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 CALA2016042895317Frame · damagedLEFT UPPER FUSELAGE FRAME 47, BUTT JOINT HOLE 35 AT STRINGER 7, HAS REJECT ABLE NDT INDICATIONS. REAMED HOLE IAW SRM 51-43- 00. NDT IAW NTM51-10-01, NO INDICATIONS. FINAL REAM & COLD WORK IAW SRM 51-43-00 & EA 5330-04861 OP 1.Apr 26, 2016 · N445UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2016042895318Door Sill · corrodedR2 DOOR SILL HAS CORROSION AT FRAME 66. REPLACED R2 DOOR SILL IAW SRM 51-42-11 & 51-72-11.Apr 26, 2016 · N445UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016042695303Battery · dischargedEMERGENCY LIGHT TEST FAILURE. EPSU BATTERY EMER RT. ACCOMPLISHED TSM TASK 33- 51-00-810-801-A. REPLACED EPSU BATTERY 12WL IAW AMM TASK 33-51-3 8.Apr 25, 2016 · N467UA · Airbus A320232 · Emergency LightingSDR CALA2016042695301Cleat · corrodedFRAME 31 CLEAT, BETWEEN STRINGER 43L & 43R, HAS CORROSION. R & R CLEAT FRAME 31 IAW SRM 51-42-11-001 & 53-21-12, NO FURTHER DAMAGE NOTED IN AREA.Apr 24, 2016 · N445UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016041895277Warning System · false activationAUTO BRAKE FAULT DISPLAYED ON UPPER ECAM SCREEN. TRIED NEW BSCU, SAME FAULTS, NO HELP. ACCOMPLISHED WIRING CHECK OF TACHOMETER WHEEL 4, 22GG, IAW AWD 32-11-02 & AWD 32-42-06. ALL CHECKED OK.Apr 14, 2016 · N417UA · Airbus A320232 · Landing Gear Brake SystemSDR CALA2016041895274Skin · gougedFORWARD CARGO DOOR EXTERIOR SKIN, UPPER AFT SKIN GOUGED. REPAIRED IAW SRM 52-31-00-201 FIG 209.Apr 12, 2016 · N477UA · Airbus A320232 · Cargo/Baggage DoorsSDR AALA201604099004Engine · slowAIRCRAFT WAS GNDED. 2 ENG SLOW TO SPOOL TO FLEX POWER TAKEOFF ABORTED. FOUND NO FAULTS ON THE ECAM, ACCOMPLISHED ACCELERATION & DECELERATION TEST IAW AMM 71-00-00-700-011-B13 & BOTH ENGS WERE WITHIN LIMITS. ACFT WAS RETURNED TO SERVICE.Apr 8, 2016 · N654AW · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2016041195266Skin · gougedFORWARD CARGO DOOR HAS A SKIN GOUGE AT THE UPPER AFT AREA. INSTALLED DOUBLER REPAIR IAW SRM 52-31-00-201 FIG 209Apr 8, 2016 · N477UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2016041195267Skin · corrodedLAVATORY BLOWER VENT HAS AREA OF SHEET METAL DAMAGE & CORROSION TO ACFT SKIN. INSTALLED INTERIM REPAIR IAW ECRA & 5341-01071 PART 1.Apr 8, 2016 · N421UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016040495249O-Ring · damagedLOW YELLOW QTY. FOUND LINE LOOSE PRESS MANIFOLD. REPLACED O RING, SECURED & LEAK CHECKED GOOD. SERVICED YELLOW SYS TO FULL.Apr 1, 2016 · N464UA · Airbus A320232 · Hydraulic System, MainSDR CALA2016033195243Fastener · looseFOUND LT MLG DOOR HINGE & ACT FITTING FASTENERS LOOSE. INTERIM REPAIRED MLG DOOR FITTING & KEEL BEAM SUPPORT STRUCTURE