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 UALA2012031901789Valve · faultyABORTED TAKEOFF ABOVE 80 KTS BELOW 110. MAX BRAKE TEMP 290 RT OUTBOARD. INSPECT WHEELS & BRAKES FOR DEFECTS RELATED TO MAX BRAKING, OVERHEAT. USE CAUTION APPROACHING LANDING GEAR AREA. ACCMP'D INSPECTION OF LANDING GEAR WHEELS, ALL FUSE PLUGS INTACT.SDR UALA2012031901748Computer · activatedSIDE STICK ISSUE, RTFL. ACP LM3282, ELAC2 RPL REF PTT 9676004. ACP EG6805 FMGC NR 2 RPL. ALL CHECKS NORMAL.SDR UALA2012031601742Unknown · odorOIL SMELL IN CABIN. RAN BOTH PACKS TOGETHER AND INDIVIDUALLY WITH APU AS PNEU SOURCE, DID NOT HAVE OIL SMELL IN CABIN WITH APU AS PNEU SOURCE. RAN BOTH ENGINES WITH AND WITHOUT ANTI-ICE. NO SMELL NOTED. RAN APU WITH BOOST SLIGHT SMELL NOTICED WITH LEFT PACSDR UALA2012031901777Slat · dentedLEFT SLAT NR 2 HAS A DENT 18" FROM INBD EDGE 3" X 4 X .25" DEEP. SAMC TEXT: EDGE OF DENT IS 1.25" FROM NEAREST RIVET ROW AND IS IN AREA 3. REQUIRES TEMP FILLER REPAIR PER SRM AND APPLICATION OF SPEED TAPE PER SRM. ACP INTERIM REPAIR SRM. REQUIRES DAILY RESDR UALA2012031901778Stowage Box · leakingCREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW O2 LEAKING MORE THAN 20 PSI PER HOUR. USING LEAK CK, CHECK PRESS REG XMITTER, DISTRIBUTION MANIFOLD, AND LINES AT O2 BOTTLE FITTINGS. REMOVED CAPT O2 ACCESS PANEL FOR O2 BOXES AND CHECK LINESSDR UALA2012031601741Computer · faultyCLASS 2 AIR BLEED MSG. SEE HIST. BMC BITE NO FAULTS. CFDS MSG "APU LOOP INOP OR BMC IDENT CKT" REF TSM 36-22-00-810-812 A. POSSIBLE PART BMC1 PCN 482-9057. REF TSM36-22-00-810-812 ALL RESISTANCES CK NORMAL 10.9 OHMS AND GROUND AT 9A. RPL BMC1. OPS CHECKSDR UALA2012031401683Battery · dischargedCABIN EMERGENCY LIGHT TEST FAILS FAULTING EPSU BATTERY AFT L 33-51-38. REPLACED AFT EMERGENCY LIGHTS BATTERY PER AMM 31-51-38.SDR UALA2012031401670Unknown · malfunctionedNR 1 ENGINE STATOR VANE ECAM. ECAM DIRECTED US TO SHUT DOWN ENGINE. GROUND FAULTS ON FADEC 1A AND 1B. REF TSM 75-30-00 PG 295 (TASK 810-843) AND TSM 75-30-00 PG A224 (TASK 810-845). CFDS SHOWED SVATK & MAINT MSG 75-32-41 CHA & CHB VSV ACT-HC-EEC1. PER TSMSDR UALA2012031401671Bottle · defectiveFOUND 3 EACH PORTABLE O2 BOTTLES NOT CONNECTED TO O2 MASK. ONE IN FRONT HAD CANNULA STRAPPED TO IT. THE TWO BACK HAD NO MASK CONNECTION AND GREEN ELBOWS WERE ALL INSTALLED BACKWARDS. INSTALLED AND CORRECTED ALL DISCREPANCIES ON PORTABLE O2 BOTTLES IN CABIN.SDR