IAE V2527-A5
Service difficulty reports · 8,011
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UALA2012092805477Scuff Plate · leakingDOOR 2L SILL PLATE LEAKING. REMOVED AND CLEANED BOTH AFT AND FWD SCUFF PLATES AT 2L. RESEALED AND INSTALLED FWD PLATE APPLIED VACUUM AT 2030 HRS OUTSIDE TEMP 64 DEGREES F. RESEALED AND INSTALLED AFT PLATE. APPLIED HEAT AND VAC AT 2330 AFTER CURE NEEDS FAYISDR UALA2012092905522Skin · damagedLEFT WING TIP DAMAGED AT THE FIXED L/E DUE TO AIRCRAFT DAMAGE THE EDGE OF THE SKIN IS TORN 1.75 INCH AND BENT UP ALONG 4 INCH.SDR UALA2012092905496Flap · dentedMULTIPLE DENTS ON RIGHT INBOARD TRAILING EDGE FLAP. FOUND 7 DENTS ON FLAP. ALL DENTS ARE LESS THAN .118\ DEEP AND AND LESS THAN 1.575\ IN WIDTH. PER SRM 57-52-00 PAGE 137 OK TO FLY FOR 1000 FC BEFORE REPAIR NECESSARY. TAP TEST ACCOMPLISHED NO DELAMINATION SDR UALA2012092905497Flap · dentedMULTIPLE DENTS ON LEFT INBOARD TRAILING EDGE FLAP. FOUND 16 DENTS ON FLAP. ALL DENTS ARE LESS THAN .118\ DEEP AND LESS THAN 1.575\ IN WIDTH. PER SRM 57-52-00 PG 137 OK TO FLY FOR 1000 FC BEFORE REPAIR REQUIRED. ACCOMPLISHED TAP TEST NO DELAMINATION FOUND.SDR UALA2012092905498Flap · dentedMULTIPLE DENTS ON LEFT OUTBOARD TRAILING EDGE FLAP. FOUND 18 DENTS ON FLAP. ALL DENTS ARE LESS THAN .118\ IN DEPTH AND LESS THAN 1.575\ IN WIDTH PER SRM 57-53-00 PAGE 129 OK TO FLY FOR 1000 FC BEFORE REPAIR NECESSARY. TAP TEST ACCOMPLISHED NO DELAMINATION FSDR UALA2012092905495Light · inoperativeCAPT DOME LIGHT INOP IN DIM POSITION. OK IN BRIGHT. REPLACED LAMPS. CHECKED NORMAL.SDR UALA2012092905531Controller · inoperativeF/O'S WINDSHIELD HEAT IS INOP. REPLACED F/O WINDOW HEAT CONTROLLER AS PER AMM.SDR UALA2012092705457Louver · brokenLEFT ENGINE TAI EXHAUST LOUVER IS BROKEN AND LOOSE. REMOVED DAMAGED LOUVER. OK TO CONTINUE IN SERVICE UNTIL GRILL REPLACEMENT.SDR UALA2012092405406Drain Line · brokenNR 2 ENGINE ACOC DRAIN LINE BROKEN OFF AT DRAIN MAST. REPLACED NR 2 ENGINE DRAIN MAST ASSY.SDR UALA2012092505436Shade · brokenF/O SUN SHADE BROKEN. REPLACED AND INSTALLED SUN SHADE.SDR UALA2012092705458Toilet · noisyCREW REPORT: FORWARD AFT LAV EXTREMELY LOUD - AS IF A PRESSURE LEAK. CABIN PRESSURIZATION SHOWS NORMAL. REPLACED THE TOILET ASSY IAW AMM AND TOILET FLUSHES NORMALLY.SDR UALA2012092505437Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ON SHUTDOWN. REPLACED ELAC COMPUTER. LAND VERIFY PASSED. AIRCRAFT REMAINS FULLY CAPABLE.SDR UALA2012092605449Skin · gougedLEFT WINGTIP DAMAGE DUE TO CONTACT. REMOVED DAMAGED AND