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 UALA2010061402073Oxygen Mask · leakingCREW O2 PRESSURE AT 1750 AS REPORTED BY CREW. O2 SERVICED EARLIER TODAY. PERFORM VISUAL AND AUDIBLE CHECK OF O2 CONNECTORS AT BOTTLE. CHECKED SECURITY OF ALL 4 CREW O2 MASKS. FOUND LEAK IN THE 1ST OBSERVERS OXYGEN-MASK STOWAGE-BOX. WILL NEED STOWAGE BOX (USDR UALA2010061402069Power Supply · failedEMERGENCY LIGHT TEST FAIL. EPSU UNIT EMERGENCY LIGHT. REPLACED LIGHT EMERGENCY POWER SUPPLY UNIT PN 3214-54-10.SDR UALA2010061402066Smoke Warning · false activationAVIONICS SMOKE ECAM. INSPECTED AVIONICS COMPARTMENT AND NO SMOKE PRESENT. REMOVED SMOKE DETECTOR, AIRFLOW THRU TUBES NORMAL. REINSTALLED SMOKE DETECTOR. CYCLED CB'S TO RESET THE AEVC AND FWC'S. RAN BITE TEST OF AEVC AND ALL NORMAL. NO ECAM MSG'S PRESENT.SDR UALA2010061102042Unknown · odorAFTER DMC 3 FAULT AT CRUISE CREW AND PAX EXP ACRID SMELL. ACCOMPLISHED TSM 24-00-00- 201 PAGES 25 AND 26. FOUND NO IRREGULARITES DURING OPS OR SNIFF CHECK TO DMC3. FOUND NO TRIPPED C-B'S, ECAM MESSAGES AND NO CIDS OR DEU PROBLEMS. CHECKED ALL E&E COMPARTMENSDR UALA2010060902004Connector · inoperativeSEAT 15C EMERGENCY EXIT LIGHT INOP. FOUND CONNECTOR REMOVED. REINSTALLED. LIGHT OPS NORMAL 15C.SDR UALA2010060801993Floor Support · corrodedFWD & AFT CORROSION. UNDER CABIN FLOOR PANEL STRUCTURES ARE CORRODED AT STA FR 16 TO FR 23 FROM LBL 12 IN TO RT SIDEWALL. ALL FLOORBOARDS INSTL'D. ACCOMPLISHED AT SMB ON WU R1879N.SDR UALA2010060801999Battery · failedEMERGENCY LIGHT TEST FAILS. REPLACED FWD LT BATTERY, TESTED GOOD.SDR UALA2010060701984Hydraulic System · leakingGREEN HYD ECAM, FLIGHT DIVERTED. FREEFALL EXTENTION OF GEAR WAS UTILIZED. CREW REPORTED THAT THEY FOLLOWED ECAM PROCEDURE AND SHUTOFF GREEN PUMP AND PTU. FOUND FLUID LOSS TO GREEN SYS. SERVICED GREEN SYS & ACCOMPLISHED MANUAL EXTENSION RESET.SDR UALA2010060701968Floorbeam · corrodedFLOORBEAM CORROSION. VISUALLY VERIFIED INTERIM RPR. DETERMINED ACFT AIRWORTHY FOR FERRY FLIGHT.SDR UALA2010060701987Oxygen Mask · failedF/O 02 MASK FAILS TO TEST. REPLACED MASK AND BOX ASSY.SDR UALA2010060401955Controller · failedANTI-ICE L WINDSHIELD MSG. REPLACED WHC NR 1. BITE TEST STILL FAILS L/E SLIDING WINDOW. NEEDS MORE TS.SDR UALA2010060701960Light · inoperativeSEATS ROWS 16 AND 21 EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSY. GROUND TEST OK.SDR UALA2010060301935Slide · low pressureDOOR 2, RT ESCAPE SLIDE LOW PRESSURE. BELOW GREEN BAND BY 50 LBS. TEMP STABLE AT 65 DEG F. REPLACED SLIDE ASSY.SDR UALA2010060401951Unknown · odorELECTRICAL BURNING ODOR FROM OVERHEAD GALLEY AREA ON DESCENT 10 MIN FROM LANDING. ODOR DISSIPATED. CHECKED FWD GALLEY AREA, COFFEEMAKER, HOTPLATES, OVEN, CHILLER, LIGHT BALLASTS, VIDEO SYS, CB PANELS (ALSO IN COCKPIT), EMERGENCY LIGHTS AND AVIONICS IN LOWER ESDR UALA2010060101855Line · leakingLOSS OF THE YELLOW HYD FLUID. FOUND LEAK FROM