Allison AE-3007A1P

Service difficulty reports · 849

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 = 'AE3007A1P'
  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 CHQA20130606196Light · inoperativeDURING INSPECTION, THE FWD F/A CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE FORWARD F/A CEILING EMERGENCY LIGHT BULB. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jun 6, 2013 · N293SK · Emb EMB145LR · Emergency LightingSDR CHQA20130605194Light · inoperativeDURING INSPECTION, THE RT FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE RT FORWARD EXTERNAL EMERGENCY LIGHT ASSEMBLY. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jun 5, 2013 · N286SK · Emb EMB145LR · Emergency LightingSDR CHQA20130604195Connector · dirtyCREW REPORTED THAT THEY RECEIVED A FLAP FAIL MESSAGE IN FLIGHT. THE CREW DECLARED AN EMERGENCY AS A PRECAUTION AND LANDED WITHOUT INCIDENT AT THEIR INTENDED DESTINATION. MX CLEANED AND RESEATED THE CONNECTOR PLUGS ON THE FLAP ELECTRONIC CONTROL UNIT AND RESEJun 4, 2013 · N277SK · Emb EMB145LR · Flight Control System WiringSDR CHQA20130603210Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR LOWER FRAME AROUND THE NUT PLATE HOLES. THE FRAME WAS REPAIRED IAW ETD 2013-145-011762.Jun 3, 2013 · N563RP · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20130602213Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR ANGLE AT FRAME 23. THE REPAIR DOUBLER WAS REPLACED IAW SRM 51-40-02.Jun 2, 2013 · N563RP · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20130601200Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FRAME 14 AT STRINGERS 20-21R. FRAME REPAIRED IAW SRM 53-00-04 AND SRM 51-40-02.Jun 1, 2013 · N275SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20130601212Frame · corrodedDURING INSPECTION, A GOUGE WAS FOUND ON FRAME 60 BETWEEN STRINGERS 4L AND 5L. THE FRAME WAS REPAIRED IAW SRM 53-00-04.Jun 1, 2013 · N563RP · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20130601214Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE LOWER DOOR PLATE. THE FRAME WAS REPAIRED IAW SRM 53-31-04 AND SRM 51-40-02.Jun 1, 2013 · N563RP · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20130531192Switch · faultyCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A PACK 1 OVERLOAD MESSAGE. THE CREW FOLLOWED THE QUICK REF HANDBOOK AND STARTED TO DESCEND. THE CREW THEN REPORTED THAT THEY HAD A FAINT SMELL OF SMOKE IN THE COCKPIT WITH NO WARNING MESSAGE AND VISUAL SIGNS OF May 31, 2013 · N288SK · Emb EMB145LR · Cabin Cooling SystemSDR CHQA20130531215Skin · damagedDURING INSPECTION, THE LEFT HAND ENGINE PYLON WAS FOUND TO HAVE DAMAGE AROUND THE DRILLED SCREW SHANK ON THE UPPER FORWARD SURFACE. THE DAMAGE WAS REPAIRED IAW SRM 54-50-01 AND ETD 2013-145-011772.May 31, 2013 · N563RP · Emb EMB145LR · Nacelle/Pylon, Plate/SkinSDR CHQA20130530202Trunnion · corrodedDURING INSPECTION, THE LT MLG TRUNNION WAS FOUND TO HAVE PITTING AND CORROSION ON THE BEARING TRACK. LT MLG TRUNNION REPAIRED IAW ETD 2013-145-011061.May 30, 2013 · N275SK · Emb EMB145LR · Fuselage, Landing Gear Attach FittingsSDR AALA20130529008Governor · failedCREW REPORTED NO INFLIGHT RESTART ON LT ENGINE. LEFT ENGINE VALVE ILLUMINATED WITH EICAS MESSAGE WHEN FUEL SWITCH PLACED IN EITHER ON OR OFF POSITION. FLIGHT LANDED WITHOUT INCIDENT. REPLACED LT FUEL FLOW GOVERNOR. SYS GROUND CHECK NORMAL OPS.May 29, 2013 · N197AN · Boeing 757223 · Fuel Controlling SystemSDR CHQA20130528197Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R AT FRAME 12-13. THE STRINGER WAS REPLACED IAW SRM 51-40-02.May 28, 2013 · N275SK · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR CHQA20130528198Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER AFT FRAME OF THE SERVICE DOOR AROUND THE NUT PLATE HOLES. THE FRAME WAS REPAIRED IAW ETD 2013-145-011083.May 28, 2013 · N275SK · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20130528199Web · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE AILERON QUADRANT SUPPORT WEB AT STRINGERS 20R-21R AND FRAME 12-13. THE AILERON QUADRANT SUPPORT WEB WAS REPLACED IAW SRM 51-40-02.May 28, 2013 · N275SK · Emb EMB145LR · AileronsSDR CHQA20130528201Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER AFT FRAME OF THE MAIN CABIN DOOR. DOOR FRAME REPAIRED IAW SRM 51-40-02.May 28, 2013 · N275SK · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20130520171Pressure