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 UALA2012050802654Stringer · corrodedSTRINGER 43L CORRODED BETWEEN FR 54 AND 56. INSTALLED NEW STRINGER.SDR UALA2012050402628Power Supply · no test3SVC EMERGENCY LIGHT TEST FAILS. REPLACED EPSU 10WL, REF AMM. REPLACED EPSU 11WL BATTERY.SDR GTIA20120504412Cylinder · low pressureR1 DOOR EMERGENCY ACCUMULATOR LOW. SERVICED R1 DOOR EMERGENCY ACCUMULATOR IAW AMM 52-10-00-614-001.SDR UALA2012050802664Light · no test3SVC EMERGENCY LIGHT TEST FAILS.SDR UALA2012050802665Warning Light · illuminatedNR 1 ENGINE FADEC B FAULT DISPLAYED DURING START. RETURN TO BLOCKS.SDR UALA2012050302620Girt Bar · damagedFWD RT ENTRY DOOR SLIDE IS BROKEN. LACED GIRT BAR ONTO NEW SLIDE.SDR UALA2012050302619Actuator · leakingNR 2 OTBD THRUST REVERSER COWL OPEN ACTUATOR LEAKING. REPLACED ACTUATOR.SDR UALA2012050402635Rod End · faultyAIRFRAME VIBRATION ON CLIMB-OUT AT FL300. 78MLT VIBRATION IN COCKPIT LT-MOD VIBRATION IN AFT GALLEY. CREW REPORTED VIBRATION IN AFT CABIN RATED AT MODERATE. BLUE AND YELLOW ROD ENDS REPLACED. SSDR UALA2012050302607Computer · malfunctionedOUTFLOW VALVE FAULT DISPLAYED ON UPPER ECAM SCREEN DURING TAKEOFF. REPLACED THE AVEC.SDR UALA2012050302609Apu · malfunctionedAPU FAILED TO START 3 TIMES ON TAXI IN. OPS CHECK IAW AMM. STARTED 4 TIMES, BOTH PACKS OPERATED, IGNITION, EGT ALL NORMAL.SDR UALA2012050302614Apu · malfunctionedAPU FAILED TO START 3 TIMES ON TAXI IN. OPS CHECKED IAW AMM 49-0 0-00-201. STARTED 4 TIMES, BOTH PACKS OPERATED, IGNITION, EGT ALL NORMAL.SDR UALA2012050402647Socket · shortedFWD GALLEY CHILLER SHOCK. PERFORMING RING OUTS, SUSPECT BACK SOCKET. ACCOMPLISHED STEPS AS REQUIRED. REPLACED BLUE CHILLER LIGHT SOCKET DUE TO INTERMITTENT RESISTANCE READINGS WHILE RINGING OUT POWER PANEL. ALL OTHER READINGS AND INSPECTIONS CHECKED NORMAL.SDR UALA2012050102578Skin · wornNR 1 PYLON LOWER SKIN WORN, AS DEEP AS .020 ALONG ENTIRE WIDTH OF PYLON. LOCATED 12 INCHES AFT OF AFT ENGINE MOUNT. BLENDED AREA. AREA LOCATED 5.125 AFT OF RIB 5. INSTALLED DOUBLER RPR PER EC-RA 5451-01084.SDR UALA2012050202593Microphone · inoperativeCAPTAIN'S HAND MICROPHONE INOPERATIVE. SWAPPED THE CAPT'S MICROPHONE WITH THE FIRST OBS'S MICROPHON.SDR UALA2012050302615Microphone · inoperativeCAPTAIN'S HAND MICROPHONE INOPERATIVE, SWAPPED THE CAPTAIN'S MICROPHONE WITH THE FIRST OBS'S MICROPHONE. INSTALLLED NEW MICROPHONE.SDR UALA2012050202589Smoke Detector · inoperativeAFT CARGO COMPARTMENT SMOKE DETECTOR