IAE V2522-A5

Service difficulty reports · 3,460

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 = 'V2522A5'
  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 CALA2015061893983Battery · defectiveEPSU BATTERY FWD LT MSG AFTER EMER LIGHT TEST. ACCOMPLISHED EPSU TEST FAULT MSG EPSU BATTERY LT DISPLAYED. REPLACED LT EPSU BATTERY IAW AMM 33-51-38. TEST OPERATES NORMAL.Jun 17, 2015 · N822UA · Airbus A319131 · Emergency LightingSDR CALA2015061893982Beam · crackedRIGHT & LEFT SIDE BOX BEAM UPPER FLANGE AT FRAME 43 HAS CRACK INDICATIONS. ACCOMPLISHED EA 5331-01704 TO BOTH LT & RT FRAME 43.Jun 16, 2015 · N819UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2015061893986Servo · out of adjustSUDDEN SEVERE VIBRATION AT 26K FT, 320 KTS PILOT TURNED OFF AP, THROTTLES TO IDLE, MOVED FLT SURFACES, NO HELP. SLOWED TO 280 KTS, TURB STOPPED. ENTIRE ACFT SHUTTERED. PILOT REPORTED SEVERE VIBRATION STARTED & STOPPED SUDDENLY, NOT GRADUAL. NO MACH TUCK REPJun 15, 2015 · N831UA · Airbus A319131 · Elevator Control SystemSDR CALA2015061093887Warning System · activatedAT 40 KNOTS THE EGT INDICATION WAS RED & SHOWED 850 DEGREES. TAKEOFF WAS ABORTED. REVIEWED THE ENG UNUSUAL REPORT WHICH SHOWS EGT 999. NO OBVIOUS DAMAGE OR DEBRIS FOUND IN TAILPIPE. INSPECTED EGT HARNESS, NO DEFECTS FOUND. CLOSED UP & REPORTED FINDINGS.Jun 9, 2015 · N829UA · Airbus A319131 · Engine EGT/TIT Indicating SystemSDR CALA2015060893873Actuator · faultyPASSENGER O2 MASKS DO NOT DEPLOY IN AFT LAVATORY. REPLACED DOOR ACTUATOR. DROP CHECK, CHECKED GOOD.Jun 7, 2015 · N815UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2015060893874Door Sill · corrodedR2 DOOR SILL CORRODED FRAME 66 - 68. REPLACED R2 DOOR SILL IAW SRM 51-42-11.Jun 7, 2015 · N819UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015060893875Intercostal · corrodedFRAME 70 RT INTERCOSTAL UNDER SHEAR WEB IS CORRODED. REPLACED INTERCOSTAL IAW SRM 51-42-11.Jun 7, 2015 · N819UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015060893883Latch · out of adjustAT ARRIVAL INBD FLIGHT ATTENDANT REPORTS ROW 32 ABC O2 MASK DEPLOYED. ADJUSTED LATCH & PERFORMED DROP TEST IAW AMM 35-23-00. OPERATIONS CHECKED GOOD.Jun 5, 2015 · N831UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2015060493854Contactor · faultyLOSS OF ELEC ESSENTIAL POWER BUSS ON CLIMB OUT. REPLACED 15XE CONTACTOR IAW WD 24-24-06 AS PRECAUTION IAW AMM 24-24-55-401. WIRES CHECKED IAW TSM 24-50-00-810-814-A & BOTH 15XC ,16XC RELAYS REPLACED.Jun 1, 2015 · N855UA · Airbus A319131 · AC Generation SystemSDR CALA2015060293850Skin Panel · saturatedRIGHT ELEV, UPPER SKIN PANEL HAS TRAPPED WATER INDICATION, 143" FROM INBD & 15" FROM END OF TE, 2" DIAMETER. REPAIRED ELEV UPPER SKIN IAW SRM 55-21-11 REPAIR 5E PARA 2D CONFIG 1 ZONE 1 SRI 55-21-11-2-002-00 TABLE 203.May 31, 2015 · N819UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015052993844Unknown · odorFLIGHT ATTENDANT REPORTED PLASTIC BURNING SMELL IN AFT GALLEY AREA. OVENS & COFFEE MAKERS NOT ON. UNABLE TO DUPLICATE SMELL. CHECKED AFT LAVATORY WATER HEATER, ALL OVENS, ALL COFFEE POTS & COFFEE MAKERS. CHECKED CHILLERS WITH NO DEFECTS FOUND. FLIGHT CREWMay 25, 2015 · N834UA · Airbus A319131 · Air Distribution SystemSDR CALA2015051893793Sensor · faultyGEAR DID NOT RETRACT ON 1ST TRY. REPLACED SENSOR 24GA. BITE TEST OF SENSOR GOOD IAW MM 32-31-73.May 16, 2015 · N834UA · Airbus A319131 · Landing Gear Position and WarningSDR CALA2015051993800Sensor · corrodedCREW RETURNED TO THE FIELD DUE TO MLG NOT RETRACTING WHEN SELECTED UP. AHM IS FAULTING THE LT GEAR EXTEND PROX SENSOR 21GA. REPLACED 21GA SENSOR DUE TO CORROSION. REPLACED LT MLG MAIN GEAR HARNESS CONNECTOR INSIDE J BOX. REPLACED LT 1M HARNESS, LT 2M ENHANMay 15, 2015 · N814UA · Airbus A319131 · Landing Gear Position and WarningSDR CALA2015051593784Battery · dischargedEMERGENCY LIGHT TEST FAILED FWD LT BATTERY. REPLACED EMER LT BATTERY AT DOOR 1L. OPERATIONS CHECKED NORMAL IAW MM 33-51-38.May 14, 2015 · N835UA · Airbus A319131 · Emergency LightingSDR CALA2015051193758Power Supply · inoperativeEMERGENCY LIGHT TEST FAILED ON NR 2 SVC. MSG IS EPSU INIT LOAD EMER LT. REPLACED POWER SUPPLY & BATTERY IAW MM 33 51 38.May 11, 2015 · N854UA · Airbus A319131 · Emergency LightingSDR CALA2015051193759Control Unit · malfunctionedSMOKE DETECTOR FAULT. IAW AMM 26-10-00 RESET SDCU CBS. ALL INDICATIONS NORMAL.May 11, 2015 · N826UA · Airbus A319131 · Smoke DetectionSDR CALA2015051193760Light · inoperativeEMERGENCY EXIT LIGHTS, FLOOR MARKING LIGHTS INOPERATIVE ROWS 23 & 24 LT, 27 & 28 LT, 31 & 32 LT. ROW 31 & 32 WERE DIM FOR 5 MINUTES THEN WENT OUT. REPLACED 11WL & RELAMPED ALL SEATS. OPERATIONS NORMAL.May 11, 2015 · N854UA · Airbus A319131 · Emergency LightingSDR CALA2015051393776Container · defectiveO2 MASKS DEPLOYED 10ABC. DUE TO HISTORY & MT 35-002 REPLACE CONTAINER IAW AMM 35-21-41 TASK 35-21-41-420-050.May 11, 2015 · N820UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2015051593788Container · defectiveO2 MASKS DEPLOYED SEAT 10 ABC. REPLACED O2 CONTAINER AT SEAT 10 ABC IAW AMM 35-21-41.May 11, 2015 · N820UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2015050793681Epsu · inoperativeAFT EMER LIGHT EPSU 13WL FAIL LOCAL TEST. REPLACED EPSU 13WL IAW MM 33-51-39-401. TEST PASSED.May 7, 2015 · N806UA · Airbus A319131 · Emergency LightingSDR CALA2015051193761Proximity Sensor · faultyAIR RETURN FOR LGCIU FAULT, L - G NO UPLOCK. REPLACED PROX SENSOR 25GA & NGL M2 HARNESS.May 7, 2015 · N854UA · Airbus A319131 · Landing Gear Position and WarningSDR CALA2015051193763Computer · malfunctionedLOSS OF NR 1 ILS, FLIGHT MGMT & GUIDANCE CMPT FMGC NR 2 INOPERATIVE. ACCOMPLISHED RESET OF FMGC 1/2. ACCOMPLISHED AFS TEST IAW AMM 