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.

SDR CHQA20130815314Valve · leakingCREW REPORTED DURING CLIMB, FUEL REPORTED TO BE LEAKING FROM LEFT WING. VERIFIED VAPOR COMING FROM THE LT WING AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. MX REPLACED THE FUEL TANK VALVE AT THE LT WING RIB 19. OPS CHECKED GOOD WITH NO LEAKS NOTED.Aug 15, 2013 · N562RP · Emb EMB145LR · Fuel StorageSDR CHQA20130813309Battery · dischargedDURING INSPECTION, BOTH EMERGENCY LIGHT EXIT SIGNS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Aug 13, 2013 · N296SK · Emb EMB145LR · Emergency LightingSDR CHQA20130805313Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE BOTTOM OF THE PASSENGER DOOR FRAME. THE FRAME WAS REPLACED IAW SRM 51-20-03 AND 51-40-02.Aug 5, 2013 · N289SK · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20130803308Battery Pack · inoperativeDURING INSPECTION, THE LT AND RT EXTERNAL OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OP CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Aug 3, 2013 · N281SK · Emb EMB145LR · Emergency LightingSDR CHQA20130802300Smoke Detector · dirtyCREW REPORTED THAT THEY RECEIVED A BAGGAGE COMPARTMENT SMOKE WARNING MESSAGE IN FLIGHT. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MX CLEANED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Aug 2, 2013 · N288SK · Emb EMB145LR · Smoke DetectionSDR CHQA20130802301Smoke Detector · dirtyCREW REPORTED THAT THEY RECEIVED A BAGGAGE COMPARTMENT SMOKE WARNING MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MX CLEANED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Aug 2, 2013 · N288SK · Emb EMB145LR · Smoke DetectionSDR CHQA20130802306Light · inoperativeDURING INSPECTION, EMERGENCY LIGHT AT ROW EIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE LIGHT AND OPS CHECKED GOOD.Aug 2, 2013 · N288SK · Emb EMB145LR · Emergency LightingSDR CHQA20130802307Light · inoperativeDURING INSPECTION, THE LT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE LT HOUSING ASSY AND OPS CHECKED GOOD.Aug 2, 2013 · N574RP · Emb EMB145LR · Emergency LightingSDR CHQA20130802310Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIPS AT FRAME 65 BETWEEN STINGERS 7L AND 9L. MX REPLACED THE SHEAR CLIPS IAW SRM 51-40-02.Aug 2, 2013 · N289SK · Emb EMB145LR · Fuselage Internal Mounting StructureSDR CHQA20130802311Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIPS AT FRAME 65 BETWEEN STINGERS 7L AND 9L. MX REPLACED THE SHEAR CLIPS IAW SRM 51-40-02.Aug 2, 2013 · N289SK · Emb EMB145LR · Fuselage Internal Mounting StructureSDR CHQA20130802312Frame · bentDURING INSPECTION, FRAME 72 WAS BENT BETWEEN STRINGERS 14-15R. FRAME REPAIRED IAW SRM 53-00-04.Aug 2, 2013 · N289SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20130728196Flap System · malfunctionedDURING CRUISE, RECEIVED A FLAP FAIL MESSAGE. FOLLOWED QUICK REF HANDBOOK AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MX RESET THE FLAP SYS. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 28, 2013 · N271SK · Emb EMB145LR · Trailing Edge Flap Control SystemSDR CHQA20130728298Wire · looseCREW REPORTED THAT THEY RECEIVED A WINDSHIELD HEAT 2 FAIL MESSAGE IN FLIGHT ACCOMPANIED BY AN ELECTRICAL BURNING ODOR. LANDED WITHOUT INCIDENT. MX RESECURED A LOOSE WIRE ON THE NR 2 WINDSHIELD HEAT SENSOR AT THE TERMINAL STRIP. OPS CHECKED GOOD WITH NO FURTJul 28, 2013 · N259JQ · Emb EMB145LR · Ice/Rain Protection System WiringSDR CHQA20130728299Light · inoperativeDURING INSPECTION, THE EMERGENCY LIGHT STRIP AT THE FORWARD GALLEY WAS FOUND TO BE INOPERATIVE. MX REPLACED THE LIGHT STRIP. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.Jul 28, 2013 · N286SK · Emb EMB145LR · Emergency LightingSDR CHQA20130726191Wire Harness · faultyAFTER TAKEOFF, WHEN LANDING GEAR WAS SELECTED UP, RECEIVED A LANDING GEAR AIR-GROUND FAIL MESSAGE AND LANDING GEAR DID NOT RETRACT. FOLLOWED THE QUICK REF HANDBOOK AND DECLARED AN EMERGENCY. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. ACFT FOUND SAFE FOJul 26, 2013 · N574RP · Emb EMB145LR · Landing Gear System WiringSDR CHQA20130726192Proximity Switch · faultyAFTER TAKEOFF, WHEN LANDING GEAR WAS SELECTED UP, RECEIVED A LANDING GEAR AIR-GROUND FAIL MESSAGE AND THAT THE LANDING GEAR DID NOT RETRACT. FOLLOWED THE QUICK REF HANDBOOK AND DECLARED AN EMERGENCY. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. ACFT FOUNJul 26, 2013 · N574RP · Emb EMB145LR · Landing Gear Position and WarningSDR CHQA20130726194Velocity Sensor · faultyDURING FLIGHT, RECEIVED A FLAP LOW SPEED MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FLAP ELECTRONIC CONTROL UNIT AND LT VELOCITY SENSOR WERE REPLACED. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 26, 2013 · N271SK · Emb EMB145LR · Trailing Edge Flap Control SystemSDR CHQA20130726195Control Unit · failedDURING FLIGHT, RECEIVED A FLAP LOW SPEED MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FLAP ELECTRONIC CONTROL UNIT AND LT VELOCITY SENSOR REPLACED. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 26, 2013 · N271SK · Emb EMB145LR · Trailing Edge Flap Control SystemSDR ASOA20130725079Unknown · odorF/A REPORTED THERE WAS AN OIL SMOKE ODOR THROUGHOUT THE CABIN DURING THE LAST FEW MINUTES OF THE FLIGHT. MX RAN NR 2 ENGINE WITH BLEED & PACKS ON AND NO ODOR NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 25, 2013 · N15574 · Emb EMB145LR · Air Distribution SystemSDR CHQA20130725189Inverter · inoperativeDURING INSPECTION, THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 3 INVERTER. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jul 25, 2013 · N268SK · Emb EMB145LR · Emergency LightingSDR CHQA20130725190Inverter · inoperativeDURING INSPECTION, THE AISLE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 2 INVERTER. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 25, 2013 · N268SK · Emb EMB145LR · Emergency LightingSDR ASOA20130724078Unknown · odorPILOT REPORTED A STRONG ODOR OF PLASTIC/ELECTRICAL SMOKE INFLIGHT DURING DESCENT WITH THE TOP OF GLARESHIELD/AVIONICS PANEL EXTREMELY HOT TO THE TOUCH. MX INSPECTED CABIN AND COCKPIT FOR PLASTIC/ELECTRICAL ODOR WITH NONE FOUND OR NOTED. ALSO RAN BOTH ENGINESJul 24, 2013 · N11565 · Emb EMB145LR · Air Distribution SystemSDR CHQA20130724186Unknown · unknownCREW REPORTED AN ABNORMALLY LOUD NOISE FROM THE NOSE AREA OF THE ACFT AFTER GEAR RETRACTION. NOISE PRESENT FOR REMAINDER OF FLIGHT. ALL 3 LANDING GEAR SHOWED UP AND LOCKED AND LOWERED AS NORMAL DURING GEAR EXTENSION. LANDED WITHOUT INCIDENT. MX INSPECTED THEJul 24, 2013 · N564RP · Emb EMB145LR · Standard Practices/StructuresSDR CHQA20130724187Control Lever · inoperativeCREW REPORTED THAT AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT AND THAT THE LANDING GEAR HANDLE WAS STUCK IN DOWN POSITION. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. THE ACFT WAS FOUND SAFE FOR FERRY FLIGHT. SDF MX REPLACED THE LANDING CJul 24, 2013 · N564RP · Emb EMB145LR · Landing Gear SelectorSDR CHQA20130724188Wire · damagedMX REPORTED THAT THE MAIN ENTRY DOOR HANDRAIL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPAIRED WIRE W737-0034-20. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 24, 2013 · N272SK · Emb EMB145LR · Light System WiringSDR CHQA20130723302Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 59. THE BEAM WAS REPAIRED IAW ETD-2013-145-021249.Jul 23, 2013 · N269SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130721282Valve · faultyCREW RECEIVED A NR 2 BLEED LOW TEMPERATURE MESSAGE DURING ICING CONDITIONS IN FLIGHT. DIVERTED AND LANDED WITHOUT INCIDENT. MX REPLACED NR 2 HIGH STAGE VALVE. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 21, 2013 · N575RP · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20130720280Control Valve · leakingRECEIVED A NR 2 A/C PACK VALVE CLOSED MESSAGE. FOLLOWED QUICK REF HANDBOOK AND DESCENDED TO 10,000 FT. ELECTED TO RETURN TO FIELD AND LANDED WITHOUT INCIDENT. BLEED AIR DUCT AND DUAL TEMP CONTROL VALVE REPLACED. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTEJul 20, 2013 · N291SK · Emb EMB145LR · Cabin Cooling SystemSDR CHQA20130720281Duct · leakingNR 1 COOLING PACK ON DEFERRAL, RECEIVED A NR 2 PACK VALVE CLOSED MESSAGE. FOLLOWED QUICK REFERENCE HANDBOOK AND DESCENDED TO 10,000 FT. ELECTED TO RETURN TO FIELD AND LANDED WITHOUT INCIDENT. BLEED AIR DUCT AND THE DUAL TEMPERATURE CONTROL VALVE WERE REPLAJul 20, 2013 · N291SK · Emb EMB145LR · Air Distribution SystemSDR CHQA20130719304Threshold · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR THRESHOLD BENEATH THE FLOOR PANEL 271FF. THRESHOLD REPAIRED IAW SRM 51-40-02.Jul 19, 2013 · N566RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130719305Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT LOWER BEAM. THE THRESHOLD PLATE WAS REPAIRED IAW SRM 53-40-02.Jul 19, 2013 · N566RP · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20130719279Overheat Sensor · failedAFTER TAKEOFF, A BRAKE OVERHEAT MESSAGE APPEARED. FOLLOWED QUICK REF HANDBOOK AND LOWERED LANDING GEAR. MESSAGE CLEARED BUT RT INBD BRAKE STAYED IN THE AMBER TEMPERATURE RANGE. ELECTED TO RETURN TO FIELD AND LANDED WITHOUT INCIDENT. INSPECTED LANDING GEAR Jul 19, 2013 · N370SK · Emb EMB145LR · Landing Gear Brake SystemSDR CHQA20130717278Battery Pack · inoperativeDURING INSPECTION, EMEREGENCY EXIT LIGHTS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 3 BATTERY PACK. OPS CHECKED GOOD.Jul 17, 2013 · N578RP · Emb EMB145LR · Emergency LightingSDR CHQA20130717303Frame · damagedDURING INSPECTION, A DAMAGED NUTPLATE ON FRAME 69 ON THE RT SIDE BETWEEN STRINGERS 13R AND 14R WAS FOUND. THE DAMAGED AREA WAS REPAIRED IAW ETD 2013-145-018588 A.Jul 17, 2013 · N269SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20130715273Bleed Valve · inoperativeCREW REPORTED A BLEED 2 SYSTEM FAIL MESSAGE IN FLIGHT, DIVERTED TO AN ALTERNATE FIELD, AND LANDED WITHOUT INCIDENT. MX REPLACED THE PRESSURE REDUCING SHUTOFF VALVE, OPS CHECKED GOOD.Jul 15, 2013 · N278SK · Emb EMB145LR · Compressor Bleed ValveSDR CHQA20130714272Valve · leakingCREW REPORTED THAT THEY RECEIVED A BLEED 2 LEAK MESSAGE DURING CLIMB. THE CREW UTILIZED THE QUICK REF HANDBOOK AND THE ISSUE DID NOT RESOLVE. THE CREW DIVERTED AND LANDED WITHOUT INCIDENT. MX REPLACED THE BLEED 2 VALVE. OPS CHECKS WERE GOOD WITH NO FURTHER DJul 14, 2013 · N574RP · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20130713271Uplock · inoperativeCREW REPORTED A THUMPING NOISE DURING GEAR RETRACTION ON CLIMB OUT, RETURNED TO THE FIELD, AND LANDED WITHOUT INCIDENT. MX REPLACED THE NLG UPLOCK BOX AFTER WHICH ALL OPS CHECKS AND TEST FLIGHT WERE SATISFACTORY.Jul 13, 2013 · N259JQ · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR CHQA20130712270Radar · malfunctionedCREW REPORTED THAT DURING FLIGHT, WEATHER RADAR BEGAN MALFUNCTIONING. DUE TO WEATHER CONDITIONS ALONG FLIGHT ROUTE, ELECTED TO RETURN TO FIELD. LANDED WITHOUT INCIDENT. MX COULD NOT DUPLICATE MALFUNCTION AND PERFORMED SUCCESSFUL OPS CHECK OF WEATHER RADARJul 12, 2013 · N562RP · Emb EMB145LR · Weather Radar SystemSDR CHQA20130709262Control Module · faultyRECEIVED A BAGGAGE EXTINGUISHING BOTTLE INOPERATIVE MESSAGE DURING CRUISE. MESSAGE CLEARED ON ITS OWN AND THE F/A REPORTED THAT THERE WAS NO INDICATION OF SMOKE OR FIRE IN THE BAGGAGE AREA. DURING DESCENT BAGGAGE EXTINGUISHING LIGHT CAME ON WITH NO OTHER MESSJul 9, 2013 · N566RP · Emb EMB145LR · Extinguishing SystemSDR CHQA20130709265Wire · brokenDURING INSPECTION, EMERGENCY LIGHT AT ROW 7 FOUND TO HAVE A BROKEN WIRE. WIRE REPAIRED. OPS CHECKED GOOD, WITH NO FURTHER DEFECTS NOTED.Jul 9, 2013 · N279SK · Emb EMB145LR · Light System WiringSDR CHQA20130708261Control Valve · faultyCREW REPORTED THAT ON GEAR EXTENSION, RECEIVED A BRAKE DEGRADED MESSAGE ON THE EICAS DISPLAY. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX REPLACED THE RT BRAKE CONTROL VALVE. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jul 8, 2013 · N572RP · Emb EMB145LR · Landing Gear Brake SystemSDR CHQA20130708274Stringer · corrodedDURING INSPECTION, STRINGER 21R FROM FRAME 7 TO FRAME 13 WAS FOUND TO BE CORRODED. THE STRINGER WAS REPLACED IAW SRM 51-40-02.Jul 8, 2013 · N567RP · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR CHQA20130707276Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE OMEGA BEAM UNDER DIGITAL AT Y=0.0 AT FRAMES 18, 20, AND 23. THE BEAM WAS REPAIRED IAW ETD 2013-145-014355.Jul 7, 2013 · N567RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130707277Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE AILERON DISCONNECT, RT QUADRANT SUPPORT WEB FRAME 13-14. THE SUPPORT WAS REPLACED IAW SRM 51-40-02.Jul 7, 2013 · N567RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130706260Wire Harness · inoperativeDURING INSPECTION, EMERGENCY LIGHT ON MAIN ENTRY DOOR HANDRAIL WAS FOUND TO BE INOPERATIVE. MX REPLACED THE CAUTION INDICATION HARNESS OPS CHECKED GOOD.Jul 6, 2013 · N276SK · Emb EMB145LR · Light System WiringSDR CHQA20130705256Inverter · inoperativeDURING INSPECTION, EMERGENCY LIGHT ABOVE F/A SEAT FOUND TO BE INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.Jul 5, 2013 · N286SK · Emb EMB145LR · Emergency LightingSDR CHQA20130705257Inverter · inoperativeDURING INSPECTION, RT EMERGENCY EXIT SIGN FOUND TO BE INOPERATIVE. MX FOUND NR 5 INVERTER TO INOPERATIVE AND REPLACED IT, OPS CHECKED GOOD.Jul 5, 2013 · N282SK · Emb EMB145LR · Emergency LightingSDR CHQA20130705258Inverter · inoperativeDURING INSPECTION, THE EMERGENCY EXIT SIGN ON THE AFT WALL OF THE GALLEY WAS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 3 INVERTER, OPS CHECKED GOOD.Jul 5, 2013 · N257JQ · Emb EMB145LR · Emergency LightingSDR CHQA20130705259Inverter · inoperativeDURING INSPECTION, RT EMERGENCY EXIT SIGN FOUND TO BE INOPERATIVE. MX FOUND NR 5 INVERTER TO INOPERATIVE AND REPLACED IT, OPS CHECKED GOOD.Jul 5, 2013 · N257JG · Emb EMB145LR · Emergency LightingSDR CHQA20130705269Fastener · misinstalledDURING HEAVY MX 1 FASTENER ON THE THE LT WING AT THE TORQUE BOX EXCEEDS CLASS 3 FIT TOLERANCE. THE FASTENER WAS REPAIRED IAW ETD 2013-145-014014.Jul 5, 2013 · N259JQ · Emb EMB145LR · Wing Main, Frame Structure
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