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 UALA2011050902254Switch · faultyEMERGENCY LIGHTS COME ON. HISTORY OF EMERGENCY LIGHTS COMING ON WITH SWITCH IN "ARM" POS. FOLLOW TSM AND REPLACE SWITCH 4WL (565-2161). REPLACED EMERGENCY LIGHT SWITCH (4WL). OPERATION CHECK EMERGENCY LIGHT SYSTEM. LIGHTS OP CHECKS OKAY. PERFORMED CIDS ESDR UALA2011050902276Thrust Reverser · dentedCREW REPORT: SMALL DENT ON RT ENGINE OTBD SIDE. AMC TEXT: FBO TO EVALUATE AND REPORT FINDINGS TO SAMC-EMC. FBO FOUND DENT .5 X .5 AND .010D. NO DELAMINATION, CREASES OR CRACKS. MUST BE REPAIRED PER MT WITHIN 50T. SAMC REMARKS: THIS DENT ON NR 2 ENG TRUSTSDR UALA2011050902268Power Supply · inoperativeOVERHEAD EMERGENCY LIGHT(S) INOP. CREW COMMENTS: CABIN EMERGENCY EXIT LIGHTS CAME ON IN FLIGHT. WILL EXTINGUISH WITH EMERGENCY LIGHT SWITCH IN OFF. REPLACED EMERGENCY POWER SUPPLY 11WL AND 12WL PER AMM. EMERGENCY LIGHT TEST CHECK WAS NORMAL.SDR UALA2011050502216Actuator · faultyELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN - F-CTL. CREW COMMENTS: HAPPENED AFTER TAKEOFF. REPLACED ELAC 2. ACP'D LAND TEST. ALL GND TESTS GOOD, A-C IN CAT III STATUS. FAULT RECURRED. ELAC PREVIOUSLY REPLACED. REPLACED PITCH TRIM ACTUATOR. LEAKSDR UALA2011050202131Valve · faultyO2 SYSTEMS FAULTY, FLIGHT DIVERTED. FOUND TANK DUMP OVERFLOW VALVE PARTIALLY OPEN. CYCLED FILL AND DUMP VALVES. ALL OP'S NORMAL. RESERVICED AND PRESSURIZIED SYSTEM. NO LEAKS NOTED.SDR UALA2011050202162Bottle · reads lowCIDS CAUTION AT DEPARTURE. LT EMERGENCY SLIDE BOTTLE PRESSURE LOW. CANNOT APPLY MEL AS BOTTLE PRESSURE NEEDLE IN RED. BOTTLE REPLACED.SDR UALA2011050302164Handle · looseL2 DOOR HAS A LOUD SQUEAL AND EXTERIOR HANDLE LOOSE. L2 EXTERIOR DOOR HANDLE NOT EXTENDING WHEN DOOR HANDLE LIFTED UP. THE LEVER FOR THE LOWERING SHAFT OF THE DOOR INNER HANDLE, HAS NO SPRING LOAD AND STICKS IN ANY POSITION. FOUND LOWERING SHAFT INNER AND OUSDR UALA2011050302172Circuit Breaker · faultyCB'S ARE TRIPPING. ASSURE ALL WIRING THAT WAS EFFECTED UNDER EG5429 WAS DONE PROPERLY AND IS PROPERLY ROUTED. AFTER REPLACEMENT OF CB 9002ML3 AND REPLACEMENT OF 9004ML3 CB ALL CB AND GALLEY EQUIPMENT CHILLERS,WORK LIGHTS, COFFEEMAKERS & CBS OP CHECKED OKAY.SDR UALA2011042902098Retainer · stuckGIRT BAR AFT RETRAINING CLIP STUCK IN DOWN POSITION AT DOOR 1L. CLEANED AND LUBRICATED FLOOR RETAINING CLIP.SDR UALA2011042802085Duct · leakingCIDS CAUTION LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE FOUND APU DUCT BLEED LEAK RIGHT NEXT TO THE OFFWING SLIDE INFLATION CYLINDER, CAUSING THE COMPARTMENT TO BE EXTREMELY HOT. MESSAGE SAYS EMERGENCY SLIDE PRESS LOW. REPLACED LEFT EMERGENCY ESCAPE SLIDE BOTSDR UALA2011042602025Lock · lack of lubeFOUND FWD FLOOR FITTING FOR THE SLIDE GIRT BAR STUCK IN THE UNLOCKED POSITIONED AT DOOR 2R. LUBED FLOOR FITTING LOCK, OPS CHECKED OKAY.SDR UALA2011042702051Actuator · malfunctionedMAIN LANDING GEAR DID NOT EXTEND USING ALTERNATE GEAR SWITCH. ON 2ND ATTEMPT HAD RT MAIN BUT STILL NO LEFT. REPLACED LT MLG DOOR ACTUATOR IAW MM. LEAK AND OPS CHECK GOOD IAW MM. PERFORMED ALTERATE EXTENSION SYSTEM TEST IAW MM. TEST GOOD.SDR UALA2011042501988Skin · dentedON WALK AROUND APPARENT DENT ON NR 4 SLAT RT SIDE. SLAT REPAIRED PER SRM 57-40-00. OKAY FOR SERVICE.SDR UALA2011042501990Radome · damagedCREW REPORTED A BIRD STRIKE ON TAKEOFF. 