IAE V2527-A5

Service difficulty reports · 8,009

Newest first. General aviation reporting is voluntary.

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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 CALA2014071191421Door Sill · corrodedR2 DOOR SILL HAS CORROSION FRAME 66 & STRINGER 23R. BLENDED CORROSION ON R2 DOOR SILL BEAM OUT OF LIMITS IAW SRM51-41-14 FIG 101. R & R BEAM IAW SRM 51-42-11 PAGES 6 - 7.Jul 5, 2014 · N491UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014071191425Control Unit · malfunctionedNUMBER 2 GENERATOR WILL NOT COME ON LINE, LOW VOLTS. ACCOMPLISHED NR 2 IDG CONTROL UNIT RESET IAW TSM -24-22-00-810-818. RAN BOTH ENGS PERFORMED LOAD SHED ON AC BUS, NR 2 ENG IDG OPERATIONS CHECKED NORMAL.Jul 5, 2014 · N495UA · Airbus A320232 · AC Generator-AlternatorSDR CALA2014071191429Skin · scratchedEXTERIOR FUSELAGE SKIN HAS SCRATCH JUST BELOW AOA VANE MOUNT PLATE. BLENDED SCRATCH ON LT FUSELAGE SKIN, 6.5 INCHES FWD OF FRAME 24 ABOVE SKIN LAP AT STRINGER 28 IAW SRM 51-73-00 PARA F PG 5. HFEC REVEALED NO CRACK INDICATION.Jul 5, 2014 · N463UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2014071191416Door Sill · corrodedCABIN R2 DOOR SILL FRAME 66 HAS EVIDENCE OF CORROSION. R & R R2 DOOR SILL AT FRAME 66 - 68 IAW SRM51-42-11. NO SRI INSPECTION NOTED.Jul 4, 2014 · N482UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014071191428Selector Valve · leakingFLUID COMING OUT AROUND NOSE STRUT. R & R LEAKING NLG STEERING SWIVEL SELECTOR VLV.Jul 4, 2014 · N423UA · Airbus A320232 · Landing Gear Steering SystemSDR CALA2014071191414Skin Panel · saturatedRIGHT ELEVATOR UPPER SKIN PANEL HAS A WATER INGRESS INDICATION AT 39 INCHES FROM INBD END 6 INCHES FROM TE 6 INCHES IN DIAM. DRILLED WITNESS HOLES, CUT OUT 28.26 SQ INCHES OF SKIN. REMOVED WATER & APPLIED A NEW CORE PLUG. THIS REPAIR REFERS TO IIR 55-21-11-Jul 3, 2014 · N482UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014071191415Skin · saturatedRIGHT UPPER SKIN SHOWS SIGNS OF WATER INGRESS AT 101 INCHES FROM INBD END 5 INCHES FROM TE 7 INCHES IN DIAM. REPAIRED IAW SRM 55-21-11 RPR 5 E PARA 2 A - B CONFIG 1 FIG 205. THIS REPAIR REQUIRES INSPECTION IAW SRI 55-21-11-2-002-00 TABLE 203. FIRST INSPECTIJul 3, 2014 · N482UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014070191394Cover · missingPLASTIC COVER AT LT MLG HINGE POINT IS MISSING. INTERIM REPAIR ACCOMPLISHED. REQUIRES DAILY INSPECTION TO ENSURE INTEGRITY OF THE REPAIR & A NEW LT MLG LEG BEARING BLANKING PLUG MUST BE INSTALLED WITHIN 25 FLT HRS IAW ECRA 3211-01346. DL2030 CREATED TO MONIJul 1, 2014 · N407UA · Airbus A320232 · Main Landing GearSDR CALA2014070191395Door Sill · corrodedL2 DOOR SILL HAS CORROSION AT FRAME 66 STRINGER L23 BOTTOM SURFACE. CORROSION FOUND OUT OF LIMITS IAW SRM 53-41-14 PB 102 FIG 101. 