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 CHQA201000015Transceiver · faultyCREW REPORTED THAT AFTER TAKEOFF TRANSPONDERS 1 AND 2 WERE INOP WITH NO TCAS INFORMATION. ATC RECEIVERS HAD PRIMARY RADAR TARGET ONLY AND NO ALTITUDE INFORMATION. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 COMMSDR CHQA201000016Bleed Valve · inoperativeCREW REPORTED A BLEED 1 VALVE FAIL MSG WITH ASSOCIATED BLEED 1 VALVE CLOSED MESSAGE AND WERE UNABLE TO RESET. DUE TO ICING CONDITIONS AT DESTINATION, THE AIRCRAFT DIVERTED TO CMH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 BLEED VALVE IAWSDR CHQA201000014Unknown · odorCREW REPORTED THAT DURING DESCENT, NOTICED AN OIL LIKE SMELL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE ENGINES IAW ROLLS ROYCE AE3007 FIM 72-00-00-810-814 AND WERE UNABLE TO DUPLICATE THE FAULT WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000012Windshield · crackedCREW REPORTED THAT DURING CLIMBOUT, THE OUTER PANE OF THE FIRST OFFICER'S WINDSHIELD SHATTERED. THE AIRCRAFT RETURNED TO SDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000013Electronic Unit · faultyAFTER TAKEOFF FROM EWR, THE LANDING GEAR WOULD NOT RETRACT AND CREW RECEIVED AN LG AIR/GND FAIL MESSAGE ON EICAS. THE AIRCRAFT DIVERTED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LGEU DUE TO LGEU FAIL MESSAGE ON CMC. THE AIRCRAFT WAS THEN SDR V0XR201001190003Sill · corrodedRT SILL FROM FRM 48 - 52 CORRODED BEYOND LIMITS AT FRM 50. REMOVED AND REPLACED SILL.SDR V0XR201001190004Sill · corrodedFLOOR SILL AT LT Y.739 FROM FRM 59 - 61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL.SDR V0XR201001190005Seat Track · corrodedSEAT TRACK YL 479.0 BETWEEN FRM 30 - 35 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK.SDR V0XR2010011900005Seat Track · corrodedSEAT TRACK Y 0.0 BETWEEN FRM 30-35 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK.SDR V0XR2010011900006Seat Track · corrodedSEAT TRACK Y0.0 BETWEEN FRM 24-30 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK.SDR V0XR2010011900008Profile · corrodedSHORT PROFILE IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED PROFILE. W/C 1081SDR V0XR2010011900009Floor Support · corrodedPROFILE ANGLE ON LT OMEGA BEAM AT FRM 20 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED ANGLE.SDR V0XR2010011900010Floor Support · corrodedLT CENTRAL FUSELAGE IV OMEGA BEAM FROM FRM 58-62 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LT OMEGA BEAM.SDR V0XR2010011900012Gusset · corrodedGUSSET THAT SPANS OVER THE CTR BEAM TO LT BEAM FROM FRM 15.5-17 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED GUSSET.SDR I06B2010 01 18 JFEngine · contaminatedAFTER TAKEOFF AT APPROX 400 FT, PILOTS RECEIVED "LAV SMOKE" EICAS INDICATION. DECLARED EMERGENCY & RETURNED FOR LANDING AT DEPARTURE. ACFT GROUNDED UNTIL MX DETERMINES ROOT CAUSE. F/A INVESTIGATED ACFT LAV - OBSERVING NO FUMES OR SMOKE. ONCE ON THE GROUND SDR CHQA201000010Inverter · inoperativeDURING INSPECTION THE EMERGENCY EXIT LIGHT IN THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 1 DC/AC INVERTER AND THE EMERGENCY LIGHT OPERATED NORMALLY.SDR CHQA201000009O-Ring · blownTHE FLIGHT CREW REPORTED A BLEED 1 LEAK MESSAGE ON EICAS UPON ENTERING ICING CONDITIONS DURING CLIMB. THE CREW DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE BLEED SYSTEM AND FOUND A LEAK AT JOINT 15 UNDER THE CARGO COMPARTMENT FLOOR.SDR JO0M2008102800001Tube · failedTUBE ASSY, PRESSURE OIL TO COOLER, PN 23056413 RUBBING STARTER AIR VALVE CLAMP BURST AT CHAFE RESULTING IN LOSS OF APPROX ONE QUART OF OIL.SDR CHQA201000007Battery · dischargedDURING INSPECTION THE LAST 4 EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04 AND THE EMERGENCY LIGHTS OPERATED NORMALLY.SDR CHQA201000008Battery · dischargedDURING INSPECTION THE LEFT AND RIGHT OVERWING EXTERNAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04 AND THE EMERGENCY LIGHTS OPERATED NORMALLY.SDR CHQA201000006Light · inoperativeDURING INSPECTION THE NR 3 FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 3 FLOOR PROXIMITY LIGHT STRIP AND THE EMERGENCY LIGHTS OPERATED NORMALLY.SDR V0XR201001120005Profile · corrodedPROFILE AND BEAM AT FRM 17, YL 610 & 690 IS CORRODED OUT OF LIMITS. R & R PROFILE AND BEAM.SDR V0XR201001120008Sill · corrodedRT SILL FROM FRM 60.5-65 IS CORRODED OUT OF LIMITS. R & R SILL.SDR V0XR201001120009Gusset · corrodedCTR GUSSET FROM FRM 59-61 IS CORRODED OUT OF LIMITS. R & R GUSSET.SDR V0XR201001120010Sill · corrodedLT SILL FROM FRM 59-61 IS CORRODED OUT OF LIMITS. R & R SILL.SDR V0XR201001120012Channel · corrodedRT SILL HAT SECTION BEAM UNDER GUSSET FROM FRM 5-62 IS CORRODED OUT OF LIMITS. R & R HAT SECTION BEAM.SDR V0XR201001120013Sill · corrodedLT SILL FROM FRM 24-29 IS CORRODED OUT OF LIMITS. R & R SILL.SDR V0XR201001120014Sill · corrodedLT SILL FROM FRM 60-65 IS CORRODED OUT OF LIMITS. R & R SILL.SDR V0XR201001120015Profile · corrodedRT PROFILE AT FRM 61 IS CORRODED OUT OF LIMITS. R & R PROFILE.SDR V0XR201001120016Doubler · corrodedRT LOWER DOUBLER FWD PARTITION AT FRM 61 IS CORRODED OUT OF LIMITS. R & R DOUBLER.SDR CHQA201000003Check Valve · missingDURING CRUISE THE FLIGHT CREW REPORTED THE AUTO AND MANUAL PRESSURIZATION SYSTEMS WERE INOP AND THE AIRCRAFT DIVERTED TO BUF. MAINTENANCE DEFERRED THE AUTO AND MANUAL PRESSURIZATION SYSTEMS AND THE AIRCRAFT WAS RELEASED FOR SERVICE. THE AIRCRAFT THEN FLEW TOSDR V0XR201001110003Gusset · corrodedRT GUSSET FROM FRM 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET.SDR CHQA201000002Proximity Switch · corrodedAFTER TAKEOFF THE CREW RETRACTED THE LANDING GEAR BUT STILL HEARD A LOUD RUSHING AIR NOISE. THE CMH TOWER CONFIRMED THE NOSE GEAR DOORS WERE STILL OPEN AFTER A FLYBY. THE AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE SDR CHQA201000001Unknown · smokeAFTER TAKEOFF THE CREW REPORTED SMOKE IN THE COCKPIT THAT SMELLED LIKE CHEMICALS. BY THE TIME THE AIRCRAFT WAS PREPARED FOR LANDING THE SMOKE HAD COMPLETELY DISSIPATED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT HAD BEEN DEICED PRIOR TO TAKEOFF. SDR CHQA200900274Battery Pack · faultyWHEN THE EMERGENCY LIGHT SWITCH WAS SET TO THE ARMED POSITION, HALF OF THE EMERGENCY LIGHTS WOULD COME ON UNCOMMANDED. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK IAW EMB AMM 33-50-04, OPS CHECK GOOD.SDR CHQA200900271Coupling · crackedDURING INITIAL CLIMB OUT OF MSY THE CREW REPORTED A BLEED 1 LEAK MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE MESSAGE CLEARED. DUE TO ICING CONDITIONS IN THE AREA AND WEATHER CLOSING IN ON THE AREA, IT WAS DECIDED TO RETURN TO MSY WHERE THE AIRCRAFT LANDEDSDR CHQA200900272Solenoid Valve · faultyAFTER TAKEOFF THE CREW SELECTED THE LANDING GEAR TO THE UP POSITION WITH THREE GREEN UP AND LOCKED INDICATIONS. THE CREW NOTICED AN UNUSUAL AMOUNT OF WIND NOISE AFTER GEAR RETRACTION