IAW ECRA 5330-05417.Mar 31, 2016 · N455UA · Airbus A320232 · Landing Gear DoorsSDR CALA2016040495250Fluid · lowYELLOW HYD SYS ECAM MSG, ZERO INDICATION. SERVICED YELLOW HYD QTY AS REQUIRED, NO LEAKS NOTED.Mar 31, 2016 · N484UA · Airbus A320232 · Hydraulic System, MainSDR CALA2016033195246Light · brokenSEAT 2B EMER LIGHT ASSEMBLY BROKEN. REPLACED EMER LIGHT ASSEMBLY IN SEAT SIDE PANEL IAW AMM 33-51-18. EMER LIGHT TESTED OK IAW AMM 33-51-00-710-001.Mar 30, 2016 · N419UA · Airbus A320232 · Emergency LightingSDR CALA2016032895233Stringer · corrodedAFT CABIN UNDERFLOOR AREA, STRINGER 31R CORRODED AT FRAME 65. CORRODED OUT OF LIMITS IAW SRM 53-41-13. R & R STRINGER 31R IAW SRM 51-42-11-001 PARA 7.Mar 27, 2016 · N439UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016032895234Power Supply · faultedEMERGENCY POWER SUPPLY UNIT AFT LT, FAULT MSG WHEN PERFORMING EMER LIGHTS TEST. REPLACED EMER POWER SUPPLY UNIT 13WL AFT LT IAW AMM 33-51-38. UNIT FAILED BITE.Mar 24, 2016 · N498UA · Airbus A320232 · Emergency LightingSDR CALA2016032895235Control Handle · faultyGEAR NOT LOCKED ECAM MSG. GO AROUND, CYCLED, MSG REMAINED. MANUAL EXTENSION FOUND LG SELECTOR HANDLE AT FAULT, REPLACED SAME. OPERATIONS CHECKED GOOD.Mar 23, 2016 · N480UA · Airbus A320232 · Landing Gear SelectorSDR CALA2016032195219Door Sill · corrodedL2 DOOR SILL HAS CORROSION FRAME 68 AT NUTPLATES, STRINGER 23L. REMOVED CORROSION, L2 DOOR SILL NUTPLATES, FOUND TO BE OUT OF LIMITS. FABRICATED & INSTALLED REPAIR ANGLE IAW SRM 53-41-14-201 FIG 201 REPAIR 5.Mar 18, 2016 · N439UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016031495213Connector · looseEMERGENCY LIGHTS OPERATIONAL TEST FAILED. EPSU LT FAILED. FOUND EPSU LT FWD MSG, RESET CONNECTOR ON FWD LT EMER LIGHT POWER SUPPLY & SYS CHECKED GOOD NOW. TESTED OK.Mar 12, 2016 · N481UA · Airbus A320232 · Light System WiringSDR CALA2016030895207Door Frame · out of adjustRETURN TO FIELD. POST DEPARTURE LOUD NOISE RESEMBLING A BANG, HEARD BY FLIGHT CREW FOUND COCKPIT ENTRY DOOR HEADER JAMB OUT OF ADJUSTMENT, ALLOWING THE HINGED UPPER CORNER OF HEADER TO BUTT UP TO HINGE COVER. ADJUSTED HEADER JAMB, DOOR OPERATIONS NORMAL.Mar 4, 2016 · N487UA · Airbus A320232 · Flight Compartment EquipmentSDR YENA20160229154Eec · faultedDIVERTED BACK TO DEPARTURE, ON CLIMBOUT NR 2 ENGINE ROLLED BACK TO ABOUT 50 PERCENT THEN BACK TO CLIMB POWER THEN ROLLED BACK TO ZERO POWER. THE LOCK ENGAGED AFTER PERFORMING ECAM N1 MODE WAS COMMANDED AND EG APPEARED TO BE STABLE. PERFORMED TSM TASK 73-22-0Feb 29, 2016 · N804JB · Airbus A320232 · Fuel Controlling SystemSDR CALA2016022495133Unknown · malfunctionedFAULT, INT LOADS AFT L, DISPLAYED DURING EMER EXIT LIGHT 2CVS TESTS. CYCLED EMER LIGHT