IAE V2522-A5
Service difficulty reports · 3,465
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.
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
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 2006UALA00677Light · failedEMERGENCY LIGHT BITE TEST FAILS, WITH FAULT MSG'S -EPSU 115 VAC AFT L- & -EPSU UNIT AFT L. REPLACED EMERGENCY BATTERY SUPPLY. OPS CHECKS NORMAL.SDR 2006UALA00658Engine · fireLEFT ENGINE FIRE ON TAKEOFF ROLL WITH LOUD BOOM HEARD ON POWER UP. HPC R3 BLADE CRACKED NEAR THE BASE OF THE BLADE. REPLACED ENGINE AND BLADE.SDR 2006UALA00669Bottle · low pressureESCAPE SLIDE AT DOOR 2R PRESSURE IN THE RED. AMIS HISTORY REPORT SHOWS A SERIES OF EVENTS WITH THE 2R DOOR SLIDE BOTTLE PRESSURE HAVING A LOW PRESSURE READING. ON 4/1/2006 AT ORD, THE PRESSURE HAD A LOW READING BUT WAS WITHIN LIMITS. ON THE SAME DAY AT ORD,SDR 2006UALA00646Power Supply · failedEMERGENCY LIGHT TEST DOES NOT PASS. EPSU BATTERY EMERGENCY LIGHT IS FAULTED. REPLACED EPSU BATTERY, EMERGENCY LIGHT TEST OK.SDR 2006UALA00621Battery · failedEPSU BATTERY EMERGENCY L FAIL MSG ON 3 SERVICE EMERGENCY LIGHTS TEST. REPLACED BATTERY POWER SUPPLY. OPS TESTED GOOD.SDR 2006UALA00585Sill · corrodedFOUND DOOR 2 RT SILL BEAM HAS CORROSION BEYOND LIMITS. INSTALLED REPAIR ANGLES WHERE CORROSION OCCURRED PER SRM 53-41-14. REINFORCEMENT OF A PSE.SDR 2006UALA00521Skin · ground damageFUSELAGE STRUCK BY JETWAY AFT OF DOOR 1L. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 53-00-11, FIGURE 203.SDR 2006UALA00522Battery · no testEMERGENCY LIGHT TEST SHOWS AFT BATTERY. REPLACED BATTERY FOR EPSU 13WL.SDR 2006UALA00475Epsu · faultyAFTER REPLACING BATTERY IN REAR EPSU, PTP TEST DISPLAYS *EPSU AFT L*. REPLACED POWER SUPPLY. TESTED THROUGH PTP AND GOT GREEN OK LIGHT AND TEST OK MESSAGE.SDR 2006UALA00477Radar · failedWHILE EN ROUTE TO ORD WX RADAR FAILED. FLIGHT DIVERTED DUE TO THUNDERSTORMS/RAIN AT PLANNED DESTINATION. WEATHER RADAR TRANSCEIVER INOPERATIVE. REPLACED WEATHER RADAR TRANSCEIVER.SDR 2006UALA00474Battery · no testTHE EMERGENCY LIGHT SYS TEST ON PROGRAMMING AND TEST PANEL FAILS, INDICATING -EPSU BATT AFT L- FAULT. REPLACED BATTERY AT POSITION 13WL. TESTS GOOD.SDR 2006UALA00493Bottle · dischargedDOOR 2 RIGHT SLIDE BOTTLE PRESSURE LOW. IT WAS DETERMINED THAT ANY ONE OF THE FACTORS IN THE OPERATING ENVIRONMENT (VIBRATION, DOOR OPENING/CLOSING, CARTS IMPACTING DOORS, TEMPERATURE & PRESSURE CHANGES) COULD HAVE RESULTED IN BOTTLE LEAK. BOTTLE WAS REQUALSDR 2006UALA00476Connector · disconnectedEMERGENCY LIGHT CHECK FAILS -EPSU EXT LOAD FWD L-. PERFORMED TROUBLE SHOOTING. FOUND DOOR 2R SLIDE BATTERY CONNECTOR DISCONNECTED. SECURED AND PERFORMED TEST, TESTED OK.SDR 2006UALA00415Bottle · dischargedSLIDE