PULLED FASTENERS. BLENDED GOUGED SKIN. HFEC INSPECTION COMPLETED, FOUND NO ADDITIONAL DAMAGE.SDR UALA2012092505442Smoke Detector · failedCIDS LT ON FRONT FA WITH FWD LAV SMOKE DETECTOR FAIL MESSAGE. REPLACED FORWARD LAV SMOKE DETECTOR, CHECKS GOOD.SDR UALA2012092505440Cone · crackedNR 1 ENGINE EXHAUST CONE CRACKED 1.5 INCHES IN LENGTH ZONE-3 AT 9 O'CLOCK POSITION. REPLACED EXHAUST CONE.SDR UALA2012092405381Sill · corrodedR2 DOOR SILL HAS CORROSION AT AFT GIRT FITTING. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION FROM R2 DOOR SILL, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-11. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-42-11.SDR UALA2012092405384Valve · faultyNR 1 ENGINE HP VALVE HAS BROKEN LOCK OUT PIN. NEED NEW VALVE. REPLACED VALVE.SDR UALA2012092405371Oxygen Mask · unwanted deployTHE 02 MASK AT SEAT 27ABC DEPLOYED. SECURED MASK. DROP TEST OKAY.SDR UALA2012092505434Oxygen Mask · unwanted deploy02 MASK AT SEAT 27ABC DEPLOYED. SECURED MASK. DROP TEST OKAY.SDR UALA2012092105357Battery · dischargedCABIN EMERGENCY LIGHT TEST FAILED. (MSG: EPSU BATTERY LEFT). REPLACED BATTERY 11WL, 10WL AND 13WL PER AMM. RII CIDS TEST.SDR UALA2012092105360Skin · damagedFOUND SKIN DAMAGE ON LEFT MAIN LANDING GEAR DOOR. DAMAGE MEASURES L=.5IN X W=.375IN X D=.048IN. PER SRM 52-81-14 FIGS 103-105-107. DAMAGE WITHIN ALLOWABLE LIMITS. PERFORMED TEMPORARY REPAIR PER SRM 51-77 -12 PARAGRAPH 2A. REPAIRED LEFT MAIN LANDING DOOR SKSDR UALA2012092405410Disc · improper partAPU FIRE EXTINGUISHER OVER-PRESSURE INDICATOR BLACK-REQUIRES RED. APU FIRE EXT RED DISC IS PRESENT ON INSPECTION.SDR UALA2012092005324Engine · stalledNR 1 ENGINE STALL RECORDED. STALL WAS RECORDED IN ECM DOWNLINK AND WAS NOT REPORTED BY FLT CREW. REQUIRES TROUBLESHOOTING PER TSM 71-00-00-810-808-A WITHIN 10C. LOOKED IN NR 1 ENGINE FRONT AND BACK, NO DAMAGE NOTED AT THIS TIME, FURTHER TROUBLESHOOTING. UNSDR UALA2012092005330Windshield · faultyRIGHT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. - ANTI ICE REPLACE WINDSHIELD RAN HEAT FOR 10 MINS, NO FAULTS.SDR UALA2012092005328Engine · stalledDURING POWER ASSURANCE TEST AT NR 2 ENG, GOT STALL AT ENGINE DISACCELERATION. TEMPERATURE DID NOT EXCEED 548 EGT. PERFORMED TBS 71-00-00-81 0-809-A. INSPECTED ENGINE INLET & EXHAUST OK. FADEC SYSTEM TEST PER AMM, BURNER PRESSURE SENSOR TUBE & PURGED LINE SDR UALA2012092005341Seal · unsecureHISSING SOUND RIGHT OVERWING EXIT. FOUND FORWARD RIGHT OVERWING EXIT DOOR TOP AFT CORNER SEAL UNSECURED. REMOVED