Allison AE-3007A1P
Service difficulty reports · 849
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 = 'AE3007A1P' 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 = 'AE3007A1P' 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 C2XA10IA332Engine · leakingIAH - FLIGHT 2496, THE CREW REPORTED AN ACRID BURNING SMELL LIKE TIRES OR GUNPOWDER DESCENDING THROUGH FL270 THAT ONLY LASTED A FEW SECONDS, WITH NOTHING NOTICED BY THE F/A. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THSDR C2XA10CL179Actuator · leakingFSD FLT 5992 - THE CREW REPORTED DURING PREFLIGHT APU ON, FUEL XFEEDING ON TANK NR 1, FUEL CONTINUOUSLY STREAMING OUT OF THE SIGHT GLASS OF NR 1 ENGINE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE CVG ACTUATOR. OPERATIONAL CHECKS WERE GOOD.SDR C2XA10IA271Carbon Seal · leakingIAH - FLIGHT 2627, THE CREW REPORTED A STRONG FUEL/HYDRAULIC ODOR IN THE COCKPIT AND SEEMED STRONGER WHEN OPERATING OFF OF THE NUMBER ONE ENGINE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT, AND MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE SDR C2XA10IA223Wire · damagedIAH - FLIGHT 3083, THE CREW REPORTED THAT THE THRUST RATING WAS STUCK IN T/O MODE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FADEC 1B WIRES W191-1797-24WH AND W191-1797-24BL, OPERATIONALLY TESTED WITH NO DEFECTS, ANDSDR C2XA10IA224Wire · defectiveIAH - FLIGHT 3083, THE CREW REPORTED THAT THE THRUST RATING WAS STUCK IN T/O MODE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FADEC 1B WIRES W191-1797-24WH AND W191-1797-24BL, OPERATIONALLY TESTED WITH NO DEFECTS, ANDSDR C2XA10IA222Control Panel · inoperativeIAH - FLIGHT 2354, THE CREW REPORTED THAT THE T/O RATING WAS STUCK IN T/O MODE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE THRUST RATING CONTROL PANEL, OPERATIONALLY AND TEST FLSDR C2XA10CL115Engine · vibrationCLE FLT 5718 THE CREW REPORTED THE NR 2 ENGINE HP VIB WAS AT 1.1 IPS IN FLIGHT, HAD TO REDUCE THRUST TO MAINTAIN A MAX OF 1.1 IPS IN CRUISE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD.SDR C2XA10CL088Engine · leakingEWR FLT 2398 THE CREW REPORTED A FOUL SMELL FROM THE PACKS WHEN THE ENGINE BLEEDS WERE ON. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.SDR C2XA10IA064Packing · damagedIAH - FLIGHT 2617, THE CREW REPORTED LAV SMOKE IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TOSDR C2XA10TY019Gearbox · corrodedTYS - AIRCRAFT IN FOR A 2C INSPECTION WHEN INSPECTION FOUND CORROSION BETWEEN THE ACCESSORY GEAR BOX AND ENGINE. MAINTENANCE REMOVED THE CORROSION IAW EMB EC7220-01085. ALL WORK WAS ACCOMPLISHED AND A/C RELEASED TO SERVICE.SDR C2XA09CL157Carbon Seal · malfunctionedCLE FLT 2542 THE CREW REPORTED SMOKE IN THE CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. TEAR DOWN REPORT FROM ROLLS ROYCE INDICATED THE NR 0 CARBON SEAL RUNNER WASDR C2XA09RI203Engine · damagedFLIGHT 3046 - PHL - DURING DESCENT, FLIGHT CREW REPORTED BIRD STRIKE, CAUSING E2 EXCEEDANCE, ITT WENT INTO RED AND ENGINE SHUTDOWN. FLIGHT CREW DECLARED EMERGENCY AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 2 ENGINE AND PERFORMED OPERATIONALSDR SIMA200934106Carbon Seal · leakingON FLIGHT 3064 RIGHT AFTER TAKEOFF THE CREW REPORTED, RECEIVED A LAV SMOKE INDICATION MESSAGE ON EICAS. THE FLIGHT ATTENDANT REPORTED, SMELLED A STRANGE ODOR IN THE CABIN. THE CREW DECLARED AN EMERGENCY. THE FLIGHT DECK CREW DONNED OXYGEN MASK AND RETURNED SDR CHQA200900215Socket · dirtyDURING INSPECTION THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOP. MAINTENANCE CLEANED THE LIGHT BULB SOCKET