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 CHQA20140625228Fitting · 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.Jun 25, 2014 · N571RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140625229Fitting · 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.Jun 25, 2014 · N571RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140625231Skin · crackedDURING INSPECTION, THE EXTERNAL FUSELAGE SKIN WAS FOUND TO BE CRACKED BELOW STRINGER 2L & FRAME 75. THE SKIN WAS REPAIRED IAW ETD 2014-145-056101.Jun 25, 2014 · N571RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20140625233Stringer · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE DOOR STRUCTURE AT Z 5225.5, STRINGER 6L & BENEATH DOOR STOP 10. THE STRINGER WAS REPLACED IAW SRM 51-40-02.Jun 25, 2014 · N571RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140624194Tire · separatedCREW REPORTED DURING TAKEOFF THERE WAS A VIBRATION IN THE ACFT. ATC REPORTED THAT THE ACFT HAS LT TIRE DEBRIS ON THE RUNWAY. THE CREW DECLARED AN EMER & RETURNED TO FIELD. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MX PERFORMED A TREAD SEPARATION INSPECTIONJun 24, 2014 · N294SK · Emb EMB145LR · TireSDR CHQA20140625230Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 20. THE LT OMEGA BEAM WAS REPAIRED IAW SRM 53-00-10 & SRM 51-40-02.Jun 24, 2014 · N571RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140621190Solenoid Valve · failedCREW REPORTED THAT THERE WAS A LOUD NOISE IN COCKPIT DURING FLIGHT. THE CREW SUSPECTED THAT THE NLG DOORS WERE OPEN. THE ACFT WAS RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE NLG DOOR SOLENOID VLV. OPERATIONAL & LEAK CHECKS WERE GOOJun 21, 2014 · N268SK · Emb EMB145LR · Landing Gear Door Retract SectionSDR CHQA2014612188Light · inoperativeDURING INSPECTION, THE EMER FLOOR LIGHTING LOCATED NEAR THE GALLEY FLOOR WAS FOUND TO BE INOPERATIVE. MX REPLACED THE GALLEY FLOOR LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jun 17, 2014 · N270SK · Emb EMB145LR · Emergency LightingSDR CHQA20140612188Light · inoperativeDURING INSPECTION, THE EMER FLOOR LIGHTING NEAR ROW 2A WAS FOUND TO BE INOPERATIVE. THE LIGHTING IS CURRENTLY ON DEFERRAL & THE FINAL CORRECTIVE ACTION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT.Jun 12, 2014 · N273SK · Emb EMB145LR · Emergency LightingSDR CHQA20140612196Threshold · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR THRESHOLD AT FRAME 66. THE CARGO DOOR THRESHOLD WAS REPLACE IAW SRM 51-40-02.Jun 12, 2014 · N576RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140612197Skin · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT FRAME 75 & STRINGER 2L. THE SKIN WAS REPAIRED IAW ETD 2014-145-049612.Jun 12, 2014 · N576RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20140612198Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FRAME 64 BETWEEN STINGERS 15L & 16L. THE FRAME WAS REPAIRED IAW SRM 51-40-02.Jun 12, 2014 · N576RP · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20140612199Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP & T FITTING AT FRAME 65 BETWEEN STINGERS 15L & 16L. THE SHEAR CLIP & T FITTING WERE REPLACED IAW SRM 51-40-02.Jun 12, 2014 · N576RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140612200Tee Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP & T FITTING AT FRAME 65 BETWEEN STINGERS 15L & 16L. THE SHEAR CLIP & T FITTING WERE REPLACED IAW SRM 51-40-02.Jun 12, 2014 · N576RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140612201Skin · crackedDURING HEAVY MX, A CRACK IN THE FUSELAGE SKIN AT FRAME 75 WAS REPAIRED IAW ETD 2014-145-049612.Jun 12, 2014 · N576RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20140611202Skin · gougedDURING INSPECTION, A GOUGE WAS FOUND ON THE RUDDER 1 EXTERIOR SKIN ON THE RT SIDE. RUDDER 1 WAS REPAIRED IAW ETD 2014-145-051285.Jun 11, 2014 · N576RP · Emb EMB145LR · Rudder, Plate/SkinSDR CHQA20140608187Flapper Valve · brokenCREW REPORTED THAT THE AUTO PRESSURIZATION SYS WAS INOPERATIVE DURING FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX FOUND THE MANUAL PRESSURIZATION SYS TO BE WORKING & DEFERRED THE AUTO PRESSURIZATION. THE DEFERRAL WAS CLEARED ON 