UALA2012031501720Controller · faultyRT WINDSHIELD HEAT ECAM, RT WINDOW HEAT ECAM DISPLAYED ON TAXI OUT. CREW COMPLIED WITH MEL. REPLACED WHC NR 2. TESTED OKAY.SDR UALA2012031201597Windshield · faultyL WINDSHIELD (CF575) IS IN THE SPARE CONFIGURATION PER MT 30-003. WILL NEED TO BE RETURNED TO NORMAL CONFIGURATION WHEN NEW WINDSHIELD IS INSTALLED. INSTALLED NEW WINDSCREEN. ANTI-ICE TEST GOOD.SDR UALA2012031201579Hydraulic Line · faultyON ACCT PRESS LINE REPLACED. INSIDE NR 1 PYLON, ON SMB W-U P4669G, NEED TO ACCOMPLISH RSVR PRESS TEST PER TASK 29-14-00-720-002 (LINE WAS BKN). TESTS GOOD PER MM.SDR UALA2012031201636Skin · delaminatedLT ELEV UPPER SURFACE AREA OF DELAMINATION - MISSING SURFACE MATERIAL, APPROX 3.5"W X 1", APPROX 1-32" IN DEPTH. AREA OF DELAMINATION EXTENDS OUTBOARD FROM MISSING MATERIAL APPROX 36". WILL NEED FURTHER EVALUATION. REPAIRED THE LT ELEV UPPER SURFACE PER SRMSDR UALA2012031201574Stringer · damagedSTRINGER 23L AT FRAME 23 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPLACED STR 23L AT FR 23. N-R E7256I-376078-45240.SDR UALA2012031201572Structure · dentedDOUBLER REPAIR AFT OF DOOR 1L IS DENTED AT FRAME 23 JUST ABOVE FLOOR LEVEL. MAJOR REPAIR ACCOMPLISHED: HFEC INSP FOR DAMAGE REMOVE REF NTM51-10-08PB6, NO DAMAGE NOTED. INSTALLED DOUBLER REPAIR. N-R E38251-376078-45059.SDR UALA2012030901549Oxygen Mask · out of positionO2 MASK DROPPED AT SEAT 28DEF. INSPECTED MASK CONTAINER, INSIDE AND OUT, ALL CHECKS NORMAL, LANYARD NORMAL, DOOR HINGE AND LATCH SECURE NORMALLY AND SHOW NO SIGNS OF DEFECT. SEAT OK FOR SERVICE, WILL NEED FULL MASK DROP WITHIN 3 DAYS REF MT 35-003.
ACCOMPLSDR UALA2012030901548Antenna · noisyF/A REPORTS LOUD PRESSURE LEAK AT FWD JUMPSEAT, LOUDEST MIDWAY BETWEEN 1L AND 1R. FLT ATTD NOTICED A HUM AT 10,000 FT, WHEN SHE GOT THE 2 DINGS FROM FLT DECK, THAT ITS OK FOR HER TO GET UP. SITTING DOWN SHE COULD NOT HEAR THE HUM. HUM IS COMING FROM TOP OF SDR UALA2012030601446Display · faultyCREW COMMENTS: DISPLAY UNIT TOO DIM TO CLEARLY READ IN DAYLIGHT. FLIGHT DIVERTED DUE TO EXTENSIVE HOLD. PER TOMC ONLY LOWER CAN BE DEFERRED. RPLC'D LWR ECAM DISPLAY 4WT2 AND SELECTED PROPER SWITCH SETTINGS, CKS OK. (ALSO REPLACED P/N 3907130302 - DASH NUMSDR UALA2012030501397Wire Harness · damagedENG 2 FIRE LOOP A FAULT DISPLAYED ON ECAM INTERMITTANTLY ENG 2, LOOP A INOP. INOP'D PER MEL. REPAIRED DAMAGE TO OUTER JACKET PER AMM. WORKED WITH MT26-001, ACCOMPLISHED