22-96-00-501. AUTOLAND DOWNGRADED.May 7, 2015 · N855UA · Airbus A319131 · Autopilot ComputerSDR CALA2015050693664Door Frame · corrodedR1 DOOR CUT OUT AFT LOWER CORNER CORRODED FRAME 20R. ORGINAL MATERIAL THICKNESS IN THIS AREA IS .120 TO .160. REMOVED CORROSION .023 TO .031 IN AREAS & FOUND TO BE IN LIMITS IAW SRM 53-11-12 PARA 4A TABLE 1. NDT INSPECTED AREA IAW NTM 51-10-04PB4 TO VERIFY May 5, 2015 · N804UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2015050693660Control Lever · faultyON EXTENSION LGCIU 1 & 2 FAILED. GEAR HAD TO BE MANUALLY EXTENDED IAW ECAM. REPLACED LG CONTROL LEVER, OK NO FAULTS.May 4, 2015 · N803UA · Airbus A319131 · Landing Gear SelectorSDR CALA2015050493654Skin · damagedRIGHT WING 640 RB FUEL ACCESS LANDING AFT FLANGE THIRD HOLE INBD FROM CTR LINE HAS AN ELONGATED HOLE. REAMED HOLE & FABRICATED REPAIR BUSHING & INSTALLED IAW SRM 57-21-11 FIG 203 SRI57-21-11-2-003-00 TABLE 204.May 3, 2015 · N804UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2015050693656Door Frame · corrodedRIGHT AFT ENTRY DOOR CUT OUT AFT FRAME FWD FACE HAS ONE CORRODED FASTENER HOLE, 3 INCH ABOVE FLOOR LINE & 4 INCH INBD OF FUSELAGE. EXCESSIVE MATERIAL LOSS DURING CORROSION REMOVAL. REQUIRED INSTALLING DOUBLER IAW SRM 53-41-12-201 FIG 201.Apr 27, 2015 · N815UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2015050693662Door Frame · corrodedRIGHT AFT ENTRY DOOR CUT OUT AFT FRAME FWD FACE HAS ONE CORRODED FASTENER HOLE, 3 INCHES ABOVE FLOOR LINE & 4 INCHES INBD OF FUSELAGE. EXCESSIVE MATERIAL LOSS DURING CORROSION REMOVAL. REQUIRED INSTALLING DOUBLER IAW SRM 53-41-12-201 FIG 201.Apr 27, 2015 · N815UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2015040793509Engine · fireNUMBER 2 ENG FIRE AT START. APPROACHED EGT LIMIT & APPEARED FUEL VLV DIDN'T CLOSE. BORECOPE INSPECTION OF HP TURBINE BLADE & COMBUSTION CHAMBER WITH NO LIMITING DEFECTS FOUND. PNEUMATIC HEALTH CHECKS COMPLETE. R & R PCMIA CARD & REVIEW.Apr 4, 2015 · N852UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR CALA2015040793504Skin · saturatedLEFT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION 97" FROM INBD, 6" FROM TE 1"X 2" DIAMETER. CUT OUT AREA OF TRAPPED WATER IN ZONE 3 & APPLIED REPAIR & RESTORED FINISH IAW SRM 55-21-11 PAR 5E CONFIG 1, SRI 55-21-1 1-2-002-00 TABLE 3 REQUIRED 1ST INSApr 3, 2015 · N820UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015032093449Stringer · corrodedAFT CARGO HAS CORROSION ON STRINGER 38R BETWEEN FRAME 59 & 60. R & R STRINGER IAW SRM 51-42-11 PGS 7-10 & 30-31.Mar 19, 2015 · N803UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2015032093443Panel · damagedRIGHT WING FUEL PANEL 640MB LANDING HAS AN ELONGATED SCREW HOLE AFT SIDE 1ST HOLE OTBD OF CTR LINE. REPAIRED SCREW HOLE IAW REO-L18752 REV IR & UAL ECRA 5720 636. THIS REPAIR HAS BEEN APPROVED AS CAT B PERMANENT