AS REQUIRED AND THE EMERGENCY OVERWING EMERGENCY LIGHT OPERATED NORMALLY.SDR C2XA09IA247Engine · leakingIAH - DURING MAINTENANCE INSPECTION AN OIL SMELL WAS REPORTED IN THE CABIN WITH THE NR 2 ENGINE BLEED AND PACS ON FULL HOT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETUSDR CHQA200900213Pressure Switch · defectiveFLIGHT 5344 STL TO RDU. IN FLIGHT AT FL330 THE FLIGHT CREW RECEIVED AN AUTO PILOT FAIL AND YAW DAMPER FAIL MESSAGE FOLLOWED SHORTLY AFTER WITH A RUDDER 1-2 INOP MESSAGE. THE CREW RAN THE QRH PROCEDURE AND DIVERTED TO SDF. MAINTENANCE CHECKED THE WIRING FROMSDR CHQA200900194Warning System · activatedON TAKEOFF FROM IAD THE CREW RECEIVED A MASTER WARNING OF "TAKEOFF TRIM". THE TAKEOFF WAS ABORTED WITHIN 5 KTS OF V1. AFTER CLEARING THE RUNWAY AND COMPLETING THE CHECKLISTS THE "BRAKES OVERTEMP" MESSAGE APPEARED. TAXI CONTINUED SLOWLY UNTIL TAXIWAY "Y" WASSDR CHQA200900176Uplock · defectiveON TAKEOFF FROM CMH THE CREW RECEIVED A LANDING GEAR DISAGREE MSG. THE FLIGHT RETURNED TO THE FIELD AND MADE A NORMAL LANDING. UPON INSPECTION BY MAINTENANCE AND AFTER SEVERAL GEAR SWINGS, WAS ABLE TO DUPLICATE THE FAULT. MAINTENANCE REPORTED THAT THE LT MLSDR CHQA200900177Fcu · defectiveJUST AFTER TAKEOFF FROM CVG THE FLIGHT CREW REPORTED THAT THE LT FUEL QUANTITY SHOWED ZERO AND RECEIVED A FUEL IMBALANCE MESSAGE. THE FLIGHT RETURNED TO THE FIELD AS A PRECAUTION AND PERFORMED A NORMAL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND ITSDR C2XA09CL087Blade · fracturedCLE - FLT 2135 - THE CREW REPORTED A NR 2 ENGINE UNCOMMANDED SHUTDOWN IN FLIGHT. ENGINE WOULD NOT RESTART AND THE AIRCRAFT DIVERTED INTO CVG AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOSDR CHQA200900146Windshield · arcedON APPROACH TO LANDING IN YYZ THE FLIGHT CREW NOTICED AN ODOR SIMILAR TO AN OVERHEATING PACK. THE PACKS WERE TURNED OFF AND THE ODOR BEGAN TO INCREASE IN STRENGTH AND SMELL OF ELECTRICAL. AS A PRECAUTION THE CREW PERFORMED THE COCKPIT/CABIN FIRE OR SMOKE MEMSDR CHQA200900143Tire · blownON TAKE OFF THE RT IB MAIN LANDING GEAR TIRE BLEW. THE FLIGHT CONTINUED NORMALLY UNTIL REACHING DCA WHERE IT WAS NOT ALLOWED TO LAND. THE FLIGHT THEN DIVERTED TO IAD WHERE IT LANDED WITHOUT INCIDENT. UPON INSPECTION AFTER THE FLIGHT THE FWD WOW HARNESS WAS SDR C2XA09CL076Turbine Wheel · crackedDURING COMPLIANCE WITH SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND DURING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL061Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL060Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR C2XA09CL057Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR C2XA09CL054Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL051Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR C2XA09CL050Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR C2XA09CL052Case · crackedDURING COMPLIANCE OF SB AE3007A-72-368 MAINTENANCE FOUND THE NR 2 ENGINE FAN CASE HAD MULTIPLE CRACKS AROUND THE CIRCUMFERENCE OF THE CASE. THE COMPOSITE CONTAINMENT RING WAS ALSO DELAMINATED. THE FAN CASE WAS REPLACED.SDR C2XA09CL049Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL044Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR C2XA09CL047Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL046Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL043Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR C2XA09TY059Housing · leakingIAH/IND- NR 2 ENGINE LOST OIL/OIL PRESSURE IN FLIGHT AND THE ENGINE WAS SHUTDOWN. AN EMERGENCY WAS DECLARED AND A/C LANDED SAFELY. UPON INSPECTION