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 UALA2012111906658Door · missingLEFT VEST DOOR FOR 2ND OBSERVER IN THE FLIGHT DECK IS MISSING. SEAT IS INOP, SHOULD HAVE COVER AND VEST. AC NOT ON COA LIST, NEED COVER AND VEST.Nov 16, 2012 · N428UA · Airbus A320232 · Emergency EquipmentSDR UALA2012111906659Lever · brokenF/O OXYGEN MASK STOWAGE CONTAINER PRESS TO TEST LEVER BROKEN OFF. REPLACED F/O O2 MASK BOX PER MM. OPS AND LEAK CHECKED OK.Nov 16, 2012 · N411UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012112006695Unknown · malfunctionedREPEAT GRIPE. COCKPIT COLD. WHEN COCKPIT WARMED FIRST CLASS AND FWD CABIN GETS HOT. PERFORMED TIS MANUAL 21-6 3-00-810-815-A TEST WAS OK. INSPECTED VISIBLE DUCTING IN LOWER ACCESS COMP. NO DEFECTS NOTED.Nov 16, 2012 · N481UA · Airbus A320232 · Cabin Temperature Control SystemSDR UALA2012112606764Control Panel · inoperativeCAPT MIC STAYS HOT AND UNABLE TO SELECT VHF NR 1 AND VHF NR 2. SWITCHED TO CAPT ON 3 AND CLEARED HOT MIC. OK TO DF REF MEL 2351AK. REPLACED CAPT ACP. INSTALLED NEW ACP AMM & TESTED PER AMM. ALL TESTS OKAY. REV'D DF #060 AC OK FOR SERVICE.Nov 16, 2012 · N401UA · Airbus A320232 · Communications SystemSDR UALA2012111906657Acoustic Panel · crackedDURING WALK AROUND FOUND ACOUSTIC PANEL REPAIR ON 1 ENGINE CRACKED AND LOOSE. DAMAGED AREA MEASURES APP ROX 1.5 SQ IN AT 6 O CLOCK POSITION. CF PER MT-72-017. PARTS: 841-0591 ADH3002-48 AVL SFR RES/17NOV. ACCOUSTICAL PANEL DAMAGED AREA HAS PROGRESSED TO 6"XNov 16, 2012 · N460UA · Airbus A320232 · Turbine Engine Air Inlet SectionSDR UALA2012111606583Alternator · faulty1 ENGINE FADEC ALTERNATOR, ENGINE 1 STALL, ENGINE 1 SENSOR FAULT, ENGINE 1 FAIL ECAM, REPLACE DEDICATED ALTERNATOR DRIVE PER MM. REPLACED DEDICATED ALTERNATOR ROTOR ASSEMBLY PER MM. LEAK CHECK GOOD WITH EDA DRIVE. ENGINES 1 AND 2 SERVICED TO FULL AFTER ENGINNov 16, 2012 · N403UA · Airbus A320232 · AC Generator-AlternatorSDR UALA2012111906656Stud · out of positionSEAT ROW 37DEF IS LOOSE AT FLOOR ATTACH POINT --NOT CONNECTED TO FLOOR. FOUND FRONT STUD BACKED OUT OF SEAT LEG. CHECKED STUD AND LEG THREADS ALL INTACT. REINSTALLED STUD AND ANTI RATTLE NUT. RE-INSTALLED SEAT INTO TRACK IN PROPER POSITION. SEAT IS SECURENov 16, 2012 · N431UA · Airbus A320232 · Passenger Compartment EquipmentSDR UALA2012111606620Cover · missingEXIT SIGN COVER MISSING AT LEFT OVERWING EXIT KICK PANEL. REPLACED COVER.Nov 15, 2012 · N426UA · Airbus A320232 · Emergency LightingSDR UALA2012111606624Shrader Valve · looseHYDRAULIC FLUID ON BOTTOM OF FUSELAGE BEHIND BOTH MAIN GEAR DOORS AND AFT. FOUND SHREADER VALVE LOOSE ON BOTTOM OF RESERVOIR. TIGHTENED VALVE, NO NEW LEAKS.Nov 15, 