Allison AE-3007C
Service difficulty reports · 793
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 = 'AE3007C' 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 = 'AE3007C' 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 C2XA03BT098Wire · brokenEWR---CO3256, CREW REPORTED (ON WALKAROUND), THAT THE EMERGENCY EXIT SIGN NEAR THE PASSENGER DOOR IS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE NEAR PASSENGER DOOR, REPAIRED BROKEN WIRE, AND OPS CHECKED EMERGENCY LIGHTS GOOD.SDR RAIA00310262Indicator · malfunctioned5689-STL- EADI NR 2 ROLLS CONTINUOUSLY. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS.SDR SIM2004F00000Floorbeam · corrodedDURING INSPECTION THE LT FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMIT BETWEEN FRAMES 24 AND 25. COMPLETELY REMOVED THE CORROSION BY CREATING A CUT OUT IN THE DAMAGED FLANGE AND WEB OF THE LT FLOORBEAM. FABRICATED A REPAIR ANGLE, FILLER AND SHIMS FOR RESDR C2XA03CL173Light · inoperativeCLE FLIGHT NR 2066 THE CREW REPORTED THE EMERGENCY LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT EXIT LOCATOR. OPERATIONAL CHECKS WERE GOOD.SDR CNQ2003F00002Controller · shortedWHILE DESCENDING THROUGH FL330, THE COCKPIT TEMPERATURE CIRCUIT BREAKER TRIPPED. COCKPIT DISPLAY UNITS NR 1 AND NR 2 WENT INOPERATIVE. UPON FURTHER DESCENT, COCKPIT DISPLAY UNITS NR 4 AND NR 5 WENT INOPERATIVE. ALL DISPLAY UNITS WORKED OK AFTER COOLING OFFSDR RAIA00309248Fuse · blownLEFT ELECTRICAL HYD PUMP FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED FUSE.SDR DXTA200300126Valve · malfunctionedWHILE IN LEVEL CRUISE FLIGHT AT 29,000 FT THE (WING TANK O'FULL L-R) AMBER CAS MESSAGE ILLUMINATED. BOTH WING TANKS OBSERVED TO BE DUMPING FUEL FOR 2 MINUTES. - TROUBLESHOT AND FOUND BOTH WING VENT VALVES INOP. REMOVED AND REPLACED LEFT AND RIGHT WING VENT VSDR C2XA03SH344Rib · chafedDURING C CHECK MAINTENANCE FOUND THE NR 1 LOWER ENGINE COWLING CENTER RIB TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 51-21-04 AND 51-21-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH345Rib · chafedSHV-DURING C CHECK A NR 1 ENGINE LOWER COWLING INBOARD RIB 8 INCHES FORWARD OF AFT RIB WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH346Stiffener · chafedDURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED ALONG THE ENTIRE RADIUS. MAINTENANCE REMOVED THE DAMAGED AFT STIFFENER AND REPLACED IT WITH A NEW AFT STIFFENER IAW WITH EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETUSDR C2XA03SH347Stiffener · chafedDURING C CHECK MAINTENANCE FOUND THE NR 2 ENGINE UPPER COWLING AFT STIFFENER TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03TY166Floorbeam · corrodedDURING A SCHEDULED 2C INSPECTION THE LT FLOORBEAM WAS FOUND CORRODED. MAINT. REMOVED AND FAB. A NEW FLOORBEAM. CLEANED SURFACE CORROSION,PRIMED,PAINTED AND INSTALL THA NEW FAB. PART IAW EMB 135/145 SRM 51-10-03 AND CPM 51-21-03,05,06. ALL WORK WAS ACCOMPLISHEDSDR C2XA03SH341Threshold · corrodedDURING C CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SEVICE.SDR C2XA03IA096Wire · looseTHE CREW NOTED THAT THE EMERGENCY LIGHTS POP THE CIRCUIT BREAKER WHEN SELECTED ON DURING POST-FLIGHT. STL- MAINTENANCE RESECURED WIRE TO THE EMERGENCY LIGHT BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCSDR DXTA200300122Bungee Cylinder · loosePITCH VIBRATION IN FLIGHT CONTROLS WITH AUTO PILOT ON, VIBRATION INCREASED AS SPEED INCREASED. NOTICED AT 250 KTS AND 10000FT, VIBRATION ALSO COULD BE HEARD AS LOW FREQUENCY SOUND. TIGHTENED LT ELEVATOR BUNGEE AND ADJUSTED ELEVATOR CABLE TENSION IAW CESSNA 75SDR C2XA03IA097Light · inoperativeTHE CREW NOTED DURING PREFLIGHT THE EMERGENCY FLOOR PROXIMITY LIGHTS WERE INOPERATIVE. BNA- MAINTENANCE PLACED FLOOR LIGHTING ON DMIDO TO PARTS NOT IN STOCK.THE AIRCRAFT WAS RETURNED TO SERVICE. IAH- MAINTENANCE REMOVED AND REPLACED THE FLOOR PROXIMITY LIGSDR DXTA200300116Bleed Valve · malfunctionedUPON CLEARED FOR TAKEOFF, ADVANCED THROTTLES AND THE RED CAS MESSAGE, ENGINE FAIL R APPEARED. ENGINE AUTO SHUTDOWN. EXCEEDS PAGE SHOWED IT WAS TRIGGERED BY R ITT 1020 DEGREES COMPARED TO LEFT ITT OF 644 DEGREES. BORESCOPED COMBUSTION SECTION & TURBINE ASSEMSDR DXTA200300117Filter · cloggedFUEL FILTER BYPASS L CAS MESSAGE CAME ON ABOUT 5 SECONDS AFTER TAKEOFF POWER APPLIED. TAKEOFF ABORTED. INSTALLED NEW FUEL FILTER & RESET BYPASS INDICATOR IAW AE3007C MM CHAPTER 73-30-00, LEAK AND OPS CHECKED GOOD.SDR C2XA03TY150Gusset · corrodedDURING A SCHEDULED INSPECTION THE GALLEY FLOOR AFT GUSSET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT GUSSET IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA03SH252Floorbeam · corrodedSHV-DURING C CHECK THE CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR DXTA200300069Downlock Switch · inoperativeRIGHT MAIN LANDING GEAR INDICATION REMAINED GREEN AFTER GEAR WAS RETRACTED, USED EMERGENCY BLOW DOWN GEAR. LANDING WAS UNEVENTFUL. DETERMINED THE RIGHT GEAR ACTUATOR DOWNLOCK SWITCH WAS FAULTY, REMOVED AND REPLACED WITH NEW SWITCH, PERFORMED GEAR OPERATIONSDR C2XA03BT069Inverter · failedBTV---CO2316, DURING SERVICE/ROUTINE CHECK FOUND EMERGENCY LIGHT AISLE PATH LIGHTING FROM SEAT ROW 11 THROUGH 19 INOPERATIVE. REMOVED AND REPLACED AC/DC INVERTER IAW AMM NR 33-50-11. OPS. CHECKED LIGHTS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CA030703004Wire Harness · shorted(CAN) RT WINDSHIELD HEAT INOPERATIVE ON ENGINE INDICIATING AND CREW ALERT SYSTEM POPPED. SB HK062 AC POWER TO RT WINDSHIELD. WIRE BUNDLE PQ020 AND JE004 TOUCHING AND HEAT SHRINK FAILURE CAUSING SB HK 062 TO POP.REPLACED HEAT SHRINK PROBLEM ELIMINATED.SDR DXT2003F00000Manifold · shortedAFTER TAKEOFF LANDING GEAR FAILED TO RETRACT AND OPENED LEFT MLG BREAKER. RSETTING BREAKER OPEN AGAIN. EMERGENCY GEAR BLOW-DOWN INITIATED AND LANDED AT AIRPORT HANGER. OPERATIONAL CHECK CONFIRMED DISCREPANCY. FOUND SHORTED SOLENOID IN GEAR CONTROL MODULE. SDR DXTA200300037O-Ring · failedON LANDING ROLL, HAD A COMPLETE LOSS OF SYSTEM