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 CHQA201000101Light · disconnectedDURING INSPECTION, THE FLOOR PROXIMITY EMERGENCY LIGHT NEXT TO SEAT 1A WAS INOP. MAINTENANCE FOUND DISCONNECTED WIRES ON THE LIGHT STRIP AND RE-ATTACHED IN ACCORDANCE WITH EMB 140 MM 33-50-00, NO FURTHER DEFECTS WERE NOTED.SDR CHQA201000098Tire · low pressureTHE CREW REPORTED THAT ON LANDING IN LGA THE AIRCRAFT HAD POOR BRAKING AND DRIFTED TO THE RIGHT AT HIGH SPEED. THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. UPON POST FLIGHT INSPECTION THE LEFT OUTBOARD TIRE WAS LOW. MAINTENANCE REPLACED BOTH TIRES ON TSDR CHQA201000099Connector · misinstalledTHE CREW REPORTED THAT ON LANDING IN CMH THE BRAKES WERE NOT AS EFFECTIVE AS NORMAL. DURING POST FLIGHT INSPECTION THE LEFT OUTBOARD TIRE WAS FLAT SPOTTED AND BLOWN. MAINTENANCE INSPECTED THE LEFT GEAR AND FOUND THE WHEEL SPEED TRANSDUCER CONNECTORS FOR THE SDR CHQA201000097Battery Pack · dischargedDURING INSPECTION MAINTENANCE FOUND THE OVERWING EMERGENCY EXIT LIGHTS TO BE INOP WHEN TESTED. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000096Rod · wornDURING CLIMB THE CREW REPORTED A LOUD VIBRATION HEARD THROUGHOUT THE AIRCRAFT AFTER RETRACTING THE FLAPS AND RETURNED TO FIELD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INITIALLY FOUND A LOOSE SEAM ON THE LEFT RAM AIR INLET AND REPLACED THE LEFT RAM AIR VSDR CHQA201000095Transducer · failedAFTER LANDING THE CREW REPORTED THAT HIGH SPEED BRAKING WAS INEFFECTIVE. BOTH BRAKE PEDALS WENT TO THE FLOOR WITH LITTLE EFFECT. CREW ALSO REPORTED THAT BRAKING SEEMED TO IMPROVE AT LOWER SPEEDS. MAINTENANCE FOUND FAULTS ON THE CMC FOR BRAKE PPTAN 3 FAIL ANSDR CHQA201000094Light · inoperativeDURING INSPECTION, TWO FLOOR PROXIMITY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY LIGHT STRIPS IAW AMM 33-50-12.SDR V0XR201005040001Seat Track · corroded(V0XR) LT LOWER SEAT TRACK FR 17-23 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.SDR V0XR201005040002Seat Track · corroded(V0XR) RT UPPER SEAT TRACK FR 36-46 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK.SDR V0XR201005040003Fairing · cracked(V0XR) RT WING TO FUSELAGE FAIRING STRIP X=14967.0 - X=16143.5 IS CRACKED. R & R FAIRING.SDR CHQA201000090Float Valve · leakingWHILE CLIMBING THROUGH 4,000FT, THE FLIGHT CREW WAS NOTIFIED OF FUEL LEAKING FROM THE LEFT WING. THE AIRCRAFT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT FUEL VENT FLOAT VALVE LEAKING. THE LEFT FUEL VENT FLOAT VALVE WAS REPLACED SDR CHQA201000091Light · inoperativeDURING INSPECTION THE EMERGENCY LIGHT STRIP BETWEEN ROWS 8 AND 9 WAS NOT WORKING WHEN TESTED. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT BETWEEN ROWS 8 AND 9 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000093Connector · damagedDURING INSPECTION A FLOOR PROXIMITY LIGHT STRIP WAS FOUND WITH DAMAGED CONNECTORS. THE FLOOR LIGHT STRIP WAS REPLACED BY MAINTENANCE IAW AMM 33-50-12.SDR V0XR201005030004Gusset · corroded(V0XR) FWD GUSSET AT FR 14-16.5 LY 780.0 - RY 780.0 IS CORRODED BEYOND LIMITS. R & R GUSSET.SDR V0XR201005030005Gusset · corroded(V0XR) GUSSET AT FR 16.5-18 LY 479.0 - Y0.0 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED GUSSET.SDR V0XR201005030008Floor Support · corroded(V0XR) FLOOR SUPPORT ANGLE AT FR 23 Y0.0 - RY 780.0 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT ANGLE. W/C 1082SDR V0XR201005030007Floor Support · corroded(V0XR) SCALLOPED FLOOR SUPPORT ANGLE AT FR 18 LY 479.0 - RY 780.0 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT ANGLE. W/C 1082SDR V0XR201005030009Angle · cracked(V0XR) ANGLE AT FR 14 LY 780.0 IS CRACKED BEYOND LIMITS. R & R ANGLE.SDR V0XR201005030012Sill · corroded(V0XR) LT SILL AT FR 18-23 LY 780.0 IS CRACKED BEYOND LIMITS. R & R SILL.SDR V0XR201005030013Sill · corroded(V0XR) SERVICE DOOR SILL IS CORRODED BEYOND LIMITS. R & R SILL.SDR V0XR201005030014Floor Support · corroded(V0XR) FLOOR SUPPORT ANGLE FR 18-20 AT Y0.0 IS CORRODED BEYOND LIMITS. R & R ANGLE.SDR V0XR201005030015Channel · corroded(V0XR) RT HAT CHANNEL BEAM FR 16-25 AT RY 479.0 IS CORRODED BEYOND LIMITS. R & R BEAM.SDR V0XR201005030016Angle · corroded(V0XR) ANGLE FR 23 AT RY 780.0 IS CORRODED BEYOND LIMITS. R & R ANGLE.SDR V0XR201005030019Guide · broken(V0XR) LEFT NR 4 CABLE GUIDE BROKEN. R & R CABLE GUIDE.SDR V0XR201005030020Guide · broken(V0XR) RIGHT NR 2 CABLE GUIDE SUPPORT AT FR 25 IS BROKEN. R & R CABLE GUIDE.SDR V0XR201005030023Bolt · corroded(V0XR) NR 1 RUDDER ACTUATOR CTR ATTACHMENT BOLTS ARE CORRODED BEYOND LIMITS. R & R ACTUATOR BOLTS.SDR CHQA201000088Unknown · malfunctionedCREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS AFTER TAKE-OFF AND THE GEAR LEVER WOULD NOT MOVE TO THE UP POSITION. THE AIRCRAFT RETURNED TO IAH AND LANDED WITH OUT INCIDENT. UPON LANDING THE THRUST REVERSERS WOULD NOT DEPLOY AND AN IDLE STOP SDR CHQA201000089Electronic Unit · faultyAFTER TAKEOFF ON THE FERRY FLIGHT FROM IAH THE CREW REPORTED THAT THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION AND A LANDING GEAR AIR/GROUND FAIL MESSAGE APPEARED ON EICAS. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESDR C2XA10CL065Engine · faultyMHT-CLE FLT 2582 THE CREW REPORTED A PUNGENT ODOR FROM THE PACKS THROUGHOUT THE ENTIRE FLIGHT. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.SDR V0XR201004300001Profile · corroded(V0XR) PROFILE AT FR 17 LY 479.0 -780.0 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 1077.SDR V0XR201004300002Profile · corroded(V0XR) PROFILE AT FR 17-18 OUTBOARD OF LY 479.0 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 1078.SDR V0XR201004300003Channel · corroded(V0XR) CTR HAT CHANNEL BEAM AT Y0.0 IS CORRODED BEYOND LIMITS. R & R BEAM. W/C 1083.SDR V0XR201004300004Profile · corroded(V0XR) PROFILE AT FR 22 FROM OMEGA BEAM TO RY 780.0 IS CORRODED BEYOND LIMITS. R & R BEAM. W/C 1117.SDR V0XR201004290001Sill · corroded(V0XR) RT SILL FWD OF SERVICE DOOR FR 17-20 RY 780.0 IS CORRODED BEYOND LIMITS. R & R RT SILL. W/C 1065.SDR V0XR201004290002Floor Support · corroded(V0XR) OMEGA BEAM AT FR 20 RY 479.0 IS