INOPERATIVE. REPLACED SMOKE DETECTOR.SDR UALA2012043002535Spring · failedNOSE GEAR RT LOCK SPRING IS UNSERVICEABLE REPLACE PER 3SVC AND MM 32-21-18. NOTE THIS RT SPRING WAS JUST INSTALLED 12-06-2011, FAILED IN 5 MONTHS OF USE. REPLACED RT NLG SPRING IAW AMM.SDR UALA2012043002536Servo · failedNW STEER FAULT DISPLAYED ON UPPER ECAM SCREEN. UPON GEAR EXTENSION INFLIGHT. FOUND FAILURE MESSAGE FOR LT LG DOOR CLOSED PROXIMITY SENSOR 29GA, INSTALLED NEW REF MM32-31-73. TESTED, NO HITS. REPLACED NOSE WHEEL STEERING SERVO CONTROL IAW AMM 32-51-51. OPS SDR UALA2012043002539Oxygen Bottle · failedOXYGEN BOTTLE MISSING, USED AT AFT CABIN, FWD CABIN FLIGHT ATTENDANT REPORTED THAT THE OXYGEN BOTTLE WAS FULL BUT FAILED TO PROVIDE OXYGEN TO PASSENGER. REPLACED OXYGEN BOTTLE AT AFT CABIN.SDR UALA2012050102576Control Unit · malfunctionedFLIGHT RETURNED TO BLOCKS DUE TO LAV/SMOKE WARNING. REPLACED SDCU 10WQ, LAV SMOKE FAULT CLEARED AND CHECKED GOOD.SDR UALA2012043002537Wire · shortedNOSE LANDING GEAR DID NOT RETRACT ON FIRST ATTEMPT. SECOND ATTEMPT NORMAL. ASSOCIATED STANBY PITOT DISPLAYED ON ECAM. 25GAM SENSOR FAULTED ON CFDS. REPLACED SHORTED WIRES IN CONDUIT TO 25GA NLG SENSOR PER ESPM 20-33-11 AND AWM 32-21-03. ACCOMPLISHED OP CSDR UALA2012043002538Wire · shortedSTBY PITOT DISPLAYED ON UPPER ECAM SCREEN. ANTI ICE STANDBY PITOT RIGHT AFTER TO WENT OUT 20 SECS LATER. REPLACED SHORTED WIRE IN CONDUIT 25GA REF PTT 6312001. PERFORMED TEST OF PHC3 IAW A320 MM 30-31-00. SYSTEM OP CHECKED GOOD. LGC1U PHC3 INTERFACE CORRESDR UALA2012043002541Computer · faultyCREW REPORTS ELAC 2 FAULT ON CLIMB OUT OF DEN. 2ND REPEAT FAULT. REPLACED NR 2 ELAC. ALL TESTED OK INCLUDING SIDE STICK OPS, REF AMM 27-93-00. ALSO, PERFORMED AFS LAND TEST, 22-97-00.SDR UALA2012042702519Seat · faultyFIRST OFFICER SEAT WILL NOT MOVE WITH MANUAL LEVER. ELECTRIC MOTOR OK. REPLACED SEAT ASSY.SDR UALA2012042502488Actuator · malfunctionedSTABILIZER CAN NOT TRIM NOSE UP FROM 0.5 NOSE DOWN TO UP. REMOVED AND REPLACED THS ON PTT SEQ NR 3032019 AND ACCOMPLISHED ALL STEPS ON ECRA 0550- 01095. ALL OPS CHECKED GOOD.SDR UALA2012042402473Brake Assy · draggingLEFT BRAKES EXCEEDED 300 DEGREES DURING NORMAL TAXI OAT 26 POSSIBLE DRAGGING BRAKE. REMOVED AND REPLACED BRAKES ASSY NR 1. BRAKE ASSY LEAK & OPS CHECKED NORMAL.SDR UALA2012042402452Battery · inoperativeTEST FLT, NR 2 ENGINE FIRE LOOP A FAULT IN FLT. REMOVED AND REPLACED ENGINE AND APU FIRE PANEL FOR TROUBLESHOOTING. NO CHANGE, INSTALLED ORIGINAL