HYD FLUID AND EMERGENCY BRAKE WAS USED, AIRCRAFT HYDROPLANED BUT STOPPED SAFELY, NO VISIBLE DAMAGE TO AIRCRAFT. REPLACED ORING PLUG, ON "A" HYDRAULIC MANIFOLD, AND OPERATIONALLY TESTED, BLED SYSTEM AND LEAK CHECKSDR C2XA03CL086Light · inoperativeDURING ROUTINE MAINTAINENCE EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE AT ROW/SEATS 6. MAINTENANCE INSPECTED AND REPLACED EMERGENCY LIGHT FLOOR STRIP. OPERATIONAL CHECKS GOODSDR C2XA03BT048Relay · inoperativeCO2573, CREW REPORTED THAT (E1/E2 FIRE EXTINGUISHER BOTTLE A IS INOPERATIVE). MAINTENANCE REMOVED AND REPLACED THE PRESSURE RELAY FOR ENGINE FIRE BOTTLE (A). OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR DXTA200300001Circuit Board · failedON APPROACH TO GSO, (LT TR AUTOSTOW) AMBER CAS MESSAGE ILLUMINATED AND THROTTLE ROLLED BACK TO IDLE.SDR UG8AG0243Control Module · malfunctionedSHORTLY AFTER TAKEOFF THE (RUDDER LIMIT FAIL) CAS MESSAGE ILLUMINATED. PERFORMED RUDDER CONTROL LIMITER TEST IAW MM. NO FAULTS DURING 3 HOURS OF TESTING. RESET RUDDER LIMIT CONTROL MODULE NK123. PERFORMED OPERATIONAL CHECK FLIGHT. NO PROBLEMS WERE ENCOUNTSDR DXTA200300004Circuit Board · failedUPON LANDING THE LT THRUST REVERSER DEPLOYED, BUT THE HANDLE WOULD NOT LET THRUST GO ABOVE IDLE.SDR UG8AG0342Flap Track · contaminatedAFTER SELECTING FLAPS UP, AMBER FLAPS FALL LIGHT CAME ON. UNABLE TO RESET. RETURN TO DTW. SLATS OK. ZERO FLAPS. ICE, WATER AND SAND FOUND IN THE LT AND RT INBOARD FLAP WELLS AND FLAP TRACKS. CAUSED FLAP MOTOR OVERCURRENT DURING FLAP ACTUATION.SDR CNQ2003F00000Hose · rupturedON CLIMB OUT, HYDRAULIC SYSTEM (A) LOST ALL FLUID. UPON INSPECTION THE HOSE THT RUNS FROM SYSTEM (A) PRESSURE FILTER TO POWER TRANSFER UNIT WAS NOTED TO BE REPTURED. THE HOLE WAS SENT TO TEAM (X) AT ICT.SDR SIMA200234506Sill · corrodedDURING AN IMBV INSPECTION THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED DAMAGED CENTER SILL AND REPLACED WITH SERVICEABLE SILL. REPAIR DONE IAW SRM.SDR C2XA02IA244Light · inoperativeDURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY AISLE PATH LIGHTS FORWARD STRIP FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY AISLE PATH LIGHT STRIP. PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVSDR C2XA02CL233Control Handle · intermittentTHE CREW REPORTED A LANDING GEAR LEVER DISAGREE DURING GEAR EXTENSION. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR C2XA02CL229Light · inoperativeTHE CREW REPORTED A FLOOR EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FLOOR EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.SDR SIMA200229403Display · lightning strikeCREW REPORTED A BRIGHT FLASH AT CAPTAINS WINDOW FOLLOWED BY AN ELECTRICAL SMOKE SMELL, LOSS OF NUMBER 4 GENERATOR. NUMBER 2 COMM, AND FMS SCREEN. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE COMPLIED WITH A LIGHTESDR UG82002F00011Display · malfunctionedAFTER TAXIING FROM RAMP, RETURNED TO PARKING RAMP WITH EICAS YELLOW CAUTION MESSAGE FOR THE NR 5 COCKPIT DISPLAY UNIT. MESSAGE CREATED IN WRAP AROUND CIRCUIT BETWEEN THE NR 1 AND NR 5 DISPLAY UNITS. CYCLED AVIONICS MASTER SWITCH OFF THEN BACK ON. SYSTEM OPESDR DXT2002F00004Manifold · inoperativeAFTER 1.5 HOURS AT FL430, WHILE DESCENDING THROUGH FL180 AT 240 KNOTS, THE CREW HEARD A LOUD RUSHING NOISE FROM FRONT OF THE AIRCRAFT AND THE NOSE GEAR LIGHT CAME ON FOR 2 SECONDS. THE LIGHT THEN WENT OUT, THE NOISE STOPPED AND THE GEAR LOWERED NORMALLY IN TSDR SIMA200228217Floorbeam · corrodedDURING A IMBV INSPECTION LEFT HAND BEAM AT FRAME 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF DAMAGED BEAM. FABRICATED A FILLER, TWO SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM.SDR SIMA200228224Sill · corrodedDURING AN MBV INSPECTION, CORROSION WAS FOUND ON SERVICE DOOR CENTER SILL THAT WAS BEYOND SRM LIMITS. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE BLENDED AREAS. NO DEFECTS NOTED. FABRICATED THREE REPAIR DOUBLERS. REPAIR DONE IAW SRM.SDR SIMA200228207Floorbeam · corrodedDURING AN IMBV INSPECTION, CORROSION WAS FOUND ON THE GALLEY CENTER FLOORBEAM. REMOVED CORRODED GALLEY CENTER FLOORBEAM INSTALLED NEW BEAM IAW SRM.SDR SIMA200228220Floorbeam · corrodedDURING AN IMBV INSPECTION, THE DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED SECTION OF THE FORWARD DIGITAL BY CUT OUT. FABRICATED A REPLACEMENT STRAP AND TWO DOUBLERS, SHIMS. REPAIR DONE IAW SRM.SDR SIMA200228222Doubler · corrodedDURING AN IMBV INSPECTION CORROSION WAS FOUND ON A PREVIOUS REPAIR TO THE LEFT HAND OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND INSPECTION THE UNDERLYING BEAM. NO ADDITIONAL DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS, PLATE. REPASDR SIMA200228208Stringer · chafedDURING AN IMBV INSPECTION FOUND STRINGER 19L CHAFED. BLENDED CHAFE. PERFORMED AND NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIR DONE IAW SRM.SDR SIMA200228223Floorbeam · corrodedDURING AN IMBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM AT FRAME 29. REMOVED CORROSION BY CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS. REPAIR DONE IAW SRM.SDR SIMA200228216Floorbeam · corrodedDURING AN IMBV INSPECTION THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 23. BLENDED THE DAMAGED AREA TO COMPLETELY REMOVED THE CORROSION. FABRICATED A U SHAPED DOUBLER. REPAIR DONE IAW SRM.SDR SIM2002F00000Frame · crackedDURING AN INSPECTION OF AN EXISTING REPAIR TO FRAME 73 AT STRINGER 15L ADDITIONAL DAMAGE IN THE FORM OF A .75 INCH LONG CRACK, WAS FOUND. REMOVED THE EXISTING REPAIR PERFORMED AN EDDY CURRENT INSPECTION TO CONFIRM CRACK ENDED AT A RIVET HOLE. FABRICATED AN LSDR SIMA200228226Sill · corrodedDURING AN IMBV INSPECTION OF AIRCRAFT, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL. INSTALLED SERVICEABLE SILL IAW SRM.SDR SIMA200228218Frame · chafedDURING A IMBV INSPECTION FOUND LOWER FRAME 81 CHAFED BEYOND SRM LIMITS. REMOVED EXISTING LOWER FRAME 81. INSTALLED NEW FRAME IAW SRM.
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