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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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.SDR 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.SDR 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.SDR 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 INSPECTIONSDR 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.SDR 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 GOOSDR 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.SDR 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.SDR 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.SDR 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.SDR CHQA20140612198Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FRAME 64 BETWEEN STINGERS 15L & 16L. THE FRAME WAS REPAIRED IAW SRM 51-40-02.SDR 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.SDR 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.SDR CHQA20140612201Skin · crackedDURING HEAVY MX, A CRACK IN THE FUSELAGE SKIN AT FRAME 75 WAS REPAIRED IAW ETD 2014-145-049612.SDR 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.SDR 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 SDR 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.SDR 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 SDR 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 FURSDR 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. SDR 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.SDR 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.SDR CHQA20140527195Door · dentedDURING HEAVY MX, A DENT ON THE BAGGAGE DOOR ABOVE THE VENT FLAP WAS REPAIRED IAW ETD2012-145-014619-A.SDR 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.SDR 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.SDR 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.SDR 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.SDR CHQA20140514157Frame · crackedDURING INSPECTION, FRAME 23 AT STRINGER 15L WAS FOUND TO BE CRACKED. FRAME 23 WAS REPAIRED IAW SRM 53-00-04.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR CHQA20140511147Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER AIRSTAIR DOOR SKIN. THE DOOR WAS REPAIRED IAW ETD2014-145-039320.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR CHQA20140510174Floor Support · corrodedDURING INSPECTION, THE RT OMEGA BEAM REPAIR AT FRAME 23 HAS CORROSION. THE REPAIR DOUBLER WAS REPLACED IAW ETD 2014-145-041404.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.
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