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 UALA2011112706474Snubber · faultedCAPTAIN'S RUDDER PEDALS DO NOT AUTO ADJUST OUT. LUBED ACTUATOR PEDALS OPS CHECK NORMAL. PROBLEM RECURRED. REPLACED SNUBBER.SDR UALA2011112706454Floorbeam · damagedFLOORBEAM DAMAGED, MAJOR REPAIR ACCOMPLISHED.SDR UALA2011112706457Pump · faultedGREEN HYDRAULIC SYS OVERHEAT ILLUMINATED, FLIGHT DIVERTED. REPLACED OVERHEAT SWITCH 1381 GR, CHECKED CASE DRAIN FILTER NO DEFECTS. ACCOMPLISHED INTERNAL LEAK CHECK. NO DEFECTS. ACCOMPLISHED TSM 29-11- 00-810-802, ALL CHECKED GOOD. RAN ENGINE FOR 20 MINUTSDR UALA2011112206429Switch · faultyEMERGENCY EXIT LIGHTS CAME ON AT ROTATION ON TAKEOFF WILL NOT TURNOFF. REPLACE DEFECTIVE SWITCH.SDR UALA2011112306448Actuator · failedCAPTAIN'S RUDDER PEDALS STUCK OR JAMMED. REMOVED & REPLACED PEDAL ADJUSTER ACTUATOR, OPS CHECKED OKAY.SDR UALA2011112106392Battery · failedEMERGENCY LIGHT TEST FAILED WITH MSG 'EPSU BATTERY AFT L'. REPLACED BATTERY ON AFT L EPSU CHARGER. EMERGENCY LIGHTS TEST OKAY.SDR UALA2011112706491Computer · faultyFQI CHANNEL 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED FQIC PER AMM.SDR UALA2011112206413Seal · cutF/A REPORTS VERY LOUD NOISE FROM DOOR 2R STARTING ON CLIMBOUT AND SUNLIGHT AROUND IT. FOUND DOOR 2R SEAL CUT. REPLACED DOOR SEAL.SDR UALA2011111806329Window · delaminated1ST OFFICER FIXED SIDE WINDOW HAS DELAMINATION INTO AREA "A". \==REF: 56-11-12 P. 608== NOT ACCEPTABLE-FIGURE 605 BY- 7715 :RT FIXED WINDOW REMOVED REF AMM 56-11-12, TASK 56-11-12-000-001. FINISHED INSTALLATION OF FIRST OFFICER FIX WINDOW PER AMM.SDR UALA2011111806321Oxygen Mask · faultyON CAPTS O2 MASK THE RED TEST BUTTON MIGHT BE MISSING TOP. REPLACED MASK, OPS GOOD PER SUBTASK.SDR UALA2011111706305Oven · faultyCREW REPORT: ODOR LIKE BURNT TOAST OR COFFEE AT DOOR 2L AND REAR CABIN. SAMC TEXT: CHECK BEHIND COFFEEMAKERS AND OVENS FOR EVIDENCE OF ARCING, INSIDE OVENS, COFFEEMAKERS AND HOTPLATES FOR POSSIBLE SOURCES OF SMOKE, ALSO CHECK LIGHTING BALLASTS FOR EVIDENCE SDR UALA2011111706311Wire · pulledSEAT 32C EMERGENCY LIGHT INOPERATIVE. WIRE PULLED OUT OF CONNECTOR AT LIGHT. REPAIRED WIRE AND FINAL OPS CHECK SATISFACTORY.SDR UALA2011111706296Plate · missingNR 1 ENGINE FWD MOUNT FWD & AFT ENGINE MOUNT BOLT NUTS ON INBD SIDE ARE MISSING ANTI-ROTATION PLATES. INSTALLED ANTI-ROTATION PLATES.SDR UALA2011111506250Fan · failedLAV-GALLEY FAN FAULT ON UPPER ECAM. OK TO DEFER PER MEL 2123A MEL