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 CHQA20130305084Floor Support · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE LEFT OMEGA BEAM OUTBOARD SUPPORT BETWEEN FRAMES 47 AND 48. THE OMEGA BEAM SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Mar 5, 2013 · N574RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130307085Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 53-31-04.Mar 5, 2013 · N574RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130227067Ils System · erraticCREW REPORTED THAT DURING FLIGHT, BOTH LOCALIZERS BECAME ERRATIC THE CLOSED THE AIRCRAFT GOT TO THE STATION. THE CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE RE-RACKED BOTH NAVIGATIONAL UNITS. OPERATIONAL CHECKS OF BOTH NAVIGATION SYSTEMS WERE GOOFeb 27, 2013 · N579RP · Emb EMB145LR · Localizer/VOR SystemSDR CHQA20130227068Ils System · erraticCREW REPORTED THAT DURING FLIGHT, BOTH LOCALIZERS BECAME ERRATIC, CLOSED THE AIRCRAFT GOT TO THE STATION. THE CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE RE-RACKED BOTH NAVIGATIONAL UNITS. OPERATIONAL CHECKS OF BOTH NAVIGATION SYSTEMS WERE GOOD WFeb 27, 2013 · N579RP · Emb EMB145LR · Localizer/VOR SystemSDR CHQA20130226064Control Unit · faultyCREW REPORTED THAT ON LANDING, WITH THE BRAKES FULLY DEPRESSED, THE BRAKING WAS POOR BELOW 80 KNOTS. THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL AND TAXI CHECKS WERE GOOD WITH NO FURTHER DEFECTSFeb 26, 2013 · N290SK · Emb EMB145LR · Landing Gear Brake SystemSDR CHQA20130226065Dau · faultyCREW REPORTED THAT THERE WAS ELECTRICAL SMOKE SMELL AND HAZE IN THE COCKPIT IN FLIGHT. THE CREW DIVERTED TO KUNV AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE IC-600 NUMBER 1 AND THE DATA ACQUISITION UNIT 1. OPERATIONAL CHECKS WERE GOOD AND NO SMELLFeb 26, 2013 · N294SK · Emb EMB145LR · Central ComputersSDR CHQA20130226066Computer · faultyCREW REPORTED THAT THERE WAS ELECTRICAL SMOKE SMELL AND HAZE IN THE COCKPIT IN FLIGHT. THE CREW DIVERTED TO KUNV AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE IC-600 NUMBER 1 AND THE DATA ACQUISITION UNIT 1. OPERATIONAL CHECKS WERE GOOD AND NO SMELLFeb 26, 2013 · N294SK · Emb EMB145LR · Central ComputersSDR CHQA20130226074Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 7L AND 9L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-41-00 AND SRM 51-43-00.Feb 26, 2013 · N257JQ · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201302225073Floor Support · corrodedDURING INSPECTION, MAINTENANCE FOUND CORROSION ON THE REPAIR DOUBLER ON THE LEFT OMEGA FRAME 20. THE FRAME DOUBLER WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10 AND SRM 51-40-02.Feb 25, 2013 · N257JQ · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130225075Stringer · gougedDURING INSPECTION, A GOUGE WAS FOUND IN STRINGER 2L AFT OF FRAME 20. THE STRINGER WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-003717.Feb 25, 2013 · N257JQ · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR CHQA20130225076Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON SHEAR CLIP AT FRAME 61 BETWEEN STRINGERS 6R AND 7R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND SRM 51-43-03.Feb 25, 2013 · N257JQ · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130224062Transducer · failedCREW REPORTED A NR 1 ENGINE ANTI-ICE VALVE FAIL MESSAGE IN FLIGHT. DIVERTED TO AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE ANTI-ICING PRESSURE TRANSDUCER. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Feb 24, 2013 · N285SK · Emb EMB145LR · Air Intake Anti/De-Ice SystemSDR CHQA20130222061Connector · corrodedCREW REPORTED THAT ON TAKEOFF THEY SELECTED THE CLIMB THRUST RATING AND THE MODE AUTOMATICALLY REVERTED TO T/O THRUST MODE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED CORROSION FROM THE PINS ON RESISTOR MODULES A7055 AND A705Feb 22, 2013 · N266SK · Emb EMB145LR · Engine Control System WiringSDR CHQA20120217063Fitting · crackedDURING INSPECTION, A CRACK IN THE SHEAR CLIP FRAME 25 BETWEEN STRINGER 15R AND 16R WAS NOTED. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Feb 17, 2013 · N293SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130213049Electronic Unit · faultyCREW REPORTED THAT AFTER TAKEOFF, DURING GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR DID NOT SHOW UP AND LOCKED. THE OTHER GEAR HAD GREEN INDICATIONS AND SHOWED UP AND LOCKED. THE CREW ALSO RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE. THEY FOLLOWED THE Feb 14, 2013 · N561RP · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR CHQA20130214050Light · inoperativeDURING INSPECTION, THE FIRST EMERGENCY LIGHT FLOOR PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT PROXIMITY STRIP AT ROWS 1 AND 2. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Feb 14, 2013 · N567RP · Emb EMB145LR · Emergency LightingSDR CHQA20130213051Wire Harness · faultyCREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER ROTATION AND REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS HARNESS. OPERATIONAL Feb 13, 2013 · N272SK · Emb EMB145LR · Landing Gear System WiringSDR CHQA20130212047Battery · dischargedDURING INSPECTION MAINTENANCE FOUND LEFT FUSELAGE FORWARD EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 1 EMERGENCY BATTERY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD AND NO FURTHER DEFECTS WERE NOTED.Feb 12, 2013 · N570RP · Emb EMB145LR · Emergency LightingSDR CHQA20130212048Coupling · brokenCREW REPORTED THEY RECEIVED THE BLEED 1 VALVE FAIL MESSAGE IN FLIGHT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE COUPLING TO TEMPERATURE CONTROL VALVE AND OPERATIONAL CHECKS WEREFeb 12, 2013 · N278SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20130208046Display · inoperativeCREW REPORTED THE PRIMARY FLIGHT DISPLAY NUMBER 1 FAILED IN FLIGHT WITH AN ELECTRICAL ODOR PRESENT IN THE COCKPIT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SWAPPED THE NUMBER 1 PRIMARY FLIGHT DISPLAY WITH NUMBER 2 MULTI-FUNCTION DISPLAY AND Feb 8, 2013 · N276SK · Emb EMB145LR · Central DisplaySDR CHQA20130205045Clamp · looseCREW REPORTED, DURING CLIMBOUT THEY RECEIVED A BLEED 1 LEAK MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE CLEARED. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED, CLEANED, AND REINSTALLED THE V-BAND CLAFeb 5, 2013 · N278SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20130203043Indication Sys · malfunctionedCREW REPORTED THAT DURING FLIGHT THE CABIN PRESSURIZATION INDICATION WAS DASHED. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE AIRCRAFT'S POWER AND THE INDICATIONS RETURNED. AN OPERATIONAL CHECK OF THE PRESSURIZATION SYSTEM WAS Feb 3, 2013 · N277SK · Emb EMB145LR · Cabin Pressure IndicatorSDR CHQA20130202054Skin · chafedDURING INSPECTION, THE PASSENGER DOOR CUTOUT INTERNAL SKIN WAS CHAFED AT THE LOWER HOLE FOR THE LEFT COCKPIT BULKHEAD. THE SKIN WAS REPAIRED IN ACCORDANCE WITH IC2006-145-4495-C.Feb 2, 2013 · N285SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20130202055Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 60 BETWEEN STRINGERS 19R AND 20R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Feb 2, 2013 · N285SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130202056Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE THE SKIN BETWEEN FRAMES 38 AND 39 AND STRINGERS 21R AND 21L. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-002043.Feb 2, 2013 · N285SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20130201040Fuel Filter · dirtyCREW REPORTED THAT THEY RECEIVED AN ENGINE 1 AND ENGINE 2 FUEL IMPENDING BYPASS MESSAGE DURING FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE 1 AND ENGINE 2 FUEL FILTERS. OPERATIONAL CHECKS WERE GOOD WITH NO Feb 1, 2013 · N267SK · Emb EMB145LR · Engine Fuel DistributionSDR CHQA20130201052Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SILL FROM FRAME 23 TO FRAME 29. THE LEFT OUTBOARD SILL AT FROM FRAME 23 TO FRAME 29 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Feb 1, 2013 · N285SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130201053Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SILL FROM FRAME 41 TO FRAME 48. THE RIGHT OUTBOARD SILL FROM FRAME 41 TO FRAME 48 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Feb 1, 2013 · N285SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130128032Light · damagedDURING INSPECTION, THE EMERGENCY LIGHTING STRIP THAT IS FARTHEST AFT WAS FOUND TO HAVE A BROKEN LEAD. THE EMERGENCY FLOOR LIGHT STRIP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jan 28, 2013 · N280SK · Emb EMB145LR · Emergency LightingSDR CHQA20130127031Control Unit · faultyCREW REPORTED THAT ON LANDING THE CAPTAIN'S BRAKES SEEMED TO LOSE PRESSURE FOR APPROXIMATELY ONE SECOND AND THEN WOULD GRAB. THE AIRCRAFT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD Jan 27, 2013 · N272SK · Emb EMB145LR · Landing Gear Brake SystemSDR CHQA20130125035Skin · damagedDURING HEAVY MAINTENANCE, ELONGATED HOLES IN THE EXTERIOR SKIN AT THE SERVICE DOOR THRESHOLD WERE REPAIRED IN ACCORDANCE WITH ETD2013-145-001508.Jan 25, 2013 · N267SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20130120036Window Frame · damagedDURING INSPECTION, THE RIGHT EMERGENCY EXIT HATCH OUTSIDE FRAME WAS FOUND GAUGES AND SHEET METAL DIVIDERS WERE FOUND TO BE PEELED BACK AND BENT. DAMAGED AREA WAS REPAIRED IAW ETD 2013-145-001467-A.Jan 20, 2013 · N267SK · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20130120037Frame · gougedDURING INSPECTION, A GOUGE WAS FOUND IN FRAME 60 BETWEEN STRINGERS 4L AND 5L. THE FRAME WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04 AND SRM 53-00-01.Jan 20, 2013 · N267SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20130119033Floor Support · damagedDURING HEAVY MAINTENANCE, AN ELONGATED HOLE IN THE LEFT OMEGA BEAM AT THE SPLICE BRACKET BETWEEN FRAME 16 AND 17 ON THE LEFT SIDE OF THE BEAM WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-001286B.Jan 19, 2013 · N267SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130119034Floor Support · damagedDURING HEAVY MAINTENANCE, AN ELONGATED HOLE IN THE CENTER OMEGA BEAM AT THE SPLICE BRACKET BETWEEN FRAME 16 AND 17 ON THE LEFT SIDE OF THE BEAM WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-001286B.Jan 19, 2013 · N267SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130118038Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLES ON THE SERVICE DOOR THRESHOLD BEAM. THE THRESHOLD BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Jan 18, 2013 · N267SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130118039Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE GUSSET AT THE CENTER OMEGA FRAME AT SCREW HOLE FRAME 59. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Jan 18, 2013 · N267SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20121217120Unknown · odorCREW REPORTED A FUEL ODOR IN COCKPIT DURING POWER CHANGES. MX PERFORMED ENGINE RUNS AT HIGH POWER AND VARIABLE SETTINGS WITH BOTH PACKS ON AND COULD NOT DUPLICATE ANY FUEL ODOR IN COCKPIT OF CABIN. ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 17, 2012 · N11535 · Emb EMB145LR · Air Distribution SystemSDR CHQA20121112424Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R BETWEEN FRAMES 13 AND 14. THE STRINGER WAS REPLACED.Nov 12, 2012 · N284SK · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR CHQA20121111423Support Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE AILERON TORQUE TUBE SUPPORT BETWEEN STRINGERS 21R AND 20R AT FRAME 12. THE AILERON TORQUE TUBE SUPPORT WAS REPLACED.Nov 11, 2012 · N284SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20121017115Beam · corrodedDURING C CHECK, CARGO LOWER BEAM FRAME 65-68 IS CORRODED. MX R & R CARGO LOWER BEAM BETWEEN FRAME 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 17, 2012 · N14977 · Emb EMB145LR · Fuselage Structure (General)SDR ASOA20121010091Fmu · faultyCREW REPORTED ENGINE NR 2 STARTED SURGING (ERRATIC ACCEL & DECEL) ON DESCENT BETWEEN FL 260& FL250 N1 SPIKE 45-65 ITT SPIKE BETWEEN 400-600. MX R & R ENGINE NR 2 FPMU WITH OPS AND LEAK CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 10, 2012 · N12540 · Emb EMB145LR · Fuel Controlling SystemSDR ASOA20120919139Skin · gougedGOUGE FORWARD OF SERVICE DOOR BETWEEN FRAMES 19A AND 19, STRINGER 12R AND 13R. CUT OUT DAMAGE, FABRICATED AND INSTALLED A FILLER AND DOUBLER IAW ETD2012-145-011864-A. ACFT RELEASED AND RETURNED TO SERVICE.Sep 18, 2012 · N14907 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20120918077Inverter · inoperativeDURING ROUTINE INSPECTION, MX THE FORWARD 3 EMERGENCY AILSE PATH LIGHT STRIPS WERE INOPERATIVE. MX REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.Sep 18, 2012 · N17984 · Emb EMB145 · Emergency LightingSDR ASOA20120915077RFire Detector · malfunctionedCREW REPORTED E1 FIRE DETECTOR FAIL ON EICAS, THREE TIMES DURING ANTI-ICE OPERATION IN CRUISE. MX INSPECTED E1 FIRE DETECTION SYS AND PERFORMED OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Sep 15, 2012 · N17560 · Emb EMB145LR · Smoke DetectionSDR ASOA20120904102Support · corrodedDURING C-CHECK THE TOILET WASTE VALVE SUPPORT WAS FOUND TO BE CORRODED. MX R & R THE SUPPORT ASSY IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Sep 11, 2012 · N12563 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20120907075Unknown · smokeTHE CREW REPORTED AFTER APU START RECEIVED ARUAL WARNING UNIT 1 CHANNEL AND SMOKE BEGAN POURING OUT OF OPENING PLUS ABOVE FMS NR 2. THE ACFT WAS SHUTDOWN AND SMOKE STOPPED. MX INSPECTED AND PERFORMED OPS CHECKS OF BLEED SYS. OPS CHECKS WERE GOOD AND NO SMOKSep 7, 2012 · N16918 · Emb EMB145 · Airborne Auxiliary Power Unit (APU) SystemSDR ASOA20120904119Sign · inoperativeDURING MX INSPECTION THE AFT FACING OVERHEAD EMERGENCY EXIT SIGN AT ROW 12 WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Sep 4, 2012 · N15926 · Emb EMB145EP · Emergency LightingSDR ASOA20120831072Gcu · faultyTHE CREW REPORTED SMOKE IN THE COCKPIT & SPARKS COMING OUT OF APU STARTER GENERATOR APU OUTLET. MAINTENANCE REPLACED THE APU GENERATOR CONTROL UNIT AND REPLACED THE APU STARTER GENERATOR. OPS CHECKS WERE GOOD.Aug 31, 2012 · N11548 · Emb EMB145 · AC Generator-AlternatorSDR ASOA20120830080Seat Track · corrodedDURING C-CHECK PILOT INBD SEAT TRACK BUTTSTRAP CORRODED (LOCAL LEVEL 2). MX PERFORMED REPAIR TO PILOTS INBD BUTTSTRAP IAW EC5310-01623. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Aug 30, 2012 · N16919 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
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