HARNESSES CHECK AND FOUND COUPLE OF HARNESSES DAMAGED. ALSO REMOVED PLUGS AT JUNCTION BSDR UALA2012030501410Sliding Window · defectiveCAPTAIN'S SIDE WINDOW IS TOO HOT TO TOUCH. CAPTAIN'S SIDE WINDOW IS TOO HOT TO TOUCH, IT IS NOTICEABLY HOTTER THAN F-O SIDE AT CRUISE. CAPTS SLIDING WINDOW CREW STATED THAT THEY ALSO HAD A BURNING SMELL WITH THE OVHT. RPLC'D LEFT SLIDING WINDOW. REPLACED WSDR UALA2012030501326Stringer · corrodedFORWARD CARGO COMP STRINGER 41R CORRODED BTWN FRAMES 30-31. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED DAMAGE REF SRM 53-21-13. FABRICATED & INSTALLED ANGLE & FILLER REPAIR REF SRM 53-00-13 FIG 201. THIS REPASDR UALA2012030501335Stringer · corrodedFORWARD CARGO COMPARTMENT STRINGER & RIVET BUCKTAILS CORRODED BETWEEN FRAME 30-34 AT STRINGER 42R. MAJOR REPAIR ACCOMPLISHED. RMV'D RIVETS & RMV'D CORROSION TO STRINGER. FOUND MATERIAL LOSS OUT OF LIMITS OF SRM. ACP NDT FOR CRACKS REF PEMCO EA PT 19-53-003SDR UALA2012030501392Structure · damagedDURING THE HMV3 6 HOLES LOCATED BETWEEN FR27 & FR28 AT S39L & S42L WERE INADVERTENTLY OVERSIZED. CLEANED HOLES REF PEMCO EA PT19-53-004 & ECRA # 5320-02056. ACP NDT FOR CRACKS REF NTM. FABRICATED & INSTALLED COUNTERSINK BUSH FOR SKIN & PROTRUDING BUSH FOR ISDR UALA2012030501325Spoiler · excess playLEFT WING NR 2 SPOILER FAILS FREE PLAY CHECK. REMOVED & REPLACED THE NR 2 SPOILER ASSY. PERFORMED FREEPLAY CHECKS REF AMM. ALL CHECKS GOOD.SDR UALA2012030101292Bracket · brokenBRACKET FOR HALON EXTINGUISHER ON AFT WALL BROKEN. REPLACED AFT CABIN FIRE EXT BRACKET.SDR UALA2012022801216Stringer Clip · crushedCLIP CRUSHED AT FRAME 65, 5 O`CLOCK POSITION. CLIP REMOVED. NEW CLIP IN CARGO PIT. DRILLED NEW CLIP. AWAITING FASTENERS. REPLACED STR CLIP AT FRA 65 STR 40R.SDR UALA2012022701171Battery · dischargedTHE 3SV EMERGENCY LIGHT TEST FAILED. *UNIT FWD L*. RPLC'D 10W POWER SUPPLY DOOR 1L PER MM. REPLACE EMERGENCY POWER SUPPLY BATTERY AT DOOR 1L DUE TO POWER SUPPLY UNIT FAILURE. REPLACED BATTERY WITH SERVICEABLE UNIT FROM STOCK.SDR UALA2012022701194Windshield · defectiveCAPT FWD WINDSCREEN HAS SPARKS VISIBLE ON THE INNER PANEL OF THE WINDSCREEN. MAINT TEXT: CREW REPORTS SMALL INTERMITTENT ORANGE GLOW ON LOWER LEFT CORNER CAPTAINS WINDSHIELD. NO ECAM, NO SMOKE, NO SMELL. APPEARED FROM ABOUT 10,000 FT DOWN TO 2,000 FT. FOUNSDR UALA2012022701161Proximity Switch · faultyHYDRAULIC RAM AIR TURBINE WILL NOT STOW. FOUND