CB`S, RESET SYS. OPERATIONS CHECKED GOOD.Feb 22, 2016 · N417UA · Airbus A320232 · Emergency LightingSDR CALA2016022495132Fire Bottle · dischargedAFT CARGO DET FAULT DISPLAYED ON UPPER ECAM SCREEN, SHOWING AFT CARGO SMOKE DISCHARGE AGENT 2 DISPLAYED. INSPECTION FOUND SECURE. REPLACED FWD CARGO FWD BOTTLE IAW AMM 26-23-00-200-005-A SEE PTT 5002010.Feb 21, 2016 · N482UA · Airbus A320232 · Fire Bottle, FixedSDR CALA2016021995118Slat · dentedNUMBER 2 RT SLAT, PN 5746022700100, SN SA22 90, DENTED 4" FROM OTBD EDGE. CUT OUT DAMAGE & REPAIRED IAW SRM 57-4 0-00 FIG 207 SHEET 5, SR I57-40-00-2-003-00 PARA 3C TBL 204.Feb 19, 2016 · N464UA · Airbus A320232 · Leading Edge DevicesSDR CALA2016021995121Battery · failedFORWARD EMER LIGHT POWER BATTERY FAILED. REPLACED FWD EPSU BATTERY IAW AMM 33-51-38. OPERATIONS CHECKED GOOD.Feb 18, 2016 · N433UA · Airbus A320232 · Emergency LightingSDR CALA2016021995120Slide · faultedEMERGENCY LIGHTS OPERATIONAL TEST FAILED SHOWING FAULT, EXT LOADS FWD L. REPLACED DOOR SLIDE AT 1L IAW AM 25-62-44-400-006. OPERATIONS CHECKED GOOD.Feb 16, 2016 · N428UA · Airbus A320232 · Escape SlideSDR AALA201602069001Actuator · defectiveABORTED TAKEOFF, ACFT WAS GNDED. SHORTLY AFTER APPLICATION OF TAKEOFF POWER, FLEX, GOT ECAM ENG 2 COMPRESSOR VANE PLUS ECAM ACTION. AVOID RAPID THRUST LEVER CHANGE, THRUST LEVER IDLE. CREW ABORTED TAKEOFF AT 85 KNOTS & RETURNED TO THE GATE WITHOUT FURTHER IFeb 5, 2016 · N664AW · Airbus A320232 · Compressor Bleed ControlSDR CALA2016020995095Ptu · malfunctionedLOST GREEN QTY, PFR INDICATES HYD G RSVR LO LVL, HYD G ENG 1 PUMP LO PR & HYD G SYS LO PR. R & R THE PTU IAW AMM 29-23-41.Feb 5, 2016 · N425UA · Airbus A320232 · Hydraulic Pump, AuxiliarySDR CALA2016020495089Slide · defectiveDOOR 2R ARMING LEVER WILL NOT STAY FLUSH WITH DOOR. INSTALLED SERVICEABLE R2 DOOR SLIDE PACK IAW AMM 25-62-44. OPERATIONS CHECKED ARMING LEVER SEVERAL TIMES, NO DEFECTS NOTED AT THIS TIME.Feb 4, 2016 · N445UA · Airbus A320232 · Escape SlideSDR AALA201602049001Filter · cloggedAIRCRAFT WAS NOT GNDED. AFTER TAKEOFF, ECAM ENG 2 FUEL FILTER CLOG. REPLACED BOTH ENG FUEL FILTERS & ACCOMPLISHED SATISFACTORY LEAK & OPERATIONAL CHECKS IAW AMM 73-12-42-0401-13.Feb 3, 2016 · N661AW · Airbus A320232 · Engine Fuel DistributionSDR CALA2016020395072Flap · faultedF CTL FLAP SYS 1 FAULT. CYCLED CB B6 - B7, NO HELP. REPLACED SFCC1 COMPUTER PERM 27-51-34, SYS OPERATIONS OK. POST FLIGHT REPORT, FAULTED SFCC1.Feb 1, 2016 · N481UA · Airbus A320232 · Trailing Edge Flap Control SystemSDR CALA2016020395077Blower · seizedELECTRICAL BURNING ODOR IN COCKPIT. BLOWER FAULT DISPLAYED ON UPPER ECAM SCREEN 20HQ CONTROL CB POPPED. FOUND BLOWER SEIZED WITH STRONG BURNT ODOR. R & R BLOWER. CHECKS