IAE V2527-A5

Service difficulty reports · 8,011

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 UALA2012042002353Handle · out of adjustL2 DOOR HANDLE RIDES UP IN FLIGHT DISARMING DOOR SLIDE. ADJUSTED DOOR ESCAPE SLIDE MECHANISM PER AMM. PRESSURIZED ACFT & CHECK DOOR HANDLE ALL INDICATIONS & DOOR HANDLE CHECKS NORMAL.Apr 17, 2012 · N405UA · Airbus A320232 · Escape SlideSDR UALA2012041702321Wire · chafedCAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. SWAPPED CAPT'S AND SECOND OBS O2 STORAGE BOXES DUE TO A CHAFED WIRE. CAPT'S MASK NOW OPS CHECKS NORMAL FOR AUDIO AND O2.Apr 16, 2012 · N467UA · Airbus A320232 · Oxygen System WiringSDR UALA2012041502265Socket · dirtyEXT OVERWING EMERGENCY LIGHTS INOPERATIVE BOTH SIDES OF ACFT. TROUBLESHOT PER MM, CLEANED FWD LIGHT SOCKET ON AFT LIGHT ASSY. OPS CHECKED GOOD.Apr 15, 2012 · N401UA · Airbus A320232 · Emergency LightingSDR UALA2012041502266Connector · unsecureSEAT 32 LT EMERGENCY LIGHT INOPERATIVE. RESEATED ELECTRICAL CONNECTOR REF ESPM. OPS CHECKED GOOD.Apr 15, 2012 · N418UA · Airbus A320232 · Light System WiringSDR UALA2012041702292Stringer · corrodedAFT CARGO PIT STRINGER 42L CORRODED BETWEEN FR56 AND FR59. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED STRINGER SECTION AND EXISTING STRINGER SPLICES. FABRICATED & INSTALLED NEW STRINGER SECTION FROM FR53 - FR59 WITH STRINGER SPLICE REPAIRS LOCATED BETWEEN Apr 15, 2012 · N418UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2012041502276Conduit · unsecureCREW REPORT: STILL HAVE OCCASIONAL LOUD HUMMING IN FWD GALLEY ONCE PRIOR TO LEVEL OFF AND JUST AFTER DESCENT. OPENED CEILING PANELS IN FWD GALLEY FOUND ENTRY LIGHT CONDUITS NOT SECURED, SECURED CONDUITS. NO OTHER DEFECTS FOUND. REINSTALLED PANELS.Apr 15, 2012 · N484UA · Airbus A320232 · Passenger Compartment LightingSDR UALA2012041502253Strap · looseDOOR 2L SLIDE ARMING HANDLE IS NOT FLUSH WHEN IN THE ARMED POSITION. SECURED LOOSE SLIDE COVER STRAPS. ARMING HANDLE OPERATES NORMAL.Apr 14, 2012 · N405UA · Airbus A320232 · Emergency EquipmentSDR UALA2012041502259Panel · no testEMERGENCY LIGHT SYS WON`T TEST FROM FWD FLT ATT PANEL. REPLACED PTP PANEL PER MM, ALL GND TESTS GOOD.Apr 14, 2012 · N429UA · Airbus A320232 · Emergency LightingSDR UALA2012041502260Arm · crackedNR 3 RUDDER HINGE ARM CRACKED. REMOVED AND REPLACED NR 3 RUDDER HINGE ARM.Apr 14, 2012 · N418UA · Airbus A320232 · Rudder StructureSDR UALA2012041502261Stringer · corrodedAFT CARGO COMPARTMENT, STRINGER 43L CORRODED BETWEEN FR 54 & 55. REMOVED CORROSION & FOUND MATERIAL LOSS OUT OF LIMITS OF SRM. REMOVE STRINGER SECTION FROM FR54 - FR60. FABRICATED & INSTALLED NEW STRINGER SECTION. MAJOR REPAIRApr 14, 