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 CALA2013092391367Damper · faultyDOOR 1R DAMPER CYLINDER WILL NOT ALLOW DOOR TO OPEN FULLY & LOCK. R & R DOOR 1R EMERGENCY DAMPER CYLINDER IAW AMM, OPERATIONS CHECKED NORMAL.Sep 22, 2013 · N413UA · Airbus A320232 · Service DoorsSDR CALA2013092391368Barrel Nut · damagedCREW REPORTS FASTENER LOOSE & HANGING FROM BELLY PANEL 192KB. REPLACED DAMAGED BARREL NUTS & REINSTALLED PANEL IAW AMM 53-35-13-400-002-A.Sep 22, 2013 · N423UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013092391369Wire · brokenSYS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN, BRAKES. FOUND BROKEN WIRE ONE FOOT FROM 41GG. SPLICE IN NEW WIRE PAIR & REPLACED CANNON PLUG ON 41G G IAW ESPM 20-53-29, 20-53-31, 20-43-11.Sep 22, 2013 · N438UA · Airbus A320232 · Landing Gear System WiringSDR CALA2013092391372Oxygen Mask · unsecureO2 MASK DROPPED AT 29 DEF. SECURED O2 MASK AT 29 DEF. REPACKED & ENSURE LATCH FULL ENGAGED IAW MT35-003.Sep 22, 2013 · N430UA · Airbus A320232 · Passenger Oxygen SystemSDR CALA2013092391357Regulator · leakingCREW OXYGEN SYSTEM LOW. REPLACED O2 PRESSURE REGULATOR LEAKS CHECKED OK. NO DROP IN PRESSURE ON 20 MIN.Sep 21, 2013 · N476UA · Airbus A320232 · Crew Oxygen SystemSDR CALA2013092391358Test Switch · brokenFIRST OFFICER`S O2 DOOR PRESS TO TEST BUTTON IS BROKEN. REPLACED O2 STORAGE BOX.Sep 21, 2013 · N437UA · Airbus A320232 · Crew Oxygen SystemSDR CALA2013092391373Skin · damagedON INITIAL LIGHTNING STRIKE INSPECTION FOUND FOUR STRIKES ALL INDICATING CRACK USING EDDY CURRENT. TWO EACH STRIKES IN RT FWD FS RVSM AREA & TWO EACH IN SKIN LAP BELOW DOOR 1R. BLENDED IAW SRM. ACP HFEC INSP AT BLEND REPAIR AREA IAW SRM, NO CRACKS INDICATIOSep 21, 2013 · N413UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013092091295Engine · bird ingestionCREW REPORTS EVIDENCE OF BIRD STRIKE ON THE FAN EXIT GUIDE VANES OF THE NR 1 ENGINE AT THE 6 O'CLOCK POSITION.Sep 20, 2013 · N416UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2013092091314Battery · failedEMERGENCY LIGHTS TEST FAILED WITH MESSAGE "L FWD BAT". REPLACED BATTERY ON LT FWD EMERGENCY LIGHTS POWER SUPPLY UNIT. EMERGENCY LIGHTS TEST PASSED.Sep 20, 2013 · N410UA · Airbus A320232 · Emergency LightingSDR CALA2013092091315Battery · dischargedEMERGENCY LIGHTS TEST WILL NOT PASS IAW 2 SVC, GIVES MESSAGE EPSU BATTERY EMERGENCY. REPLACED BATTERY ON RT EMERGENCY LIGHTS POWER SUPPLY UNIT. EMERGENCY LIGHTS TEST PASSED.Sep 20, 2013 · N497UA · Airbus A320232 · Emergency LightingSDR CALA2013092091319Sill · corrodedL2 DOOR SILL HAS CORROSION AT FR 68-69. INSTALLED REPAIR ANGLE IAW SRM 53-41-14 FIG 201 PRINCIPLE 5.Sep 20, 2013 · N475UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013092091320Sill · corrodedR2 DOOR SILL CORRODED AT FR68. REPLACED R2 DOOR SILL IAW SRM 51-42-11.Sep 20, 2013 · N475UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013092391323Interface Unit · failedGEAR RETRACT FAILURE, FLT DIVERTED. TROUBLESHOT IAW TSM 73-25-00-810-830-A. REPLACED LGCIU2 IAW MM 32-31-71, BITE TESTED NORMAL. ACCOMPLISHED FUNCTIONAL TEST OF LANDING GEAR EXTENSION & RETRACTION IAW 32-31-00. CHECKED NORMAL.Sep 20, 2013 · N407UA · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR CALA2013092391324Skin · dentedNR 2 ENG INLET COWL UPPER INBD LIP EXTERIOR SKIN HAS DENT 2 O'CLOCK. MEASURE DENT NR 2 ENG INLET COWL UPPER LIP AT 2 O'CLOCK WITH DEPTH GAGE TLC 2815 .023" & 8.0" TO NEAREST RIVET SRM 54-10-00 FIG 101 DENT REQ INSP 6000FH, 4500 FC, R 20 MONTHS SRM 54-10-00 FISep 20, 2013 · N475UA · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR CALA2013092391346O-Ring · leakingLT ENG LEAKING FLUID. FOUND OIL SCAVENGE TUBE LEAKING ABOVE OIL DRAIN MAST LOWER MCD. REPLACED O-RING AS IAW IPC 79-22-41-80A ITEM 90. CREW RAN ENGINE, LEAK CHECKED GOOD.Sep 20, 2013 · N458UA · Airbus A320232 · Engine Oil Distribution (Airframe Furnished)SDR CALA2013092391348Cover · delaminatedPROTECTIVE FILM DELAMINATING ON VERTICAL STAB LE. IAW 55-003 MX ACTION 3 NO DAMAGE HAS TAKEN PLACE, CUT AWAY ANY LOOSE PORTIONS. CHECKED LIMIT A-CHECK & REPAIR LIMIT C-CHECK.Sep 20, 2013 · N431UA · Airbus A320232 · Vertical Stabilizer, Plate/SkinSDR CALA2013092391350Seal · damagedSEAL AT RT INBD TRAILING FLAP NEXT TO FS HAS A LARGE CHUNK MISSING & RUBBING. ACF -2.5" SECTION OF SEAL MISSING, TAPED OVER AREA WITH SPEED TAPE IAW ECRA 5751-01167,Sep 20, 2013 · N432UA · Airbus A320232 · Trailing Edge FlapsSDR CALA2013092391371Seal · missingAIRFRAME VIBRATION INFLIGHT MORE NOTICEABLE IN REAR CABIN AREA. STARTED FL 280 MACH .79. ACCOMPLISHED MT 53-005 IAW TSM 05-50-00-810-801-A. NO NOTICEABLE PLAY IN RUDDER OR ELEVATORS. FOUND YELLOW HYDRAULIC BAY ACCESS PANEL 196BB LOOSE WITH PIECES OF SEAL Sep 20, 2013 · N476UA · Airbus A320232 · Fluid Service DoorsSDR CALA2013092591428Plenum · delaminatedLT AIR CYCLE MACHINE PLENUM DELAMINATION ON INSIDE. REMOVED LT AIR CYCLE MACHINE PLENUM. INSTALLED SERVICEABLE AIR CYCLE MACHINE IAW AMM 21-51-21 THRU STEP 4.D. INSTALLED SERVICEABLE FAN AIR PLENUM CHAMBER IAW AMM. COMPLETED ACM INSTALL OPERATIONS CHECKED GSep 20, 2013 · N408UA · Airbus A320232 · Cabin Cooling SystemSDR CALA2013092091287Stringer · corrodedSTRINGER 43L AT FRAME 34 IS CORRODED. REPLACED FACTORY STRINGER SECTION IAW SRM 51-42-1.Sep 19, 2013 · N474UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2013092091288Sill · corrodedR2 DOOR SILL CORRODED AT PREVIOUS REPAIR BETWEEN FR 66-68. REINSTALLED REPAIR IAW SRM 53-41-14.Sep 19, 2013 · N474UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013092091296Tire · faultyNOSE WHEEL VIBRATION & SPINNING FOR 2 MINUTES AFTER TAKEOFF. REPLACED BOTH NOSE TIRES IAW AMM. LT TIRE SERIAL B1551 OFF, 8661P ON RT TIRE SERIAL A2262 OFF, 8726P ON.Sep 19, 2013 · N440UA · Airbus A320232 · TireSDR CALA2013092091298Bolt · shearedCUSHION SEAL ONE EACH BOLT SHEARED, LT WING OTBD FLAP IAW MT-57-008 IPC57-53-21-05 ITEM 150, SRM57-53-00 FIG 220 OR 224, REPLACED NEW SCREW.Sep 19, 2013 · N483UA · Airbus A320232 · Trailing Edge FlapsSDR CALA2013092091299Bolt · shearedCUSHION SEAL ONE EACH BOLT SHEARED, RT WING, OTBD FLAP IAW MT-57-008 IPC 57-53-21-05 ITEM 150, SRM 57-53-00 FIG 220 0R 224, IAW CDL 27L REPLACED NEW SCREWSep 19, 2013 · N483UA · Airbus A320232 · Trailing Edge FlapsSDR CALA2013092391347Acm · faultyA-C PACKS NOT ABLE TO KEEP PLANE COOL ON GROUND. PUTTING OUT AMBIENT AIR GOT TO 88 DEGREES. R & R LT ACM IAW AMM, OPERATIONS CHECKED