0.035 LOSS REPAIRED SILL IAW SRM53-41-14 PB202 P5-A FIG 101 PRP 1 SHEET 2 CAT A REPAIR NO FURTHER ACTION.Jul 1, 2014 · N491UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014070191396Transmitter · faultyCAPTAINS NOSE WHEEL STEERING PEDALS DISCONNECT PUSH BUTTON INOPERATIVE WHEEL. FIRST OFFICERS BUTTON OPERATES NORMAL. TRIED NEW TRANSMITTER BUT WOULD NOT PASS FUNCTION TEST AMM 32-51-00-720-007. NEW TRANSMITTER IS BAD FROM STOCK. INSTALLED ORIGINAL TRANSMITTJul 1, 2014 · N435UA · Airbus A320232 · Landing Gear Steering SystemSDR CALA2014063091366Sign · inoperativeEXIT SIGN ABOVE FWD LT ENTRY DOOR INOPERATIVE. REPLACED LT FWD OVER DOOR EMER LIGHT ASSEMBLY. OPERATIONS CHECKED GOOD.Jun 30, 2014 · N441UA · Airbus A320232 · Emergency LightingSDR CALA2014063091367Battery Pack · malfunctionedIAW JC 4-2020 ITEM 26 FAILS CABIN EMER LIGHTING CHECK. MSG EPSU INT LOAD AFT LT. RESET EMER POWER SUPPLY BATTERY PACK. OPERATIONS CHECKED GOOD IAW MM 33-51-00 PG 501.Jun 30, 2014 · N441UA · Airbus A320232 · Emergency LightingSDR CALA2014063091368Structure · crackedLEFT MLG WW LT SIDE TORSION BOX LOWER SIDE SHELL HORIZONTAL FLANGE CRACKED AT FASTENER HOLE COMMON TO FRAME 43. REPAIR WAS ACCOMPLISHED IAW ECRA 5330-04864 REV A. THIS ECRA ACCOMPLISHED SBA 320-53-1251 TO BOTH THE LT & RT SIDES.Jun 28, 2014 · N490UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014063091369Switch · unsecureRIGHT RETRACTABLE LAND LIGHT SWITCH NEEDS SECURING. SECURED RT RETRACTABLE LANDING LIGHT SWITCH. OPERATIONS CHECKED OK.Jun 28, 2014 · N421UA · Airbus A320232 · Exterior LightingSDR CALA2014063091370Oxygen System · lowCREW OXYGEN SYS LOW. SERVICED CREW OXYGEN IAW AMM 12-14-35-0301. OPERATIONS & LEAK CHECKED OK. PRESS PRIOR TO SERVICING 1250PSI.Jun 28, 2014 · N421UA · Airbus A320232 · Crew Oxygen SystemSDR CALA2014063091371Button · inoperativeCAPTAIN'S NOSE WHEEL STEERING PEDALS DISCONNECT PUSH BUTTON INOPERATIVE. FIRST OFFICERS BUTTON, OPERATIONS NORMAL.Jun 28, 2014 · N435UA · Airbus A320232 · Landing Gear Steering SystemSDR CALA2014063091372Computer · faultyFUEL QTY DISCREPANCY BETWEEN COCKPIT & REFUELING PANEL. STICKED ALL TANKS, COCKPIT GAUGES READ CORRECTLY, UNDERWING GAUGES READING INCORRECTLY. REPLACED FQIC IAW MM 28-4 2-34 & STUCK TANKS, FOUND TO BE WITHIN LIMITS IAW FUELING MANUAL.Jun 28, 2014 · N454UA · Airbus A320232 · Fuel Quantity IndicatorSDR CALA2014062791345Light · brokenR2 DOOR SLIDE LIGHT BROKEN. R & R BULB IAW MM 52-73-21-400-002. OPERATIONS CHECKED GOOD IAW MM 52-73-00-710-001-A. IDT TASK.Jun 27, 2014 · N490UA · Airbus A320232 · Door Warning SystemSDR CALA2014062791344Door Seal · dirtyHISSING NOISE AT EMER EXIT PLUG DOOR AT 20A. INSPECTED & CLEANED FWD LT HATCH SEAL & SEAL MATING SURFACE & OUTSIDE HANDLE GASKET IAW MT 53-004 & MM 52-21-11-000-001-A. NO SEAL OR GASKET DAMAGE NOTED.Jun 26, 2014 · N483UA · Airbus A320232 · Emergency ExitsSDR CALA2014062491332Warning System · false