DOOR 1R BOTTLE PRESSURE LOW. REPLACED DOOR 1R SLIDE.SDR 2006UALA00433Indication Sys · brokenDOOR 2R SLIDE PACK ARMED IND BROKEN OFF. FAILURE ATTRIBUTED TO BROKEN GIRT BAR ASSY. REPLACED GIRT BAR ASSEMBLY AND SLIDE PACK.SDR 2006UALA00343Blade · damagedCREW REPORTS MOMENTARY ENGINE 2 COMPRESSOR STALL UPON LEVEL OFF AT FL310. HPC BORESCOPE INSPECTION REVEALED 6TH STAGE BLADE DAMAGE BEYOND LIMITS. REPLACED HPC STG 6 BLADES.SDR 2006UALA00325Power Supply · failedEMERGENCY EXIT LIGHT TEST FAILED DURING TEST FOR 3SVC. REPLACED 10WL EMERGENCY LIGHT POWER SUPPLY. TESTED OK.SDR 2006UALA00326Battery · no testEMERGENCY LIGHT BITE TEST FAILS, WITH EPSU L BATTERY FAULT MSG. REPLACED LEFT EPSU BATTERY PACK. TESTS NORMAL.SDR 2006UALA00337Structure · damagedDAMAGE TO THE HORIZONTAL STABILIZER AND TAIL CONE. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLERS INSTALLED WITH AIRBUS RAS APPROVALS.SDR 2006UALA00316Sensor · malfunctionedMLG WOULD NOT RETRACT. SUSPECT LG SELECTOR VALVE 40GA. CYCLED NLG ALONE & WITH MAINS. MLGCYCLED NORMAL. ACCPD MANUAL EXTENSION, OPS CHECK OK. ON FIRST ATTEMPT GEAR FELT LIKE IT DIDN'T GO UP ALL THE WAY. WHEN GEAR HANDLE WAS SELECTED DOWN, GEAR LEVER FELTSDR 2006UALA00292Cooler · malfunctionedFUEL TEMP IN LEFT OUTBOARD FUEL TANK EXCEEDED LIMIT-39C. REPLACED NR 1 ENGINE FUEL DIVERTER AND RETURN VALVE [P/N 17300G04]. ALSO REPLACED NR 1 ENGINE FUEL COOLED OIL COOLER [P/N 55022001-11]SDR 2006UALA00183Cabin Pressure · unknownRETURN TO FIELD DUE TO A PRESSURIZATION PROBLEM.SDR 2006UALA00147Wire Harness · misroutedLEFT & RIGHT FWD DOOR SLIDE ELECTRICAL HARNESSES MISROUTED. PER AMIS 8392033 A FLEET CAMPAIGN TO VERIFY PROPER WIRE HARNESS INSTALLATION (CALLOUT LM4118 & LM4119). CALLOUT EQ3148 WAS ISSUED FOR ACFT 4047 TO REPLACE 1R SLIDE (MR25611-113) DUE TO MR TIME. THE SSDR 2006UALA00088Power Supply · faultyLEFT EPSU POWER SUPPLY MSG WHEN ACCOMPLISHING 3SVC.SDR 2006UALA00093Wire · damagedPATH GUIDE EMERGENCY LIGHTS OUT AT SEATS 19 & 20. FOUND WIRES RIPPED OUT OF CONNECTOR PLUG TO WALL AT ROW 19. THE CONNECTOR PLUG WAS ALSO MISSING BACK SHELL. PER UA-EVA-60002 SPLICED WIRE TOGETHER AROUND CONNECTOR 7260VC8 AND 7260VC8-A. CONNECTOR 7260VC8 STSDR 2006UALA00075Fuel Sys · malfunctionedUNWANTED FUEL TRANSFER IN FLIGHT FROM LEFT MAIN TO CENTER TANK. ACCOMPLISHED FAULT ISOLATION PROCEDURE PER MM 28-12-00-818-801 AND RESULTS WERE *NO FAULTS FOUND*. ACCOMPLISHED VISUAL STATIC CHECK OF CENTER FUEL TANK RESULTING IN -NO DEFECTS-. TRANSFERED APPSDR 2006UALA00066Light · faultyEMERGENCY LIGHTS FAILED 3SV TEST. FAILED *EPSU BATTERY AFT L*.SDR 2006UALA00067Light · faultyCABIN EMERGENCY LIGHT CHECK DOES NOT PASS PER 3SVC.SDR 2006UALA00059Warning Light · illuminatedRTF DUE