PANEL IAW AMM. NR 2 MAIN BATTERY WAS FOUND INOPERATIVE AND IS THE SOURCE OF THE POWER FOR THE NR 2 ENGINE LOOPSDR UALA2012042402480Bolt · dislodgedDURING TEST FLIGHT, HAD JAMMED HORIZONTAL STABILIZER DUE TO OBSTRUCTION. BOLT CAME LOOSE IN STAB COMPARTMENT & JAMMED HORIZONTAL STAB, INSPECTED ENTIRE STABILIZER COMPARTMENT IAW AMM. DETERMINED DISLODGED BOLT DID NOT DAMAGE ANY OTHER COMPONENTS.SDR UALA2012042502482Ram Air Turb · inoperativeDURING TEST FLT, RAT DOES NOT POWER. REMOVED AND REPLACED BLUE HYDRAULIC SYSTEM CSMG IAW AMM 24-24-51. OPS CHECKED GOOD.SDR UALA2012042402451Brake Assy · draggingTEST FLT, LT MLG BRAKES DRAGGING. REMOVED AND REPLACED NR 1 & 2 WHEEL BRAKE ASSYS IAW MM. REMOVED & REPLACED NR 1 & 2 BRAKE SERVO VALVES IAW MM. OPS CHECKED GOOD.SDR UALA2012042402456Valve · shortedPOTABLE WATER DRAIN WILL NOT CLOSE REF DF0790. REPLACED FWD WATER DUMP VALVE ACTUATOR. DURING OPS CHECK VALVE FAILED TO CLOSE AND WATER SYSTEM DRAIN CIRCUIT BREAKER LOCATED IN AFT GALLEY CEILING POPS REPEATEDLY. FOUND NEW VALVE SHORTED INSIDE, REPLACED FWD SDR UALA2012042402472Coupling · leakingFUELER REPORTS THAT SINGLE POINT RECEPTACLE IS LEAKING 1 DROP EVERY 3 SECONDS. REPLACED REFUEL COUPLINGSDR UALA2012042402478Drain Valve · leakingRAMP REPORTS FUEL LEAK ON RT WING. RESEATED WATER DRAIN VALVE. NO FURTHER LEAKS NOTED.SDR UALA2012042302434Blade · faultyLEFT WINDSHIELD WIPER INOPERATIVE. CAP WIPER DOES NOT PARK PROPERLY. REPLACED LT WINDSHIELD WIPER ARM-BLADE ASSY.SDR UALA2012042302404Access Panel · damagedLEFT WING FUEL PANEL 540 HB AS FOUR MISDRILLED HOLES INTO BOTTOM WING SKIN. THREE HOLES OUT OF LIMIT, REAMED TO .362' AND COLD WORKED HOLES, REAMED TO .391'. INSTALLED BUSHINGS PER SRM 57-27-11. HFEC INSP PER NTM51-10-01, NO CRACKS NOTED. N-R'S V5283H, ANDSDR UALA2012042302435Igniter · failedAPU HANGS BELOW 20 PERCENT WITH NO EGT RISE DURING ACCELERATION. REPLACED IGNITER PLUGS PER MM.SDR UALA2012042302436Switch · stickingRADIO TRIGGER SWITCH ON F/O SIDE STICK SOMETIMES STICKS IN TRANSMIT POSITION. REPLACED FIRST OFFICER'S PUSH TO TALK SWITCH ON THE SIDE STICK.SDR GTIA20120420403Cylinder · low pressureR1 DOOR EMERGENCY ACCUMULATOR LOW. SERVICED IAW AMM 52-10-00-614-001-A.SDR UALA2012042002381Hinge · crackedLEFT NR 4 ELEVATOR HINGE ARM ON HORIZONTAL STAB IS CRACKED ON TOP ON INBD FLANGE. REMOVED DAMAGED HINGE & INSTALLED NEW HINGE. MAJOR REPAIR.SDR UALA2012042302424Hinge · crackedLT NR 4 ELEV HINGE ARM ON HORIZONTAL STAB IS CRACKED ON TOP ON