STOW SOLENOID IN RAT ACTUATOR (1GE) OPEN. RMV'D RAT ACTUATOR. INSTALLED ROBBED ACTUATOR FROM ACFT 4049, NO HELP. REF TSM 29-22-810-803 ADJUSTED INTERLOCK PROX SWITCH REF MM. PERFORMED OP TEST OF RAT TEST DEPLSDR UALA2012022701183Controller · faultyREPLACE WINDOW HEAT COMPUTER 1. REPLACED NR 1 WHC.SDR UALA2012022401107Panel · inoperativeRADIO MANAGEMENT PANEL 3 SELECTION KEY - VHF 3 INOP - COM. REPLACED RADIO MGMT PANEL NR 3 PER MM, OPS NORMAL.SDR UALA2012022301098Battery · failedEMERGENCY LIGHTS TEST FAILED. REPLACED EMERGENCY LIGHT BATTERY ON AFT EPCU. EMER LIGHT TEST PASSED.SDR UALA2012022000987Rivet · missingLEFT ENG MISSING RIVET AT THE EXHAUST NOZZLE 12 O'CLOCK POSITION. REPAIR WITHIN 50 FLT HOURS. REPLACED MISSING RIVET PER MT 78-001 PG 3 ITEM G.SDR UALA2012022001042Connector · disconnectedPER 3 SERVICE CHECK, CABIN EMERGENCY LIGHT TEST FAILED. EPSU BATTERY FWD LEFT AND EPSU COMM AFT LEFT. FOUND CONNECTOR DISCONNECTED AT ROW 22ABC, RECONNECTED CABIN EMERGENCY LIGHTS TESTED GOOD.SDR UALA2012021600953Skin · leakingFOUND A FUEL LEAK ON THE LT WING ROOT. TANK ENTRY CREW FOUND LEAK, WILL ACP TANK ENTRY AFTER ON COMPLETION OF ACFT 2885 TANK REPAIRS. FUEL LEAKING FROM LT WING ROOT AT 45 DROPS PER MINUTE. ACCOMPLISHED TROUBLESHOOTING FUEL LEAKS USING BLOW BACK METHOD. LEASDR UALA2012021300861Skin · puncturedUPON INSPECTION OF LAV TRUCK DAMAGE FOUND 2EA 1INCH LONG PUNCTURES THRU OUTER SKIN OF LAV SERVICE PANEL DOOR. REF SMC16 FOR DAMAGE REMOVED. REMOVE FUSELAGE SKIN FASTENERS REF SMC16 & PTT 3582009 & PTT 3582026. GOING TO REPLACE SKIN PER AIRBUS. REMOVED FASTESDR UALA2012021300857Sensor · faultyNOSE WHEEL STEERING PULLING LEFT AND REQUIRES RUDDER TRIM TO TRACK STRAIGHT. STRAIGHT TRACKING REQUIRED RUDDER TRIM (UNITS LEFT OR RIGHT) TO BE SET AT: CREW COMMENTS: 4 UNITS RUD TRIM. WORKED WITH PTT 1672008 & 1672009, RPL'D SENSOR (3GC) AND ADJ'D PER MM. SDR UALA2012020800756Fitting · leakingFOUND HYDRAULIC LEAK FROM TAIL DRAIN DURING 1 SVC WALK AROUND. YELLOW SYSTEM HAS HISTORY OF SERVICING SINCE 13 JAN. APPEARS TO BE FROM TAIL AREA. FOUND RT YELLOW SYS HYD RETURN LINE FROM RUDDER SERVO CONTROL LEAKING AT BULKHEAD ELBOW AT Z310. (MKD WITH TAPSDR UALA2013020700756Stowage Box · damagedFIRST OFFICER'S OXYGEN MASK MISSING RIGHT DOOR LID. REPLACED FIRST OFFICER'S OXYGEN MASK STOWAGE BOX.SDR UALA2012020300663Blade · missingREF LM2891-1 BLADE 13 READS RGA23183 UNABLE TO LOCATE RGA 