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.
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
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 CHQA201100219Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FRAME BAGGAGE DOOR SHEAR CLIP. MAINTENANCE REPLACED THE LOWER FRAME BAGGAGE DOOR SHEAR CLIP WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100221Servo · inoperativeCREW REPORTED THAT DURING CLIMB, AT 22,000 FEET, LOST AILERON CONTROL AND THE CONTROL WAS LOCKED. WITH EXCESSIVE FORCE, THE CREW FREED THE AILERON CONTROL. THE CREW RETURNED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AILERON SERVO MOTOR. SDR CHQA201100231Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE LEFT GUSSET 1. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE LEFT GUSSET 1 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100232Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE LEFT OUTBOARD SEAT TRACK 1. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE LEFT OUTBOARD SEAT TRACK 1 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100233Channel · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE SERVICE DOOR CHANNEL. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE SERVICE DOOR CHANNEL WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100234Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT TRACK 3. MAINTENANCE REPLACED THE RIGHT OUTBOARD SEAT TRACK 3 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100235Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT TRACK 4. MAINTENANCE REPLACED THE RIGHT OUTBOARD SEAT TRACK 4 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100236Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK 4. MAINTENANCE REPLACED THE LEFT OUTBOARD SEAT TRACK 4 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100237Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK 5. MAINTENANCE REPLACED THE LEFT OUTBOARD SEAT TRACK 5 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100239Tee Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE ENTRANCE AREA FORWARD AND AFT "T" FITTING. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE ENTRANCE AREA FORWARD AND AFT "T" FITTING WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100240Plate · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE ENTRANCE AREA FORWARD SIDE PLATE. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE ENTRANCE AREA FORWARD SIDE PLATE WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100241Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE ENTRANCE AREA FORWARD SIDE PLATE ANGLE. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE ENTRANCE AREA FORWARD SIDE PLATE ANGLE WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100242Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE LEFT OMEGA BEAM FLANGE ANGLE AT FRAME 20. MAINTENANCE REPAIRED THE CABIN FLOOR STRUCTURE LEFT OMEGA BEAM FLANGE ANGLE AT FRAME 20 IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA201100243Strap · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE LEFT AND RIGHT WING BOX STRAP BETWEEN FRAMES 49 AND 50. MAINTENANCE PERFORMED A THICKNESS MEASUREMENT BY ULTRASOUND INSPECTION ON REWORKED AREAS PER NDI MANUAL INTRO P.22-F MINIMUM MATERIAL RESDR CHQA201100238Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE ENTRANCE AREA LOWER BEAM. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE ENTRANCE AREA LOWER BEAM WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100220Light · inoperativeCREW REPORTED THAT WHILE AT THE GATE THE EMERGENCY LIGHT FLOOR STRIP AT ROWS 7 AND 8 WAS INOPERATIVE. MAINTENANCE DEFERRED THE EMERGENCY LIGHT STRIP AT ROWS 7 AND 8. ORD MAINTENANCE REPLACED THE EMERGENCY LIGHT FLOOR STRIP AT ROW 7 AND 8. OPERATIONAL CHECKSSDR CHQA201100217Brake Assy · wornCREW REPORTED THAT WHEN THE LANDING GEAR WAS SELECTED DOWN, RECEIVED A BRAKE DEGRADED MESSAGE ON THE EICAS. FURTHER REPORTED THAT WHEN THE BRAKES WERE APPLIED BRAKES FELT "SPONGY" ON THE LEFT SIDE AND THAT THE LEFT OUTBOARD BRAKE TEMPERATURE REMAINED COLD. MSDR CHQA201100211Duct · blownCREW