Switch · malfunctionedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WAS ABLE TO RESET THE SYSTEM, HOWEVER, THE MESSAGES RETURNED. DISPATCHMay 20, 2013 · N280SK · Emb EMB145LR · Rudder Control SystemSDR CHQA20130520172Relay · failedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WAS ABLE TO RESET THE SYSTEM, HOWEVER, THE MESSAGES RETURNED. DISPATCHMay 20, 2013 · N280SK · Emb EMB145LR · Rudder Control SystemSDR CHQA20130520173Relay · failedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WAS ABLE TO RESET THE SYSTEM, HOWEVER, THE MESSAGES RETURNED. DISPATCHMay 20, 2013 · N280SK · Emb EMB145LR · Rudder Control SystemSDR CHQA20130520186Attach Bolt · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FLAP POWER DRIVE UNIT ATTACH POINTS. THE ATTACH POINTS WERE REPAIRED IN ACCORDANCE WITH ETD 2013-145-010207.May 20, 2013 · N561RP · Emb EMB145LR · Trailing Edge FlapsSDR CHQA20130520187Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21 AT FRAME 13. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 51-20-03.May 20, 2013 · N561RP · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR CHQA20130519188Doubler · corrodedDURING INSPECTION, CORROSION WAS FOUND ON A REPAIR DOUBLER ON THE INBOARD SIDE OF THE LEFT OMEGA BEAM AT FRAME 20. THE DOUBLER WAS REPLACED IN ACCORDANCE WITH 53-00-10.May 19, 2013 · N561RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130519189Floor Support · corrodedDURING INSPECTION, A CRACK WAS FOUND ON THE LEFT OUTBOARD OMEGA BEAM SUPPORT BETWEEN FRAMES 47 AND 48. THE OMEGA BEAM SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.May 19, 2013 · N561RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130519190Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM AT THE SCREW HOLE FRAME 23. THE FRAME WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-010149.May 19, 2013 · N561RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130519191Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT. THE SERVICE DOOR CUT OUT WAS REPAIRED IAW SRM 53-21-02.May 19, 2013 · N561RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130517182Angle · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE ANGLE BRACKET AT THE TOP OF FRAME 10 AND THE RIGHT COCKPIT WINDOW SEAL. THE ANGLE WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND SRM 53-12-02.May 17, 2013 · N277SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130516164Generator · failedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A GENERATOR OFF BUSS MESSAGE FROM GENERATORS 1, 3, 4, AND THE APU GENERATOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE GENERATORS DID NOT COME BACK ONLINE. DURING THE RETURN TO FIELD FOR THIS ISSUMay 16, 2013 · N271SK · Emb EMB145LR · DC Generator-AlternatorSDR CHQA20130516165Gcu · failedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A GENERATOR OFF BUSS MESSAGE FROM GENERATORS 1, 3, 4, AND THE APU GENERATOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE GENERATORS DID NOT COME BACK ONLINE. DURING THE RETURN TO FIELD FOR THIS ISSUMay 16, 2013 · N271SK · Emb EMB145LR · AC RegulatorSDR CHQA20130515179Floor Support · damagedDURING INSPECTION, A MISDRILLED HOLE WAS IDENTIFIED ON A REPAIR DOUBLER ON THE RIGHT OMEGA BEAM AT FRAME 23. THE BEAM WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-009615.May 15, 2013 · N277SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130514184Torque Box · damagedDURING INSPECTION, THE LEFT WING LOWER SURFACE MOST INBOARD RIB/FLAP TORQUE BOX FORWARD MOST INBOARD HOLE SHOWS DAMAGE INDICATIONS. THE AREA WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-009827.May 14, 2013 · N277SK · Emb EMB145LR · Trailing Edge FlapsSDR CHQA20130513177Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND UNDER THE COCKPIT FLOOR ON THE SHEAR FOOT AT FRAME 11 AND STRINGER 21L. THE SHEAR FOOT WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-009728.May 13, 2013 · N277SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130513178Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM FRAME 20 REPAIR AT THE CARBON FIBER CROSSMEMBER ATTACH POINT. THE ARE WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-01.May 13, 2013 · N277SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130513180Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 9L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.May 13, 