DOOR, SECURED SEAL RE-INSTALLED DOOR PER AMM.SDR UALA2012092105358Switch · defectiveF/O SEAT ELECTRICAL ADJUSTMENT, HORIZONTAL ADJUSTMENT INOP - INTERIOR. ELECTRICAL HORIZONTAL ADJUSTMENT SWITCH INTERMITTENT. REPLACE HORIZONTAL ELECTRIC SWITCH. OPS CHECKS OKAY.SDR UALA2012092005327Controller · faultyRIGHT WINDSHIELD DISPLAYED ON LOWER ECAM AFTER SITTING AT GATE FOR 1HR 30MIN. REPLACED WHC-2 PER MM, OPS CHECK NORMAL. MSG CLEARED.SDR UALA2012092105365Tie Bolt · shearedNR 3 MLG TIRE HAS 1 EA WHEEL TIE BOLTS SHEARED. REPLACED NR 3 MAIN TIRE ASSY PER AMM.SDR UALA2012092005322Fastener · poppedFASTENER POPPED NEAR LEFT PACK OUTFLOW. RE-SECURED FASTENER.SDR UALA2012091905314Bottle · low pressureDOOR 2L PRESSURE APPEAR LOW POSSIBLY. REF AMM 52-10-00-614-001-A FOR SVR OF DOOR ASSIST BOTTLE. SERVICED L2 DOOR SLIDE BOTTLE TO NORMAL LIMITS. LEAK CHECK GOOD, OK TO CONTINUE.SDR UALA2012091705241Slat · damagedBIRD STRIKE CLIMBOUT FROM 3000FT. REMOVED NR 2 SLAT PER MM 27-84-64-000-001 DUE TO DAMAGE. INSTALLED LEADING EDGE SLAT NUMBER 2 REF 27-84-64-400-002-A UP TO STEP B3 OF PAGE 8.SDR UALA2012091905279Skin · dentedEXISTING DENT (CF9042) AT FR 23 BETWEEN STR 22L-23L WAS EVALUATED & FOUND OUT OF SRM LIMITS. CUT OUT DAMAGE & FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR REF SRM 53-11-11 FIG 212.SDR UALA2012091705217Computer · faultyFQI CH 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. FUEL REPLACED FQIC, SYSTEM CHECKS GOOD.SDR UALA2012091805270Computer · faultyFUEL FQI CH 2 FAULT PER MEL 2840B. CFDS FAULTING FWC1: NO DATA FROM FQIC2A-2B. ACP TSM 31-53-00-810-820. REPLACED FQI COMPUTER. NO FAULT MESSAGES.SDR UALA2012091905301Seal · damagedCREW REPORTS SEAL BETWEEN LEFT INBOARD AND OUTBOARD FLAP LOWER SURFACE IS DAMAGED AT THE AFT AFT END. SEAT HAS SMALL TEAR AT AFT SIDE, NO LOOSE PIECES. NEEDS LEFT WING FLAP KINK SEAL (110-1856) ITEM #180 OF IPC 57-52-21 PG6A. REPLACED FLAP SEAL.SDR UALA2012091805272Unknown · malfunctionedNOSE WHEEL STEERING PULLING RIGHT AND REQUIRES RUDDER TRIM TO TRACK STRAIGHT. STRAIGHT TRACKING REQUIRED RUDDER TRIM (UNITS LEFT OR RIGHT) TO BE SET AT: CREW COMMENTS: 4.5-ACCOMPLISHED TSM32-51-00- 201 REVIEW OF AMSDIS AND PFR. NO FAULT HISTORY NOTED. ACCOSDR UALA2012091705216Slat · damagedBIRD STRIKE ON CLIMBOUT. LARGE SIZE LEFT ENGINE. REMOVED NR 2 SLAT PER MM 27-84-64-000-001 DUE TO DAMAGE. INSTALLED LEADING EDGE SLAT NR 2.SDR UALA2012091805271Control Panel · faultyFOUND ENGINE AND APU FIRE PANEL 1WD CAUSE OF DISCHARGE LEGEND OF ENGINE 2 AGENT 