CW. SYSTEM TEST FAILED WITH EXTRACTION FAN 1HU AT FAULT, NO PART IN SEAL. PART IS: 565-0036. REPLACED EXTRACTION FAN, OPS CHECKS NORMAL.SDR UALA2011111606287O-Ring · leakingFUEL LEAKING FROM LT 1 ENGINE. REPLACED IDG OIL COOLER FUEL FITTING O-RINGS. IDLE RUN 5 MIN. OPS CHECK GOOD, NO LEAKS.SDR UALA2011111406211Rivet · poppedRT ENGINE NOSE COWL ON RIVET HEAD POPPED. REPLACED RIVET.SDR UALA2011111506268Fence · damagedCREW REPORT: LIGHTNING STRIKE. NOT SURE OF ACTUAL LOCATION. SAMC TEXT: CONTACT SAMC, INSPECT PER MM 05-51-18 (FAXED) LEFT WINGTIP FENCE, DAMAGED BY LIGHTNING IN "NO DAMAGE" AREA, REMOVE PER AMM AND CDL PER 57BA. COMPLETED LIGHTNING STRIKE INSPECTION PER AMSDR UALA2011111606277Ram Air Turb · deployedECAM CAUTION MESSAGE - RAT FAULT MESSAGE INOP - HYD. CREW COMMENTS: RAT IS DEPLOYED. RAT WAS DEPLOYED ON THE GROUND. STOWED RAT PER MM.SDR UALA2011111606288Drain Line · faultyPRESSURE SQUEAL COMING FROM FWD GALLEY CHILLER DRAIN HOSE, BEHIND ACCESS PANEL (REMOVED) JUST BELOW FWD GALLEY CHILLER. SQUEAL STARTS WHEN HULL IS PRESSURIZED TO 5.2 DIFFERENTIAL PRESSURE. REPLACED 2 EACH HOSES BY GALLEY CHILLER DRAIN. PRESSURIZED CABIN UP SDR UALA2011111406226Computer · faultyAT LANDING GEAR DEPLOYMENT A-C ROLLED HARD LEFT. HALF CONTROL. STICK INPUT TO STOP ROLL. SAMC TEXT: *UPDATE* NO WIND OR WAKE PRESENT WHEN ROLLING MOMENT OCCURED. INBD CREW REPORTS A-S 190 KTS, FLAPS 1, SPEED BRKS FULLY EXTENDED, ROLL OCCURRED AT MOMENT GEASDR UALA2011111406196Light · malfunctionedF/A'S REPORT EMER EXIT LIGHTING CYCLING ON AND OFF INTERMITTENTLY. INBOARD CREW STATED IT DID NOT CYCLE AFTER CYCLING THE SWITCH. TESTED LIGHT NORMAL.SDR UALA2011111406198Computer · faultyFLIGHT CONTROL BUMPING. AFTER 90 MINUTES AT CRUISE FL360 HAD LOW AMPLITUDE BUMPS FELT IN COCKPIT, OBSERVED BOTH AILERONS PULSE UP ONE INCH SIMULTANEOUSLY. WITH ELAC1 OR ELAC2 OFF, THE BUMPING STOPPED. SIMILAR BUMP NOTED WHEN SWITCHING ELAC1 OFF. NOTED BY MSDR UALA2011111106175Actuator · faultyF/O RUDDER PEDALS DO NOT MOVE TOWARD PILOT WITHOUT MANUAL ASSISTANCE. REPLACED PEDAL ADJUSTER ACTUATOR, OPS CHECK NORMAL.SDR UALA2011111006143Computer · faultyELAC-2 ISSUES, FLIGHT DIVERTED. NR 2 ELAC REF MM. PERFORMED OPERATIONAL TEST OF ELAC. PERFORMED EFCS 1&2, NO FAULTS FOUND. PERFORMED AFS TEST REF MM, TEST PASSED ON GND. KNOWN GOOD ELAC1 AND 2 DUE TO CONTINUING ELAC 1 AND 2 FAULTS WITH MULTIPLE SEPARATE REPLACSDR UALA2011111006150Seal · faultyCREW REPORT: F/A REPORTS