2013 · N277SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130513185Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 66 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.May 13, 2013 · N277SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130511183Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE NUT PLATE ON THE RIGHT OMEGA BEAM AT FRAME 23. THE BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-02 AND ETD 2013-145-009615.May 11, 2013 · N277SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130509163Battery · dischargedDURING INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.May 9, 2013 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20130508166Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM SURFACE AT THE FORWARD NUT PLATE HOLE FOR THE GUSSET AT FRAME 20. THE RIGHT OMEGA BEAM AT FRAME 20 WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-10 AND 51-40-02.May 8, 2013 · N578RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130507145Inverter · inoperativeTHE LEFT EMERGENCY DOOR SIGN WAS REPORTED INOPERATIVE. MAINTENANCE REPLACED THE NUMBER FIVE INVERTER FOR FOR THE LEFT EMERGENCY DOOR SIGN. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.May 7, 2013 · N291SK · Emb EMB145LR · Emergency LightingSDR CHQA20130506167Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SCREW HOLES ON THE SERVICE DOOR LOWER BEAM. THE SERVICE DOOR LOWER BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-02.May 6, 2013 · N578RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130506168Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA INBOARD SIDE AT CARBON CROSSMEMBER AT FRAME 29. THE BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.May 6, 2013 · N578RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130506169Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PREVIOUS REPAIR OF LEFT OMEGA INBOARD SIDE AT FRAME 20. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10 AND 51-40-02.May 6, 2013 · N578RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130506170Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 22 BETWEEN STRINGERS 15L AND 16L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-30-01 AND 51-40-02.May 6, 2013 · N578RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130504144Battery · dischargedDURING INSPECTION, THE LEFT AND RIGHT EXTERNAL OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.May 4, 2013 · N281SK · Emb EMB145LR · Emergency LightingSDR CHQA20130501142Battery · dischargedDURING INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.May 1, 2013 · N279SK · Emb EMB145LR · Emergency LightingSDR CHQA20130427137Fitting · crackedDURING INSPECTION, A CRACKED SHEAR CLIP WAS FOUND AT FRAME 10 UNDER THE RIGHT DIRECT VISION WINDOW. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Apr 27, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130426136Fitting · damagedDURING INSPECTION, FRAME 10 WAS FOUND TO BE ELONGATED AND THE HOLES MISALIGNED ON THE UPPER ATTACH SHEAR CLIP. THE SHEAR CLIP WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-02 AND 53-00-04.Apr 26, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130424127O-Ring · leakingCREW REPORTED THAT THEY RECEIVED A BLEED 2 LEAK MESSAGE ON CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE O-RINGS AT JOINT 20 AND 22. OPERATIONAL AND LEAK CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Apr 24, 2013 · N284SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20130424128O-Ring · leakingCREW REPORTED THAT THEY RECEIVED A BLEED 2 LEAK MESSAGE ON CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE O-RINGS AT JOINT 20 AND 22. OPERATIONAL AND LEAK CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Apr 24, 2013 · N284SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20130424129Battery · dischargedDURING INSPECTION, THE EMERGENCY EXIT PROXIMITY LIGHTS AND THE LOWER EXIT SIGNS ON THE DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Apr 24, 2013 · N571RP · Emb EMB145LR · Emergency LightingSDR CHQA20130424141Floor Support · damagedDURING INSPECTION, A MISDRILLED HOLE IN THE OMEGA BEAM SPLICE AT THE CENTER OMEGA BEAM LEFT SIDE WAS REPORTED. THE FINAL CORRECTIVE ACTION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT.Apr 24, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure
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