2012 · N418UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2012041502273Structure · scratchedFOUND 12 INCH SCRATCH 8 INCHES FWD OF AFT UPPER RVSM CORNER MARKER RT SIDE. VERTICAL SCRATCH WITH 5 INCHES INTO RVSM AREA AND 7 INCHES UPWARD TOWARD F/O SLIDING WINDOW. APROX LOCATION FR6. REPAIRED REF SRM 53-11-11 DIAG 101 SHT 2 AND SRM ITEM 'B' AND EDDY CUApr 14, 2012 · N442UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012041502287Fan · faultyVERY LOUD ELEC MOTOR NOISE BETWEEN BULKHEADS IT IS VIBRATING THE FLOOR. RPLD MIXED FLOW FAN PER MM. OPERATE PACKS. NO NOISE NOTEDApr 14, 2012 · N477UA · Airbus A320232 · Air Distribution FanSDR GTIA20120413401Cylinder · low pressureR2 DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001. NO OTHER DEFECTS NOTED AT THIS TIME.Apr 13, 2012 · N607NK · Airbus A320232 · Passenger/Crew DoorsSDR UALA2012041302235Cover · missingL2 DOOR EMERGENCY LIGHT COVER MISSING. REPLACED AFT ATTENDANT LIGHT PANEL, OP CHECKED GOOD. EMERGENCY EXIT PATHWAY AND EXIT LIGHTING OPS CHECKED GOOD.Apr 13, 2012 · N417UA · Airbus A320232 · Emergency LightingSDR UALA2012041202206Actuator · leakingRAMP REPORTS FUEL LEAK ON ENGINE 2 AFTER ENGINE START. ACCOMPLISHED IDLE ENG RUN TWICE, STEADY STREAM FUEL LEAKS FROM CORE DRAIN BEYOND LIMITS OF MM. ISOLATED TO SLAVE LPC BLEED ACTUATOR. REPLACED ACTUATOR PER MM, IDLE LEAK CHECK OK.Apr 12, 2012 · N457UA · Airbus A320232 · Compressor Bleed ControlSDR UALA2012041302224Skin · dentedDENT IN NR 4 SLAT BOTTOM SURFACE. SLAT REPAIRED. REINSTALLED ORG SLAT PER AMM 27-84-66.Apr 12, 2012 · N471UA · Airbus A320232 · Leading Edge DevicesSDR UALA2012041302232Floor Panel · damagedFLOOR PANEL 192LB DAMAGED HAS A 2 INCH CRACK IN THE LIP AREA.Apr 12, 2012 · N438UA · Airbus A320232 · Fuselage Floor PanelSDR UALA2012041302243Seal · leakingOIL LEAKING FROM BACK OF NR 1 ENGINE 1ST STAGE COMPRESSOR BLADES BEHIND SPINNER CONE AT 6 O'CLOCK POSITION. REPLACED BOTH SEALS IN THE LOW PRESS TURBINE SHAFT BLIND CAP COMPARTMENT. ALSO COMPLIED WITH COMPARTMENT OIL RETURN LINE COKING INSPECTION. NO COKINGApr 12, 2012 · N409UA · Airbus A320232 · Turbine Engine Compressor SectionSDR UALA2012041302239Support Bracket · crackedLT BELLY FAIRING SUPPORT BRACKET UPPER ANGLE HAS .5 INCH CRACK AT FRAME 46 BELOW KEEL BEAM. VIEW FROM AFT SIDE OF WHEEL WELL WITH PANEL 147EB REMOVED. VERIFIED WITH HFEC, CRACK TO BE 1 INCH LONG. MAX LIMIT IS 4.5 INCH. NEEDS VISUAL REINSPECT EVERY 500 CYCLApr 12, 2012 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012041302240Angle · crackedRT BELLY FAIRING SUPPORT BRACKET UPPER ANGLE HAS .5" CRACK AT FRAME 46 BELOW KEEL BEAM. VIEW FROM AFT SIDE OF WHEEL WELL WITH PANEL 147EB