Allison AE-3007A

Service difficulty reports · 3,309

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 = 'AE3007A'
  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 CHQA20120725225Unknown · odorCREW REPORTED A BURNING ODOR DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE ISOLATED THE BURNING ODOR TO COOLING PACK 1. MAINTENANCE COULD NOT DUPLICATE THE BURNING ODOR AND OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 25, 2012 · N258JQ · Emb EMB145LR · Air Distribution SystemSDR CHQA20120723250Dome · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE BACK SIDE OF THE LAVATORY SERVICE PAN AND SUPPORT ANGLES. MAINTENANCE REPLACED THE LAVATORY DOME IN ACCORDANCE WITH SRM 51-40-02.Jul 23, 2012 · N291SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120722233Shear Plate · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE CARGO DOOR CUTOUT FORWARD AND AFT LOWER CORNERS. MAINTENANCE REPLACED THE FRAME 65 AND FRAME 68 SHEAR FOOTS IN ACCORDANCE WITH ETD 2012-145-010345 REVISION A.Jul 22, 2012 · N291SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120722234Shear Plate · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE CARGO DOOR CUTOUT FORWARD AND AFT LOWER CORNERS. MAINTENANCE REPLACED THE FRAME 65 AND FRAME 68 SHEAR FOOTS IN ACCORDANCE WITH ETD 2012-145-010345 REVISION A.Jul 22, 2012 · N291SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120722237Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND AT FRAME 22 TO FRAME 23 ON THE RIGHT CABIN FLOOR BEAM SILL. MAINTENANCE REPLACED THE RIGHT CABIN FLOOR BEAM SILL IN ACCORDANCE WITH SRM 51-40-02 AND ETD 2012-145-010607.Jul 22, 2012 · N291SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120722238Stiffener · corrodedDURING INSPECTION, CORROSION WAS FOUND AT FRAME 22 TO FRAME 23 ON THE RIGHT CABIN FLOORBEAM SILL. MAINTENANCE REPLACED THE SERVICE DOOR STIFFENER IN ACCORDANCE WITH ETD 2012-145-010607.Jul 22, 2012 · N291SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120720243Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE CARGO DOOR CUTOUT FRAME 65. MAINTENANCE REPAIRED THE CARGO DOOR CUTOUT FRAME 65 IN ACCORDANCE WITH ETD 2012-145-010345 REVISION A.Jul 20, 2012 · N291SK · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20120713212Light · inoperativeDURING INSPECTION, THE LEFT FORWARD FUSELAGE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT FORWARD FUSELAGE EMERGENCY LIGHT ASSEMBLY. OPS CHECKED GOOD, WITH NO FURTHER DEFECTS NOTED.Jul 13, 2012 · N257JQ · Emb EMB145LR · Emergency LightingSDR CHQA20120713224Stop Fitting · damagedDURING INSPECTION, AN ELONGATED SCREW HOLE WAS FOUND ON THE DOOR STOP NR 2 ON THE PASSENGER DOOR. THE HOLE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-010068.Jul 13, 2012 · N571RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20120712211Strut · leakingCREW REPORTED THAT AFTER TAKEOFF, LANDING GEAR LEVER WOULD NOT MOVE AND THAT THEY RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR LEG ASSEMBLY. OPS CHECKED GOOD, WITH Jul 12, 2012 · N564RP · Emb EMB145LR · Nose/Tail Landing Gear Strut/AxleSDR CHQA20120711210Connector · disconnectedCREW REPORTED THAT AFTER TAKEOFF, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SECURED NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH ELECTRICAL CONNECTOR. OPS CHECKED LANDING GEAR EXTENSIJul 11, 2012 · N573RP · Emb EMB145LR · Landing Gear System WiringSDR CHQA20120710207Sensor · faultyCREW REPORTED THAT THEY RECEIVED A TAT 1 HEAT FAIL MESSAGE AFTER TAKEOFF. DUE TO WEATHER RESTRICTIONS, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 TAT 1 HEAT SENSOR. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTEDJul 10, 2012 · N374SK · Emb EMB135KL · Outside Air Temperature Indicator/SensorSDR CHQA20120709206Transducer · faultyCREW REPORTED THAT ON LANDING ROLL OUT BRAKING WAS NORMAL, BUT AFTER SEVERAL SECONDS BRAKING EFFECTIVENESS BECAME DECREASED. MAINTENANCE REPLACED THE NR 2 WHEEL SPEED TRANSDUCER DUE TO CMC MESSAGING. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 9, 2012 · N382SK · Emb EMB135KL · Landing Gear Brake SystemSDR CHQA20120707205Electronic Unit · faultyCREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND MULTIPLE AURAL WARNINGS REGARDING THE FLAPS AND TRIM AFTER TAKEOFF. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS Jul 7, 2012 · N378SK · Emb EMB135KL · Landing Gear System WiringSDR CHQA20120705204Light · inoperativeDURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jul 5, 2012 · N281SK · Emb EMB145LR · Emergency LightingSDR CHQA20120705214Skin · damagedDURING INSPECTION, RUDDER II DEFLECTION TOOL NUT PLATE WAS MISSING AND A RIVET HOLE WAS ELONGATES IN THE SKIN OF THE RUDDER. MAINTENANCE REPLACED THE DAMAGED SECTION OF THE RUDDER SKIN IN ACCORDANCE WITH ETD 2012-145-009625.Jul 5, 2012 · N289SK · Emb EMB145LR · Rudder, Plate/SkinSDR CHQA20120705215Shear Tie · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR TIE AT FRAME 65 AND THE CARGO DOOR THRESHOLD. MAINTENANCE REPLACED THE DAMAGED SECTION IN ACCORDANCE WITH ETD 2012-145-009622.Jul 5, 2012 · N289SK · Emb EMB145LR · Fuselage Internal Mounting StructureSDR CHQA20120705216Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE CARGO DOOR THRESHOLD. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED IAW NIM INTRO ITEM E, WITH NO CRACK LIKE INDICATIONS FOUND. REPAIRED IAW ETD 2012-145-009560 REVISION A.Jul 5, 2012 · N289SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120705217Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FORWARD OMEGA BEAM AT FRAME 20. MAINTENANCE REPLACED THE OMEGA BEAM AT Y=0.0 IAW SRM 53-21-04.Jul 5, 2012 · N289SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120703222Skin · damagedDURING INSPECTION, THE RIGHT AFT FUSELAGE SKIN WAS FOUND TO BE DAMAGED AT FRAME 80 AND STRINGER 9L. THE RIGHT AFT FUSELAGE SKIN AT FRAME 80 AND STRINGER 9L WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-009769.Jul 3, 2012 · N290SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120703223Skin · damagedDURING INSPECTION, THREE CREASES WERE FOUND ON CENTER FUSELAGE, BETWEEN FRAME 19 AND FRAME 20 AND STRINGERS 1L AND 2L. THE CREASES ON CENTER FUSELAGE, BETWEEN FRAME 19 AND FRAME 20 AND STRINGERS 1L AND 2L WERE REPAIRED IN ACCORDANCE WITH ETD 2012-145-010111 REJul 3, 2012 · N290SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120702213Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE OMEGA BEAM Y=479.0 AT FRAME 20. REPAIR DOUBLER FABRICATED AND INSTALLED IAW SRM 51-20-03 AND 51-40-02.Jul 2, 2012 · N289SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120702218Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE DOOR SILL FRAME 65-68. MAINTENANCE REPLACED THE CARGO DOOR SILL THRESHOLD BEAM IN ACCORDANCE WITH SRM 51-40-02.Jul 2, 2012 · N289SK · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20120701219Battery · dischargedDURING INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT AND THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 1, 2012 · N289SK · Emb EMB145LR · Emergency LightingSDR CHQA20120701220Light · inoperativeDURING INSPECTION, RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT AND THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 1, 2012 · N289SK · Emb EMB145LR · Emergency LightingSDR CHQA20120701221Bulb · inoperativeDURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT BULB. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 1, 2012 · N289SK · Emb EMB145LR · Emergency LightingSDR CHQA20120628200Wire · brokenEMERGENCY LIGHT AT ROW 8 HAS BROKEN WIRES. REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jun 28, 2012 · N286SK · Emb EMB145LR · Light System WiringSDR CHQA20120628201O-Ring · leakingCREW REPORTED A BLEED 1 LEAK MESSAGE IN FLIGHT. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED O-RING AT JOINT 11. OPS AND LEAK CHECKED GOOD, WITH NO FURTHER DEFECTS NOTED.Jun 28, 2012 · N279SK · Emb EMB145LR · Engine Bleed Air SystemSDR CHQA20120628208Frame · damagedDURING INSPECTION, A HOLE WAS FOUND IN FRAME 65 ON THE RIGHT SIDE NEAR STRINGER 12R. MAINTENANCE INSTALLED A NEW REPAIR DOUBLER IN ACCORDANCE WITH ETD2012-145-009260.Jun 28, 2012 · N268SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120628209Support · corrodedDURING INSPECTION, THE AFT RIGHT FUSELAGE INSIDE ACCESS DOOR 272AR TOILET DRAIN VALVE SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE DISCHARGE CUP IN ACCORDANCE WITH SRM 51-40-02.Jun 28, 2012 · N268SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120624202Nut Plate · corrodedDURING INSPECTION, THE FORWARD NUT PLATE AT THE SERVICE DOOR THRESHOLD AFT OF FRAME 19 WAS FOUND TO BE CORRODED. THE CORROSION WAS REMOVED IN ACCORDANCE WITH SRM 51-10-03. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED WITH NO DEFECTS NOTED IN ACCORDJun 24, 2012 · N380SK · Emb EMB135KL · Fuselage Main, Attach FittingsSDR CHQA20120623203Frame · corrodedDURING INSPECTION, RIGHT FRAME 23 WAS FOUND TO BE CRACKED AT THE OUTBOARD EDGE AND BELOW THE FLOORBOARD. FRAME 23 WAS REPLACED IN ACCORDANCE WITH ETD 2012-145-008993.Jun 23, 2012 · N380SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA20120619195Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE OMEGA BEAM FRAME 60 AND 61 ON THE RIGHT SIDE. THE OMEGA BEAM BETWEEN FRAME 60 AND 61 ON THE RIGHT SIDE WAS REPLACED IN ACCORDANCE WITH ETD 2012-145-008765.Jun 19, 2012 · N576RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120617197Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE OMEGA BEAM AT Y=0.0 AT FRAME 20. THE OMEGA BEAM AT Y=0.0 AT FRAME 20 WAS REPLACED IN ACCORDANCE WITH SRM 51-20-03 AND SRM 51-40-02.Jun 17, 2012 · N576RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120615194Inverter · inoperativeDURING INSPECTION THE EMERGENCY LIGHTS OVER THE MAIN ENTRY DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER ONE INVERTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jun 15, 2012 · N281SK · Emb EMB145LR · Emergency LightingSDR CHQA20120614193O-Ring · leakingCREW REPORTED THAT DURING CLIMB RECEIVED A HYDRAULIC 2 LOW QUANTITY MESSAGE WITH THE FLUID LEVEL SLOWLY DECREASING. THE CREW DIVERTED TO KCLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT OUTBOARD SPOILER ACTUATOR FITTING O-RINGS. OPERATIONAL Jun 14, 2012 · N371SK · Emb EMB135KL · Drag Control ActuatorSDR CHQA20120614198Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON LEFT OMEGA BEAM FRAME 20 AT CROSS MEMBER. THE DOUBLER AT LEFT OMEGA BEAM FRAME 20 WAS REPLACED IN ACCORDANCE WITH SRM 35-00-10.Jun 14, 2012 · N576RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120614199Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE LEFT OMEGA BEAM AT CROSSMEMBER BETWEEN