activationYAW DAMPER 2 FAULT AFTER ENG START. CYCLED 2 FAC SWITCH & RESET CB FAULT CLEARED & BITE CHECKED OK IAW AMM22-96-00.Jun 22, 2014 · N451UA · Airbus A320232 · Autopilot SystemSDR CALA2014062091316Door Sill · corrodedL2 DOOR SILL IS CORRODED AT 7 LOCATIONS AT FWD & AFT ENDS. AFTER BLENDING CORROSION AT 7 LOCATIONS MATERIAL LOSS WAS .065 OUT OF LIMITS IAW SRM 53-41-14 FIG 101. ORIGINAL MATERIAL T=.177 & REMAINING T=.112. R & R L2 DOOR SILL IAW SRM 53-41-14 FIG 101.Jun 20, 2014 · N490UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014062091314Door Sill · corrodedR2 DOOR SILL IS CORRODED ALONG ENTIRE LENGTH. FOUND CORROSION TO BE OUT OF LIMITS FOR BLENDING. R & R R2 DOOR SILL & SPLICE BETWEEN FRAME 66 - 68. RESTORED THE AREA, HIS IS A MAJOR REPAIR.Jun 19, 2014 · N490UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014062091315Stringer · corrodedSTRINGER 42R IS CORRODED BETWEEN FRAME 63 & 64 IN AFT CARGO COMPARTMENT. CORROSION WAS OUT OF LIMITS FOR BLENDING. CUT OUT STRINGER BETWEEN FRAME 62 & 63 & REMOVED FACTORY INSTALLED SPLICE. INSTALLED NEW STRINGER & SPLICE. THIS REPAIR REQUIRES RE-INSPECTIJun 19, 2014 · N490UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014062091317Connector · dirtyNOSE WHEEL STEERING FAULT. FLIGHT CREW CLEARED MSG ON GND WITH NWS SWITCH CYCLE. PFR MSG STEERING ELECTRO HYD MODULE. TWICE WITH BSCU 1 & BSCU2 AS SOURCE. NO PREVIOUS HISTORY. CLEANED & INSPECTED STEERING MODULE CONNECTOR. SYS OPERATIONS CHECKED NORMAL.Jun 19, 2014 · N435UA · Airbus A320232 · Landing Gear System WiringSDR CALA2014062091311Cover · unsecureSLIDE PACK AT DOOR 1L IS PREVENTING THE DOOR FROM BEING CLOSED. SECURED DOOR 1L DECORATIVE COVER IAW AMM 25-62-44-000-012-A.Jun 18, 2014 · N402UA · Airbus A320232 · Emergency EquipmentSDR CALA2014061791299Warning System · false activationNW STEER FAULT DISPLAYED ON UPPER ECAM SCREEN. CYCLED NOSE STEERING SWITCH ON FWD INSTRUMENT PANEL. ACCOMPLISHED BITE OF BSCU 1 & 2 TEST PASSED NO FAULTS DISPLAYED.Jun 17, 2014 · N404UA · Airbus A320232 · Landing Gear Steering SystemSDR CALA2014061791300Hydraulic System · lowHYDRAULIC QTY LOW, YELLOW SYS. SERVICED YELLOW HYD SYS AS NEEDED IAW AMM 12-12-00.Jun 17, 2014 · N410UA · Airbus A320232 · Hydraulic System, MainSDR CALA2014062091312Spar · chafedNUMBER 1 PYLON LOWER SPAR FOUND CHAFED AT LOWER SPAR RIB 5. ACP REPAIR IAW SRM 54-51-12 FIG 202. THIS IS A CAT B REPAIR & REQUIRES SUBSEQUENT INSPECTIONS.Jun 17, 2014 · N490UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/RibSDR CALA2014062091313Spar · chafedNUMBER 2 PYLON LOWER SPAR FOUND CHAFED AT LOWER SPAR RIB 5. ACCOMPLISHED REPAIR IAW SRM54-51-12 FIG 202. THIS IS A CAT B REPAIR & REQUIRES SUBSEQUENT INSPECTIONS.Jun 17, 2014 · N490UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/RibSDR CALA2014061691292Rub Strip · chafedNUMBER 1 PYLON LOWER RUB STRIP CHAFED BETWEEN