RT ENG PYLON SIDE FIREWALL DISCONNECT, LINE ON AOG ETA OPEN. INSTALLED RING LOCK REPAIR ON HYD LINE.SDR UALA2010060301921A/C Pack · odorIAW CREW: ODOR COMING FROM AFT GALLEY AREA. FOUND NR 2 PACK PUTTING OUT A RANCID ALMOST ELECTRICAL BURNING SMELL. INOPED PACK NR 2 IAW THE MEL. REPLACED AFT TRIM AIR VALVE, RT RECIRCULATION FILTER AND RT OZONE FILTER IAW MM. OPS NORMAL, LEAK CHECKS GOOD. PSDR UALA2010060101879Electrical Box · odorELECTRICAL ODOR IN CABIN. FLIGHT DIVERTED. ELEC SMELL DISSIPATED CREW TURNED OFF SIDEWALL, CEILING AND READING LIGHTS. FEW PASSENGERS ALSO REPORTED SEAT AUDIO STARTED CRACKING AND POPPING, SO CREW ALSO TURNED OFF PES. ALL THIS WAS IN VICINITY OF ROWS 21-23. SDR UALA2010060101880Line · brokenGREEN & YELLOW HYD ISSUE, RTFL. CONFERED WITH LM, CREW SHUT SYS PUMPS OFF TO GREEN SYS, HYD QTY DID NOT DEPLETE. FOUND LT GEAR DOOR ACTUATOR HYD LINE BROKEN, RPLED LINE AND RPLED SYS HYD FILTERS PRECAUTIONARY. SVC HYD SYS QTY TO FULL AND PERFORMED OPS CHECK SDR UALA2010052801846Pump · failedLOST BLUE HYD SYSTEM ON DESCENT. DIVERSION FOR ADDITIONAL RUNWAY LENGTH. REPLACED HP FILTER & BLUE SYS ELECTRIC PUMP. OPS ARE GOOD.SDR UALA2010052601807Electrical Box · failedSTEERING INOP WHEN ACFT GOT TO GATE. CYCLED ANTI-SKID NOSE WHEEL STEERING SWITCH SEVERAL TIMES AND STEERING CONTROL RETURNED. REPLACED NOSE WHEEL STEERING ELECTICAL BOX. NO FURTHER ISSUES.SDR UALA2010052501798Bottle · out of toleranceCREW O2 BOTTLE PRESSURE GAUGE OUT OF DATE. REPLACED CREW O2 BOTTLE AND ACCOMPLISHED SUCCESSFUL LEAK CHECK OF FITTINGS.SDR UALA2010052401771Fire Detector · faultyFIRE LOOP B FAULT DISPLAYED ON UPPER ECAM SCREEN. -ENG 2. FIRE LOOP B CAME ON AFTER FIRST POWER REDUCTION REPEAT. CHRONIC PROBLEM AND SUSPECT LOOP ISSUE, WORK WITH SW1746. PREVIOUS HAND-OVER-HAND CK OF FAN LOOP INDICATED POSSIBLE HIGH RES AT HYD FILTER AREA. RSDR UALA2010052401741Position Sensor · out of rigFOUND LT WING APPU FLAP POSITION PICK OFF UNIT ASYMMETRY OUT OF RIG. ZERO MARK TO DRIVE SHAFT MARK AT FLAPS FULL UP. DRIVING GEAR ZERO MARK DOES NOT LINE UP WITH FIXED POINTER BY ABOUT ONE DRIVE SHAFT SPLINE. REPLACED LT WING APPU. OPS TEST OF THE FLAP SYS.SDR UALA2010052401739Control Cable · bindingRIGHT AFT SLIDE INDICATION INOP ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY. DOOR 2R HANDLE WILL NOT STAY FLUSH IN FLIGHT. LOOKS GOOD ON THE GROUND. ECAM PAGE NORMAL. REPLACED FLEXIBLE CONTROL CABLE. OPS CK NORMAL.SDR UALA2010052101729Sliding Window · delaminatedFO-S SLIDING WINDOW HAS DELAMINATION AT BOTTOM EDGE. VISIBILITY IS NOT IMPAIRED. DELAMINATION MEASURED AT APPROX 5.25 X 3.25. EXCEEDS LIMIT IAW MM. ACCOMPLISHED F/O SLIDING WINDOW REPLACEMENT.SDR UALA2010052101730Lanyard · damagedCREW REPORT 2L WILL NOT ARM PROPERLY. MAINT TEXT: FOUND RELEASE STRAP AND SURVIVAL KIT LANYARD PINCHED UNDER GIRT BAR FWD END. REMOVED STRAP AND LANYARD FROM UNDER BAR AND ARM-DISARM OK