2012 · N440UA · Airbus A320232 · Hydraulic Reservoir, MainSDR UALA2012111906654Coupling · leakingFUELER REPORTED FUEL LEAKING FROM REFUELING FLANGE WHILE PUMPING FUEL. TIGHTENED ALL SCREWS IN FLANGE ABOUT 1-2 TURN. NO HELP. TRIED ANOTHER TRUCK TO VERIFY PROBLEM WAS NOT THE HOSE. FLANGE STILL LEAKED. REPLACED FUELING COUPLING, FUELER ADDED FUEL NO LEANov 15, 2012 · N490UA · Airbus A320232 · Aircraft Fuel Distribution SystemSDR UALA2012111906633Starter · faultySPARKS FROM FRONT OF ENGINE 2 DURING START. COCKPIT INDICATIONS NORMAL. MAINT ATTEMPTED AUTO START AND START VALVE MANUAL START WITH NO ROTATION. WILL NEED TO REPLACE START VALVE AND STARTER PER MM. REPLACED THE STARTER AND START VALVE PER MM. ACP FUNCTIONov 15, 2012 · N469UA · Airbus A320232 · Engine StarterSDR UALA2012111606632Battery · failedEMERGENCY LIGHT TEST FAILED INT LOAD EMERGENCY LEFT AND INT LOAD EMERGENCY RIGHT. REPLACED LEFT AND RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT BATTERIES IAW MM. EMERGENCY LIGHTS TEST GOOD.Nov 15, 2012 · N425UA · Airbus A320232 · Emergency LightingSDR UALA2012111606589Bottle · faultyON CONDITION - RIGHT OFF WING INFLATION CYL - REPLACE ACP PER TC 4S2592014 SEQ# 801.Nov 14, 2012 · N438UA · Airbus A320232 · Emergency EquipmentSDR UALA2012111606587Slide · faultyTHE 1L MEDIUM SLIDE PRESSURE GAUGE NOT VISIBLE. REPLACED FWD LEFT DOOR SLIDE.Nov 14, 2012 · N438UA · Airbus A320232 · Escape SlideSDR UALA2012111406549Strut · low pressureNOSE STRUT FOUND LOW ON WALKAROUND.Nov 13, 2012 · N444UA · Airbus A320232 · Nose/Tail Landing Gear Strut/AxleSDR UALA2012111406556Structure · damagedG1 AND G4 GALLEYS HAVE HEAT DAMAGE BEHIND WORK LIGHTS. GALLEYS WERE REFURBISHED AT HMV2 VISIT PER JD-CE-40-25-30-02-JD1.Nov 13, 2012 · N467UA · Airbus A320232 · Buffet/GalleysSDR UALA2012111406557Fcu · malfunctionedFCU DISPLAY MALFUNCTIONING CLIMB-DESCENT. VERTICAL SPEED WINDOW SHOWS ZEROS IN OPEN CLIMB. REPLACED FCU PER MM WITH KNOWN GOOD UNIT FROM ACFT 4019. ACCOMPLISHED OPERATIONAL TEST OF THE AFS PER 22-96-00 AND LAND CAT III CAPABILITY TEST PER MM 22-97-00, OPS Nov 13, 2012 · N461UA · Airbus A320232 · Flight ControllerSDR UALA2012111406569Handset · unknownCABIN HANDSET. REPLACED AFT HANDSET.Nov 13, 2012 · N448UA · Airbus A320232 · Audio/Video MonitoringSDR UALA2012111406551Shutoff Valve · failedNR 2 ENGINE FIRE EXT TEST SUB FUNCTION FAIL TASK CARD 4R2640020 ITEM D 5 A. REPLACE NR 2 HYD PUMP FIRE VALVE PER AMM, LEAK AND OPS TEST GOOD PER TASK 29-10-00-720-001 AND JIC 4R2640020 SEQ #402.Nov 13, 2012 · N438UA · Airbus A320232 · Hydraulic System, MainSDR UALA2012111406573Coupling · faultyLEFT MAIN GEAR HAS DISCONNECTED HYDRAULIC LINE BRAKE