6/11/14 Jun 8, 2014 · N272SK · Emb EMB145LR · Cabin Pressure Control SystemSDR CHQA20140602180Fuel Filter · cloggedCREW REPORTED THAT THEY RECEIVED AN ENG 1 & 2 FUEL IMPENDING BYPASS MSG IN FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE ENG 1 & 2 FUEL FILTERS. ENG RUNS WERE GOOD & NO FURTHER DEFECTS WERE NOTED.Jun 2, 2014 · N378SK · Emb EMB135KL · Engine Fuel DistributionSDR CHQA20140602182Tire · separatedCREW REPORTED THAT THEY RECEIVED A MSG ATC THAT THE RT INBD TIRE HAD SEPARATED ON TAKEOFF. A FLYBY OF THE TOWER AT THEIR INTENDED DESTINATION CONFIRMED THE TIRE FAILURE. THE CREW DECLARED AN EMER. THE ACFT LANDED AT ITS INTENDED DESTINATION WITHOUT FURTHER Jun 2, 2014 · N273SK · Emb EMB145LR · TireSDR CHQA20140602183Flap · damagedCREW REPORTED THAT THEY RECEIVED A MSG FROM ATC THAT THE RT INBD TIRE HAD SEPARATED ON TAKEOFF. A FLYBY OF THE TOWER AT THEIR INTENDED DESTINATION CONFIRMED THE TIRE FAILURE. THE CREW DECLARED AN EMER. THE ACFT LANDED AT ITS INTENDED DESTINATION WITHOUT FURJun 2, 2014 · N273SK · Emb EMB145LR · Trailing Edge FlapsSDR CHQA20140602184Control Unit · faultyCREW REPORTED THAT THEY RECEIVED A BRAKE OTBD INOPERATIVE CAUTION MSG WHEN THE LG WAS SELECTED DOWN. THE CREW DECLARED AN EMER. THE ACFT LANDED WITHOUT INCIDENT & SAFETY CREWS INSPECTED THE BRAKE & FOUND THE ACFT SAFE TO TAXI TO THE GATE UNDER ITS OWN POWER. Jun 2, 2014 · N562RP · Emb EMB145LR · Landing Gear Brake SystemSDR CHQA20140601177Light · damagedDURING INSPECTION, THE RT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE DAMAGED. MX REPLACED THE RT OVERWING EMERGENCY LIGHT HOUSING ASSEMBLY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jun 1, 2014 · N290SK · Emb EMB145LR · Emergency LightingSDR CHQA20140601178Battery · dischargedDURING INSPECTION, THE NR 4 EMER LIGHT BATTERY WAS REPORTED TO BE INOPERATIVE. MX REPLACED THE NR 4 EMER LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jun 1, 2014 · N290SK · Emb EMB145LR · Emergency LightingSDR CHQA20140527195Door · dentedDURING HEAVY MX, A DENT ON THE BAGGAGE DOOR ABOVE THE VENT FLAP WAS REPAIRED IAW ETD2012-145-014619-A.May 27, 2014 · N576RP · Emb EMB145LR · Cargo/Baggage DoorsSDR CHQA20140526175Light · inoperativeDURING INSPECTION, THE RT AFT WING EMER LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE LIGHT BULB. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.May 26, 2014 · N270SK · Emb EMB145LR · Emergency LightingSDR CHQA20140523153Battery · dischargedDURING INSPECTION, THE EMERGENCY EXIT MARKING SIGN WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.May 23, 2014 · N293SK · Emb EMB145LR · Emergency LightingSDR CHQA20140518151Battery · dischargedDURING INSPECTION, THE OVERHEAD MAIN ENTRY DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 1 EMERGENCY LIGHT BATTERY & ALL OPERATIONAL CHECKED GOOD.May 18, 2014 · N273SK · Emb EMB145LR · Emergency LightingSDR CHQA20140515158Floor Support · corrodedDURING INSPECTION, THE CTR OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. THE FRAME WAS REPAIRED IAW SRM 51-40-02.May 15, 2014 · N561RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140514157Frame · crackedDURING INSPECTION, FRAME 23 AT STRINGER 15L WAS FOUND TO BE CRACKED. FRAME 23 WAS REPAIRED IAW SRM 53-00-04.May 14, 2014 · N561RP · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20140514162Floor Support · corrodedDURING INSPECTION, THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 & 60. THE BEAM WAS REPAIRED IAW ETD 2014-145-040625.May 14, 2014 · N561RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140514173Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 20. THE FRAME WAS REPLACED IAW SRM 53-0010 & SRM 51-40-02.May 14, 2014 · N561RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140512156Hinge Fitting · damagedDURING INSPECTION, THE RT AILERON OTBD HINGE ATTACH FITTING ON THE AILERON HAT BUSHING WAS FOUND TO BE MIGRATED & THE INBD SIDE HOLE ELONGATED. THE RT AILERON OTBD HINGE FITTING WAS REPLACED IAW SRM 51-40-02.May 12, 2014 · N561RP · Emb EMB145LR · AileronsSDR CHQA20140512159Fitting · gougedDURING INSPECTION, THE LT AILERON DAMPNER ROD END FITTING WAS FOUND TO BE GOUGED ON THE INBD SIDE. THE LT