REMOVED. VERIFIED WITH HFEC, CRACK TO BE .5" LONG. MAX LIMIT IS 4.5". TRIMMED DRILLED AND DEBURRED REPAIR ANGLE IAW SApr 12, 2012 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012041302241Skin · damagedLEFT WING ACCESS HOLE FOR FUEL PANEL 540HB HAS 1 EA ELONGATED HOLE IN WING LOWER SKIN. HOLE IN LANDING LOCATED BETWEEN RIBS 13 AND 14. EVALUATED HOLE FOR OVERSIZING, GENERATED AN RFTS TO EG. REAMED HOLE TO FINAL SIZE OF .578 ", ACCMP'D BHEC PER NDT 6-51-10Apr 12, 2012 · N454UA · Airbus A320232 · Wing, Plate/SkinSDR UALA2012041302244Sleeve · damagedDURING NR 1 ENGINE INBOARD BLISTER FAIRING REPAIR PER MAINT TIP 78-014A ACCIDENTALLY DRILLED THE BEAM FITTING LOCATED BELOW THE FAIRING. NR 1 ENGINE THRUST REVERSER SLEEVE REPLACED PER MM. SYS OPS AND INSTALL OK NORMAL.Apr 12, 2012 · N447UA · Airbus A320232 · Engine Thrust ReverserSDR UALA2012041202221Control Unit · faultySYS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. MAINT CHECKED PFR, AND PLR SHOWED CFDS FAULT MESSAGE NO BSCU 2 DATA REPEATEDLY. REPLACED BSCU, GROUND CHECKED OK PER MM. ALSO ACCOMPLISHED CAT III CHECK. OK PER MM.Apr 11, 2012 · N424UA · Airbus A320232 · Landing Gear Brake SystemSDR UALA2012041302226Trunnion · wornRIGHT INBOARD FLAP TRUNNION WORN TO MAX LIMIT. REPLACED TRUNNION PER MT57-019.Apr 11, 2012 · N454UA · Airbus A320232 · Trailing Edge FlapsSDR UALA2012041202195Wire Harness · damagedSEAT 21C & 26C EMERGENCY FLOOR LIGHTS ARE INOP. NO TIME. FOUND LOOSE CONNECTION ON SEAT 26C. SECURED CONNECTOR UNDER SEAT 26C, OPS CKS NORMAL. SEAT 21C STILL INOPERATIVE. REPLACED HARNESS AT 21C. OPS GOOD.Apr 10, 2012 · N409UA · Airbus A320232 · Light System WiringSDR UALA2012041202205Battery · no testTHE 1 LT EPSU FAILED EMERGENCY LIGHT TEST. REPLACED BATTERY PER AMM, TESTED NORMAL.Apr 10, 2012 · N408UA · Airbus A320232 · Emergency LightingSDR UALA2012040902165Knob · looseCAPTAIN`S RMP UPPER FREQUENCY KNOB LOOSE. BOTH KNOBS AND THE RMP OPS OK, JUST LOOSE. REMOVED AND REPLACED CAPTAIN`S RMP PANEL, OPS CHECKED GOOD.Apr 9, 2012 · N401UA · Airbus A320232 · Flight Compartment EquipmentSDR UALA2012040902191Scavenge Pump · failedTOWER REPORTED SMOKE FROM NR 2 ENGINE. ACCOMPLISHED BOROSCOPE OF OIL FEED LINES PER MT72-022 NO COKING NOTED. ACCOMPLISHED INSPECTION OF NR 5 BEARING COMPARTMENT PER MT72-033, NO BLOCKAGE NOTED. REINSTALLED LINES AND COVERS. FOUND OIL PUDDLING AT BASE OF TApr 8, 2012 · N404UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR UALA2012040902181Starter · failedON NR 1 ENGINE START UP, GROUND CREW NOTICED SPARKS UNDER FAN COWL. FLT CREW NOTICED NO INDICATIONS. R & R NR 1 ENGINE STARTER PER MM, OPS CHECKED NORMAL WITH NORMAL ENGINE START AND RUN.Apr 8, 2012 · N449UA · Airbus A320232 · Engine StarterSDR UALA2012040902150Spring · migratedDURING WALK AROUND FOUND NR 2 NLG DOWNLOCK SPRING MIGRATING. REPLACED SPRING.Apr 7, 2012 · N478UA · Airbus A320232 · Nose/Tail Landing GearSDR UALA2012040902148Sill · corrodedR2 DOOR SILL HAS CORROSION AT DRAIN HOLES. INSTALLED NEW SILL, MAJOR REPAIRApr 6, 2012 · N454UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012040902178Amu · malfunctionedCAPTAIN CAN HEAR FIRST OFFICER LOUD AND CLEAR WITH ALL SWITCHES OFF. BLEED OVER ONLY OCCURS WHEN FIRST OFFICER TRANSMITS ON VHF 2. BLEED OVER ONLY OCCURS ON MINITEL, NOT SPEAKER. REPLACED AUDIO MGMT UNIT AND TASK.Apr 6, 2012 · N426UA · Airbus A320232 · Audio Integrating SystemSDR UALA2012040602133Cover · delaminatedRIGHT OFF WING SLIDE COVER DELAMINATED AFT EDGE ABOVE SLIDE OPENING. REPLACED OF WING SLIDE. SLIDE ASSY IS SECURE ON ACFT, LINE IS SECURE, INFLATION CYL SAFETY PIN IS REMOVED AND STOWED, EMERGENCY LIGHTS TEST OK. ACFT RETURNED TO NORMAL OPS.Apr 6, 2012 · N458UA · Airbus A320232 · Escape SlideSDR UALA2012040502102Battery Pack · failedTHE 3SV EMERGENCY LIGHT TEST FAILED. REPLACED BATTERY PACK PER MM, TESTED GOOD.Apr 5, 2012 · N460UA · Airbus A320232 · Emergency LightingSDR UALA2012040602128Oil Cooler · leakingNR 1 ENGINE HAS OIL LEAKING AFT OF DRAIN MAST FROM BOTH SIDES OF COWL LATCH. NO EVIDENCE OF OIL LEAK FROM ENGINE DRAINS WITH FAN COWL OPENED DURING IDLE RUN, ALSO CHECKED OIL COOLER AREA ON RT SIDE UNDER FAN COWL, EVIDENCE OF OIL LEAK AT OIL COOLER WITHIN 10Apr 5, 2012 · N429UA · Airbus A320232 · Engine Oil CoolerSDR UALA2012040602134Skin · wornNR 1 PYLON LOWER SKIN WORN AS DEEP AS .020 ALONG ENTIRE WIDTH OF PYLON. LOCATED 12" AFT OF AFT ENG MOUNT. BLENDED AREA. AREA LOCATED 5.125 AFT OF RIB 5. OKAY TO CF PER SRM. NEEDS TO BE RE-EVALUATED AND REPAIRED AT NEXT "C" CHECK OR 4500 FLIGHT CYCLES OR 20Apr 5, 2012 · N454UA · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR UALA2012040602145Tail Cone · crackedNR 1 EXHAUST TAIL CONE HAS A CRACK AT 10 O'CLOCK POSITION APPROX 6 INCHES LONG. FOUND CRACK TO BE 4.5 INCH LONG, STOP DRILLED CRACK.Apr 5, 2012 · N486UA · Airbus A320232 · Engine Collector/Tailpipe/NozzleSDR UALA2012040602144Seal · unsecureFLIGHT ATTENDANT REPORT LOW FREQUENCY VIBRATION CENTER AISLE AROUND EXIT ROW. CYCLES ON AND OFF. FOUND TAPE TORN, NOTED RT FAIRING PANEL SEAL LOOSE AND LIFTED UP. APPLIED TAPE OVER SEAL PER MT 53-04. NO OTHER DEFECTS. FOUND SEAL IN GOOD CONDITION. Apr 5, 2012 · N462UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012040402081Rub Strip · damagedLEFT WING RUB STRIP STICKING UP ON INBOARD FLAP. REPLACED RUB STRIP IAW SRM.Apr 4, 2012 · N470UA · Airbus A320232 · Wing Miscellaneous StructureSDR UALA2012040402087Windshield · faultyECAM LEFT WINDSHIELD HEAT INOPERATIVE. WINDOW HEAT SENSOR & SPARE IS INOPERATIVE. INSTALLED CAPTAIN'S WINDSHIELD UP TO STEP E8 OF MM. ALSO COMPLETED STEP 'F' CHECK OF CLEARANCES. ICE DETECTION PROBE WIRES NOT CONNECTED. FINISHED INSTALLATION OF CAPTAIN'SApr 4, 2012 · N465UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2012040502119Sensor · faultyECAM IN FLIGHT. DOOR R AFT CABIN. LASTED 1 MINUTE. DOORS PAGE SHOWED OPEN. REPEAT GRIPE. REPLACED SENSOR 17WV2 & ADJUSTED PER MM, CHECKED GOOD.Apr 4, 2012 · N428UA · Airbus A320232 · Door Warning SystemSDR UALA2012040402083Line · chafedBLUE SYS HYD LOSS. FOUND LINE CHAFED BY CLAMP. REPLACED LINE.Apr 4, 2012 · N432UA · Airbus A320232 · Hydraulic System, MainSDR GTIA20120403396Cylinder · low pressureR1 DOOR ASSIST BOTTLE HAS LOW PRESSURE. SERVICED 1RT DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001.Apr 3, 2012 · N606NK · Airbus A320232 · Passenger/Crew DoorsSDR UALA2012040302064Ram Air Turb · no testRAT FAILED TEST. OPENApr 3, 2012 · N401UA · Airbus A320232 · Hydraulic System, AuxiliarySDR UALA2012040402088Circuit Breaker · unknownCOND AFT CARGO HEAT FAULT. RESET CIRCUIT BREAKER FOR CARGO HEAT AND PERFORMED POWER UP BITE TEST FOR CARGO HEAT CONTROLLER, OPS CHECKED OK.Apr 3, 2012 · N464UA · Airbus A320232 · Air Conditioning System WiringSDR UALA2012040402090Smoke Detector · faultedSMOKE LAVATORY DETECTOR FAULT. REPLACED THE LAV 'A' SMOKE DETECTOR, OPS CHECK GOOD.Apr 3, 2012 · N466UA · Airbus A320232 · Smoke DetectionSDR UALA2012040402095Sleeve · out of positionGAP BETWEEN ENGINE THRUST REVERSER SLEEVE AND FAN COWLING. NR 1 ENGINE APPROX 7 O'CLOCK POSITION. REPAIRED RUB STRIP. STILL MISMATCHED BY 070. OK PER MT 71-031 AND AMM 71-10-00-607 FOUND THAT .070 INCH UNDERFAIR (OUT OF WIND) TO BE ACCEPTABLE. THE REVERSApr 3, 2012 · N465UA · Airbus A320232 · Engine Thrust ReverserSDR UALA2012040402089Lock · lack of lubeF/O RUDDER PEDALS DO NOT LOCK IN PLACE. LUBE & CLEAN LOCKING PLATE, OPS CHECK GOOD.Apr 3, 2012 · N459UA · Airbus A320232 · Rudder Control SystemSDR UALA2012040302066Oil Cooler · leakingDURING ENGINE RUN, FOUND WETNESS AT BOTTOM OF FUEL OIL COOLER BOTTOM FWD CAP. UNABLE TO IDENTIFY POSITIVE SOURCE, WETNESS IS ENTIRE BOTTOM AREA OF OIL COOLER. UNABLE TO FIND LEAK ON NR 2 ENG FUEL OIL COOLER. REPLACED FUEL OIL COOLER.Apr 3, 2012 · N431UA · Airbus A320232 · Engine Oil CoolerSDR UALA2012040302067Battery Pack · faulty"INTL LOADS FWD L" FAULT MESSAGE WHEN PERFORMING EMERGENCY LIGHTS TEST. REPLACED BATTERY PACK AND GROUND CHECKED OKAY.Apr 3, 2012 · N431UA · Airbus A320232 · Emergency Lighting
Back to IAE V2527-A5