24278 AFTER REMOVING ALL BLADES ON NR 1 ENGINE. REMOVE ALL NR 1 ENG BLADES REF MM. RE-INSTALLED BLADES PER MM AND OPBLM DIST PROGRAM DATE FEB 02-2012. HIGH VIBS OFF OF IDLE. NEED TO RE-EVALUATE. RESDR UALA2012013000581Tube · leakingNR 1 ENG LEAKING FUEL-FOUND FUEL TUBE AND HOUSING LEAKING AT TOP OF FUEL OIL COOLER. (LINE IS ITEM #340 PER IP C73-12-41 FIG 81A, DETAIL J) TUBE END AND HOUSING WORN. REPLACED FUEL TUBE & HOUSING. LEAK CHECKED NORMAL, NO LEAKS NOTED.SDR UALA2012013000577Battery · dischargedEMERGENCY LIGHT TEST IS NOT PASSING ON FWD ATT PANEL. REPLACED BATTERY ON AFT EPSU. EMER LIGHTS TEST PASSED.SDR UALA2012013000579Battery · faultyEMERGENCY EXIT LIGHT TEST SHOWS EPSU AFT LEFT BATTERY FAULT. REPLACED AFT POWER SUPPLY BATTERY, CHECKS OKAY.SDR UALA2012012600552Wedge · dentedLT WING LT O/B FLAP T/E HAS LARGE DENT OTBD OF ENGINE. WEDGE IS REMOVED AND ROUTED TO SHOP 273, UNDER R29994. DAMAGE PRECISE LOCATION IS APPROX 20" OUTBOARD OF GAP SEAL ON TRAILING EDGE OF OUTBOARD FLAP, IN ZONE 2 AS IDENTIFIED IN FIGURE 101 OF SRM 57-53-00 SDR UALA2012012400497Acoustic Liner · tornTEMP REPAIR OF NR 1 ENG ACOUSTIC LINER IS PEELING BACK AND COMING OFF. RE-SECURED TAPE REF MT 78- 010, SEE CF405 FOR INTERIM REPAIR. NR 1 ENGINE ACOUSTIC LINER INBOARD AFT OF REVERSER HAS TORN PROTECTIVE LINER. FOUND APPROX 900 SQ OF SCREEN MISSING. PER MTSDR UALA2012012400499Pylon · gougedNR 1 ENG INBOARD PYLON HAS GAUGES FROM FLEXIBLE SEAL CONTACTING IT. SAMC TEXT: GOUGES ARE .031 MAX DEPTH & 2 3-4 INCH IN LENGTH. INSPECTED AREA: NO CRACKS. HAND BLENDED, REPAIR TO BE DETERMINED BY AIRBUS AT CONCLUSION OF FLT 498. CONTACT SFOLE FOR REPAIR SDR UALA2012012500513Computer · faultyLEFT INNER FUEL CELL READS 1000 LBS LOWER THAN ACTUAL ON FUELING PANEL AND IN COCKPIT. FUEL TANKS DRIP FULL. LEFT TANK FUEL QTY INDICATOR INOP. REPLACED FQIC 3QT, OP CK OKAY.SDR UALA2012012300459Valve · failedSUSPECT THE RIGHT WING FUEL PUMP SUCTION VALVE FAILED. REPLACED RIGHT WING SUCTION VALVE PER MM. (P/N 644-1004). REPLACED FQIC (P/N SIC5059-13-10). NEW FLSCU OPS CHECKED GOOD.SDR UALA2012012300442Battery Pack · faultyOVERWING EMERGENCY EXIT LIGHT IS FLASHING. REPLACED BATTERY PACK AT RT OVERWING DOOR. OPS NORMAL.SDR UALA2012012000431Smoke Detector · faultyCIDS CAUTION LIGHT ON AND LAV 'A' SMOKE DET FAULT ON PRE-DEPARTURE. REPLACED FWD LAV SMOKE DETECTOR 1WQ, TESTS GOOD.
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