REPAIR & TO ACP INITIAL INSPECTION IAW PART 2 OMar 18, 2015 · N803UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2015022093149Skin · dentedFUSELAGE DENTED AT FRAME 5 BETWEEN STRINGER 35L & 36L. DENT MEASURES 1.4W X .025D & .5" FROM FRAME. REPAIRED AREA IAW SRM 53-00-41 FIG 232. SRI 53-00-11-2-017-00 REQUIRES FIRST INSP 60000C AFTER REPAIR EMBODIMENT. CURRENT CYCLES 23,653C.Feb 18, 2015 · N803UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2015022093163Power Supply · inoperativeEPSU BATTERY FWD LIGHT MSG WHEN PERFORMING EMER LIGHT TEST. REPLACED BATTERY SUPPLY IAW AMM 33-51-00. OPERATIONS CHECKED OK.Feb 17, 2015 · N855UA · Airbus A319131 · Emergency LightingSDR CALA2015021293119Door Sill · corrodedR2 DOOR SILL HAS CORROSION AT FRAME 66. REPLACED R2 DOOR SILL IAW SRM 51-44-11 & 51-42-11.Feb 11, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015021293143Fitting · corrodedFRAME 66 R2 DOOR FWD CORNER FITTING CORRODED. R & R CORNER FITTING IAW SRM 53-41-14 FIG 101.Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015021293144Fitting · corrodedR2 DOOR CUT OUT AFT CORNER FITTING AT FRAME 68 IS CORRODED. REMOVED & REPLACED FITTING IAW SRM 53-41-14 FIG 101.Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015021293145Door Sill · corrodedSHAPE SILL ON R2 DOOR SILL IS CORRODED. R & R DOOR SILL IAW SRM 53-41-14 FIG 101.Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015021293146Door Frame · crackedRIGHT NR 2 DOOR FRAME 68, NR 7 DOOR STOP, LOWER INBD HOLE HAS CRACK INDICATION. REAMED HOLE IAW SRM 52-41-12 FG 202, NDT INSPECTION IAW 51-10-01 & NO CRACK NOTED. FABRICATED FREEZE PLUG & WASHER & INSTALLED IAW 53-41-12.Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2015021293136Connector · not seatedEMERGENCY LIGHT TEST FAILED WITH MSG EPSU INTERNAL LOAD EMER RT IAW TSM 33-51-00-810-807A. RESEAT CONNECTOR 12WL. GND OPERATIONS TESTED AMM 33-51-58 & NO DEFECTS NOTED.Feb 8, 2015 · N805UA · Airbus A319131 · Light System WiringSDR CALA2015021293140Skin · corrodedR2 DOOR CUT OUT HAS CORROSION UNDER SCUFF PLATE AT FRAME 67R - 68R ON EXTERNAL SKIN, STRINGER 22 - 23R. BLENDED IAW SRM 51-74-00 PAR 6, MAX THICKNESS .240", MAT LOSS =.013". MATERIAL REMAINS .227" & IS WITHIN LIMITS IAW SRM 53-41-11 FIG 106 SHEET 1. FLAT PEFeb 8, 2015 · N803UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2015021293135Door Sill · corrodedL2 DOOR SILL FRAME 68 HAS CORROSION AROUND THE LAST TWO NUTPLATE HOLES AFT END AT DOOR SILL. REMOVED CORROSION & FABRICATED REPAIR DOUBLER & INSTALLED IAW SRM 53-41-14 PARA 5A FIG 201 REPAIR PRINCIPLE 5.Feb 7, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015021293130Door Sill · corrodedL1 DOOR SILL HAS CORROSION AROUND FWD GIRT BAR FITTING, FWD INBD HOLE & AFT OTBD HOLE. REMOVE CORROSION FROM BOTH HOLES IAW SRM 53-11-14 FIG 108. NDT INSPECTION IAW 51-10-01 & NO CRACKS