Allison AE-3007A1/2

Service difficulty reports · 289

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 = 'AE3007A12'
  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 V0XR201011120005Gusset · corroded(V0XR) GUSSET AT FRAME 17-18 YO.O - LY 470.0 IS CORRODED BEYOND LIMITS. R & R GUSSET.Nov 12, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR201011120006Angle · corroded(V0XR) SCALLOPED ANGLE AT RY 780.0 - Y0.0 FRAME 23.5 IS CORRODED BEYOND LIMITS. R & R ANGLE.Nov 12, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR201011120007Gusset · corroded(V0XR) CTR GUSSET FRAME 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET.Nov 12, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR201011120008Gusset · corroded(V0XR) LT GUSSET FRAME 53-59 IS CORRODED BEYOND LIMITS. R & R LT GUSSET.Nov 12, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR201011120009Gusset · corroded(V0XR) LT GUSSET OMEGA BEAM AT FRAME 30 IS CORRODED BEYOND LIMITS. R & R LT GUSSET.Nov 12, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR201011120010Gusset · corroded(V0XR) CTR GUSSET AT FRAME 39-46 IS CORRODED BEYOND LIMITS. R & R CTR GUSSET.Nov 12, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR201011120011Gusset · corroded(V0XR) LT DIGITAL PLATE AT FRAME 19-23 IS CORRODED BEYOND LIMITS. R & R LT DIGITAL PLATE.Nov 12, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR201011120012Doubler · corroded(V0XR) RT DOUBLER PARTITION AT FRAME 60 IS CORRODED BEYOND LIMITS. R & R RT DOUBLER PARTITION.Nov 12, 2010 · N836HK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR V0XR201011090001Support Bracket · corroded(V0XR) PAX DOOR THRESHOLD SUPPORT BRACKETS ARE CORRODED BEYOND LIMITS. R & R DOOR SUPPORT BRACKETS.Nov 9, 2010 · N836HK · Emb EMB145LR · Passenger/Crew DoorsSDR V0XR201011090002Floor Support · corroded(V0XR) SUPPORT ANGLE AT LY-479.0, FRAME 18-19 IS CORRODED BEYOND LIMITS. R & R SUPPORT ANGLE.Nov 9, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR2010110900032Floor Support · corroded(V0XR) SUPPORT ANGLE AT LY-479.0, FRAME 18-19 IS CORRODED BEYOND LIMITS. R & R SUPPORT ANGLE.Nov 9, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR2010110900006Gusset · corroded(V0XR) CTR GUSSET FROM FRAMES 53-59 ON CTR OMEGA BEAM IS CORRODED BEYOND LIMITS. R & R CTR GUSSET. W/C 1086Nov 9, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR2010110900007Sill · corroded(V0XR) LEFT SILL FROM FRAMES 53-59 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1088Nov 9, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR2010110900010Sill · corroded(V0XR) RIGHT SILL FROM FRAMES 53-59 IS CORRODED BEYOND LIMITS. R & R RT SILL. W/C 1091Nov 9, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR2010110900011Sill · corroded(V0XR) RIGHT SILL FROM FRAMES 31 IS CORRODED BEYOND LIMITS. R & R RT SILL. W/C 1092Nov 9, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR2010110900012Sill · corroded(V0XR) RIGHT SILL FROM FRAMES 24-29 IS CORRODED BEYOND LIMITS. R & R RT SILL. W/C 1094Nov 9, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR2010110900013Partition · corroded(V0XR) LEFT FWD PARTITION AT FRAME 60 IS CORRODED BEYOND LIMITS. R & R DOUBLER. W/C 2082Nov 9, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR2010110900014Sill · corroded(V0XR) RIGHT SILL