1 INSTALLED PANEL PER AMM. NEED TO OP CHECK PER AMM(S) 26-22-00-710-004 26-22-00-710-001 26-12 -00-710-001, 26-21-00-720-001 & 26-21-00-720-005. OPS CHECKED GOOD. ENG 2 PANEL 1WSDR UALA2012091705246Oxygen Box · defectiveCAPTAIN'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). REPLACED O2 BOX, OPS CHECK GOOD.SDR UALA2012091405212Cover · missingCARGO SMOKE TEST SWITCH KNOB FELL OFF. BUTTON COVER MISSING. STILL USEABLE. BUTTON PCN 565-2090, REF IPC 26-16-08-1C. INF- :ORDERED BUTTON IN TEXT, NEW BUTTON WILL ALSO NOT REMAIN ON SWITCH. REPLACED BUTTON TO SWITCH, OPS CHECK OK.SDR UALA2012091705247Fairing · dentedDENT IN FORWARD MOST END OF MAIN BODY FAIRING ON LEFT SIDE OF ACFT. DAMAGE IS 2 IN BY 1 IN AND 0.03125 IN DEEP. DENT IS 15 INCHES FROM TOP OF FAIRING AND 1 INCH 3 INCHES FROM TRAILING EDGE. REF ECRA5325-01001 NO UNDERLYING CRACKS OR LOOSE FASTENERS AND EXTERSDR UALA2012091305158Power Supply · failedCABIN EMERGENCY LIGHT TEST FAILS WITH MSG EPSU INTERNAL FAULT LEFT. REPLACED OVERWING POWER SUPPLY AND BATTERY.SDR UALA2012091405203Oil Cooler · leakingENGINE 2 ACOC LEAKING OIL, CHRONIC. RAN ENGINE FOR 10 MINUTES FOUND NR 2 ACOC LEAK AT 4 DROPS PER MINUTE ACOC NEEDS REPLACEMENT WITHIN 25 HOURS PER MT79-007. REPLACED NR 2 ENGINE ACOC REF MM 79-21-51-000-010A, MM 79-21-42-0000-010-A, MM 79-21-51-400- 010-A ASDR UALA2012091305157Bottle · low pressureDOOR 1L EMERGENCY ASSIST BOTTLE PSI LOW. SERVICED DOOR 1L EMERGENCY ASSIST BOTTLE PER MM.SDR UALA2012091305186B-Nut · looseHYDRAULIC FLUID ON UNDERSIDE OF FUSELAGE ON AFT SIDE OF LEFT MAIN GEAR DOOR. CLEANED AREA TIGHTENED B-NUT ON TOP OF PTU, NO LEAKS FOUND.SDR UALA2012091405204Actuator · faultyNOSE GEAR PIN INSTALLED. RETURN TO AIRCRAFT AFTER REPLACEMENT OF NOSE GEAR RETRACT ACTUATOR. INSTALLED MAIN GEAR LOCKS.SDR UALA2012091405202Actuator · faultyLEFT WING FUEL TRANSFER CHRONIC AND FUEL IMBALANCE ISSUE. DUE TO CHRONIC REPORTS OF THE LEFT WING FUEL TRANSFER VALVE INDICATION AMBER AND IN-TRANSIT, ACP TSM TASK 28-15-00-810-818-A. NO RELATED CFDS FAULTS NOTED. REPLACED L FWD (9QP) AND L AFT (11QP) XFR VSDR UALA2012091205126Spar · gougedNR 1 PYLON AFT FIXED FAIRING HAS DEEP GOUGE ON LOWER SPAR. WELD REPAIRED GOUGE IAW A320 SRM 54-50-00 AND 54-54-11, REPAIR REQUIRES RE-INSPECT AT NEXT C-CHECK PER SRI 54-50-00, TBL 105.SDR UALA2012091305167Shoulder Belt · frayedFLIGHT ATTENDANT JS 252 SHOULDER STRAP FRAYED-UNSERVICEABLE. REPLACED FLIGHT ATTENDANT HARNESS, OPS OKAY.
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