QUICK DISCONNECT COUPLING: IPC 32-11-12-03B ITEM 10: PCN 110-1909. REPLACED LEFT GEAR BRAKE AFT QUICK DISCONNECT LINE SECURED.Nov 13, 2012 · N422UA · Airbus A320232 · Hydraulic System, MainSDR UALA2012111206491Oxygen Bottle · unknownOXYGEN PRESSURE WENT FROM 870 TO 820 PSI OVER 2 1/2 HOURS WITH NO USE. SERVICED CREW O2 BOTTLE. OPS CHECKED GOOD, NO LEAKS NOTED.Nov 12, 2012 · N428UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012111306529Oxygen Mask · faultyCAPTS O2 MASK HAS OXY FLOW BY PRESSING EMERGENCY TEST BUTTON W-SLIDE LVR RELEASED. REPLACED CAPT O2 MASK. OP CHECKS NORMAL.Nov 12, 2012 · N432UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012111306530Seal · looseHIGHER THAN NORMAL WIND NOISE CAPT L3 WINDOW. SAMC TEXT: PERFORM REPAIR PER AMM 56-11-12-300-002-A, USE PCN 841-0098 (B 1-6TH SEALANT), AIRBUS MATERIAL 09-045. GPM REF 6-0- 00-028, PG 49. USE HEAT GUN TO ACCELERATE CURE TIME. REPAIRED L3 WINDOW WEATHER SEANov 12, 2012 · N486UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2012111406570Controller · faultyWARM AIR IS STILL SUPPLIED TO FORWARD CABIN WITH RESPECTIVE ZONE TEMP CONTR IN FULL COLD. CLEAN AND TEST TEMP SENSORS (21HK AND 22HK). REPLACED 8HK ZONE CONT PER AMM 21-63-34. GND TEST OKAY.Nov 12, 2012 · N422UA · Airbus A320232 · Cabin Temperature ControllerSDR UALA2012111306531Panel · unsecureROW 20 DEF OXYGEN MASK HANGING DOWN. SECURED THE PAX VENT PANEL; IT WAS NOT O2 MASK.Nov 12, 2012 · N425UA · Airbus A320232 · Passenger Compartment EquipmentSDR UALA2012111206473Selector Valve · faultyL/G DOOR OPEN, RTFL. REMOVED AND REPLACED LANDING GEAR DOOR SELECTOR VALVE IAW AMM. PERFORMED OPERATIONAL TEST OF THE LANDING GEAR DOORS (WITHOUT FALSE TARGETS) IAW AMM. LANDING GEAR DOORS, OPS CHECK NORMAL.Nov 11, 2012 · N444UA · Airbus A320232 · Landing Gear SelectorSDR UALA2012111206486Door · dentedL2 DOOR DENT FOUND OUT OF LIMITS AT HMV2 VISIT. MAJOR REPAIR. INSTALLED DOUBLER REPAIR PER SRM 52-10-00 FIG 206.Nov 11, 2012 · N464UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2012111206516Regulator · leakingCREW OXYGEN SYSTEM LOW. FOUND FIRST OBSERVERS O2 REGULATOR LEAKING. BOX AND CRUSH GASKET HAVE BEEN REPLACED WITH NO LEAKS.Nov 11, 2012 · N428UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012111206474O-Ring · leakingWATER COMING OUT OF 4 DRAIN HOLES LOCATED BETWEEN FWD CARGO COMPT AND WING ROOT. REPLACED POTABLE WATER TANK LOWER SERVICE LINE FITTING O-RING. PRESSURE LEAK TEST REF AMM 38-10-00-614-001A CHECK GOOD. PERFORMED WATER CLEAN UP REF GNMM 4-06-004.Nov 11, 2012 · N401UA · Airbus A320232 · Potable Water SystemSDR UALA2012111206507Stowage Box · faultyF/O O2 MASK MICROPHONE