AT FRAMES 61-65 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 2083Nov 9, 2010 · N836HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR V0XR2010110900015Seat Track · worn(V0XR) (CORRECTION) PILOT AND CO-PILOT SEAT TRACK WORN BEYOND LIMITS. REMOVED AND REPLACED PILOT AND CO-PILOT SEAT TRACKS. W/C 2113Nov 9, 2010 · N836HK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA201025602Carbon Seal · leakingON FLIGHT 2829 SMOKE BEGAN TO FILL THE COCKPIT AND CABIN WHEN THROTTLES WERE SET FOR TAKEOFF. THE SMOKE STOPPED AFTER THROTTLES BROUGHT TO IDLE DURING ABORTED TAKEOFF. ENGINE BLEEDS AND PACKS WERE OPEN WHILE AUXILIARY POWER UNIT WAS OFF DURING THE SMOKE. THSep 10, 2010 · N928AE · Emb EMB145LR · Turbine Engine Oil SystemSDR C2XA10TY122Sensor · contaminatedTYS - A/C WAS DIVERTED TO TYS FROM BNA DUE TO E1 OVERTEMP. TYS MAINTENANCE FOUND A LOOSE B-NUT THAT WAS LEAKING HOT AIR ONTO A TEMP SENSOR. TIGHTEN B-NUT AND OPD CHECK GOOD AND WAS RELEASED BACK TO SERVICE.Sep 9, 2010 · N13990 · Emb EMB145LR · Engine Temperature Indicating SystemSDR C2XA10TY123Engine · malfunctionedTYS - IN BNA THE CREW EXPERIENCED A FUNNY SMELL AND VIBES AT 5000 FEET ON DESCENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE AND WILL BE RELEASED AT THE END OF THE CHANGE AND OPS CHECKS.Sep 9, 2010 · N26549 · Emb EMB145LR · Engine (Turbine/Turboprop)SDR V0XR201008250001Seat Track · corrodedSEAT TRACK C BETWEEN FR 24-30 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK C. W/C 2096Aug 25, 2010 · N851HK · Emb EMB145LR · Fuselage Main, StructureSDR V0XR201008170001Sill · corrodedPAX DOOR SILL ANGLES ARE CORRODED BEYOND LIMITS. R & R PAX DOOR SILL ANGLES.Aug 17, 2010 · N851HK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA201023002Metering Unit · failedON FLIGHT 3924 DURING CRUISE THE CREW REPORTED AT FLIGHT LEVEL 240 THE NR 2 ENGINE SURGED CONTINUOUSLY FOR APPROXIMATELY 2 MINUTES WHILE ALL OTHER INDICATIONS WERE NORMAL. LARGE FLUCTUATIONS N1, N2 & ITT, IGNITION AB DISPLAYED AS IF IT WAS TRYING TO RELIGHT AAug 15, 2010 · N682AE · Emb EMB145LR · Fuel Control/Turbine EnginesSDR FDKA2010073100188Engine · malfunctionedSMOKE AND FUMES DET DURING CLIMB. AS CREW WENT THROUGH PROCEDURES IN THE MANUAL THE FUMES WENT AWAY, THE CREW DETERMINED THAT A DIVERSION OR RTF WASN'T NECESSARY. ON FINAL TO DTW, THE NR 1 ENGINE INDICATED VIBES IN THE YELLOW RANGE, THE CREW PULLED NR 1 ENGIJul 31, 2010 · N828MJ · Emb EMB145LR · Engine (Turbine/Turboprop)SDR C2XA10IA098Fadec · malfunctionedIAW - FLIGHT 2758, THE CREW REPORTED THAT ENGINE 1 SURGES IN FLIGHT. CRUISE THRUST N1 FLUCTUATES =/-15 PERCENT WITH AN ITT RISE AND FALL; N1 REQUEST CARAT ALSO FLUCTUATES =/- 15 PERCENT, AND THE CRZ THRUST SETTING AUTO ADVANCED TO TO1. ENGINE 1 FADEC AUTO ALMar 14, 2010 · N13992 · Emb EMB145LR · Fuel Control/Turbine EnginesSDR C2XA10CL017Bleed Valve · faultyORD FLT 5666 THE CREW REPORTED A NR 1 ENGINE BLEED VALVE CLOSED MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.Feb 2, 2010 · N14542 · Emb EMB145LR · Compressor Bleed ValveSDR SIMA200935504Engine · odorAFTER LANDING THE CREW OF FLIGHT 3762 REPORTED A STRONG ELECTRICAL SMELL IN THE COCKPIT. AFTER ENGINE RUNS A STRONG OIL SMELL WAS PRESENT IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE RUN PER THE GROUND HANDLING CHECKLIST AND