WITH NO EICAS MESSAGE. THE NOSE LANDING GEAR DOORS WERE CONFIRMED OPEN BY ISDR CHQA200900270Controller · malfunctionedWITH THE AUTO PRESSURIZATION ON MEL THE CABIN ALTITUDE INDICATION DASHED AT FL080. THE AIRCRAFT LEVELED OFF AT FL100 AND PER MEL CABIN ALTITUDE INDICATION IS REQUIRED, AND THE AIRCRAFT RETURNED TO CHS AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE MANSDR CHQA200900268Solenoid Valve · defectiveAFTER TAKEOFF AND GEAR RETRACTION THE CREW REPORTED EXCESSIVE WIND NOISE COMING FROM THE NOSE LANDING GEAR AREA. THE FLIGHT CONTINUED BELOW 250KTS AND LANDED IN CMH WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOOR SOLENOID IAW EMB MM 32-33-0SDR CHQA200900269Light · inoperativeDURING THE OPS CHECK OF THE EMERGENCY LIGHTS DUE TO A TIME REQUIRED CHANGE OF THE NR 3 BATTERY, THE FLOOR PROXIMITY LIGHT STRIP AT SEAT 7A WAS INOP. MAINTENANCE REPLACED THE FLOOR PROXIMITY LIGHT STRIP AND OPS CHECK NORMAL PER EMB AMM 33-50-12.SDR CHQA200900265ASeal · detachedCREW REPORTED THAT AT FL320 THE CAPTAIN'S DV WINDOW BEGAN SQUEALING AND BECAME SO LOUD THAT COMMUNICATION WAS NEARLY IMPOSSIBLE. THE FLIGHT CREW DECIDED TO RETURN TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAPTAIN'S DV WINDOW SEAL IAW MM 56SDR C2XA09IA325Thermocouple · inoperativeIAH - FLIGHT 2411, THE CREW REPORTED A ENGINE ONE EXCEEDANCE AT TOP OF CLIMB WITH THE THRUST LEVER IN DETENT ITT AMBER JUST ABOVE 900 DEGREES AND N2 AT ABOUT 101 PERCENT, THE ENGINE STABILIZED WITH REDUCED THRUST, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDSDR C2XA09IA326Control Valve · dirtyIAH - FLIGHT 2411, THE CREW REPORTED A ENGINE ONE EXCEEDANCE AT TOP OF CLIMB WITH THE THRUST LEVER IN DETENT ITT AMBER JUST ABOVE 900 DEGREES AND N2 AT ABOUT 101 PERCENT, THE ENGINE STABILIZED WITH REDUCED THRUST, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDSDR CHQA200900264ASign · inoperativeWHILE AT GATE, GROUND PERSONNEL PULLED GROUND POWER WHILE STILL IN USE CAUSING THE EMERGENCY LIGHTS TO ACTIVATE. ALL LIGHTS ACTIVATED EXCEPT THE FORWARD CEILING EMERGENCY EXIT SIGN. MAINTENANCE REPLACED THE FORWARD CEILING EMERGENCY EXIT SIGN WITH NO FURTHERSDR CHQA200900263ATransmission · failedAFTER TAKEOFF THE CREW RECEIVED A FLAP FAIL MESSAGE ON EICAS. RAN THROUGH THE APPROPRIATE CHECK LISTS AND RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE CMC FOR MESSAGES AND FOUND A RT TRANSMISSION FAIL CMC. THE RIGHT FLAP TRANSMISSIONSDR CHQA200900262Engine · bird ingestionTHE FLIGHT CREW REPORTED A BIRD STRIKE ON ROTATION AT ABOUT 20FT. E2 ITT FLUCTUATED 100 DEGREES FOR 3 OR 4 MINUTES AFTERWARDS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION IAW EMB 140 AMM 5-50-08 WITSDR C2XA09IA310Engine · leakingIAH - FLIGHT 2379, THE CREW REPORTED A LAV SMOKE INDICATION ON EICAS WITH AN ASSOCIATED SMOKE SMELL ON CLIMBOUT. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWOSDR CHQA200900261Battery Pack · dischargedDURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT AND THE NR 4 BATTERY PACK WITH NO FURTHER DEFECTS NOTED.SDR CHQA200900260Light · inoperativeDURING INSPECTION THE NR 2 EMERGENCY LIGHT FLOOR STRIP WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT FLOOR STRIP AND THE EMERGENCY LIGHTS OPERATED NORMALLY.SDR CHQA200900259Battery Pack · dischargedDURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK WITH NO FURTHER DEFECTS WERE NOTED.
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