FRAMES 24 AND 25. THE SECTION WAS REPLACED IN ACCORDANCE WITH SRM 53-00-10.Jun 14, 2012 · N576RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120612191Light · inoperativeDURING INSPECTION, THE FORWARD OVERWING EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD OVERWING EMERGENCY LIGHT ASSEMBLY AND THE NR 1 EMERGENCY BATTERY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jun 12, 2012 · N577RP · Emb EMB145LR · Emergency LightingSDR CHQA20120612192Battery · dischargedDURING INSPECTION, THE FORWARD OVERWING EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD OVERWING EMERGENCY LIGHT ASSEMBLY AND THE NR 1 EMERGENCY BATTERY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jun 12, 2012 · N577RP · Emb EMB145LR · Emergency LightingSDR CHQA20120609184Flapper Valve · brokenCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED ONE LEAK MESSAGE. APPROXIMATELY ONE MINUTE LATER THE CABIN PRESSURIZATION WOULD NOT KEEP UP WITH THE CABIN ALTITUDE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE Y-DUJun 9, 2012 · N279SK · Emb EMB145LR · Cabin Pressure Control SystemSDR CHQA20120609185Sleeve · failedCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED ONE LEAK MESSAGE. APPROXIMATELY ONE MINUTE LATER THE CABIN PRESSURIZATION WOULD NOT KEEP UP WITH THE CABIN ALTITUDE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE Y-DUJun 9, 2012 · N279SK · Emb EMB145LR · Cabin Pressure Control SystemSDR CHQA20120609186Control Valve · malfunctionedCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED ONE LEAK MESSAGE. APPROXIMATELY ONE MINUTE LATER THE CABIN PRESSURIZATION WOULD NOT KEEP UP WITH THE CABIN ALTITUDE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE Y-DUJun 9, 2012 · N279SK · Emb EMB145LR · Cabin Pressure Control SystemSDR CHQA20120609187Battery Pack · dischargedDURING INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jun 9, 2012 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20120607190Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND AT A SCREW HOLE ON THE LOWER SERVICE DOOR CUT-OUT AT FRAME 22. FRAME 22 WAS REPAIRED IN ACCORDANCE WITH ETD2012-145-008241 REVISION A.Jun 8, 2012 · N566RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120609183Ballast · failedCREW REPORTED AN ELECTRICAL ODOR FROM THE CEILING LIGHT AT SEAT 1A. REMOVED AND REPLACED CEILING LIGHT BALLAST. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jun 8, 2012 · N272SK · Emb EMB145LR · Passenger Compartment LightingSDR CHQA20120607196Skin · dentedDURING INSPECTION, A DENT WAS FOUND IN THE FUSELAGE SKIN APPROXIMATELY SIX FEET FORWARD OF THE CARGO DOOR. THE DAMAGED AREA WAS CUT OUT AND REPLACED PER ETD 2012-145-008658.Jun 7, 2012 · N576RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120605180Transducer · disconnectedCREW REPORTED LOSS OF BRAKING EFFECTIVENESS ON LANDING ROLL. A BRAKE DEGRADED MESSAGE APPEARED AS WELL. AFTER PUSHING THE BRAKES TO THE FLOOR BRAKES BEGAN WORKING AGAIN. MAINTENANCE FOUND THE RIGHT OUTBOARD MAIN LANDING GEAR WHEEL SPEED TRANSDUCER NOT CONNEJun 5, 2012 · N268SK · Emb EMB145LR · BrakeSDR ASOA20120604051Engine · leakingCREW REPORTED SMOKE IN THE LAVATORY. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. ENGINE LEAKING, MX REPLACED THE NR 2 ENGINE. OPS CHECKED GOOD.Jun 4, 2012 · N14180 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR CHQA20120603179Light · inoperativeDURING INSPECTION, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jun 3, 2012 · N267SK · Emb EMB145LR · Emergency Lighting
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