GOOD, FAULT CLEARED.Jan 31, 2016 · N488UA · Airbus A320232 · Air Distribution SystemSDR CALA2016020395069Stringer · corrodedCORROSION FOUND ON STRINGER 31R AT AFT OF FRAME 65. R & R STRINGER 31R AT FRAME 64 - 67 IAW SRM 51-42-11 PARA 6 & 7.Jan 30, 2016 · N462UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016020395067Relay · faultyGEAR EXT LIGHTS DID NOT ILLUMINATE ON LANDING. GEAR PANEL ECAM WHEEL PAGE SHOWED MX TEXT. ALL GREEN INDICATIONS RETURNED ALL GREEN AT 500' RA. FOUND BOTH RED & GREEN LIGHTS NOT WORKING WHILE CYCLING GEAR. GREEN D & L WOULD COME ON AFT ER 3 - 5 MIN. REPLACJan 29, 2016 · N417UA · Airbus A320232 · Landing Gear Position and WarningSDR YENA20160129091Eec · failedDIVERTED, ENGINE 2 EPR MODE FAIL; R & R ENGINE NR2 ENGINE, ELECTRONIC ENGINE CONTROL IAW AMM 73-22-34.Jan 29, 2016 · N784JB · Airbus A320232 · Fuel Controlling SystemSDR CALA2016012595023Panel · malfunctionedON TAXI, CAPTAINS CRT ELEC BURN SMELL IN COCKPIT, THEN RETURNED TO NORMAL. SWAPPED PANEL WITH LOWER ECAM PANEL, PFD MR 31622-362, SERIAL 2512729 IN LOWER ECAM POSITION, ECAM PANEL INSTALLED IN PFD MR 3162 2-132, SERIAL 1917428.Jan 22, 2016 · N485UA · Airbus A320232 · Central DisplaySDR CALA2016020495085Display · malfunctionedON TAXI CAPTAINS CRT BLANK WITH ELEC BURN SMELL IN COCKPIT & THEN RETURNED NORMAL. REPLACED AS A PRECAUTION CAPTAINS PFD IAW AMM 31-63-22 7 TESTED EIS IAW AMM 31-60-00-710-00 1A. ACCOMPLISHED AFS TEST & AUTO LAND TEST IAW AMM 22-97-00-710-001.Jan 22, 2016 · N485UA · Airbus A320232 · Central DisplaySDR CALA2016012595022Light · malfunctionedREF 2 SVC, EMER LIGHTS FAILED TEST. RESET CIDS PANEL. EMER LIGHT TEST PASSED.Jan 21, 2016 · N436UA · Airbus A320232 · Emergency LightingSDR CALA2016012295013Battery · faultedEMERGENCY POWER SUPPLY UNIT BATTERY EMER LIGHT FAULT DURING TEST. REMOVED & REINSTALLED BATTERY, FAULT CLEARED & BITE CHECKED GOOD.Jan 20, 2016 · N480UA · Airbus A320232 · Emergency LightingSDR CALA2016011895007Connector · looseAIRCRAFT RETURNED TO FIELD DUE TO INABILITY TO PRESSURIZE. DURING TROUBLESHOOTING FOUND CONNECTOR 2421VC, BEHIND 25VU IMPROPERLY CONNECTED. LOOSE, NOT TIGHTLY CONNECTED. INSPECTED & SECURED. PERFORMED PRESSURIZATION TEST IAW 21-31-00-710-002-A. ALL TEST PJan 17, 2016 · N456UA · Airbus A320232 · Air Conditioning System WiringSDR CALA2016011895005Doubler · corrodedLAVATORY SERVICE PANEL, INTERIOR DOUBLER HAS CORROSION. EVALUATED CORROSION, FOUND TO BE OUT OF LIMITS. R & R INTERIOR DOUBLER.Jan 15, 2016 · N414UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016011895006Skin · corrodedDURING HORIZONTAL STAB INSPECTION FOUND SKIN TO HAVE INTERGRANULAR CORROSION, FWD OF DOOR 312AR, AT APPROX STRINGER 25 RT, STATION 3366, FRAME 70 