RIB 5 & RIB 10. REPAIRED LOWER SPAR PLATE CNA ANTI-CHAFE IAW SRM54-51-12 P207 RPR 5 BA. REQUIRES INSPECTION. INITIAL THRESHOLD TO BEGIN AT 102297 PTT 66453 PTC.Jun 15, 2014 · N490UA · Airbus A320232 · Nacelle/Pylon Miscellaneous StructureSDR CALA2014061691293Rub Strip · chafedNUMBER 2 PYLON LOWER RUB STRIP FOUND CHAFFED AT RIBS 5 & 10. REPAIRED LOWER SPAR PLATE CNA ANTI- CHAFE IAW SRM54-51-12 P 207 REPAIR 5 BA REQUIRES INSPECTION IAW SRI 54-51-12-2-001-00. INITIAL INSPECTION THRESHOLD TO BEGIN AT 102297 PTT 66543PTC.Jun 15, 2014 · N490UA · Airbus A320232 · Nacelle/Pylon Miscellaneous StructureSDR CALA2014061391258A/C Pack · inoperativeNUMBER 1 PACK IS INOPERATIVE REF MEL CARD. INOPERATIVE PACK 1 IAW MEL 215 2A.Jun 13, 2014 · N437UA · Airbus A320232 · Cabin Cooling SystemSDR CALA2014061691279A/C Pack · inoperativeNUMBER 1 PACK IS INOPERATIVE. INOPED PACK 1 PER MEL 215 2A.Jun 13, 2014 · N437UA · Airbus A320232 · Cabin Cooling SystemSDR CALA2014061391257Slide · deployedRIGHT OVERWING SLIDE DEPLOYED. REPLACED RT OVERWING SLIDE IAW AMM 25-62-42-400-001-A. REPLACED RT OVERWING INFLATION RESERVOIR IAW AMM 25-62-46-400-001-A. INSTALLED EMER EXIT HATCH IAW AMM 52-21-11-400-001-A.Jun 10, 2014 · N483UA · Airbus A320232 · Escape SlideSDR CALA2014060991250Aileron · malfunctionedRIGHT AILERON DEFLECTED DOWN 2 - 3 SCALE WITH ASSOCIATED ROLL OBSERVED.Jun 9, 2014 · N484UA · Airbus A320232 · Aileron Control SystemSDR CALA2014060991235Oxygen Mask · defectiveCAPTAIN'S OXYGEN HARNESS FAILS TO INFLATE, IS LEAKING. REPLACED CAPTAIN`S O2 MASK, OPERATIONS CHECKED OK.Jun 6, 2014 · N465UA · Airbus A320232 · Crew Oxygen SystemSDR CALA2014060591217Stringer · corrodedSTRINGER 41R CORRODED BETWEEN FRAME 63 & 64. STRINGER SECTION WAS R & R FROM FACTORY SPLICES AT FRAME 58 TO 64 IAW SRM 51-42-11 PG 7 & PG 25.Jun 4, 2014 · N487UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014060591218Lens · missingEMERGENCY EXIT SIGN LENS COVER MISSING AT DOOR 2RT LOWER AFT CORNER. REPLACED LENS COVER AT DOOR 2RT, OPERATIONS CHECKED GOOD.Jun 3, 2014 · N491UA · Airbus A320232 · Emergency LightingSDR CALA2014060591216Skin · damagedRUDDER PN 5547100001400 SN TS-1274 WAS FOUND TO HAVE WATER INGRESS & DISBOND DAMAGE. ACCOMPLISHED ALL REPAIRS IAW ECRA 5541-01046 REV A. WORK ACCOMPLISHED ON WU'S 49575, 49576, 49577, 49578, 49579 & 49580. CURRENT PTT 41377 PTC 17871. REPAIR TO RUDDER SIDJun 2, 2014 · N483UA · Airbus A320232 · Rudder, Plate/SkinSDR CALA2014060591219Pump · faultyENGINE 2 EDP LOW PRESS DISPLAYED. YELLOW RESERVOIR QTY IS DECREASING. EDP & PTU SELECTED OFF IAW QRH. ACCOMPLISHED CHECK OF ALL DPI NONE WERE POPPED & NO METAL FOUND IN FILTER. REPLACED ENG CASE DRAIN FILTER IAW MM29-11-43-000-010-A 13 & REPLACED ENG HYD PJun 2, 2014 · N433UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR CALA2014060291204Unknown · odorSMELL OF SMOKE PASSING THROUGH 