REPORTED THAT DURING CLIMB RECEIVED A PACK 2 VALVE CLOSED MESSAGE. THE CREW RETURNED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BLOWN DUCT ON PACK 2 AND DEFERRED THE PACK 2 SYSTEM. OVERNIGHT MAINTENANCE REPLACED THE DUCT TO THE HEAT EXCHASDR CHQA201100210Duct · crackedCREW REPORTED THAT AFTER TAKEOFF, AT APPROXIMATELY 7,000FT, RECEIVED AN ENGINE 1 BLEED LEAK MESSAGE. FOLLOWED THE QUICK REFERENCE HANDBOOK AND ABOUT 2 MINUTES LATER THE MESSAGE WENT AWAY. THE CREW RETURNED TO KIAH AND LANDED WITHOUT INCIDENT. ON CALL MAINTESDR CHQA201100208Battery · dischargedDURING INSPECTION, THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100209O-Ring · wornCREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED A BLEED 1 LEAK MESSAGE ON THE EICAS. FOLLOWED THE QUICK REFERENCE HANDBOOK AND APPROXIMATELY ONE MINUTE LATER THE MESSAGE WENT AWAY. RETURNED TO KIAH AND LANDED WITHOUT INCIDENT. ON CALL MAINTENANCE SECURED THSDR CHQA201100206Valve · inoperativeCREW REPORTED THAT AFTER TAKEOFF RECEIVED A BLEED 1 OVERTEMP MESSAGE ON THE EICAS. DESELECTED THE NR 1 BLEED PER THE QUICK REFERENCE HANDBOOK AND TEMPERATURES RETURNED TO NORMAL. THE CREW RETURNED TO KMKE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THSDR CHQA201100207Battery · dischargedDURING INSPECTION, THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100203Unknown · malfunctionedCREW REPORTED THAT DURING CLIMB RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND THAT THE LANDING GEAR WOULD NOT RETRACT. THE CREW DIVERTED TO KLGA AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED ALL PROXIMITY SWITCHES AND ALL WERE TESTING GOOD. MAINTENSDR CHQA201100205Thermostat · inoperativeCREW REPORTED THAT AFTER TAKEOFF RECEIVED A BLEED 1 OVERHEAT MESSAGE ON THE EICAS. CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND RETURNED TO KMKE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FAN AIR VALVE THERMOSTAT. OPERATIONAL CHECKSSDR CHQA201100204Electronic Unit · failedCREW REPORTED THAT DURING CLIMB RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS. THE CREW RETURNED TO KLGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPORTED, CMC MESSAGE FOR LGEU FAIL. REPLACED THE LGEU AND PERFORMED LANDING GEAR SWINGS. OPERASDR CHQA201100199Warning System · false activationFLIGHT CREW REPORTED THAT WHILE CLIMBING THROUGH 9,000FT, THE HAD A BLEED 1 LEAK MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT THEN RETURNED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN OPS CHECK OF THE SDR CHQA201100200Floor Support · damagedDURING INSPECTION THE CENTER FUSELAGE III OMEGA BEAM WAS FOUND TO BE DAMAGED. THE OMEGA BEAM WAS REPAIRED IAW SRM 53-23-02-RE AND EMBRAER ETD 2011-145-100373.SDR CHQA201100201Shear Plate · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FRAMES BAGGAGE DOOR SHEAR CLIP. THE DAMAGED AREA OF THE SHEAR CLIP WAS REMOVED AND A NEW SECTION WAS INSTALLED.SDR CHQA201100198Unknown · odorDURING CRUISE AT FL350 THE CAPTAIN AND FIRST OFFICER NOTICED AN ACRID SMELL. THE FLIGHT ATTENDANT WAS ASKED ABOUT THE ODOR AND REPORTED SMELLING IT AS WELL. SHORTLY AFTER, THE CAPTAIN REPORTED SEEING A LIGHT STREAM OF SMOKE COMING FROM THE CAPTAIN'S WINDOW HSDR CHQA201100195Proximity Switch · intermittentDURING CLIMB, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE. THE QRH WAS FOLLOWED, AND MAINTENANCE CONTROL CONTACTED TO DISCUSS THE ISSUE. IT WAS THEN DECIDED TO DIVERT TO KCMH. THE CREW DECLARED AN EMERGENCY. THE LANDING GEAR WAS LOWERED NORMALSDR CHQA201100196Light · inoperativeDURING INSPECTION, THE COCKPIT STEP EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. THE COCKPIT STEP EMERGENCY EXIT SIGN WAS REPLACED WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100197Light · inoperativeDURING INSPECTION, THE RIGHT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED.SDR CHQA201100213Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE LEFT OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA201100214Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE MID OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA201100215Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE RIGHT OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA201100194Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FRAME 65, BETWEEN STRINGERS 15L AND 17L. THREE AREAS WERE FOUND WITH THE DEEPEST DAMAGE BEING 0.022" DEEP. THE DAMAGE WAS BLENDED OUT, AND A 0.051" DOUBLER INSTALLED PER EMBRAER ETD 2011-145-100340 WITH NO FURTHER DESDR CHQA201100202Skin · damagedDURING INSPECTION, A PREVIOUS BLEND ON THE RIGHT CENTER FUSELAGE SKIN, SECTION I BETWEEN FRAME 16-17 AND STRINGER 19R-20R, WAS FOUND TO BE OUT OF LIMITS. THE DAMAGE WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-01.SDR CHQA201100193Switch · intermittentCREW REPORTED AN ELECTRICAL ABNORMAL AND EMERGENCY LIGHTS NOT ARMED MESSAGE ON EICAS DURING FLIGHT. THE CREW DIVERTED TO KIND WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE EIC ESSENTIAL INTERCONNECTION CONTACTOR, AND DURING OPERATIONALSDR CHQA201100192Ballast · burnedCREW REPORTED THAT DURING FLIGHT THERE WAS A STRONG BURNING SMELL FROM ROWS 6, 7, 8. MAINTENANCE FOUND THE SIDEWALL LIGHTING BALLAST AT ROW 7 TO BE BURNT. MAINTENANCE REPLACED THE ROW 7 LIGHTING BALLAST AND THE PASSENGER SERVICE UNIT. OPERATIONAL CHECKS WERSDR CHQA201100189Brake Sys · contaminatedCREW REPORTED THAT DURING TAXI RECEIVED A BRAKE DEGRADED MESSAGE ON THE EICAS AND NOTED THAT THE BRAKES FELT SPONGY AND UNRESPONSIVE. THE CREW RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE FOUND AIR IN THE BRAKE SYSTEM AND BLED ALL FOUR BRAKES. OPERATISDR CHQA201100190Solenoid Valve · inoperativeCREW REPORTED THAT DURING CLIMB THAT THE NOSE GEAR DOORS WERE NOT CLOSED. AT 10,000 FEET THE NOSE GEAR DOORS CLOSED AND EVERYTHING REMAINED NORMAL FOR THE REST OF THE FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR DSDR CHQA201100191Proximity Switch · faultyCREW REPORTED THAT AFTER TAKEOFF THE NOSE LANDING GEAR DOORS DID NOT CLOSE UNTIL 9000 FEET. ALL LANDING GEAR INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR SEQUENCE PROXIMITY SWITCH AND RELAY K0642.SDR CHQA201100187Wire Harness · intermittentCREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON TAKEOFF AND REPORTED THE LANDING GEAR LEVER WAS STUCK IN THE DOWN POSITION. CREW NOTED THAT ALL LANDING GEAR INDICATIONS WERE NORMAL. RETURNED TO KORD AND LANDED WITHOUT INCIDENT. MAINTENANCESDR CHQA201100188Anti-Ice Valve · inoperativeCREW REPORTED THAT DURING FLIGHT RECEIVED AN ENGINE 2 ANTI-ICE VALVE FAIL MESSAGE AND A WING ANTI-ICE FAIL MESSAGE ON THE EICAS. THE CREW DIVERTED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH THE ENGINE 2 ANTI-ICE VALVE AND THE RIGHT WING ASDR CHQA201100185Switch · inoperativeCREW REPORTED THAT THERE WAS A LOUD NOISE COMING FROM THE NOSE LANDING GEAR DURING FLIGHT AND BELIEVED THAT THE LANDING GEAR DOORS DID NOT FULLY CLOSE. ALL OF THE GEAR INDICATIONS WERE GOOD. THE CREW SLOWED THE AIRCRAFT, CYCLED THE LANDING GEAR, AND THE NOISSDR CHQA201100186Switch · defectiveCREW REPORTED, HEARD A LOUD NOISE THE ENTIRE FLIGHT AND BELIEVED THAT THE NOSE LANDING GEAR DOOR DID NOT CLOSE. THE CREW INSPECTED THE AIRCRAFT AND NOTED THAT ALL OF THE PANELS WERE CLOSED. THE CREW ALSO NOTED THAT ALL GEAR INDICATIONS WERE NORMAL. THE AIRCSDR CHQA201100216Skin · dentedDURING INSPECTION THE LOWER CONTROL SURFACE OF THE LEFT ELEVATOR WAS FOUND TO BE DENTED APPROXIMATELY AT YH-1280.00. THE DENT WAS REPAIRED IN ACCORDANCE WITH ETD2011-145/100372 REV A.SDR CHQA201100182Inverter · inoperativeDURING INSPECTION, THE UPPER AFT ILLUMINATED PLACARD FOR THE RIGHT OVERWING ESCAPE HATCH WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 5 DC TO AC INVERTER. OPERATIONAL CHECKS OF THE UPPER AFT ILLUMINATED PLACARD FOR THE RIGHT OVERWING ESCAPE HATCHSDR CHQA201100183Hydraulic Line · leakingCREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE CREW STATED THAT ALL THREE GEARS HAD RED X'S ON THE EICAS. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CYCLED THE LANDING GEAR. AFTER A MOVEMENT ALL THREE GEARS, THE GEARS SHOWE
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