APB. ACCOMPLISHED REPAIR IAW ECRA 5330-05303 STEPS 1 A & B.Jan 15, 2016 · N431UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR AALA201601129011Apu · odorAFTER LANDNG USED APU BLEED, HAD A BURNED FUEL SMELL OR DIRTY SOCK SMELL. REPLACED APU & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW TASK CARD 26L31049005.Jan 10, 2016 · N657AW · Airbus A320232 · APU Core EngineSDR CALA2016010894976Skin · corrodedDURING HORIZONTAL STAB INSPECTION FOUND SKIN TO HAVE INTERGRANULAR CORROSION FWD OF DOOR 312AR AT APPROX STRINGER 25 RT, STATION 3366, FRAME 70 APB. ACCOMPLISHED REPAIR IAW ECRA 5330-05303 STEPS 1 A & B.Jan 7, 2016 · N431UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016010894962Wire Harness · damagedON TWO SERVICE FOUND LT AFT 3 EMER EXIT LIGHTS INOPERATIVE. NO VOLTAGE AT 36 ABC EMER EXIT LIGHT HARNESS. REPAIRED WIRE AT CONNECTOR, WDM 33-51-04. EMER EXIT LIGHTS CHECKED GOOD.Jan 5, 2016 · N423UA · Airbus A320232 · Light System WiringSDR CALA2016010894965Feeder Cable · unsecureLEFT AFT EMER BATTERY IS INOPERATIVE. SECURED POWER FEEDER. OPERATIONS GOOD.Jan 5, 2016 · N423UA · Airbus A320232 · Light System WiringSDR CALA2015121794909Skin · dentedFORWARD CARGO DOOR, OUTER SKIN SURFACE, FRAME 25A & RIB 4 - 5 HAS DENT. DENT ON FWD CARGO DOOR OUTER SKIN SURFACE OUT OF LIMITS IAW SRM 52-30-00 PARA 4 E FIG 105. REPAIRED INSTALLING A REPAIR DOUBLER IAW SRM 52-31-00 PARA 5 I FIG 209.Dec 17, 2015 · N411UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2015121794910Skin · dentedFORWARD CARGO DOOR OUTER SKIN SURFACE FRAME 27 & RIB 3 - 4 HAS DENT. DENT ON FWD CARGO DOOR OUTER SKIN SURFACE WAS OUT OF LIMITS IAW SRM 52-30-00 PARA 4 E FIG 105. REPAIRED INSTALLING A REPAIR DOUBLER IAW SRM 52-31-00 PARA 5 I FIG 209.Dec 17, 2015 · N411UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2015121794896Director · faultyEVAC ALARM, CANT SILENCE. REPLACED NR 2 CIDS DIRECTOR IAW AMM 23-73-34-400-001-A. BITE TEST OK IAW AMM 23-73-00-740-003.Dec 15, 2015 · N402UA · Airbus A320232 · Audio/Video MonitoringSDR CALA2015121494888Stringer · damagedSTRINGER 35R, FRAME 65 - 66 HAS OUT OF ROUND HOLES. REMOVED DAMAGED STRINGER 35R FROM FRAME 65 - 66. FABRICATED REPLACEMENT STRINGER. LOCATED, DRILLED & DEBURRED, INSTALLED & REST ORD SURFACE PRO IAW SRM 51-75-12.Dec 11, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015121494889Doubler · corrodedWASTE PANEL INTERNAL DOUBLER CORRODED. REMOVED WASTE SERVICE PANEL, REMOVED FRAME CLIPS & STRINGER CLIPS AT REQUIRED & REMOVED WASTE PANEL INT DOUBLER. FABRICATED REPLACEMENT DOUBLER, LOCATED, DRILLED & DEBURRED. INSTALLED DOUBLER, FRAME CLIPS & STRINGER CLDec 11, 2015 · N458UA · Airbus A320232 · Fuselage Main, Plate/Skin
Back to IAE V2527-A5