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 CHQA20131125439Anti-Ice Valve · failedCREW REPORTED THAT DURING CLIMB THEY RECEIVED A WING ANTI-ICE FAIL MESSAGE. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX REPLACED THE WING 2 ANTI-ICE VLV. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Nov 25, 2013 · N259JQ · Emb EMB145LR · Airfoil Anti/De-ice SystemSDR CHQA20131124435Seat Track · corrodedRIGHT SIDEWALL TRACK MOUNTING FLANGE AT FRAME 42 - 48 WAS FOUND TO BE CORRODED. THE SEAT TRACK MOUNTING FLANGE WAS REPLACED IAW SRM 51-40-02.Nov 24, 2013 · N562RP · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20131124436Seat Track · corrodedLEFT OTBD SEAT TRACK BEAM AT THE OVERWING EXIT WAS FOUND TO BE CORRODED. THE SEAT TRACK BEAM WAS REPLACED IAW SRM 51-40-02.Nov 24, 2013 · N562RP · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20131123428Battery · dischargedMULTIPLE EMERGENCY FLOOR STRIP LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NUMBER TWO EMERGENCY BATTERY & ALL OPERATIONS CHECKED GOOD.Nov 23, 2013 · N290SK · Emb EMB145LR · Emergency LightingSDR CHQA20131121437Controller · erraticCREW REPORTED THAT THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT IN THE AUTO PRESSURIZATION MODE. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. THE AUTO PRESSURIZATION FUNCTION WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 11/21/2013 WHEN MX REPLACED THE Nov 21, 2013 · N272SK · Emb EMB145LR · Cabin Pressure ControllerSDR CHQA20131118430Fitting · crackedCRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 25 BETWEEN STRINGERS 15R & 16R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Nov 18, 2013 · N281SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131118431Fitting · crackedCRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 16R & 15R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Nov 18, 2013 · N281SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131114410Icu · faultyCREW REPORTED THAT AFTER TAKEOFF BOTH RADIO MANAGEMENT UNITS SHOWED DASHES IN THE TRANSPONDER AND TCAS FIELDS. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 INTEGRATED COMMUNICATIONS UNIT. OPS CHECKS WERE GOOD WITH Nov 14, 2013 · N272SK · Emb EMB145LR · VHF Communications SystemSDR CHQA20131108409Velocity Sensor · out of toleranceCREW REPORTED A FLAP FAIL MESSAGE ON APPROACH. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT AT DESTINATION. MAINTENANCE RESET FLAP SYSTEM AND NO DEFECTS WERE NOTED. MAINTENANCE REPLACED THE RT VELOCITY SENSOR. OPS CHECKED GOOD WITH NO FURTHER DEFECTS Nov 8, 2013 · N257JQ · Emb EMB145LR · Trailing Edge Flap Control SystemSDR CHQA20131108412Beam · damagedDURING INSPECTION, DAMAGE WAS FOUND ON THE ATTACHING BEAM NUTPLATE OF THE FRAME SILL AT FRAME 64. THE DAMAGE WAS REPAIRED IAW ETD 2013-145-057468.Nov 8, 2013 · N570RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131107423Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21L BETWEEN FRAME 12 & FRAME 13. THE STRINGER WAS REPLACED IAW SRM 51-40-02.Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR CHQA20131106411Support · crackedDURING INSPECTION, THE RT OTBD OMEGA BEAM SUPPORT WAS FOUND TO BE CRACKED. THE OMEGA BEAM SUPPORT WAS REPLACED IAW SRM 51-40-02.Nov 6, 2013 · N570RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131106413Stop Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR STOP INTERNAL BACKUP STRUCTURE ON THE FWD LOWER STOP. THE STOP WAS REPLACED IAW SRM 51-40-02.Nov 6, 2013 · N570RP · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20131106414Support · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE PAX DOOR FRAME AT THE FWD CTR STEP RAIL SUPPORT. THE SUPPORT WAS REPLACED IAW SRM 51-40-02.Nov 6, 2013 · N570RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131106415Sill · corrodedDURING INSPECTION, THE SERVICE DOOR SILL WAS FOUND TO HAVE CORROSION AT THE FWD SCREW HOLE. THE SILL WAS REPLACED IAW SRM 51-40-02.Nov 6, 2013 · N570RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131106416Floor Support · corrodedDURING INSPECTION, THE RT OMEGA BEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAME 23 & FRAME 24. THE BEAM WAS REPAIRED IAW ETD 2013-145-057444.Nov 6, 2013 · N570RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131106417Stop Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE PAX DOOR FRAME AT THE FWD STOP