140KTS AT ROTATION JUST BELOW RADOME. ACCOMPLISHED INSP REF AMM, DAMAGE FOUND TO RADOME ONLY. REPLACED RADOME.SDR UALA2011042501986Filter · dirtyLGCIU 2 FAULT - ODOR IN COCKPIT, RTFL. REPLACED BOTH RECIRC FILTERS, POWERED A-C TURN ON ALL COMPUTERS IN COCKPIT, TURNED ON ALL LIGHTS IN CABIN, TURN GALLEY UNITS ON, NO ELECTRICAL ODOR THROUGH OUT ACFT.SDR UALA2011042502010Servo Valve · faultySPOILER FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: NR 1 SPLR BOTH SIDES INDICATES AMBER RETRACTED. REPLACED SERVO VALVE FOR NR 1 SERVO CONTROL. OP CHECKS GOOD, NO LEAKS.SDR UALA2011042501999Radome · damagedRADOME BIRD STRIKE. MEASURE DELAMINATED AREA 11X15 INCHES DELAMINATED. OUT OF MM LIMITS, REPLACED RADOME. ACCOMPLISHED VISUAL INSP OF AIRCRAFT AND NO DEFECTS NOTED. RADOME SECURED CLOSED.SDR UALA2011042502009Hook And Loop · unsecureCREW REPORT: SLIDE PACK COVER AT 2L HAS FALLEN OFF. RE-SECURED BUZZLE, FOUND VELCRO ON TOP UNGLUED. RESECURED WITH DOUBLESIDED TAPE AS INTERIM.SDR UALA2011042502011Lens · missingSLIDE ARMED LENS MISSING LT OVERWING EMER EXIT. REPLACED LENS.SDR UALA2011042501982Engine · vibrationNR 2 ENGINE VIBRATION. CHECKED THE MASTER MAGNETIC CHIP DETECTOR FOR DEBRIS. NR 1 ENG INSPECTED ALL 6 AND MASTER CHIP DETECTORS FOR PARTICLES. ALL CHIP DETECTORS CLEAN. ACCOMPLISHED NR 1 ENG VIBRATION SURVEY IAW MM TASK. NR 8 TEST OKAY, MAX VIB WAS 1.3 UNSDR UALA2011042101941Oil Cooler · leakingCREW REPORTED ENG 2 FUEL LEAK UNDER ENGINE. FOR ENGINE DRAINS LEAK RATE LIMITS, REPORT FINDINGS TO SAMC, CARRIED FORWARD PER SAMC. LCL UAL MAINT REP REPORTS FUEL LEAK FROM ACOC (AIR COOLED OIL COOLER) APPROX 19 DPM DURING IDLE RUN BY FLIGHT CREW, WITHIN CARRSDR UALA2011042201952Slide · crackedON PRE-DEPARTURE RT OVERWING ESCAPE SLIDE AFT EDGE HAS 8.5 INCH CRACK, OUT OF LIMITS. NOTE CRACK IS IN AREA 2. REPLACED RT SLIDE PER MM. INSP AND FORMAN PRESENT. ELEC CONNECTOR AND HOSE INSTALLED.SDR UALA2011042001914Limiter · malfunctionedCREW REPORT: F-CTL SLATS FAULT. CREW REPORTED FLAPS-SLATS FAULT GOING TO FLAPS 1. CFDS SHOWED "27-80-00 SLT 1 SYS JAM - CHECK MECH DRIVE" AND "27-80-00 SLT 2 SYS JAM - CHECK MECHANICAL DRIVE. CREW USED CAPT EMERG AUTHORITY TO CYCLE CB'S B6+B7+Q21 FAULT CLEASDR UALA2011042201953Shade · damaged11F EMERGENCY EXIT WINDOW SHADE DAMAGED. SHADE REMOVED. REQUIRES EXIT HATCH REMOVAL AND RE-INSTALLATION. REMOVED AND REPLACED LINER AND WINDW SHADE. SHADE BINDS, NEW SHADE ORDERED. RT EXIT HATCH REMOVED. REPLACED SHADE, RE-INSTALLED HATCH.SDR UALA2011042001913Ram Air Turb · lack of lubeFOUND