TO NR 2 PACK ECAM FAULT MSG AND NR 1 PACK ALREADY DEFERRED. NR 2 PACK OVERHEAT WAS REPORTED WITH NR 1 PACK ALREADY DEFERRED. NR 2 PACK FAULT DISPLAYED ON THE UPPER ECAM SCREEN. REMOVED AND REPLACED NR 2 ACM (MR21552), 11HM1, PER MM-21-52-21. OP-CHECSDR 2006UALA00027Epsu · faultyEPSU EXT LOAD AFT LT FAULT ON EMERGENCY LIGHT TEST.SDR 2006UALA00026Landing Gear · unknownLANDING GEAR WAS LOWERED BY FREEFALL METHOD. GEAR SWING ECAM GEAR NOT UP-LOCKED AND GEAR DOOR NOT CLOSED ECAM MSG'S DISPLAYED AFTER GEAR RETRACTION. CREW CYCLED GEAR HANDLE THEN GEAR NOT DOWN AND LOCKED ECAM DISPLAYED WITH ALL GEARS UP AND LOCKED AND GEAR DOORSDR 2005UALA01524Engine · fireSMOKE AND FLAME COMING FROM NR 2 ENGINE WHILE IN REVERSE. THIS ENGINE HAS ACCUMULATED 20236 TSLSV(SINCE THE NUMBER 5 BEARING COMPARTMENT WAS ACCESSED). THE NUMBER (5) BEARING WAS NOT DPI'D AT THE PRIOR SHOP VISIT SO THERE IS A GOOD CHANCE THE BEARING/CARBON SDR 2005UALA01503Engine · flamed outNR 2 ENG FLAMED OUT IN CRUISE. ENG FAIL EICAS MSG. OIL PRESS, QTY GOOD. ATTEMPTED TO RESTART TWICE, NO LIGHT OFF. FMU SHUT OFF TORQUE MOTOR FAILED INTERNALLY. THIS IS A KNOWN ISSUE AND IS BEING ADDRESS ON ATTRITION PER A CATEGORY 6 SERVICE BULLETIN. HOWEVESDR 2005UALA01474Wire · misroutedLEFT FWD PAX-CREW DOOR SLIDE ASSY EMERGENCY LIGHT WIRING IS MISROUTED. A FLEET CAMPAIGN TO VERIFY THE CORRECTNESS OF SLIDE HARNESS ROUTING. FOR THIS PURPOSE, LM CALLOUT LM4119 WAS ISSUED AND ACCOMPLISHED ON ACFT 4006 L1 SLIDE (MR25611-115) IN LAX ON 11/11/20SDR 2005UALA01453Slide · reads lowDURING 3 SVC FOUND DOOR 1R SLIDE PACK OUT OF GREEN BAND. DOOR-1R SLIDE BOTTLE WAS FOUND TO HAVE LOW PRESS IN DCA ON 12/12/2005. ACFT WAS FERRIED TO ORD FOR CORRECTIVE ACTION AND SLIDE WAS REPLACED PER AMM-25062-44 WITH A SERVICEABLE ONE ON 12/13/2005.SDR 2005UALA01425Wire · misinstalledRIGHT AFT DOOR OVER THE DOOR EMERGENCY LIGHT INOP, EXIT SIGN WORKS NORMAL. FOUND LIGHT MISWIRED. ADJ WIRE CONNECTION OPS CHECK GOOD.SDR 2005UALA01415Engine · unknownRETURN TO FIELD DUE TO NR 1 ENGINE REDUCED TO IDLE. ENGINE 1 REVERTED FROM EPR MODE TO N1 MODE DUE TO THE APPARENT LOSS OF P2T2 PROBE HEATER. THIS IS PER DESIGN. THIS IS A CHRONIC ISSUE ON THIS ENGINE FIRST RTF EVENT 3 DEC MX REPLACED P2T2 PROBE PER TSM. EPR SDR 2005UALA01394Pump · malfunctionedECAM BLUE ELECTRIC PUMP INDICATION ALONG WITH OTHER ENSUING PROBABLE ELECTRICAL ISSUES LED TO DECISION TO DIVERT FLIGHT. REPLACE B ELEC PUMP LOW PRESSURE DISPLAYED ON UPPER ECAM SCREEN. QTY CHECK OK AND PER SAMC RESELCTED PUMP ON AND SYSTEM APPEARED TO RECOVSDR 2005UALA01391Engine · malfunctionedNR 1 ENG EPR MODE FAILURE FOLLOWED BY INCREASED FUEL BURN RATIO. ENGINE 1 REVERTED FROM EPR MODE TO N1 MODE DUE TO THE APPARENT LOSS