BUT STRAP AND LANYARD END DAMAGED. CLEANED DEBRIS FROM GIRT BAR AREA AND TSDR UALA2010052101718Cover · wrong partNR 2 LT MED SLIDE ASSY HAS INCORRECT SLIDE COVER INSTALLED. INSTALLED CORRECT SLIDE COVER.SDR UALA2010052001704Bolt · sheared(2) SHEARED BOLTS FOUND AT FLOORBEAM EXPANSION JOINT FWD OF C47 FRAME. REPLACED ALL (6) BOLTS, NDT AT RMD. BOLTS LOC, NO CRACKS. TASK DONE ON SMB W-U H7313S AND H7312S. CREATED ENTRY FOR REFERENCE AND HISTORY.SDR UALA2010052001708Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. CAME ON DURING DESCENT. CYCLE R20 FOR ELAC 2 ON 121VU PANEL, ACP ELAC SYS TEST. ELACS HAD BEEN SWAPPED, BAD ELAC NOW IN NR1 POSITION. REPLACED ELAC NR 1 IAW MM, CAT III LAND TEST PERFORMED, CF482. FOUND ELAC 1 IMPRSDR UALA2010052101716Floor Support · corrodedFWD GALLEY FLOOR PANEL SUPPORT STRUCTURE 10 INCHES AFT OF FRAME 12 HAS CORROSION AND DAMAGED. MAINT TEXT: DAMAGE FLOOR PANEL SUPPORT STRUCTURE IS APPROX 20 INCHES RT OF CTR LINE OF ACFT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED UPPER FLANGE AND BEGAN MFG SDR UALA2010051901686Strip · peelingCAPT'S SLIDING GLASS WINDOW NOISY. IT SEEMS AS RUBBER STRIPPING FROM OUTSIDE IS PEELED BACK AND CREATE HIGH NOISE LEVEL. NOT FLUSH. ACFT HISTORY HAS BEEN SIGNED OFF 3 TIMES PRIOR AS CLEANED OR CKD OK. SAMC TEXT: CREW UPDATED WITH: IT IS BECOMING SO NOISY ASSDR UALA2010051901699Skin · dentedLT NR 1 SLAT HAS DENT BEYOND LIMITS. NR 1 SLAT REPAIRED.SDR UALA2010051901700Unknown · unknownACFT VEERS TO THE RT DURING TAXI WITHOUT CONTROL INPUT. DURING TAXI TEST DISCONNECTED STEERING WITH NO EFFECT. ACFT STILL VEERS TO THE RT. BRAKE TEMPS WERE ALL NORMAL. NO EVIDENCE OF DRAGGING BRAKE. ADJ 3GC REF MM. AIRPLANE TAXI STRAIGHT.SDR UALA2010051901701Bottle · reads lowCREW OXYGEN SYS-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED BOTTLE. PRESS 1470 BEFORE & 1850 PSI AT BOTTLE AFTER SERVICING.SDR UALA2010051901702Regulator · brokenCAPTAIN'S O2 MASK REGULATOR BOX IS BROKEN. SWAPPED OUT 1ST OBSERVER' S MASK TO THE CAPT'S POSITION. NO MASK FOR 1ST OBSERVER. SWAPPED CAPTAINS MASK BACK TO ORIGINAL 1ST OBSERVERS POSITION, REPLACED CAPTAINS MASK.SDR UALA2010051701663Connector · disconnectedLEFT OVERWING EMERGENCY LIGHT INOP. FOUND CONNECTOR OFF LIGHT ASSY. CORRECTED, CLEANED CONNECTION AT CHARGER IN DADO PANEL. OP CHK GOOD.SDR UALA2010051401645Seal · failedLGCIU 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. LOUD BANG ON TAKEOFF. WILL REPLACE SEALS. ACFT JACKED, STRUT REMOVED, REPLACED STRUT SEALS AND STARTED LEAK CHECK. STRUT HAS 275 PSI AIR CHARGE STARTING AT 1325. NEED TO COMPLETE STRUT INSTALLATION IAW SAME MMSDR UALA2010051401646Skin · damagedLIGHTNING STRIKE TO LT AILERON. INSP COMPLETE, WORKING REPAIRS, DAMAGE TO LT AILERON ACCOMPLISHING DOUBLER-SANDWICH REPAIR. WORKING WITH L/E FOR EVA. REPAIR COVERED BY SRM REPAIR. ACP REPAIR OF T/E DAMAGE ONLY. BLENDED DAMAGE IAW MT. REPAIR