NORMAL.Sep 19, 2013 · N413UA · Airbus A320232 · Cabin Cooling SystemSDR CALA2013092091297Cylinder · lack of lubeLOUD CONSISTENT GRINDING NOISE FROM NOSE WHEEL STEERING IN ALL LT TURNS WITH ABOUT 10. LUBED NLG STEERING CYL IAW AMM, OPERATIONS CHECKED GOOD.Sep 19, 2013 · N479UA · Airbus A320232 · Landing Gear Steering SystemSDR CALA2013091891264Stringer · corrodedSTRINGER 42R AT FRAME 34 IS CORRODED.Sep 17, 2013 · N474UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2013091891265Skin · corrodedINTERNAL FS SKIN BETWEEN FR34 & 35, STRINGER 41L & 41R HAS CORROSION. FOUND SKIN DAMAGE AROUND FASTENER HOLES.Sep 17, 2013 · N474UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013091891268Hydraulic Line · leakingFOUND LT SIDE STAY ACT LINE LEAKING.Sep 17, 2013 · N415UA · Airbus A320232 · Hydraulic System, MainSDR CALA2013091891269Smoke Warning · false activationLAVATORY F SMOKE DETECTOR. AFT LAVATORY 136 SMOKE HORN SOUNDED. ACCOMPLISHED TEST PER MM 26-00-00 OPS CKS GOOD NO FAULTS FOUND.Sep 17, 2013 · N427UA · Airbus A320232 · Smoke DetectionSDR CALA2013091891271Sill · corrodedCORROSION ON L2 DOOR SILL AFT INBD CORNER. REMOVED CORROSION IAW SRM 53-41-14. MATERIAL LOSS WAS 0.030 & MAX MATERIAL LOSS ALLOWED IS 0.017\. OUT OF LIMITS IAW ABOVE SRM.Sep 16, 2013 · N434UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013091891261Battery · faultedFOUND EPSU BATTERY EMERGENCY R FAULT WHILE PERFORMING 2 SVC.Sep 15, 2013 · N449UA · Airbus A320232 · Emergency LightingSDR CALA2013091891266Blade · chippedPOST WALK AROUND INSPECTION FOUND CHIP IN FAN BLADE OF ENGINE 1.Sep 15, 2013 · N478UA · Airbus A320232 · Turbine Engine Compressor SectionSDR CALA2013091891270Sill · corrodedR2 DOOR SILL CORRODED AT FR 68.Sep 15, 2013 · N434UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013091891262Skin · dentedDENT FOUND LT SIDE OF FS APPROXIMATELY 2\ AFT OF L1 DOOR. DENT MEASURES 5-8\BY 5-8\BY 0.031\ DEEP. WITHIN LIMITS IAW SRM 53-11-11. HFEC SCANNED INNER & OUTER SURFACE OF DENT, NO CRACKS NOTED.Sep 14, 2013 · N474UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013091891263Plate · wornNR 1 PYLON AT RIB 5 LOWER CHAFE PLATE IS WORN. REMOVED PLATE & BLENDED THE AREA. MATERIAL LOSS IS .002\ WITHIN LIMITS IAW SRM 54-51-12, PG 209-210. HFEC INSPECTED BLENDED AREA & FOUND NO CRACKS. REINSTALLED THE PLATE WITH AN EXTENDED WEAR STRIP IAW SRM 54-5Sep 14, 2013 · N474UA · Airbus A320232 · Nacelle/Pylon Miscellaneous StructureSDR CALA2013091891267Warning System · activatedRT FWD EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN.Sep 14, 2013 · N415UA · Airbus A320232 · Door Warning SystemSDR CALA2013091091163Proximity Sensor · faultyREPLACED MLG EXTENSION PROX SENSOR 23GA FOR LOG001. LT MLG EXTENSION PROX SENSOR 23GA REPLACED IAW AMM.Sep 10, 2013 · N453UA · Airbus A320232 · Landing Gear Position and WarningSDR CALA2013091091194Post · gougedFOUND LT SIDE LOWER ATTACHMENT AREA OF WINDSHIELD SIDE POST GOUGED ON TOP SIDE OF AREA IAW 53-11-00-210-014-A PAGE 5. BLENDED GOUGE IAW SRM 51-73-00.Sep 10, 2013 · N420UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2013091091159Oxygen Mask · unsecureCREW REPORTS MASKS AT ROW 30DEF FELL DOWN. RESTOWED MASK WILL REQUIRE DROP TEST