THE OIL FILTER HOUSING WAS FOUND TO BE LEAKING. MX REMOVED AND REPLACED THE OIL FILTER HOUSING AND LEAK CHECKESDR C2XA09RI067Housing · leakingFLIGHT 2586 - IND - FLIGHT CREW REPORTED NR 2 ENGINE LOSS OF OIL/PRESSURE IN FLIGHT. CREW PERFORMED INFLIGHT SHUTDOWN AND LANDED UNEVENTFULLY. MX REMOVED AND REPLACED OIL FILTER HOUSING ASSY AND PERFORMED OPERATIONAL/LEAK CHECK SUCCESSFULLY. ACFT WAS APPROVSDR C2XA09CL038Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR C2XA09RI035Engine · faultyFLIGHT 2337 - CLT - FLIGHT CREW REPORTED FUEL SMELL IN THE COCKPIT AND ENGINE NR 2 LOCKED UP. MX REMOVED AND REPLACED ENGINE NR 2 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR CHQA200900063Battery Pack · dischargedTHE OVERWING AND AFT EMERGENCY PROXIMITY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. THE NR 4 BATTERY PACK ASSEMBLY WAS REPLACED AND THE SYSTEM OPERATIONALLY CHECKED GOOD.SDR CHQA200900062Line · misalignedDURING TAKEOFF ON INITIAL CLIMB-OUT, THE CREW RECEIVED A MASTER WARNING OF A BLEED 1 LEAK. THE CREW RAN THE QRH AND ISOLATED THE PROBLEM AND THE MESSAGE CLEARED. THEY ELECTED TO RETURN TO THE FIELD DUE TO FORECASTED ICING ON THE ROUTE OF FLIGHT. A NORMAL LASDR CHQA200900061Strut · underservicedUPON GEAR RETRACTION THE CREW RECEIVED A L/G AIR/GND FAIL MESSAGE ON THE EICAS. FOLLOWED SHORTLY BY E1-2 REVERSE DISAGREE MESSAGE. THE CREW RETURNED TO THE FIELD AND BOTH MESSAGES CLEARED ON GEAR EXTENSION. A NORMAL LANDING WAS MADE. UPON INSPECTION BY MAISDR CHQA200900059Proximity Switch · failedAFTER TAKEOFF FROM DCA, THE CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON THE EICAS. THE CREW ATTEMPTED TO RETRACT THE LANDING GEAR AND THE GEAR SELECTOR WOULD NOT MOVE. SAFE CLIMB WAS NOT AFFECTED BY TERRAIN SO AN OVERRIDE WAS NOT ATTEMPTED. THE CREW FOLLOWEDSDR C2XA09IA010AEngine · malfunctionedSAT - FLIGHT 2630, THE CREW REPORTED A LAV FIRE DETECTION INDICATION IN FLIGHT. THE ACFT RETURNED TO SAT WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND PLACED THE LAV SMOKE DETECTOR ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE ACSDR C2XA09RI001Bleed Valve · inoperativeBNA - FLIGHT 2573 - FLIGHT CREW REPORTED ENGINE NR 1 BLEED VALVE CLOSED IN FLIGHT AND THEY WERE UNABLE TO REOPEN. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. MX R&R ENGINE BLEED VALVE AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETSDR C2XA08CL123Engine · faultyCLE - FLIGHT 2311 - THE CREW REPORTED AT FL320 THE NR 2 ENGINE ITT STARTED INCREASING SLOWLY TO 860 WITHOUT FULL THRUST. ASSENTING AT 91PERCENT N2 THE ENGINES HAD A 30 DEGREE DIFFERENCE. THE FUEL FLOW WAS ALSO NOTED TO BE 30 PPH HIGH. MAINTENANCE INSPECTED ASDR C2XA08CL117Oil System · fluctuatesEWR FLIGHT NR 2142 THE CREW REPORTED DURING TAKEOFF ROLL AND INITIAL CLIMBOUT THE OIL PRESSURE REMAINED ABOVE 115 PSI FOR 2 MIN ON THE NR 1 ENGINE. ALSO BELOW 13000 FT THE NR 1 ENGINE OIL PRESSURE WOULD ENTER THE AMBER RANGE WITH THRUST IN DESCENT. MX INSPECSDR CHQA200800199Smoke Detector · faultyFLIGHT 3048, RDU TO LGA. AT FL270 WHILE OVER RIC, THE FLIGHT CREW RECEIVED A BAGG SMOKE EICAS INDICATION. THE QRH WAS FOLLOWED, AND AFTER PRESSING THE BAGG SMOKE BUTTON THE MESSAGE WENT OUT AFTER TWENTY SECONDS. THE AIRCRAFT DIVERTED TO IAD AND LANDED WITHOSDR C2XA08IA160Oil System · leakingIAH - FLIGHT 2684, THE CREW REPORTED THAT THE NUMBER ONE ENGINE OIL QUANTITY DROPPED TO 3 QTS IN FLIGHT WHILE PRESSURE AND TEMPERATURE REMAINED NORMAL. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT.
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