INBD FLANGE. REMOVED DAMAGED HINGE AND INSTALLED NEW HINGE. MAJOR REPAIR.SDR UALA2012041902349Stringer · corrodedAFT PIT HAS CORROSION ON STR 43L BETWEEN FR 52 + 60. REPLACED FACTORY STRINGER SECTION ON NR #E8396E.SDR UALA2012042002385Cone · crackedNR 1 EXHAUST TAIL CONE HAS A CRACK AT THE 10 O'CLOCK POSITION. CRACK IS LOCATED IN ZONE 1, AND IS APPROX 4 1-8" LONG. STOP DRILLED CRACK WITH 1-4" DIA DRILL BIT PER AMM.SDR UALA2012042002392Rod End · out of toleranceVIBRATION REPORTED. VIBRATION FELT IN REAR CABIN. REPLACED LT ELEVATOR, BLUE PCU ROD END. ADJUSTED PER MM. NO OTHER SETTINGS OUT OF TOLERANCE.SDR UALA2012041902341Stringer · corrodedAFT PIT HAS CORROSION ON STR 42L, BETWEEN FR 53 - 60. MAJOR REPAIR. INSTALLED STRINGER REPAIR PER SRM ON NR #E8395E BY #395958 AND INSPECTED. PER SRI 53-00-13-2-001-00 TABLE 209, MUST REINSPECT AT 60000C OR 75000T FROM REPAIR EMBODIMENT. CURRENT PTC 22532 SDR UALA2012041902342Stringer · corrodedFWD CARGO PIT STRINGER 41R, BETWEEN FR 30 + 31, PREVIOUS REPAIR IS CORRODED. REMOVED DAMAGED SECTION OF STR 41R, BETWEEN FR 30 AND 32. INSTALLED NEW SECTION STR AND SPLICES. THIS RPR REQUIRES REINSP 60,000 CYC AFTER EMBODIMENT. CURRENT PTC 22532. REINSP SDR UALA2012041902343Stringer · corrodedFWD CARGO PIT STRINGER 41R, BETWEEN FR 31 + 32, PREVIOUS REPAIR AND STRINGER CORRODED. THIS ITEM REPAIRED, SEE CF9077. SAME STR REPAIRED WITH NEW SECTION OF STR 41R. THE SRI IS ALSO COVERED. THE 2 STR LOCATIONS RPR WITH ONE RPR. N-R E8399E, E8398E BETWEEN SDR UALA2012041902345Cleat · corrodedFWD PIT, FR 31, STR 42R-41R CLEAT HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW CLEAT. FABRICATED PER SRM. INSTALLED REF SRM N-R E8778E.SDR UALA2012041902346Cleat · damagedFWD PIT, FR 33, STR 44L TO 38L CLEATS HAVE CORR. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED CLEATS, FAB NEW CLEATS. INSTALL NEW CLEATS. 1. 5EA CLEATS REPLACED. N-R E8777E.SDR UALA2012042002363Fitting · wornREAR CARGO DOOR FWD LOCK FITTING HAS WEAR MARK ON AFT LUG. REMOVED DAMAGE ON FWD LATCH FITTING, ORIG MATERIAL 0.492", RMV'D 0.003", 0.489" REMAINING, FOUND TO BE WITHIN LIMITS PER SRM. PERFORMED HFEC PER NDTM 51-10-08, NO DEFECTS NOTED. ACCOMPLISHED FLAP PESDR UALA2012041902330Control Panel · faultedCABIN EMERGENCY LIGHTS COME ON WHEN GROUND POWER TURNED OFF. REPLACED AFT FLIGHT ATT PANEL, OPS CHECKED GOOD. ACCOMPLISHED OPS CHECK OF EMERGENCY LIGHTS AND LIGHT PANEL ALL CHECKED OKAY.
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