CORRODED BEYOND LIMITS. R & R BEAM. W/C 1070.SDR V0XR201004290003Floor Support · corroded(V0XR) FLOOR SUPPORT ANGLE AT LY 479.0 FR 19-20 IS CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1071.SDR DXTA2010043004080Latch · dislodgedSHORTLY AFTER TAKEOFF - WHILE CLIMBING IN MODERATE TURBULENCE - FELT A THUD, HEARD A POP AND GOT AN AMBER 'NOSE DOOR OPEN R' EICAS MESSAGE. AFTER LANDING, FOUND THE FWD LATCH ON THE RT NOSE DOOR HAD POPPED OPEN IN FLIGHT. LATCH MAY NEED ADJUSTMENT. R & R RT FSDR V0XR201004280004Seat Track · corroded(V0XR) RT UPPER SEAT TRACK FR 23-30 IS CORRODED BEYOND LIMITS. R AND R RT SEAT TRACK. W/C 1095.SDR V0XR201004280005Seat Track · corroded(V0XR) LT UPPER SEAT TRACK FR 17-23 IS CORRODED BEYOND LIMITS. R & R LT SEAT TRACK. W/C 2106.SDR CHQA201000087Light · inoperativeDURING INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOP. MAINTENANCE REPLACED THE LIGHT BULB IN THE RIGHT OVERWING EMERGENCY LIGHT WITH NO FURTHER DEFECTS NOTED.SDR V0XR201004260004Seat Track · corroded(V0XR) RT UPPER SEAT TRACK FR 52-57 CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1099.SDR V0XR201004260005Profile · corroded(V0XR) PROFILE AT FR 22 LY 479.0 - LY 780.0 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 1062.SDR V0XR201004260006Seat Track · corrodedLT UPPER SEAT TRACK AT FR 36-46 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1093.SDR V0XR201004260007Seat Track · corroded(V0XR) RT UPPER SEAT TRACK AT FR 30-36 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1096.SDR CHQA201000086Wire Harness · chafedTHE FLIGHT CREW REPORTED AN INTERMITTENT E1 FIRE DETECT FAIL MESSAGE IN FLIGHT. THE MESSAGE WOULD APPEAR FOR A FEW SECONDS THEN CLEAR. THE FLIGHT CONTINUED TO SDF AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED E1 AND FOUND A CUT IN THE W407 HARNESS. THSDR CHQA201000085Connector · looseCREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE DURING CLIMBOUT FROM CLT. THE LOG RUNWAY WAS REQUESTED AT CLE BUT NO EMERGENCY WAS DECLARED BY THE CREW. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERFORMEDSDR CHQA201000084Unknown · odorDURING CRUISE, THE FLIGHT ATTENDANT REPORTED A BURNING RUBBER SMELL. THE FIRST OFFICER WENT BACK TO CONFIRM AND THE SMELL DISSIPATED ALMOST IMMEDIATELY, AND THE FLIGHT CONTINUED. SOON AFTER THE SMELL RETURNED AND THE FLIGHT DIVERTED TO SDF WHERE IT LANDED WISDR CHQA201000083Battery · dischargedDURING INSPECTION, BOTH OF THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000082Control Lever · faultyCREW REPORTED THAT THE AIRCRAFT WOULD NOT ACCELERATE AND A RUMBLE COULD BE HEARD AND FELT. THE CREW INSPECTED THE WINGS DURING FLIGHT AND FOUND THE FLAPS SLIGHTLY EXTENDED WITH A ZERO INDICATION IN THE COCKPIT. THE FLAP HANDLE WAS CYCLED AND THE FLAPS FULLY SDR CHQA201000080Brake · faultyTHE CREW REPORTED THE FLAP POSITION INDICATION WAS INOP ON APPROACH. MAINTENANCE REPLACED THE LEFT FLAP WING BRAKE DUE TO FAIL MESSAGES FOUND ON THE CMC WITH NO FURTHER DEFECTS NOTED.
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