IS WITHIN LIMITS.SDR UALA2010051401635Extinguisher · reads lowIAW CREW, FWD LAV WASTE BIN FIRE EXTINGUISHER BOTTLE IN RED. NO PART, STILL USEABLE IAW MEL EXTINGUISHER ON PAC ORDER D6176. FIRE EXT PCN 635-0002 REF IPC26-25-09-1G ITEM 10A. REPLACED FWD LAV FIRE EXTINGUISHER.SDR UALA2010051401638Fan · failedBURNING ODOR THROUGHOUT CABIN & FLT DECK AT CRUISE ALTITUDE TWICE FOR APPROX 30 SECS. CONTINUOUS TRACE ODOR REMAINS. SEEMS TO GET WORSE WHEN CABIN TEMP IS ADJUSTED. LT RECIRCULATION FAN INDICATING AMBER ON COND PAGE A SHORT TIME AFTER SMELL WAS NOTICED. PFR GSDR 2010FA0000640Rotor · cracked((ANZY)) THIS ENGINE IS UNDERGOING MX. DURING ROUTINE FPI, QTY 45 LINEAR INDICATIONS WERE DETECTED ON THE FIR TREE ROOT PRESSURE FACES, WHICH APPEAR TO BE ASSOCIATED WITH CORROSION PITTING. THIS ISSUE HAS BEEN DETECTED ON OTHER HUBS AT THIS FACILITY, HOWEVERSDR 2010FA0000641Rotor · cracked((ANZY)) THIS ENGINE, IS UNDERGOING MX. DURING ROUTINE FPI, LINEAR INDICATIONS WERE DETECTED ON THE FIR TREE ROOT PRESSURE FACES, CONSISTENT WITH CRACKING, WHICH APPEARS TO BE ASSOCIATED WITH CORROSION PITTING. THIS ISSUE HAS BEEN DETECTED ON OTHER HUBS AT SDR UALA2010051101602Computer · faultyVENT BLOWER FAULT ON ECAM, FLT DIVERTED. REPLACED AVIONICS EQUIP VENTILATION COMPUTER (AVEC) PER AMM, TESTS OKAY.SDR UALA2010051201614Skin · dentedEXT FUSELAGE IS DENTED AT FRAME 65 PLUS 10 INCHES JUST BELOW STR 23 LEFT. MAJOR REPAIR ACCOMPLISHED. DAMAGED REMOVED, AREA HFEC INSPECTED NO DEFECTS FOUND. REPAIRED PER SRM.SDR UALA2010051001570Control Panel · faultyENG FIRE EXTING-DISCH' LIGHT OF 'AGENT 2' ILLUMINATED WITHOUT FIRING BOTTLE 2. CREW COMMENTS: AGENT 2 ENGINE 1 DISCHARGE LIGHT ON WITH ASSOCIATED ECAM. REPLACED COCKPIT ENG AND APU FIRE PANEL, TESTS GOOD.SDR UALA2010050701556Power Supply · inoperativeEPSU INT LOAD FWD L' ON PTP. REPLACED EMERGENCY POWER SUPPLY UNIT 10W. OP CHECKS GOOD.SDR UALA2010051001566Switch · malfunctionedWITH GALLEY SHED BUTTON PUSHED, G-4 GALLEY EQUIPMENT STILL OPERATES. FROM BASE W-U J5659D. W-U R1571S GENERATED TO RECORD. FROM W-U J5659D: 'TROUBLE-SHOT AND REPLACED GALLEY MICRO-CONTACTOR 13MC' IAW AMM. OP'S TEST CKS OK.SDR UALA2010051001585Panel · crackedFOUND CRACK IN L/E RT PANEL 621BB. REPLACED 621BB PANEL.SDR UALA2010050601534Skin · damagedLT WING OTBD T/E FLAP, AFT FLAP HAS LOOSE SHEET METAL REPAIR ON UPPER SURFACE AFT OF NR 3 SPOILER. AFT INBD CORNER HAS BECOME DISBONDED. WILL REQUIRE METAL BOND REPAIR. STARTNG REPAIR AFTER CONSULTING WITH EG ON ETCHING PRIMER TO BE USED AS MATERIAL LISTED SDR UALA2010050701552Selector Valve · faultedLOST NOSE WHEEL STEERING ON LANDING. RED ECAM MESSAGE WITH AUDIBLE DINGS FOR L/G GEAR NOT DOWN LOCKED, WENT AWAY AFTER 10 SEC THEN GOT \NOSE WHEEL STEERING FAULT. NEITHER TILLER HAD INPUT. STEERING DISCONNECT WAS NO HELP. REPLACED 19GA IAW MM. REPLACED S
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