RAT OIL LEVEL DRY DURING RAT CHECK. RAT REMOVED, INSTALLING NEW RAT. REPLACED RAT. MADE SMC 12 AND SMC 13 TO COVER OPS CHECKS.SDR UALA2011041901895Amu · faultyF/O COMM PANEL O2 MASK INTERCOM SWITCH DOES NOT WORK. AMU FOUND FAULTY. REPLACED AMU. OPS NORMAL.SDR UALA2011041901896Panel · faultyF/O ACP VHF2 CANNOT BE DE-SELECTED. REPLACED FAULTY PANEL. OP CHECK IS GOOD.SDR UALA2011042101931Circuit Breaker · trippedMULTIPLE CB TRIPPED RELATED TO THE ELEC SYSTEM. AFTER ACCOMPLISHMENT OF COA406283, ACFT EXPERIENCED CB TRIP, DISCOVERED CB'S AB10 (TR1 SUPPLY), AD11 (101XP SUPPLY), AD12 (L WING PUMP STBY SUPPLY), BC1 (TR2), & BG (202PP SUPPLY) TRIPPED. RESET BREAKERS & MANUSDR UALA2011042001909Blade · damagedDUE TO FAN BLADE NR 21 WAS DAMAGED, REPLACED. NR 2 ENG S-N V10523 LPC BLADE 21 MOMENT WT 2498.0 AND PERFORMED VIB SURVEY REF MM. PEAK VIB .7 N1 AND .2 N2. OPERATIONAL TEST NORMAL.SDR UALA2011041801882Rod End · faultyAIRFRAME TAIL VIBRATION DURING CLIMB. GROSS WT LASTED UNTIL FL 300. MAINT TEXT: CREW REPORTS THERE WAS NO YAW DURING VIBRATION. NO VISIBLE ANOMALY OBSERVED ON HORIZONTAL STAB. ACCOMPLISHED MT-005 REV G VIBRATION TROUBESHOOTING. ELEVATOR SERVO CONTROL FREESDR UALA2011041801883Cover · missingAFT ATTENDANT PANEL 126RT MISSING EMER LIGHT SWITCH CLEAR PLASTIC COVER. LOCATED AT DOOR 2L. REPLACE SWITCH COVER. OPS NORMAL.SDR UALA2011041801876Skin · damagedPRELIMINARY INSPECTION OF LIGHTNING STRIKE NOTED 24 STRIKE POINTS ON LEFT SIDE, BETWEEN THE WING-TO BODY FAIRINGS & THE RVSM AREA. ALL POINTS ARE MARKED STARTED INSPECTION OF A/C PER AMM. COMPLETED WING INSPECTION UPPER, LOWER SURFACES, FLAPS UPPER,LOWER SURSDR UALA2011041801888Oxygen Mask · out of positionCREW REPORT: ROW 21ABC OX MASK HANGING DOWN. SECURED. REPACKED O2 MASK AND ACP DROP TEST, OPS CHKS NORMAL.SDR UALA2011041801889Control Panel · defectiveF/O'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED F/O'S O2 MASK PER AMM, NO HELP. REPLACED F/O'S ACP CHECKS NORMAL.SDR UALA2011041501834Panel · faulty'ENG FIRE EXTING-SQUIB' LIGHT OF 'AGENT 1' PUSHBUTTON SWITCH IS OFF DURING 'LOOP-SQUIB TEST'. ENG 2 SQUIB LIGHT WILL NOT ILLUMINATE DURING FIRE TEST. COMPLETED REQUIRED CHECKS AS REQUIRED IN MEL 2621F. FOUND TO NEED FIRE TEST CONTROLLER IN COCKPIT. SEEMS TO BSDR UALA2011041501828Valve · faultyCANNOT CLOSE AFT CARGO DOOR. REPLACED VALVE.SDR UALA2011041501830Control Unit · malfunctionedCARGO HEAT INOP. REPLACED CARGO COMP TEMP SENSOR, NO HELP. TRIED CARGO HEAT CONTROLLER 10HC, NO HELP. REINSTALLED ORIGINAL CONTROLLER. CARGO HOT AIR VALVE WILL NOT OPEN. CANNOT REGULATE TEMP USING CARGO HEAT SELECTOR. REPLACED AFT CARGO PIT TEMP SENSOR, SDR UALA2011041201774Actuator · faultyNR 2 RUDDER TRIM INOPERATIVE. ACTUATOR CHANGED, BAD FROM STOCK. RUDDER DOES NOT RETURN TO ZERO POSITION WHEN TRIM RESET BUTTON PRESSED. REMOVED ACTUATOR MOUNT BOLTS AND GROUND STRAP MOUNT BOLT. NEW ACTUATOR ON AOG Z4932. RUDDER REQUIRES ABOUT 4.3 RT TRIM SDR