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 ASOA20150821048CFilter · failedTHE CREW REPORTED INFLIGHT NR 1 ENGINE OIL PRESSURE DROPPED BELOW NORMAL OPERATING RANGE. THE CREW SHUTDOWN THE ENGINE IAW QRH PROCEDURE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE OIL FILTER.Aug 21, 2015 · N15574 · Emb EMB145LR · Turbine Engine Oil SystemSDR ASOA20150730041Oil System · leakingCREW REPORTED AN OIL ODOR COMING FROM NR 1 ENGINE BLEED. MAINTENANCE R & R NR 1 ENGINE. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 30, 2015 · N29917 · Emb EMB145LR · Turbine Engine Oil SystemSDR ASOA20150609057Packing · tornTHE CREW REPORTED THAT THE ACFT HAD A VERY STRONG ODOR ASSOCIATED WITH THE PACKS. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, R & R THE NR 1 ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SEJun 9, 2015 · N12924 · Emb EMB145LR · Turbine Engine Oil SystemSDR ASOA20150603019Oil System · leakingACFT WAS FERRIED HERE, BECAUSE OF A SMOKING ENGINE AND ODORS IN CABIN. INSPECTION BOROSCOPE THE ENGINE AND FOUND OIL BUILDING UP BEHIND THE IGV'S. MAINTENANCE R & R THE ENGINE AND OPS CHECK; LEAKS CHECKS WERE GOOD AND WILL BE RELEASED AT THE END OF THESE CHEJun 3, 2015 · N16919 · Emb EMB145LR · Turbine Engine Oil SystemSDR ASOA20150506017Carbon Seal · failedACFT WAS FERRIED DUE TO SMOKE ON SHUTDOWN AND OIL PUDDLE IN THE COWLING. MAINTENANCE R & R ENGINE IAW RR MANUAL 72-00-00. OPS AND LEAK CHECKS WERE PERFORMED AND WILL BE RELEASED AT THE END OF ALL CHECKS.May 6, 2015 · N11547 · Emb EMB145LR · Turbine Engine Oil SystemSDR BUEA20150227001Transducer · failedDURING CLIMB TO FL32, NOTICE A REDUCTION IN AIRSPEED AT FL 30. NOTICED A FLUX IN NR 1 ENG ITT, N1 & N2, 91 TO 88%. PILOT LEVELED OFF AT FL32 & REDUCED POWER SETTING, POWER BACK & NOTICED A LARGER ITT, N1, N2 FLUX. WEATHER WAS VFR CLEAR WITH NO ICING. PILOFeb 25, 2015 · N974RP · Emb EMB145EP · Engine Anti-Icing SystemSDR BUEA20150214001Bearing · failedDURING CLIMB TO FL290, AT ABOUT FL220, SMELLED SMOKE, NOTICED THE ITT RISING & WENT INTO RED. PULLED THE THRUST LEVER BACK AND THE NR 2 ENG OUT POPPED PUT ON THE EICAS. DECLARED AN EMERGENCY & DIVERTED. LANDING UNEVENTFUL. AFTER ENG SHUTDOWN A LOSS OF SIFeb 14, 2015 · N975RP · Emb EMB145MP · Engine (Turbine/Turboprop)SDR UHLA2015012400047Bleed Valve · failedTHE CREW REPORTED THAT THEY RECEIVED A NR 1 BLEED VALVE FAIL MESSAGE AND A STAB ANIT-ICE VALVE FAIL MESSAGE DURING CLIMB OUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE BLEED VALVE. OPS CHECKED GOOD WITHJan 24, 2015 · N575RP · Emb EMB145LR · Compressor Bleed ValveSDR UHLA2014010500001Module · inoperativeTHE CREW REPORTED THAT DURING FLIGHT THE CABIN PRESSURIZATION RATE DASHED. THE CREW DIVERTED THE ACFT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE ACQUISITION MODULE. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jan 5, 2015 · Emb EMB145LR · Cabin Pressure Control SystemSDR 2015F00016Flap System · frozenPILOT ILS APPROACH INTO KLKN COMMANDED FLAPS AT 9 DEGREES AT 230KTS AND RECEIVED AN EICAS MESSAGE FLAP FAIL. PILOT PROCEED WITH ILS APPROACH WITH FLAPS AT 0 DEGREES WITH A TOUCHDOWN AIRSPEED OF 145KTS TO A 12,901 FT RUNWAY. LANDING WAS UNEVENTFUL. NO EMERGENCJan 3, 2015 · N359AD · Emb EMB145EP · Trailing Edge Flap Control SystemSDR CHQA20141229362Switch · faultyTHE CREW REPORTED THAT THEY RECEIVED A BLEED 2 VLV CLOSED MSG IN FLIGHT. THE CREW DIVERTED THE ACFT & LANDED WITHOUT INCIDENT. REPLACED THE BLEED SYS 2 PUSHBUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 29, 2014 · N280SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20141223361Filter · dirtyTHE CREW REPORTED THAT THEY RECEIVED A BLEED 2 OVER TEMP MSG DURING CLIMB. THE CREW UTILIZED THE QRH & RETURNED TO FIELD. THE ACFT LANDED WITHOUT FURTHER INCIDENT. CLEANED THE FAN AIR VLV FILTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 23, 2014 · N567RP · Emb EMB145LR · Pneumatic Distribution SystemSDR ASOA20141222104Module · faultyTHE CREW REPORTED DURING INITIAL CLIMB, CLIMB THRUST COULD NOT BE SET UNLESS FIRST SETTING CRUISE THRUST. MAINTENANCE REPLACED THE THRUST RATING MODULE SWITCH BOX. OPS CHECKS WERE GOOD.Dec 22, 2014 · N29906 · Emb EMB145LR · Engine ControlsSDR ASOA20141221380Engine · failedLOST NR 2 ENGINE IN FLIGHT. R & R NR 2 ENGINE IAW AMM 71-00-00. ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 21, 2014 · N16963 · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA20141213353Skin · crackedDURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 & STRINGER 1R. THE SKIN WAS REPAIRED IAW ETD2014-145-105115.Dec 13, 2014 · N296SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20141212352Fitting · damagedDURING INSPECTION, THE LT AILERON ATTACH FITTING WAS FOUND TO BE DAMAGED. THE AILERON FITTING WAS REPLACED IAW SRM 51-40-02.Dec 12, 2014 · N296SK · Emb EMB145LR · AileronsSDR CHQA20141211354Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & STRINGER 15R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211355Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 26 & STRINGER 15R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211356Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 25 & STRINGER 15R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211357Beam · corrodedDURING INSPECTION, THE LT BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE BEAM WAS REPAIRED IAW SRM 51-20-03 & SRM 51-23-04.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211358Angle · corrodedDURING INSPECTION, THE LT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. THE ANGLE WAS REPLACED IAW SRM 51-40-02.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211359Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 46 BELOW THE FLOOR SILL WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211360Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CTR BEAM FLOOR FLANGE AT FRAME 23. THE BEAM WAS REPAIRED IAW SRM 53-00-10.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141209351Seal · dirtyTHE CREW REPORTED THAT DURING FLIGHT THE CAPTAIN'S DIRECT VISION WINDOW WAS LEAKING. THE ACFT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. INSPECTED THE WINDOW & CLEANED THE WINDOW SEAL. PRESSURIZATION CHECKS WERE GOOD WITH NO LEAKS NOTED.Dec 9, 2014 · N287SK · Emb EMB145LR · Flight Compartment WindowsSDR CHQA20141203344Profile · corrodedDURING INSPECTION, THE PAX DOOR U PROFILE WAS FOUND TO BE CORRODED. THE PROFILE WAS REPLACED IAW SRM 51-40-02.Dec 3, 2014 · N562RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20141203350Profile · puncturedDURING INSPECTION, PUNCTURE DAMAGE WAS FOUND ON THE PAX DOOR U LATERAL PROFILE. THE PROFILE WAS REPLACED IAW SRM 51-40-02.Dec 3, 2014 · N562RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20141202349Step · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PAX DOOR ON THE NR 1 STEP. THE NR 1 PAX DOOR STEP WAS REPLACED IAW SRM 51-21-02.Dec 2, 2014 · N562RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20141201342Pressure Switch · faultyTHE CREW REPORTED THAT ON CLIMB OUT, THEY RECEIVED A RUDDER OVER BOOST MSG. THE CREW RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE RUDDER SYS 1 PRESS SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 1, 2014 · N271SK · Emb EMB145LR · Rudder Control SystemSDR CHQA20141201343Service Door · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE BOTTOM OF THE SERVICE DOOR. THE SERVICE DOOR WAS REPAIRED IAW ETD 2014-145-101279.Dec 1, 2014 · N562RP · Emb EMB145LR · Service DoorsSDR CHQA20141130345Support · crackedDURING INSPECTION, THE RT OMEGA BEAM INBD SUPPORT WAS FOUND TO BE CRACKED AT FRAMES 47 & 48. THE SUPPORT WAS REPLACED IAW SRM 53-23-02.Nov 30, 2014 · N562RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141130346Floor Support · corrodedDURING INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE BEAM WAS REPLACED IAW SRM 51-40-02 & SRM 53-00-10.Nov 30, 2014 · N562RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141130347Door Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR FLOOR SILL AT FRAME 66. THE CARGO DOOR SILL WAS REPLACED IAW SRM 51-40-02.Nov 30, 2014 · N562RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141130348Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND AT SHEAR CLIP AT FRAME 65. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Nov 30, 2014 · N562RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141122330Light · inoperativeDURING INSPECTION, THE OVERWING EMER EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 22, 2014 · N269SK · Emb EMB145LR · Emergency LightingSDR CHQA20141121329Light · inoperativeDURING INSPECTION, THE EMER FLOOR PROXIMITY LIGHT STRIP AT ROW 8 WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 21, 2014 · N370SK · Emb EMB145LR · Emergency LightingSDR CHQA20141121331Switch · faultyTHE CREW REPORTED THAT THE GUST LOCK LIGHT CAME ON IN CRUISE FLIGHT. THE CREW DECLARED AN EMER & LANDED WITHOUT INCIDENT AT ITS INTENDED DESTINATION. THE GUST LOCK SYS WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 11/22/2014 WHEN MX REPLACED MICRO SWITCH S0658.Nov 21, 2014 · N563RP · Emb EMB145LR · Gust Lock Damper SystemSDR CHQA20141119328Light · inoperativeDURING INSPECTION, THE EMER FLOOR PROXIMITY LIGHT STRIP AT ROW 6 WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 19, 2014 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20141119334Structure · dentedDURING INSPECTION, A DENT WAS FOUND BETWEEN FRAME 19 & 20 & STRINGERS 19R & 20R. THE DENT WAS REPAIRED IAW SRM 53-21-01.Nov 19, 2014 · N290SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141119337Elevator · crackedDURING INSPECTION, THE LT ELEVATOR WAS FOUND TO BE CRACKED. THE ELEVATOR WAS REPAIRED IAW ETD 2014-145-097861.Nov 19, 2014 · N290SK · Emb EMB145LR · Elevator StructureSDR CHQA20141115335Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE ANGLE BRACKET IN THE RT WHEEL AREA AFT SIDE. THE PROFILE WAS REPLACED IAW SRM 51-40-02.Nov 15, 2014 · N290SK · Emb EMB145LR · Wing Miscellaneous StructureSDR CHQA20141114332Floor Support · corrodedDURING INSPECTION, THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED ON A PREVIOUS REPAIR AT FRAMES 20 & 22. THE CTR OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.Nov 14, 2014 · N290SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141114338Skin · crackedDURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 ABOVE STRINGER 2L. THE STRINGER WAS REPLACED IAW SRM 51-40-02.Nov 14, 2014 · N290SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20141114339Skin · crackedDURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BELOW STRINGER 2L. THE STRINGER WAS REPAIRED IAW ETD 2014-145-096626.Nov 14, 2014 · N290SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20141114341Floor Support · corrodedDURING INSPECTION, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59 & 61. THE BEAM WAS REPAIRED IAW ETD 2014-145-096615.Nov 14, 2014 · N290SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141113333Door Sill · corrodedDURING INSPECTION, THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED IAW SRM 51-40-02.Nov 13, 2014 · N290SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141113336Floorbeam · corrodedDURING INSPECTION, THE LT FLOORBEAM WAS FOUND TO BE CORRODED ON A PREVIOUS REPAIR AT FRAME 20. THE BEAM WAS REPAIRED IAW SRM 53-00-10.Nov 13, 2014 · N290SK · Emb EMB145LR · Fuselage Main, Floor BeamSDR CHQA20141113340Floor Support · corrodedDURING INSPECTION, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 53. THE BEAM WAS REPAIRED IAW SRM 51-40-02.Nov 13, 2014 · N290SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141109321Connector · disconnectedRECEIVED A LANDING GEAR AIR & GND FAIL MSG AFTER TAKEOFF. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. REINSTALLED THE CONNECTOR ON THE LT MLG WEIGHT ON WHEELS SYS. OPERATIONAL CHECKS & LG SWINGS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 9, 2014 · N579RP · Emb EMB145LR · Landing Gear System WiringSDR CHQA20141104320Ballast · damagedBURNING SMELL NEAR ROW 3C. REPLACED THE FWD GALLEY CEILING LIGHT BALLAST. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECT NOTED.Nov 4, 2014 · N270SK · Emb EMB145LR · Passenger Compartment LightingSDR CHQA20141103312Light · inoperativeDURING INSPECTION THE FLOOR EMER PROXIMITY LIGHT STRIP AT ROW 7 WAS FOUND TO BE INOPERATIVE. REPLACED THE EMER LIGHT FLOOR STRIP AT ROW 7. OPERATIONAL CHECKS GOOD WITH NO FURTHER DEFECTS NOTED.Nov 3, 2014 · N274SK · Emb EMB145LR · Emergency Lighting
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