FOUNDDec 18, 2009 · N601DW · Emb EMB145LR · Turbine Engine Air Inlet SectionSDR CHQA200900193Battery · dischargedDURING MAINTENANCE INSPECTIONS IT WAS DISCOVERED THAT THE FRONT FAIRING EMERGENCY LIGHT AND AISLE EMERGENCY LIGHT WERE INOPERATIVE. TROUBLESHOOTING FOUND THAT NR 1 EMERGENCY BATTERY WAS NOT WORKING. THE BATTERY WAS REPLACED AND ALL CHECKS WERE OK.Sep 2, 2009 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA200900189Light · disconnectedDURING MAINTENANCE THE AFT EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 17 & 18 WAS FOUND TO BE INOPERATIVE. THE LIGHT STRIP WAS THEN FOUND TO BE UNPLUGGED. THE STRIP WAS PLUGGED IN AND IT OPERATIONALLY CHECKED GOOD.Sep 1, 2009 · N564RP · Emb EMB145LR · Emergency LightingSDR CHQA200900190Battery · dischargedDURING MAINTENANCE THE NR 4 EMERGENCY BATTERY WAS FOUND TO BE DISCHARGED. IT WAS REPLACED IAW 145AMM 33-50-04 AND THE OPERATIONAL CHECKS WERE GOOD.Sep 1, 2009 · N564RP · Emb EMB145LR · Emergency LightingSDR CHQA200900191Light · out of positionDURING THE WALK AROUND INSPECTION THE EMERGENCY LIGHT OVER THE RIGHT WING WAS FOUND TO BE UPSIDE DOWN. MAINTENANCE REPOSITIONED THE LIGHT TO THE CORRECT ORIENTATION AND CHECKS WERE SATISFACTORY. NO OTHER ACTIONS WERE REQUIRED.Sep 1, 2009 · N279SK · Emb EMB145LR · Emergency LightingSDR CHQA200900192Wire · brokenDURING THE 4Y INSPECTION IT WAS FOUND THAT THE NR 8 EMERGENCY LIGHT STRIP HAD A BROKEN WIRE. THE LIGHT STRIP WAS REPLACED IAW EMB 145 AMM 35-50-12 AND CHECKED OK.Sep 1, 2009 · N573RP · Emb EMB145LR · Light System WiringSDR CHQA200900188Warning System · malfunctionedON THE TAKEOFF ROLL THE CREW RECEIVED THE E1 & E2 FUEL LOW PRESS MSG ON THE EICAS AND THE L, R & TOTAL FUEL QUANTITY INDICATIONS BLANKED OUT. THE FLIGHT THEN ABORTED TAKEOFF AND CLEARED THE RUNWAY. CHECKLISTS WERE COMPLETED AND THE AIRCRAFT RETURNED TO THE GAug 31, 2009 · N294SK · Emb EMB145LR · Engine Fuel Indicating SystemSDR SIMA200921002Engine · shutdownON FLIGHT 3741 - CREW REPORTED ENGINE 1 FAILED (UNCOMMANDED SHUTDOWN) ON TAKEOFF AT APPROXIMATELY 10 KNOTS. AIRCRAFT REMOVED FROM SERVICE. AWAITING FOLLOW-UP.Jul 29, 2009 · N684JW · Emb EMB145LR · Engine (Turbine/Turboprop)SDR C2XA09IA116Magnetic Seal · leakingIAH - FLIGHT 3108, THE CREW REPORTED THAT APPROXIMATELY ONE HOUR INTO FLIGHT THEY STARTED LOSING OIL PRESSURE AND QTY ON THE NUMBER TWO ENGINE. THE CREW SHUT DOWN THE NUMBER TWO ENGINE AS A PRECAUTION, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENAMay 2, 2009 · N14974 · Emb EMB145LR · Turbine Engine Oil SystemSDR C2XA08TY127Flange · corrodedACFT WAS IN FOR A 3C INSPECTION AND THE NR 1 ENGINE FORWARD BOLT FLANGE WAS FOUND CORRODED. 2 BOLT HOLES AT NR 29 AND NR 45 WERE FOUND IF REPAIRED WOULD RESULT IN BEING BEYOND THE MM LIMITS AND REPAIR OF THE HOLES WOULD RESULT IN A THINWALL CONDITION. ALL OTOct 23, 2008 · N13913 · Emb EMB145LR · Engine (Turbine/Turboprop)SDR RAIA00809006O-Ring · defectiveDURING CLIMB, CREW SHUTDOWN THE NR 2 ENGINE IN FLIGHT DUE TO LOW OIL AND LOW OIL AND LOW OIL PRESSURE. MAINTENANCE INSPECTED THE ENGINE AND FOUND A BAD O-RING AT THE NR4 GENERATOR. THE O-RING WAS REPLACED AND LEAK CHECK OF THE NR 2 ENGINE DID NOT PRODUCE ANY Sep 7, 2008 · N810HK · Emb EMB145LR · Turbine Engine Oil System
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