INOPERATIVE. SWAPPED F/O AND 2ND OBS O2 BOX F/O O2 MASK MICROPHONE OPS CHECKED GOOD.Nov 10, 2012 · N451UA · Airbus A320232 · Audio Integrating SystemSDR UALA2012111206469Power Supply · faultyLEFT AFT EMERGENCY POWER SUPPLY HAS A UNIT FAULT LIGHT ON WHEN TESTED. REPLACED POWER SUPPLY, TESTED OKAY.Nov 10, 2012 · N458UA · Airbus A320232 · Emergency LightingSDR UALA2012111206467Stringer · corrodedMAJOR REPAIR - STR 42L BETWEEN FR 56 AND 57 IS CORRODED. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-00-13 FIG 201 SHEET 1&2.Nov 9, 2012 · N464UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2012110906452Tire · wornAFTER GEAR RETRACTION NOSE LANDING GEAR HAD VIBRATION. NOSE TIRES WORN, REPLACED BOTH NOSE TIRES PER MM.Nov 8, 2012 · N430UA · Airbus A320232 · TireSDR UALA2012110906453Pedal · malfunctionedAIRCRAFT DOES NOT TAXI WITHOUT EXCESSIVE EPR. SUSPECT DRAGGING BRAKES. PROG TEXT: - ITEM ROLLED FORWARD. MAINT TEXT: LEFT BRAKES 100 DEG HOTTER THAN RIGHT. CREW TAPPED LEFT BRAKE PEDAL AND AIRCRAFT ROLLED NORMAL. ACCOMPLISHED PARKING BRAKE CHECK PER TSM.Nov 8, 2012 · N460UA · Airbus A320232 · Landing Gear Brake SystemSDR UALA2012110906454Skin · scratchedSCRATCH IN OUTER SKIN AT DOOR 2L. LOCATION IS 14 INCHES AFT OF LEADING EDGE, & 1-2 TO 1-4 INCH FROM BOTTOM OF DOOR 2L. 2 1-2 INCHES LONG BY APPROXIMATELY .002 DEEP. DEPTH OF SCRATCH WAS APPROX .002 INCH IN THE .098 THICK METAL, SEE AREA "B" DAMAGE TOLERANCE.Nov 8, 2012 · N443UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2012110806435Fire Bottle · unserviceableAFT GALLEY WATER EXTINGUISHER SEAL BROKEN. WATER EXTINGUISHER REMOVED. REPLACED EXTINGUISHER.Nov 7, 2012 · N435UA · Airbus A320232 · Fire Bottle, PortableSDR UALA2012110706408Computer · faultySLAT SYS 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F -CTL. REPLACED SFCC1 AND OP CHECK SATISFACTORY.Nov 7, 2012 · N463UA · Airbus A320232 · Leading Edge Slat Control SystemSDR UALA2012110806434Wire Harness · faultyCREW REPORTS CAPT SLIDING WINDOW HEAT FAULT. CREW COMPLIED WITH MEL, CAUSED GATE RETURN AT MEX. SUSPECT WIRING HARNESS FRAYED. REMOVED AND REPLACED CAPT WINDOW HARNESS, OPS CHECK GOODNov 7, 2012 · N443UA · Airbus A320232 · Ice/Rain Protection System WiringSDR UALA2012110706396Nose Cowl · damagedNR 1 ENGINE NOSE COWL DAMAGE AT THE AT 11 O'CLOCK POSITION. REPLACED ENGINE NR 1 NOSE AIR- INTAKE COWL PER AMM. OPS AND GROUND TEST NORMAL, NO FAULTS NOTED.Nov 7, 2012 · N453UA · Airbus A320232 · Engine Cowling SystemSDR UALA2012110806419Sill · corrodedMAJOR REPAIR. R2 DOOR SILL HAS CORROSION AT FRAME 68. INSTALLED ANGLE REPAIR PER SRM 53-41-14 FIG 201. THIS REPAIR REQUIRES REINSPECT PER SRI 53-41-14-2-001-00.Nov 