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 CALA2016101995816Door Sill · corrodedCORROSION AT R1 DOOR SILL FWD GIRT BAR HOLES AT FR 16, STR 23 AND AFT GIRT BAR HOLES AT FR 20, STR 23. REPAIRED IAW SRM 53-11-14 FIG 108.Oct 17, 2016 · N813UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101995818Door Sill · corrodedL2 DOOR SILL FR68 HAS CORROSION AROUND THE LAST TWO NUT PLATE HOLES AFT END AT DOOR SILL. REMOVED CORROSION AND FABBED REPAIR DOUBLER AND INSTALLED IAW SRM 53-41-14 PARA 5A FIG201 REPAIR PRINCIPLE 5.Oct 17, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101795808Skin · damagedRT WING 640 RB FUEL ACCESS LANDING AFT FLANGE THIRD HOLE INBD FROM CENTER LINE HAS A ELONGATED HOLE. REAMED HOLE AND FABRICATED REPAIR BUSHING AND INSTALLED IAW SRM 57-21-11 FIG 203 SRI57-21-11-2-003-00 TABLE 204Oct 14, 2016 · N804UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2016101795809Skin · dentedFUSELAGE SKIN RT DENT FOUND OUT OF LIMITS AT FR1-FR2 28+WL. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-11-PH4S FIG 230.Oct 14, 2016 · N853UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016101795810Skin · dentedSKIN DENT AT FRAME 23 BELOW STR 22L. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-11-11 FIG 210.Oct 14, 2016 · N809UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016101795812Door Frame · corrodedAFT FUSE R2 DOOR CUTOUT FR68 AT STR 23R FRAME HAS CORROSION. CUTOUT DAMAGE & INSTALLED REPAIR IAW SRM53-41-12 FIG 202.Oct 14, 2016 · N811UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2016101795805Seat Track · corrodedCABIN SEAT TRACK CORRODED AT FRAME C23 BL Y-1292. REMOVED AND REPLACED SEAT TRACK FROM FR 12- FR24 BL Y-792 IAW SRM 51-42-11 PG 31 PAR A B AND PG 46 PARA D.Oct 12, 2016 · N849UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2016101395793Plate · corrodedAFT CARGO BAY SUPPORT PLATE JUST INBD OF DOOR SILL CORRODED AROUND FWD-TIE DOWN AT FR56. REMOVED AND REPLACED WITH NEW THRESHOLD PLATE AT AFT CARGO LOWER DOOR FROM FR55.5 TO FR59 IAW SRM 51-42-11.Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101395794Structure · corrodedAFT PIT THRESHOLD CONNECTION HAS CORROSION. REMOVED AND REPLACED AFT PIT THRESHOLD SHEET CONNECTION IAW 51-42-11.Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101395795Door Sill · corrodedAFT CARGO DOOR SILL CORROSION NUMEROUS AREAS BETWEEN FR59 & FR56. REMOVED AND REPLACED AFT CARGO SILL IAW SRM 51-42-11.Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101395796Shear Plate · corrodedFR 70 STR 23 RT, AFT CORNER LOWER PANEL HAS CORROSION ON PLATE. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-72-11.Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101395800Support Frame · corrodedRT WW SHEAR PLATE SUPPORT FRAME BETWEEN FR69-FR90 FOUND TO HAVE CORROSION. REMOVED AND REPLACED RT SHEAR PLATE SUPPORT FRAME IAW SRM 51-72-11.Oct 8, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016092795777Skin · dentedEXTERIOR FUSELAGE SKIN DENTED AT THREE PLACES BETWEEN FRAMES 23 & 24 AND STRINGERS 23 & 24L. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11 FIG.115. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11 FIG.232 PG. 505-506.Sep 26, 2016 · N801UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016092795778Skin · dentedSMALL DENT FOUND ON RT FUSELAGE, ONE FOOT ABOVE UPPER WINDOW LINE & 7 WINDOWS AFT OF OVERWING EXIT. DENT WAS OUT OF LIMITS IAW SRM 53-41- 11 FIG.101. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11 FIG 231, PG 503-504.Sep 26, 2016 · N801UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016092695759Warning Message · activatedECAM COMPRESSOR VANE FOLLOWED BY ENGINE STALL ECAM, AND ENGINE FAIL ECAM. SHUTDOWN ENGINE. RESTART SUCCESSFUL. UNEVENTFUL LANDING WITH BOTH ENGINES AND APU ON. REPLACED THE NR 2 ENGINE DUE CHRONIC VSV CHANNEL A FAULTS.Sep 21, 2016 · N826UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR CALA2016092095754Selector Valve · malfunctionedAIRCRAFT EXCURSION FROM TAXIWAY. CREW REPORTED LOSS OF BRAKES AND STEERING. PFR SHOWS BRAKE SELECTOR VALVE 23GG FAULT ALONG WITH MLG HYDRAULIC PIPE MESSAGE. TEST RUN ON BSCU CHANNEL 1 & 2. BSCU CHAN 1 LAST LEG REPORT - "BRK SELECTOR VALVE (23GG)/L G HYDRAULISep 18, 2016 · N840UA · Airbus A319131 · Landing Gear Brake SystemSDR CALA2016091495732Connector · disconnectedEMERGENCY EXIT LIGHT ABOVE R1 DOOR INOPERATIVE DURING TEST. SECURED THE CONNECTOR.Sep 12, 2016 · N834UA · Airbus A319131 · Light System WiringSDR CALA2016090895724Door · damagedFUEL PANEL DOOR SUSTAINED DAMAGE DUE TO CONTACT WITH LE SLAT ON RETRACTION. REPLACED FUEL PANEL DOOR IAW MM 57-41-37.Sep 6, 2016 · N813UA · Airbus A319131 · Fuel StorageSDR CALA2016090195711Power Supply · malfunctionedEMERGENCY LIGHT TEST FAILED. FOUND TWO FAULT MESSAGES FOR EPSU INT LOAD AFT L, AND EPSU COMM FWD L, AFTER EMERGENCY LIGHT TEST. TROUBLESHOT AND TESTED IAW TSM 33-51-00-810-807-ASep 1, 2016 · N843UA · Airbus A319131 · Emergency LightingSDR CALA2016083095699Connector · damagedEMERGENCY LIGHTS AT SEATS 11C, 29C DO NOT ILLUMINATE WHEN POWER OFF 11C OK, REPINNED SEAT 29C CONNECTOR, OPS CHECKED GOODAug 27, 2016 · N805UA · Airbus A319131 · Emergency LightingSDR CALA2016083095697Power Supply · malfunctionedDURING TEST AT CIDS PANEL, EPSU UNIT FWD LT DISPLAYED. REPLACED EPSU AT FWD LEFT POSITION AND TEST PASSED OKAug 26, 2016 · N812UA · Airbus A319131 · Emergency LightingSDR CALA2016083095701Warning Light · false activationRETURN TO FIELD DUE TO REAR CARGO DOOR OPEN INDICATION. UPON ARRIVAL FOUND DOOR COMPLETELY LOCKED IN CLOSED POSITION IN DETENT. AFT CARGO DOOR FUNCTIONAL CHECK, ALL CHECKS OK.Aug 26, 2016 · N802UA · Airbus A319131 · Door Warning SystemSDR CALA2016082695687Lamp · inoperativeEMERGENCY LIGHTS AT SEATS 11C, 29C DO NOT ILLUMINATE WHEN POWER IS OFF. REPLACED THE LAMPS, TESTED OK.Aug 24, 2016 · N805UA · Airbus A319131 · Emergency LightingSDR CALA2016082395663Actuator · malfunctionedHORIZONTAL STAB THSA NO BACK YOKE AFT INNER YOKE FLANGE IS CONTACTING THE BASE OF ROD SPHERE WITH DAMAGE TO FLANGE AND ROD SPHERE (AT THE PRIMER COLORED RINGS ON THE ROD SPHERE). THSA REQUIRES REPLACEMENT IAW EA 2744-01056 REV C OP 002 STEP 5.3. REF AMM27-44-Aug 19, 2016 · N816UA · Airbus A319131 · Stabilizer Control SystemSDR CALA2016081595648Battery Pack · no testEMERGENCY EXIT LIGHTS FLICKERING AT ROW 20. FOUND ESPU 10WL AND 12WL BATTERIES FAILING OP CHECK, REPLACED BATTERY PACK IAW MM 