IAW MT 35-003 IRDATA PARTS 649-2749, 110-4280, 649-2759.Sep 9, 2013 · N435UA · Airbus A320232 · Passenger Oxygen SystemSDR CALA2013091091160Pump · vibrationLOUD NOISE & VIBRATION COMING FROM MID CABIN. NOISE & VIBRATION STOP WITH ENG 2 SHUTDOWN, RETURNS WHEN RESTARTED. R&R NR 2 ENG DRIVEN PUMP IAW MM 29-13-51-400-A13, AFTER ENG RUN LEAK & OPERATION NORMAL.Sep 9, 2013 · N432UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR CALA2013090991118Selector Valve · leakingOI-HYDRAULIC STREAMING FROM GEAR DOORS TO TAIL, RIGHTSIDE MOSTLY. LEAKING RT WW AFT WALL, AT INBD END OF VALVE NEAR ALLEN BOLTS MATING SURFACE. REPLACED AUTOMATIC SELECTOR 2576GM. PRESSURIZED SYSTEM LEAK CHECKED OK.Sep 8, 2013 · N492UA · Airbus A320232 · Landing Gear SelectorSDR CALA2013090991135Valve · corrodedSKIN AIR INLET VALVE 15HQ DUCK ASSEMBLY ATTACH NUT PLATE RING HAS EXFOLIATED CORROSION IAW IPC 21-26-01-11A, & EA 2100-01271. REPLACED PER EA 2100-01271 REV A. IAW AMM 21-26-52-000-001. OPERATIONS CHECKED NORMAL.Sep 8, 2013 · N443UA · Airbus A320232 · Air Distribution SystemSDR CALA2013090991136Slide · deployedDOOR 2R SLIDE DEPLOYED AT GATE. R&R R2 DOOR SLIDE IAW AMM, GROUND CHECKED GOOD.Sep 8, 2013 · N451UA · Airbus A320232 · Escape SlideSDR CALA2013091091161Skin · scratchedSCRATCH ON FS BETWEEN FR21 & FR23 AROUND STRINGER 20. DAMAGED AREA HAS BEEN REWORKED BUT NOT DOCUMENTED. DAMAGE MEASURES 1"LONG & .100" WIDE & 0.019" MATERIAL REMOVED. DAMAGE IS UNDER 25% OF ORIGINAL SKIN THICKNESS OF 0.079".Sep 8, 2013 · N421UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013091091162Elevator · out of rigACFT VIBRATION CLIMBING-THRU FL 290 AT.80 MACH, SLOWED .78 M. WENT AWAY. SAMC TEXT: THIS AIRCRAFT HAS HISTORY OF REPORTED VIBRATION & CREW REQUESTED TO COMPLETE VIBRATION CHECK LIST & LEAVE WITH LOG BOOK TOMC ALLHOFF -ACCOMPLISHED ADJUSTMENT OF ELEVATOR PCU Sep 8, 2013 · N446UA · Airbus A320232 · Elevator Control SystemSDR CALA2013091091182Light · brokenSEAT ROW 21ABC OVERWING DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. REPLACED OVERWING DOOR LOWER EMERGENCY LIGHT AT SEAT ROW 21 ABC IAW A319-A320 AMM, OPERATIONS CHECKED OKAY.Sep 8, 2013 · N403UA · Airbus A320232 · Emergency LightingSDR CALA2013091191202Post · gougedWHILE ACCOMPLISHING EQ3412 FOUND LEFT SIDE LOWER ATTACHMENT AREA OF WINDSHIELD SIDE POST GOUGED ON TOP SIDE OF AREA. BLENDED GOUGE REF SRM 51- 73-00. BLENDED AREA AFTER REWORK IS 1.75"X1.25"X.020" DEEP. ORIGINAL MATERIAL THICKNESS AT AREA IS .600". PER FIG 1,Sep 8, 2013 · N420UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013090991092Fitting · wornRT MLG GEAR DOOR SILL FWD HINGE FITTING FACE WEAR - INTERIM REPAIR IAW ECRA 5340-01539 THIS REPAIR IS ACCEPTED IAW FAA ACCEPTED DATA, IAW AIRBUS MESSAGE 70565643-011.Sep 7, 2013 · N415UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013090991119Girt Bar · out of adjustDOOR 1L WON’T CLOSE, LEVER WILL NOT GO DOWN. ADJUSTED GIRT BAR & GIRT AREA. RE-POSITIONED RELEASE STRAP & SURVIVAL KIT LANYARD TO FWD POSITION. DOOR OPENS & ARMS NORMAL. SLIDE REMOVED & REINSTALLED TO ADJUST GIRT & LANYARDS IAW AMM.Sep 7, 2013 · N406UA · Airbus A320232 · Emergency Equipment
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