VIBRATION AND HUMMING NOISE IN FRONT OF COACH CABIN BACK TO WINDOW EXITS. ACCOMPLISH VISUAL INSPECTION FOR OBVIOUS DAMAGE AND DEFECTS. FOR POSSIBLE OVERWING FAIRING SEALS. PANEL 192BT WAS FOUND TO HAVE A SMALL PIECE OF RUBBER SEAL SDR UALA2011110906114Liner · damagedNR 2 ENG INLET ATTRITION LINER HAS MISSING MATERIAL FROM PREVIOUS REPAIR AT 12 O'CLOCK. DAMAGE LESS THAN 20 PER, MUST BE REPAIRED WITHIN 20 CYC PER MT 72-017. RECOMMEND REPAIR BE DONE IN HANGER DUE TO EXTENT OF DAMAGE AREA, ATTRITION LINER MAY NEED TO BE REMSDR UALA2011110906106Window · delaminatedRIGHT AFT F/O WINDOW DELAMINATED. DELAM MEASURES 3 AND 5-8 DEFERED PER MT56-00. REPLACED WINDOW PER AMM.SDR UALA2011110706022Wire Harness · unsecureEMERGENCY LIGHT SEAT HARNESS LIGHT IS NOT SECURED AT SEATS 7B&C. NEEDS THE HARNESS FOR SEAT BR9638-65. INPUT INTO AMIS HISTORY. SECURED HARNESS AT SEAT 7B&C AND UPDATED WITH INFO IN DF806.SDR UALA2011110706033Wire · brokenEMERGENCY LIGHT AT SEAT 7C INOP. THERE IS A BROKEN WIRE AT THE CONNECTOR UNDER SEAT 7C. BY- 177127 :BROKEN WIRE IS NOT BARE OR EXPOSED TO PAX UNDERNEATH SEAT. SECURED WIRE.^06NOV ORD INF- :PCN 565-2457 IS INCORRECT . PART # BR9638-65 IS ON AC.^06NOV SFO INFSDR UALA2011110706007Battery Pack · failedEMERGENCY LIGHT FAIL TEST FAULTING FWD AND AFT LEFT EPSU BATTERY. REPLACE BOTH BATTERY PACKS AND GROUND CHECKS NORMAL.SDR UALA2011110405978Computer · improper partDMC FAILURE, FLIGHT DIVERTED. EIS DMC FAIL FOR F/O SWITCHING F/O TO 3 GIVES ERRONEOUS DISPLAY FOUND DMC 2 HAD MR31626 INSTALLED, INSTALLED CORRECT MR31629 UNIT. REPLACED NR 2 AND NR 3 DMC'S REF MM31-63-00 PG401 AND F/O'S RELAY BOX 20WT2 REF ASM31-68-00 ALL SDR UALA2011110305951Computer · faultyELAC 1 FAULT. REPLACED ELAC 2 PER MM. OPERATIONAL CHKS OKAY.SDR UALA2011110305972Compressor Blade · out of limitsENG 1 FAN BLADE TAP TEST OUT OF LIMITS AT ONE BLADE. DURING NR 1 ENGINE FAN BLADE TAP INSPECTION FOUND ONE COMPRESOR FAN BLADE OUT OF LIMITS. VALUE OBTAINED 1880 DB SEC. REPLACED FAN BLADE NBR 9 PER AMM AND ACPD FAN BLADE REDISTRIBUTION AS PER ENG CONTROLLERSDR UALA2011110406003Shoulder Belt · faultyCAPTAIN'S RIGHT SHOULDER HARNESS WILL NOT RETRACT. REMOVED AND REPLACED CAPTAIN'S SEAT, OPS OKAY.SDR UALA2011110205942Seat Belt · damagedFWD LEFT F/A JUMPSEAT SHOULDER HARNESS MISSING ADJUSTMENT TAB. REPLACED INOPERATIVE FWD SEAT BELT HARNESS. CHECKED GOOD.SDR UALA2011110305969Stowage Box · faultyF/O O2 MASK DOES NOT TEST PROPERLY. REPLACED