UALA2011041201778Skin · damagedAFT PIT AREA NEEDS INVESTIGATING DUE TO CONTACT. DENT AND GOUGE IN FUSELAGE SKIN LOCATED APPROXIMATELY 6" BELOW AND 3 FEET AFT OF CARGO DOOR, CONTACT WITH BELT LOADER. TOTAL LENGTH OF DAMAGE IS 24 INCHES, FIRST DAMAGE DOWN TO METAL IS APPROX .5 INCHES LONG ANSDR UALA2011041201761Controller · inoperativeFO'S WINDSHIELD HEAT IS INOP. REPLACED WINDOW HEAT CONTROLLER NR 2. BITE TEST OKAY.SDR UALA2011041201776Oxygen Mask · leakingFO'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). SWAPPED FO'S WITH OBSERVER'S MASK, INSTALLED MASK. OBSERVERS SEAT CONSIDERED INOP. RPL'D 1ST OBSERVER'S O2 MASK ASSY.SDR UALA2011041101711Stringer · corrodedSTRINGER 31R AT FRAME 64-66 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: STRINGER CORROSION FOUND OUT OF LIMITS OF SRM. REMOVED CORRODED STRINGER SECTION AT PRODUCTION SPLICES. PROCURED & INSTALLED NEW STRINGER SECTION FROM FRAME 64-67.SDR UALA2011041101718Handle · lack of lubeAFT CARGO DOOR ECAM, RTFL AFT CARGO OVHT DOOR AFT CARGO. ECAM WRN: 21-43 COND AFT CRG HEAT FAULT. SUSPECT 644-0096 (11HC) PRESS REG VALVE, PROX SWITCH (50WV) 565-0047. PFR SHOWED DOOR AFT CARGO & COND AFT CARGO HEAT FAULT WITH LGCIU 1 REPORTED AFT CARGO DOSDR UALA2011041101717Controller · malfunctionedF/O'S WINDSHIELD HOT TO THE TOUCH AFTER ARRIVAL. PULLED RT WINDOW HT CB'S. RT WINDSHIELD HEAT CONTROLLER REPLACED. F/O WINDSHIELD CRACKED. REPLACED WINDOW. OPS CHECKED GOOD.SDR UALA2011041101724Smoke Detector · faultyCREW REPORTED LAV SMOKE DET ECAM. NO TIME TO WORK. REPLACED FWD LAV SMOKE DETECTOR AND RESET CIDS AND CIDS OK.SDR UALA2011041101725Strap · out of positionFOUND STRAP FROM SLIDE PACK DOOR 1L HANGING OUTSIDE DOOR WHEN AIRCRAFT ARRIVED AT GATE. STRAP CAME OFF SLIDE PACK, GLUE DID NOT HOLD STRAP TO SLIDE PACK. BONDED STRAP AND BUCKLE ASSY ONTO ESCAPE SLIDE COVER AT MED 1L. NO SLIDE REPLACEMENT REQUIRED.SDR UALA2011040801708Wire · chafedG4 GALLEY BEHIND UPPER ELECTRICAL CONTROL PANEL FEEDER WIRES 2456-1406-8 AND 2456-1407-8 CHAFED THRU TO CONDUCTOR 8 INCHES AFT OF CONNECTOR 9004ML4. ACCOMPLISHED EVA 80749. ALL AFT GALLEY COMPONENTS OPERATE NORMAL. NEEDS TO BE RECHECKED AT EACH 2A CHECK. RESDR UALA2011040701681Screw · looseFUEL LEAKING FROM RT WING OUTBOARD FIXED FLAP TRACK PORTION AT A RATE OF 2 DROPS PER MINUTE. LOWERING FLAPS DRAINED APPROX 1 CUP OF FUEL. REMOVED FWD END OF CANOE. FOUND MULTI SCREWS LOOSE. SECURED, NO FURTHER LEAKAGE.SDR UALA2011040601667Light · no testEMERGENCY LIGHT TEST FAILED MESSAGE EXT LOADS FWD L. TROUBLESHOT PER TSM. CONNECTED TESTING TOOL AT DOOR 1L TEST PASSED.SDR UALA2011040701688Wire · shortedSFCC 1-FLAP FAULTS. MEGGERED WIRES WITH CON OFF AND NR 1 LGCIU OUT FOUND WIRE 2751-5907B BETWEEN CONNECTOR 7541VC AND 7505VC SHORTED TO GROUND. REF AWD27-51-11. REPLACED R&B WIRES 2751-5907B AND 2751-5907R BETWEEN CONNECTORS 7541VC AND 7505VCA. REF WD AND ESP
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