10K FEET ON DEPARTURE. AFT FLIGHT ATTENDANT REPORTED CHIME & LAVATORY SMOKE MSG ON CIDS PANEL. NO HEAT OR VISUAL INDICATIONS OF FIRE.May 30, 2014 · N432UA · Airbus A320232 · Air Distribution SystemSDR CALA2014060291187Attach Bolt · wornNUMBER 3 RT WING FLAP AFT CANOE FAIRING ATTACH BOLT WORN. INSTALLED NEW CANOE FAIRING BOLT IAW AMM 57-55-11-400-001.May 29, 2014 · N425UA · Airbus A320232 · Trailing Edge FlapsSDR CALA2014060291188Attach Bolt · wornNUMBER 4 RT WING FLAP TRACK AFT CANOE FAIRING ATTACH BOLT WORN. INSTALLED NEW BOLT IAW AMM 57-55-11-400-001.May 29, 2014 · N425UA · Airbus A320232 · Trailing Edge FlapsSDR CALA2014060291186Unknown · malfunctionedCREW REPORTS BURNING SMELL ODOR FROM REAR GALLEY AREA. CREW REPORTS ODOR SMELLED LIKE BURNING PLASTIC. NO SMOKE OR HAZE WAS PRESENT, ONLY ODOR. CREW TURNED OFF AFT GALLEY POWER & ODOR DISSIPATED. FOUND SUPPLY RECIRC FAN CB OUT TESTED & POPPED AGAIN. COLLAMay 28, 2014 · N471UA · Airbus A320232 · Air Distribution SystemSDR CALA2014060291189Proximity Switch · dirtyDOOR 1L NOT SHOWING ARMED. VERIFIED DOOR CLOSED & ARMED PRIOR TO DEPARTURE. CLEANED PROXIMITY SWITCH 4WN1 SYS CHECK NORMAL.May 28, 2014 · N430UA · Airbus A320232 · Door Warning SystemSDR CALA2014060591215Fan · faultyCREW REPORTS BURNING PLASTIC SMELL & ODOR FROM REAR GALLEY AREA. NO SMOKE OR HAZE WAS PRESENT, ONLY ODOR. TURNED OFF AFT GALLEY POWER & ODOR DISSIPATED. IAW TSM 21-00- -00-810-802-A & SIL 21-132. CHECKED AFT GALLEY & CABIN NO ODOR. IAW MM05 51 10 200 801CMay 28, 2014 · N471UA · Airbus A320232 · Air Distribution FanSDR CALA2014052791161Engine · odorIAW CREW ON TAKEOFF, GOT AIR BLEED 2 MSG & WITHIN 30 SECONDS SMOKE ALARM IN FWD LAVATORY WENT OFF. CABIN CREW SAID THEY STARTED GETTING SMELL & ODOR AROUND ROW 23 THEN SMELL MOVED FWD TO AROUND ROW 8 & SMELL STARTED TO INTENSIFY. SMELL WAS COMING FROM NR 2 EMay 27, 2014 · N417UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2014052791163Release Mech · dirtyDURING O2 MASK DROP TEST IAW AMM 35-23-00-710-001-A, MASKS DID NOT DEPLOY AT ROW 12 ABC. CLEANED PLUNGER O2 DOOR RELEASE MECHANISM OPERATIONS CHECKS NORMAL IAW AMM 35-23 -00 IDT INSP PERFORMED.May 25, 2014 · N441UA · Airbus A320232 · Passenger Oxygen SystemSDR CALA2014052791148Door Sill · corrodedR2 DOOR SILL AFT GIRT BAR ATTACH FITTING ATTACH HOLES HAVE CORROSION. R & R R2 DOOR SILL DUE TO NO CORROSION OR REWORK ALLOWED AT JOINTS ON FRAME 66 & 68 IAW SRM 53-41-14, FIG 101, PG 103 & SRM 51-42-11, PG 1- 7.May 24, 2014 · N487UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014052791146Epsu · faultedLT CTR EPSU FAULTED DURING CABIN EMERGENCY LIGHTING CHECK IAW JOB CARD 4-2020 STEP 26. REPLACED LT CTR EPSU & BATTERY. RAN TEST AGAIN FROM PTP PANEL, FWD CABIN. SYS CHECKED GOOD.May 23, 2014 · N452UA · Airbus A320232 · Emergency Lighting
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