MASK STOWAGE BOX ASSY PER MM, CHECKS NORMAL.SDR UALA2011110105907Battery Pack · dischargedEPSU BATTERY FWD L DISPLAYED AFTER ACCOMPLISHING CABIN EMERGENCY LIGHT TEST. EPSU BATTERY AT FWD DOOR 1L CYCLE CHARGED , ACP SYSTEM TEST. PASSED TEST, OPS CHECKED OKAY.SDR UALA2011110105927Outflow Valve · failedOUTFLOW VALVE FAULTED, RTFL. REPLACED OUTFLOW VALVE 22HQ, OPS CHECKED GOOD. NO FAULTS.SDR UALA2011110205931Trim Panel · tornRUBBER TRIM AROUND CAPT'S SLIDING WINDOW HANDLE IS TORN. REPAIRED THE TORN CORNER.SDR UALA2011103105901Container · faultyCAPTAIN'S OXY MASK TEST AND RESET SLIDING SWITCH WILL NOT RESET CAPTAIN'S OXYGEN MASK. REPLACED CAPTAINS O2 BOX. CHECKS OKAY.SDR UALA2011102705815Galley Mat · damagedAFT GALLEY FLOOR MAT DAMAGED. COMPLETED MOISTURE BARRIER AND MAT INSTALLATION. PER AMM.SDR UALA2011102505793Slide · delaminatedRT OFF WING SLIDE PANEL DELAM ALONG UPPER AFT CORNER. REPLACED ESCAPE SLIDE ASSY.SDR UALA2011102505774Seal · pinchedFLIGHT ATTENDANT REPORTED A LOUD AIR LEAK NOISE ON LT SIDE OVERWING EXIT AT ROW 21. REMOVED OVERWING DOOR IAW AMM. FOUND LOWER SEAL PINCHED, ADJUSTED SEAL AND RE-INSTALL ED DOOR IAW AMM. PRESSURIZED ACFT IAW JRH. NO LEAKS NOTED.SDR UALA2011102505776Structure · damagedNR 2 ENGINE RT FAN COWL DAMAGED. DAMAGE OUT OF LIMITS PER AMM. FBO FOUND DAMAGE .125" D X 4" L X .375" W. NO CRACKS. GOUGE INTO CORE. OUT OF LIMITS PER AMM FOR ZONE 'C'. REPLACED FAN COWL.SDR UALA2011102605806Structure · crackedPLASTIC TRIM AROUND COCKPIT DOOR HANDLE IS CRACKED. REPLACED TRIM.SDR UALA2011102405735Bottle · lowDOOR 1L ASSIST BOTTLE PRESSURE IS LOW, INDICATES 1590 AT +20 DEGREES C. OTHER DOOR PRESSURES ARE BETWEEN 1750 TO 1775. SERVICED BOTTLE.SDR UALA2011102505791Microphone · inoperativeF/O'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED F/O O2 OXYGEN MASK STOWAGE BOX PER AMM.SDR UALA2011102405728Latch · wornPASS O2 MASK OPENED ON TAKEOFF 31ABC. LATCH WORN OUT. TAPED DOOR CLOSED AND MADE SEATS INOPERATIVE. REPACKED O2 MASKS, DROP TEST OKAY.SDR UALA2011102105700Unknown · vibrationLIGHT VIBRATION IN COCKPIT DURING CLIMB UP TO FL 300. FLT ATTENDANT REPORTED VIBRATION IN THE TAIL WAS STRONGER. ALL VIBRATION STOPPED AFTER FL300 WHILE STILL CLIMBING. ACCOMPLISHED VIBRATION TROUBLESHOOT IAW MT 53-005 REV G. ACCOMPLISHED ELEVATOR EXCESSIVESDR UALA2011102105688Radome · dentedDENT ON RADOME MEASURES APPROX 18 IN W BY 20 IN HIGH WITH SOFT-SPONGY AREAS. BEYOND LIMITS.
Back to IAE V2522-A5