN110-2740-PN-D291709020600. REPLACED SECTION OF LINE & SPOct 29, 2013 · N428UA · Airbus A320232 · Hydraulic System, MainSDR CALA2013103092513Acoustic Liner · damagedENG 2 ACOUSTIC LINER 11 O’CLOCK POSITION HAS 1 IN CHUNK MISSING. ACCOMPLISHED REPAIR IAW MT-72-017.Oct 29, 2013 · N432UA · Airbus A320232 · Turbine Engine Air Inlet SectionSDR CALA2013103092514Oil Filter · cloggedENG 2 OIL FILTER CLOG MESSAGE 4257-2 ESN V10058, DUE TO ENG 2 OIL FILTER CLOG ECAM, MESSAGE CLEARED ON ITS OWN. TO PREVENT IRREGULAR OPERATIONS, DELAYS ACCOMPLISHED FAULT ISOLATION ITEM 4A (1)(2)(3) & (4) OF TSM 79-30-00-810-804-A ON EDOCS PAGE 3 OF 4. ENG OOct 29, 2013 · N457UA · Airbus A320232 · Turbine Engine Oil SystemSDR CALA2013103092516Battery · faultyBCL1 FAULT DISPLAYED ON UPPER ECAM SCREEN, ELEC. REPLACED NR 1 BATTERY CFDS BITE ON BCL, CHECKED OK IAW MM 24-38-51.Oct 29, 2013 · N495UA · Airbus A320232 · Battery/Charger SystemSDR CALA2013103092517Fuel Cap · brokenFUEL CAP BROKEN. REPLACED FUEL CAP.Oct 29, 2013 · N425UA · Airbus A320232 · Fuel StorageSDR CALA2013103092518Hydraulic Line · leakingFOUND HYD LINE LEAKING ON LT WING FWD INBD FLAP OTBD ACTUATOR. REPLACED YELLOW HYD SYS PRESS LINE. NEED TO ACCOMPLISH LEAK CHECK.Oct 29, 2013 · N412UA · Airbus A320232 · Hydraulic System, MainSDR CALA2013102992456Cover · missingRUBBER COVERS FOR BRAKE TEMPERATURE SENSORS MISSING ON ALL 4 SETS OF BRAKES.Oct 28, 2013 · N461UA · Airbus A320232 · Landing Gear Brake SystemSDR CALA2013102992476Pump · leakingBLUE SYS HYD OBSERVED AT 3250PSI. STEADY STATE, REPEAT WU. REPLACED BLUE SYSTEM PUMP IAW AMM-29-12-51-000-001-A & AMM-29-12-51-400-001-A. PERFORMED OPERATIONAL BLUE SYSTEM, CHECKED OKAY.Oct 28, 2013 · N437UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR CALA2013102992492Skin Panel · delaminatedBELLY PANEL 191BB SHOWS LE DELAMINATION. INSTALLED TAPE IAW SRM 51-77-12 & PLACED ON CF.Oct 28, 2013 · N486UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013102992493Handset · intermittent1L HANDSET INTERMITTENT. REPLACED HANDSET AT 1L, OPERATION NORMAL.Oct 28, 2013 · N466UA · Airbus A320232 · Audio Integrating SystemSDR CALA2013102992494Handset · intermittentINTERPHONE IS INTERMITTENT AT DOOR 1L. CABIN INTERPHONE INTERMITTENT THROUGHOUT CABIN & FROM CABIN TO COCKPIT. REPLACED FWD HANDSET, OPERATIONS CHECKED OKAY.Oct 28, 2013 · N492UA · Airbus A320232 · Interphone/Passenger Announcement (PA) SystemSDR CALA2013102992495Contactor · faultyWHEN ONE OR BOTH BATTERIES SELECTED & NO GROUND POWER CONNECTED, NO INDICATION OF ELECTRICAL POWER SEEN. REPLACED 6BP-1 CONTACTOR IAW MM24-38-55 GROUND OPERATIONS CHECKED OKAY.Oct 28, 2013 · N456UA · Airbus A320232 · Battery/Charger SystemSDR CALA2013103092515Cone · crackedNR 2 ENG EXHAUST CONE HAS 4.5" CRACK IN ZONE 1 AT 4 O'CLOCK POSITION. STOP DRILLED CRACK IAW AMM 78-11-12-200-011-C.Oct 28, 2013 · N469UA · Airbus A320232 · Engine Collector/Tailpipe/NozzleSDR CALA2013102892416Sill · corrodedR2 DOOR SILL HAS CORROSION. REPLACED R2 DOOR SILL IAW SRM 51-42-11 ON TIMCO NR 43035.Oct 27, 2013 · N484UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013102892417Sill · corrodedDOOR 2 RT DOOR SILL CORRODED BETWEEN FRAMES 66 & 68. DOOR SILL REPLACED IAW SRM 51-42-11.Oct 27, 2013 · N485UA · Airbus A320232 · Fuselage Miscellaneous Structure
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