FOUND. FABRICATED TWO EACH BUSHINGS IAW SRM 53-11-14 FIG 108. INSTALLEFeb 6, 2015 · N803UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015021093073Door Sill · corrodedR2 DOOR SILL AFT CORNER HAS LIGHT SURFACE CORROSION 2 INCHES FWD OF FRAME 68. REPLACED R2 DOOR SILL AFT CORNER & REPAIRED ANGLE IAW SRM 53-41-14 FIG 201 SHEET 3 REPAIR PRINCIPLE 5.Feb 5, 2015 · N803UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR DALA2015020200840Transmitter · leakingON GROUND, WITH EXTERNAL AIR CONNECTED, STRONG ODOR OF FUEL AND EXHAUST FUMES FROM MID TO AFT OF ACFT. ODOR WAS PRESENT THROUGH MID CLIMB. MAINTENANCE FOUND FUEL FLOW TRANSMITTER LEAKING ON NR 1 ENGINE. R & R UPPER FLANGE O-RING IAW AMM. LEAK CHECK AND PACJan 30, 2015 · N904DA · Doug MD9030 · Engine Fuel DistributionSDR CALA2015013093043Connector · defectiveAIR RETURN, DURING CLIMB OUT INTERMITTENT REVERSER 2 UNLOCK ALSO ANTI-ICE FIRST OFFICER PITOT WAS CYCLING ON & . AFTER LANDING HAVE A LG SYS DISAGREE, FOUND BAD CONNECTOR AT 22GA1, WIRING TO CONNECTOR WAS VISUALLY OK. REPLACED CONNECTOR & PERFORMED ELEC CHECJan 28, 2015 · N821UA · Airbus A319131 · Landing Gear System WiringSDR CALA2015012393011Warning System · activatedON TAKEOFF ROLL GOT HOT BRAKE ECAM. ABORTED TAKEOFF AT 80 KTS. NR 1 INDICATED 490 DEGREES, NR 2 440, 390 & 490 DEGREES. ACFT NEVER MET 800 DEGREES & NO FUSE PLUGS MELTED SO OVERHEAT INSPECTION REQUIRED IAW AMM 05-51-16 NOT REQUIRED. CHECKED IAW TSM 32-42-0Jan 20, 2015 · N811UA · Airbus A319131 · Landing Gear Brake SystemSDR CALA2015011692987Skin · saturatedLEFT ELEVATOR HAS 1 TRAPPED WATER INDICATION THE LOWER SKIN 88" FROM INBD END & 4.5" FROM TE 3" DIA. & 7" ON UPPER SKIN 39" FROM INBD END 4.5" FROM TE 2.5" DIA 88" FROM INBD END 6" FROM TE 3.5 X 4" DIA, 94" FROM INBD END 5" FROM TE 2.5 DIA, 101.5" FROM INBD ENJan 13, 2015 · N818UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015011692988Skin · saturatedRIGHT ELEVATOR UPPER PANEL HAS 5 TRAPPED WATER INDICATIONS 54" FROM INBD END 5" FROM TE 4" DIA, 125" FROM INBD END 5" FROM TE 4" DIA, 168" FROM INBD END 4.5" FROM TE 2.5" DIA, 176" FROM INBD END 4.5" FROM TE 3" DIA, 189" FROM INBD END 4" FROM TE 3 X 3.5" DIA, Jan 13, 2015 · N818UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015011692989Skin Panel · saturatedRIGHT ELEVATOR LOWER SKIN PANEL HAS 2 TRAPPED WATER INDICATIONS 124" FROM INBD END 5" FROM TE 3 X 4" DIA, 139" FROM INBD END 4.5" FROM TE 3 X 3.5" DIA. MOISTURE PRESENT. REPAIRED IAW SRM 55-21-11 PARA 5E FIG 205. SRI 55-21-11-2-002-00 TABLE 203 REQUIRES REIJan 13, 2015 · N818UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015011392953Pressure Switch · faultyBLUE ELEC PUMP LOW PRESS & BLUE SYS LOW PRESS. NO CB`S TRIPPED. REPLACED PRESS SWITCH & WARNING CONTROL BOARD.Jan 11, 2015 · N803UA · Airbus A319131 · Hydraulic Pressure Sensor
Back to IAE V2522-A5