7, 2012 · N464UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012110706410Fitting · brokenPLASTIC FITTING ON O2 BOTTLE IN AFT CABIN IS BROKEN. REPLACED BOTTLE.Nov 6, 2012 · N425UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2012110606367Oxygen Mask · unwanted deploy36DEF OXYGEN MASKS ALL FELL DOWN. PACKED MASKS IAW AMM. ACCOMPLISHED OXYGEN MASK DROP PER MM.Nov 6, 2012 · N448UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2012110706411Nut · looseENTIRE TRIM WHEEL IS LOOSE AND RATTLES ON TAKEOFF AND LANDING. TIGHTEN LOOSE 2 EACH NUTS ON TRIM WHEEL.Nov 6, 2012 · N485UA · Airbus A320232 · Stabilizer Control SystemSDR UALA2012110706418Bearing · wornCREW REPORT EXCESSIVE VIBRATION WITH FLAPS DOWN. TEST HOP NO GOOD. FLAP VIBRATION 3-4 POSITION. BECAUSE OF REPEAT DISCREPANCIES FOR AIRFRAME VIBRATION WHEN FLAP ARE LOWERED FROM 3 TO FULL DOWN ACCOMPLISH. FLAPS HYDRAULIC ACTUATION AND POWER TRANSMISSION INNov 6, 2012 · N482UA · Airbus A320232 · AileronsSDR GTIA20121105507Accumulator · dischargedR2 DOOR ASSIST ACCUMILATOR REQUIRES SERVICE. SERVICED R2 DOOR ACCUMILATOR IAW AMM 52-10-00-614-001-A.Nov 5, 2012 · N607NK · Airbus A320232 · Passenger/Crew DoorsSDR UALA2012110506320Slide · crackedRAMP REPORTED, RIGHT OVERWING SLIDE, AFT SIDE FRAME IS CRACKED. REPLACED RT OVERWING SLIDE REF AMM. INSPECTED INSTALLATION OF RT OVERWING SLIDE ASSY.Nov 5, 2012 · N471UA · Airbus A320232 · Escape SlideSDR UALA2012110706409Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. ALSO HAD SMALL-SLIGHT UNCOMMANDED ROLL. SAMC TEXT: WORK WITH TSM 27-10-00-810-842A. REMOVED AND REPLACED ELAC 1. REF TO AMM 27-93-34. OPS CHECK GOOD PER AMM 27-96-00-740-001. LAND VERIFY TEST PASSED PER TASK 2Nov 5, 2012 · N426UA · Airbus A320232 · Flight Control SystemSDR UALA2012110506308Visor · looseCAPTS SUNVISOR STILL INOP. CANNOT TIGHTEN TO REMAIN IN POSITION. REPLACED CAPTS SUNVISOR ASSY.Nov 3, 2012 · N452UA · Airbus A320232 · Flight Compartment EquipmentSDR UALA2012110506352Seal · looseHUMMING NOISE COMING FROM FWD PILOT SEATS UNDER FLOOR. BEGAN ON CLIMB AND W- PSI DIFF 4.8. INSPECTED SERVICE DOORS IN VICINITY OF NOISE, FOUND NOSE GEAR DOOR SEAL HAD LOOSE SECTION. SECURED NOSE GEAR DOOR SEAL.Nov 3, 2012 · N454UA · Airbus A320232 · Landing Gear DoorsSDR UALA2012110506353Tail Cone · crackedNR 1 ENGINE TAIL CONE CRACKED. EXISTING 4 INCH CRACK IN ZONE ONE OF NR 1 ENGINE TAIL CONE WAS STOP DRILLED CRACK HAS NOW MIGRATED A .5 OF AN INCH FORWARD. STOP DRILLED CRACK WITH 1-4" DRILL PER MM. TOTAL CRACK LENGTH IS NOW 5 INCHES.Nov 3, 2012 · N476UA · Airbus A320232 · Engine Collector/Tailpipe/Nozzle
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