AILERON DAMPNER ROD END FITTING WAS REPLACED IAW SRM 51-60-02.May 12, 2014 · N561RP · Emb EMB145LR · AileronsSDR CHQA20150512160Fitting · damagedDURING INSPECTION, THE RT AILERON DAMPER ROD END ATTACH FITTING WAS ON THE AILERON INBD HAT BUSHING WAS FOUND TO BE MIGRATED OUT. THE FITTING WAS REPLACED IAW SRM 51-40-02.May 12, 2014 · N561RP · Emb EMB145LR · AileronsSDR CHQA20140512161Fitting · damagedDURING INSPECTION, THE LT AILERON PCA ROD END ATTACH FITTING ON THE AILERON OTBD ROD INBD HAT BUSHING WAS FOUND TO BE MIGRATED OUTWARD. THE LT AILERON PCA ROD END ATTACH FITTING WAS REPLACED IAW SRM 51-40-02, 51-20-03 & CPM 51-21-04.May 12, 2014 · N561RP · Emb EMB145LR · AileronsSDR CHQA20140511145Light · brokenDURING INSPECTION, THE EMERGENCY FLOOR LIGHT STRIP AT ROW 10A WAS FOUND TO BE BROKEN. THE FLOOR STRIP WAS REPAIRED & ALL OPERATIONAL CHECKS WERE GOOD.May 11, 2014 · N976RP · Emb EMB145MP · Emergency LightingSDR CHQA20140511147Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER AIRSTAIR DOOR SKIN. THE DOOR WAS REPAIRED IAW ETD2014-145-039320.May 11, 2014 · N575RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140510155Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 28 BETWEEN STRINGERS 15R & 16R WERE FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.May 10, 2014 · N561RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140510163Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 15L. THE FRAME PROFILE WAS REPLACED IAW SRM 51-40-02.May 10, 2014 · N561RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140510164Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & MID FRAME AT STRINGER 14L. THE FRAME PROFILE WAS REPLACED IAW SRM 51-40-02.May 10, 2014 · N561RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140510165Rib · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 12L. THE Z RIB & L ANGLE WERE REPLACED IAW SRM 51-40-02.May 10, 2014 · N561RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140510166Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 12L. THE Z RIB & L ANGLE WERE REPLACED IAW SRM 51-40-02.May 10, 2014 · N561RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140510168Floor Support · corrodedDURING INSPECTION, THE LT OMEGA BEAM CTR FLOOR FLANGE WAS FOUND TO BE CORRODED AT FRAME 24 & FRAME 25. THE BEAM WAS REPAIRED IAW SRM 53-00-10 & 51-40-02.May 10, 2014 · N561RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140510174Floor Support · corrodedDURING INSPECTION, THE RT OMEGA BEAM REPAIR AT FRAME 23 HAS CORROSION. THE REPAIR DOUBLER WAS REPLACED IAW ETD 2014-145-041404.May 10, 2014 · N561RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140509154Nut Plate · corrodedDURING INSPECTION, MULTIPLE AREAS OF CORROSION WERE FOUND ON THE NUTPLATE HOLES IN THE AFT FRAME OF THE MAIN ENTRY DOOR. THE NUTPLATE WAS REPAIRED IAW ETD 2014-145-040679.May 9, 2014 · N561RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140509167Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE STRUCTURE OF THE MAIN ENTRY DOOR AT THE AFT FRAME AT STRINGER 12L. THE FRAME PROFILE WAS REPLACED IAW SRM 51-40-02.May 9, 2014 · N561RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140509169Door Frame · corrodedDURING INSPECTION, THE MAIN ENTRY DOOR STRUCTURE AT THE MID AFT FRAME & STRINGER 14 WAS FOUND TO BE CORRODED. THE MID AFT FRAME WAS REPLACED IAW SRM 51-40-02.May 9, 2014 · N561RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140509171Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE AFT FRAME & STRINGER 10L. THE PROFILE WAS REPLACED IAW SRM 51-40-02.May 9, 2014 · N561RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140509172Profile · corrodedDURING INSPECTION, A CRACK WAS FOUND ON THE STRUCTURE UNDER THE MIDDLE FWD STEP SUPPORT BRACKET ON THE MAIN ENTRY DOOR. THE PROFILE WAS REPLACED IAW SRM 51-40-02.May 9, 2014 · N561RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140508146Light · brokenDURING INSPECTION, THE EMERGENCY FLOOR LIGHT STRIP AT ROW 10A WAS FOUND TO BE BROKEN. THE FLOOR STRIP WAS REPLACED & ALL OPERATIONAL CHECKS WERE GOOD.May 8, 2014 · N563RP · Emb EMB145LR · Emergency Lighting
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