33-51-38-401. OPS CHECKED OK.Aug 14, 2016 · N851UA · Airbus A319131 · Emergency LightingSDR CALA2016081595649Pump · failedAIR RETURN FOR ECAM CAUTION MESSAGE B HYD RESERVOIR OVEHEAT. R & R BLUE SYSTEM ELECTIC HYD PUMP, CASE DRAIN FILTER, LP FILTER. SERVICED. OPS NORMALAug 12, 2016 · N815UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), MainSDR CALA2016081295639Connector · unsecureEMERGENCY LIGHT POWER SUPPLY WARNING LIGHT APPEARED DURING CIDS TEST. SECURED CONNECTOR AT THE POWER SUPPLY, OPS CHECKED GOOD.Aug 9, 2016 · N832UA · Airbus A319131 · Light System WiringSDR CALA2016081295640Power Supply · malfunctionedEMERGENCY EXIT LIGHTS CAME ON IN CABIN WHEN SEATBELT SIGN TURNED ON. CYCLED ON/OFF AND OPS NORMAL. OP TEST OF CABIN SIGNS IAW AMM GOOD. R & R EPSU.Aug 9, 2016 · N855UA · Airbus A319131 · Emergency LightingSDR CALA2016080995610Wire Harness · not reportedNOSE WHEEL STEERING FAULT ECAM MESSAGE. EMERGENCY DECLARED AND LANDED OK. REPLACED NOSE GEAR HARNESS 2M, OPS CHECKED OK IAW MM 32-21-43-400-003-AAug 8, 2016 · N805UA · Airbus A319131 · Landing Gear System WiringSDR CALA2016080295605Battery Pack · inoperativeDURING TEST OF EMERGENCY LIGHT SYSTEM, FAULTS. BATTERY REPLACED IAW AMM 33-51-35, TESTS PASSEDJul 30, 2016 · N841UA · Airbus A319131 · Emergency LightingSDR CALA2016072895588Relay · malfunctionedON APPROACH AT 2000 AGL, GEAR HANDLE WAS PUSHED TO THE DOWN POS AND NOTHING HAPPENED. EMERGENCY DECLARED ON FOURTH ATTEMPT, GEAR CAME DOWN REPLACED RELAY 48GA AND CONNECTOR ON 49GA. WIRING SHAKEDOWN AND OPERATIONAL CHECK OF SAFETY VALVE IAW AMMJul 27, 2016 · N819UA · Airbus A319131 · Landing Gear Retraction/Extension SystemSDR CALA2016072995599Power Supply · warning lightEPSU L FAULT. REPLACED 11WL POWER SUPPLY ON ACCOUNT OF SHORT IN SLIDE CA USED UNIT FAILURE, IAW MM 33-51-38. RECONNECTED ALL UNDERSEAT LIGHT CONNECTIONS, REPLACED BULBS AND REPLACED LIGHT COVERS ON LEFT WING ROOT.Jul 26, 2016 · N854UA · Airbus A319131 · Emergency LightingSDR CALA2016072895591Light · unsecureEMERGENCY EXIT LIGHT FALLING OUT AT SEAT 35C SECURED THE LIGHT, OPS CHECKED GOODJul 25, 2016 · N849UA · Airbus A319131 · Emergency LightingSDR CALA2016072895592Power Supply · shortedEMERGENCY CABIN LIGHT TEST FAILED. R & R THE POWER SUPPLY. R & R THE SLIDE ASSEMBLY, TESTED GOODJul 25, 2016 · N854UA · Airbus A319131 · Emergency LightingSDR CALA2016072595585Line · damagedHYD EDP 1 LO PR WITH HYD G RESERVOIR LOW LEVEL AND LOW PRESSURE ECAM MESSAGES DISPLAYED. CREW REPORT FLUID LEVEL AT ZERO, TURNED ENG 1 HYD PUMP IAW QRH AS SOON AS ECAM DISPLAYED. FOUND THE ENG 1 PRESSURE LINE IN THE PYLON DAMAGED. REMOVED AND REPLACED THEJul 24, 2016 · N803UA · Airbus A319131 · Hydraulic System, MainSDR CALA2016072595583Power Supply · no testIAW CHECK CARD 4-2020 STEP 34 EMERGENY LIGHT BATTERY CAP TEST, RECEIVED A MESSAGE EPSU ARMED-ON FWD L REPLACED LEFT OVERWING EPSU IAW MM33-51-38, OPS NORMAL.Jul 23, 2016 · N847UA · Airbus A319131 · Emergency LightingSDR CALA2016072595580Fitting · no testL1 DOOR, AFT GIRT BAR FITTING STOP LEVER FAILS CHECK PER 'A' CHECK JOB 4-2060 STEP 10, AND AMM 53-11-00-210-034-A. REMOVED AND REPLACED THE GIRT BAR FLOOR FITTING. ADJUSTED AND SEALED AMM 52-11-00Jul 22, 2016 · N847UA · Airbus A319131 · Fuselage Main, Attach FittingsSDR CALA2016072295573Doubler · not reportedLEFT AIRFONE ANTENNA REQUIRES DOUBLER REPAIR FR 63-64 STR 41L-42L FABRICATED, LOCATED & DRI LLED & INSTALLED REPAIR DOUBLER IAW SRM 53-00-11-201 FIG 230Jul 20, 2016 · N813UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016072295575Warning Light · false activationLAVATORY SMOKE DETECTOR CHIMED THREE TIMES. FWD SIDS PANEL LIGHT ILLUMINATED. THEN WENT OUT. NO SMOKE DETECT BY FA . COMPLETED LAV S MOKE BITES ALL 3 LAVS, CHECKS OK. NO PRIORS.Jul 20, 2016 · N841UA · Airbus A319131 · Smoke DetectionSDR CALA2016071895564Door Sill · corrodedCORROSION AT R1 DOOR SILL FWD GIRT BAR HOLES AT FRAME 16, STR 23 AND AFT GIRT BAR HOLES AT FR 20, STR 23. REPAIRED IAW SRM 53-11-14 FIG.108.Jul 15, 2016 · N813UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016071895562Skin · contaminatedLEFT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION, 163 INCHES FROM INBD, 13 INCHES FROM TE, 2 INCHES IN DIAMETER. REPAIRED IAW ECRA 5520-01490.Jul 14, 2016 · N813UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2016071895563Skin · contaminatedRIGHT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION, 53 INCHES FROM INBD, 4.5 INCHES FROM TE, 2.75 INCHES DIAMETER. REPAIRED IAW ECRA 5520-01491.Jul 14, 2016 · N813UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2016071195558Controller · faultedCABIN PRESSURE CONTROL 1 AND 2 FAULTED, UNABLE TO PRESSURIZE, CABIN PRESSURE CONTROLLERS 1 AND 2 AND OUTFLOW VALVE FAULTED BEFORE RESET. NO FAULTS NOTED REST OF TESTS.Jul 8, 2016 · N824UA · Airbus A319131 · Cabin Pressure ControllerSDR CALA2016070895516Power Supply · malfunctioned"EPSU UNIT EMER L." FOUND BOTH INTERNAL AND EXTERNAL LOAD LIGHTS FLASHING ON 11WL. REPLACED POWER SUPPLY AND BATTERY PACK IAW AMM 33-51-38-400-001-AJul 3, 2016 · N854UA · Airbus A319131 · Emergency LightingSDR CALA2016070195501Connector · looseNR 2 ENGINE INCREASING SURGE DURING CLIMB, CLOSE TO NORMAL AT IDLE. FOUND J1 EEC CONNECTOR LOOSE. SECURED, PERFORMED POWER ASSURANCE RUNS TWICE. ALL ENGINE PARA NORMALJun 28, 2016 · N822UA · Airbus A319131 · Engine Fuel System WiringSDR CALA2016081195612Cids · malfunctionedCIDS MESSAGE, EPSU BATTERY FORWARD LEFT. CYCLED CIDS, TESTED GOOD IAW AMM.Jun 24, 2016 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2016081195613Cids · malfunctionedCIDS MESSAGE, EPSU BATTERY AFT LEFT. CYCLED CIDS, TESTED GOOD IAW AMM.Jun 24, 2016 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2016081195619Battery Pack · failedEPSU BATTERY FAULT LIGHT DURING TEST. REPLACED AFT EMERGENCY BATTERY IAW 33-51-38.Jun 23, 2016 · N843UA · Airbus A319131 · Emergency LightingSDR CALA2016062295474Power Supply · inoperativeEMERGENCY LIGHT TEST FAILS WITH MESSAGE, EPSU AFT LEFT. REPLACED POWER SUPPLY AND BATTERY PACK REF AMM33-51-38-400-002-A. CKS GOOD.Jun 20, 2016 · N819UA · Airbus A319131 · Emergency LightingSDR CALA2016081195621Power Supply · no testSYSTEM TEST SHOWED FWD LT POWER SUPPLY UNIT AND AFT L BATTERY FAILED. REPLACED FWD L POWER SUPPLY UNIT AND AFT L BATTERY. SYSTEM TESTED GOOD.Jun 17, 2016 · N855UA · Airbus A319131 · Emergency Lighting
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