OF THE P2T2 PROBE HEATER. THIS IS PER DESIGN. CREW DECIDED TO DIVERT DUE TO POSSIBLE INCREASED FUEL BURN, SAFETY CONSIDERATIONSDR 2005UALA01382Light · malfunctionedEMERGENCY EXIT LIGHT SYSTEM LIGHTS WERE FLICKERING, NOW ON FULL TIME OVERHEAD SIGNS AND PATH LIGHTS. RESET CIDS, OPS CHECKS NORMAL.SDR 2005UALA01376Battery · faultyEMERGENCY LIGHT TEST FAULTS LEFT FWD BATTERY. REPLACED BATTERY.SDR 2005UALA01375Light · damagedSEATS 9C AND 14C AISLE ARMREST MOUNTED EMERGENCY LIGHTING DAMAGED. REPLACED CABIN EMERG LIGHTING MOUNTED TO AISLE ARMREST AT SEAT 9C.SDR 2005UALA01354Wire Harness · misroutedNR 1 RT DOOR EVAC SLIDE ELECT HARNESS ROUTED WRONG DIRECTION. 2004, THERE WAS A FLEET CAMPAIGN TO VERIFY THE CORRECTNESS OF SLIDE HARNESS ROUTING. FOR THIS PURPOSE, LM CALLOUT LM4118 WAS ISSUED AND ACCOMPLISHED ON ACFT 4046 R1 SLIDE (MR25611-258) IN PHI ON SDR 2005UALA01334Smoke Detector · malfunctionedRECEIVED ECAM MESSAGE OF SMOKE IN LAVATORY & CARGO AREAS. TROUBLESHOOTING PROCEDURES FOLLOWED FOR SYSTEM OPERATION VERIFICATION. LISTED BELOW ARE THE FINDINGS FROM THE ACCOMPLISHMENT OF THOSE PROCEDURES. SMOKE DETECTOR (PPA1101-00) LOCATED IN THE FWD CARGO SDR 2005UALA01303Slide · lowDOOR SLIDE PRESSURE LOW AT DOOR 1L. SLIDE PACK ASSY FELL APART IN CONTAINER. MR TIME DATED 20SEP2005 SHOWED THAT ACFT-4044 HAD MR25611-109 INSTALLED ON 1L. MR25611-109 HAD BEEN SCHEDULED TO BE REMOVED DUE TO TIME ON 19NOV2005. MRTIME DATED 28NOV2005 AND 23DESDR 2005UALA01302Wire Harness · misroutedRIGHT FWD MAIN ENTRY DOOR SLIDE DEPLOY CABLE FOUND MISROUTED. CALLOUT LM4118 WAS DONE ON ACFT 4030 R1 SLIDE IN IAD ON 11/11/2004 TO VERIFY CORRECTNESS OF WIRE ROUTING PER AMM 25-62-44. MR25611-149 WAS REPLACED DUE TO TIME WITH MR25611-1162 IN DEC 2005. MR2561SDR 2005UALA01285Compressor · stalledNR 1 ENGINE COMPRESSOR STALL. POWER LOSS AT FL360 FOR 8-10 SEC. ENGINE RECOVERED AND FLIGHT DIVERTED INTO DEN. COCKPIT CFDS INDICATED STALL. C3 FINDING DURING BORO MAY OR MAY NOT HAVE CONTRIBUTED TO THE STALL.SDR 2005UALA01275Battery · faultyEPSU BATTERY FWD L DISPLAYED DURING 3SV CABIN EMERGENCY LIGHT CHECK. REPLACED EPSU BATTERY.SDR 2005UALA01237Floor Support · damagedAFT GALLEY FLOOR STRUCTURE IS DAMAGED. *S/D* MAJOR REPAIR ACCOMPLISHED ON AFT GALLEY FLOOR STRUCTURE, FRAME 64 RBL 21", F66 BL 0", F66-68 RBL 30", F66-68 RT AFT ENTRY THRESHOLD, F68 BL 0", F68 LBL 6, F68 RBL 12", F68 RBL 15", F68 RBL 25", F68 LBL 24" BY REPLSDR 2005UALA01178Skin · damagedLEFT EXTERNAL FUSELAGE SKIN & STRINGER AFT OF STA 897 FRAME 23 BETWEEN STR 22L & 23L IS DAMAGED. MAJOR REPAIR ACP ON LH EXTERNAL FUSELAGE SKIN AFT OF STA 897 FR 23 BETWEEN STR 22L AND 23LH PER SRM 53-00-11 FIG 220.
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