SECOND FROM THE TOP. THE STOP WAS REPLACED IAW SRM 51-40-02.Nov 6, 2013 · N570RP · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20131105382Light · inoperativeDURING INSPECTION, THE LT FLOOR PROXIMITY LIGHTS AT ROWS 15 THROUGH 17 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR PROXIMITY STRIP LIGHT AND OPS CHECKED GOOD.Nov 5, 2013 · N286SK · Emb EMB145LR · Emergency LightingSDR CHQA20131104380Battery · inoperativeDURING INSPECTION, OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND ALL OPERATIONAL CHECKS WERE GOOD.Nov 4, 2013 · N272SK · Emb EMB145LR · Emergency LightingSDR CHQA20131104381Battery · inoperativeDURING INSPECTION, FORWARD WING TO FUSELAGE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND OPS CHECKED GOOD.Nov 4, 2013 · N272SK · Emb EMB145LR · Emergency LightingSDR CHQA20131028392Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 20.THE BEAM WAS REPAIRED IAW ETD 2013-145-05335.Oct 28, 2013 · N568RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131023393Attach Angle · crackedDURING INSPECTION, THE LT OMEGA BEAM ATTACH FLANGE TO RIB 3 WAS FOUND TO BE CRACKED AT FRAME 47 AND 48. THE ATTACH FLANGE AT FRAME 47 AND 48 WAS REPLACED IAW SRM 51-40-02.Oct 28, 2013 · N568RP · Emb EMB145LR · Fuselage Main, Attach FittingsSDR CHQA20131023394Attach Angle · crackedDURING INSPECTION, THE LT OMEGA BEAM ATTACH FLANGE TO RIB 3 WAS FOUND TO BE CRACKED AT FRAME 47 AND 48. THE ATTACH FLANGE AT FRAME 47 AND 48 WAS REPLACED IAW SRM 51-40-02.Oct 28, 2013 · N568RP · Emb EMB145LR · Fuselage Main, Attach FittingsSDR CHQA20131025379Bleed Valve · faultyCREW REPORTED THAT THEY RECEIVED A BLEED ONE VALVE CLOSED MESSAGE AFTER TAKEOFF. FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE BLEED SYSTEM 1 VALVE. OPS CHECKED WERE GOOD WITH NO FURTHER DEFECTOct 25, 2013 · N284SK · Emb EMB145LR · Compressor Bleed ValveSDR CHQA20131025384Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SKIN SPLICE AT FRAMES 60 BETWEEN STRINGERS 20 - 21R. THE SPLICE WAS REPAIRED IAW ETD 2013-145-052936.Oct 25, 2013 · N568RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20131025389Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND AROUND THE LAVATORY DUMP CHUTE ON THE EXTERNAL SIDE. THE LAVATORY DUMP CHUTE CUP AND ZEE PROFILE WERE REPLACED IAW SRM 51-20-01.Oct 25, 2013 · N568RP · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20131025390Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND AROUND THE LAVATORY DUMP CHUTE ON THE EXTERNAL SIDE. THE LAVATORY DUMP CHUTE CUP AND ZEE PROFILE WERE REPLACED IAW SRM 51-20-01.Oct 25, 2013 · N568RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131025391Shear Plate · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LATERAL L-SHAPE AT THE BOTTOM OF FRAME 65. THE LATERAL L-SHAPE AT FRAME 65 WAS REPLACED IAW SRM 53-31-04.Oct 25, 2013 · N568RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131024383Structure · corrodedDURING INSPECTION, THE SERVICE DOOR LINER ATTACH POINTS AT THE BOTTOM EDGE OF THE DOOR WERE FOUND TO BE CORRODED. CORROSION REMOVED IAW ETD 2013-145-052907.Oct 24, 2013 · N568RP · Emb EMB145LR · Service DoorsSDR CHQA20131024385Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR TIE AT FRAME 24 BETWEEN STRINGERS 15 - 16R. SHEAR TIE REPLACED IAW SRM 51-40-02.Oct 24, 2013 · N568RP · Emb EMB145LR · Fuselage Internal Mounting StructureSDR CHQA20131024386Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 25 BETWEEN STRINGERS 15-16R. SHEAR TIE REPLACED IAW SRM 51-40-02.Oct 24, 2013 · N568RP · Emb EMB145LR · Fuselage Internal Mounting StructureSDR CHQA20131024387Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 26 BETWEEN STRINGERS 15-16R. THE SHEAR TIE WAS REPLACED IAW ETD 2013-145-04543.Oct 24, 2013 · N568RP · Emb EMB145LR · Fuselage Internal Mounting StructureSDR CHQA20131024388Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER AT THE CARBON CROSSMEMBER LT OMEGA FRAME 20. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10.Oct 24, 2013 · N568RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131024397Shear Tie · corrodedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 68 BETWEEN STINGERS 6L AND 7L. THE SHEAR TIE WAS REPLACED IAW SRM 53-31-04.Oct 24, 2013 · N568RP · Emb EMB145LR · Fuselage Internal Mounting StructureSDR CHQA20131024398Shear Tie · corrodedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 68 BETWEEN STINGERS 6L AND 7L. THE SHEAR TIE WAS REPLACED IAW SRM 53-31-04.Oct 24, 2013 · N568RP · Emb EMB145LR · Fuselage Internal Mounting StructureSDR CHQA20131024399Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 67 BETWEEN STRINGERS 6L AND 7L. THE SHEAR TIE WAS REPLACED IAW SRM 51-40-02.Oct 24, 2013 · N568RP · Emb EMB145LR · Fuselage Internal Mounting StructureSDR CHQA20131023395Attach Angle · corrodedDURING INSPECTION, THE RT OMEGA BEAM ATTACH FLANGE TO RIB 3 WAS FOUND TO BE CRACKED AT FRAME 47 AND 48. THE ATTACH FLANGE AT FRAME 47 AND 48 WAS REPLACED IAW SRM 51-40-02.Oct 23, 2013 · N568RP · Emb EMB145LR · Fuselage Main, Attach FittingsSDR CHQA20131023396Attach Angle · crackedDURING INSPECTION, THE RT OMEGA BEAM ATTACH FLANGE TO RIB 3 WAS FOUND TO BE CRACKED AT FRAME 47 AND 48. THE ATTACH FLANGE AT FRAME 47 AND 48 WAS REPLACED IAW SRM 51-40-02.Oct 23, 2013 · N568RP · Emb EMB145LR · Fuselage Main, Attach FittingsSDR CHQA20131019376Light · inoperativeDURING INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE RT OVERWING LIGHT ASSEMBLY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Oct 19, 2013 · N296SK · Emb EMB145LR · Emergency LightingSDR CHQA20131018373Unknown · odorCREW REPORTED THAT THERE WAS A BURNING ODOR IN THE CABIN, DURING FLIGHT AROUND ROW 5. CREW TURNED BOTH PACK SYSTEMS AND THE RECIRCULATION FAN OFF AND THE ODOR DISSIPATED. THE FLIGHT LANDED NORMALLY WITHOUT INCIDENT. MAINTENANCE INSPECTED ALL LIGHTING BALLAOct 18, 2013 · N373SK · Emb EMB135KL · Air Distribution SystemSDR CHQA20131018374Wire · damagedDURING INSPECTION, SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A WIRE TO THE EMERGENCY LIGHT. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 18, 2013 · N292SK · Emb EMB145LR · Light System WiringSDR CHQA20131018375Wire · damagedDURING INSPECTION, THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A WIRE TO THE EMERGENCY LIGHT. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 18, 2013 · N292SK · Emb EMB145LR · Light System WiringSDR CHQA20131017372Light · inoperativeDURING INSPECTION, AFT EMERGENCY LIGHT AND FORWARD EMERGENCY EXIT SIGN FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE GALLEY CEILING PANEL. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Oct 17, 2013 · N267SK · Emb EMB145LR · Emergency LightingSDR CHQA20131016370Duct · disconnectedCREW REPORTED THAT DURING CLIMB THERE WAS SMOKE IN THE CABIN AROUND SEAT 9A. DECLARED AND EMERGENCY AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AIR CONDITIONING DUCT DISCONNECTED AND PRODUCING CONDENSATION INSIDE CABIN. DUCT RECONNECTEOct 16, 2013 · N266SK · Emb EMB145LR · Air Distribution SystemSDR CHQA20131016371Switch · faultyCREW REPORTED THAT THEY RECEIVED A "BLEED 2 VALVE CLOSED" MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED SYSTEM 2 PUSH BUTTON. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 16, 2013 · N276SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20131013369A/C Pack · failedCREW REPORTED THAT DURING CRUISE, SMOKE WAS NOTICED IN THE COCKPIT. THE CREW DIVERTED AND DECLARED AN EMERGENCY. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ISOLATED THE ISSUE TO THE PACK 1 SYSTEM. THE PACK 1 SYSTEM WAS DEFERRED. ACM ON THE PACKOct 13, 2013 · N268SK · Emb EMB145LR · Cabin Cooling SystemSDR CHQA20131010377Frame · bentDURING INSPECTION, FRAME 72 WAS FOUND TO BE BENT BETWEEN STRINGERS 15R AND 16R. THE FRAME WAS REPAIRED IAW ETD 2013-145-048739.Oct 10, 2013 · N283SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20131010378Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR TIE AT FRAME 73 BETWEEN STINGERS 7 & 9R. THE SHEAR TIE WAS REPLACED IAW SRM 51-40-02.Oct 10, 2013 · N283SK · Emb EMB145LR · Fuselage Internal Mounting StructureSDR CHQA20131009367Line · cutCREW REPORTED THAT THEY RECEIVED A HYD SYS LOW QUANTITY MESSAGE FOLLOWED BY AN ENGINE 1 HYD PUMP FAIL MESSAGE ON DESCENT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PRESSURE LINE ON THE NR 1 HYD PUMP. OPS AND Oct 9, 2013 · N565RP · Emb EMB145LR · Hydraulic System, MainSDR CHQA20131009368Wire · brokenDURING INSPECTION, THE EMERGENCY LIGHT ON THE MAIN ENTRY DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND ALL OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 9, 2013 · N571RP · Emb EMB145LR · Light System Wiring
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