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 CHQA20140507170Doubler · gougedDURING INSPECTION, THE DOUBLER AT THE FWD NOSE SECTION BELOW THE EXTERNAL POWER RECEPTACLE ON THE LT SIDE AT FRAME 8 WAS FOUND TO BE GOUGED. THE DOUBLER WAS REPLACED IAW SRM 51-40-02.SDR ASOA20140506053Flapper Valve · brokenPILOT REPORTED A SUSPECTED FUEL LEAK, ENGINE NR 2, FUEL PPH AT CRUISE SET SIMILAR, YET TANK NR 2 INDICATOR SHOWED TANK NR 2 FUEL USAGE WAS MUCH GREATER. AFTER INSPECTION MX FOUND A BROKEN FLAP VALVE IN NR 2 FUEL TANK AND R & R WITH LEAK CHECK GOOD. ACFT WAS ASDR CHQA20140506130Light · brokenDURING INSPECTION, THE EMERGENCY FLOOR LIGHT STRIP AT THE EMERGENCY EXIT WAS FOUND TO BE BROKEN. REPLACED THE EMERGENCY LIGHT FLOOR STRIP AT THE EMERGENCY EXIT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140501129Battery · dischargedDURING INSPECTION, THE LIGHTS CONNECTED TO THE NR 1 EMERGENCY LIGHT BATTERY WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140501136Fitting · corrodedDURING INSPECTION, THE SHEAR CLIP AT FRAME 65 WAS FOUND TO BE CRACKED AT STRINGERS 18L & 19L. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140427125Battery · dischargedDURING INSPECTION, BOTH OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140427142Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FWD PAX DOOR STRUCTURE. THE LOWER FWD PAX DOOR STRUCTURE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140425131Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 81 & STRINGER 10R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140425132Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 81 & STRINGER 10L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140423133Door · chafedDURING INSPECTION, A CHAFE WAS FOUND ON THE INNER AFT FACE OF THE MAIN ENTRY DOOR FOLDING FLAP. THE CHAFE WAS REPAIRED IAW ETD 2014-145-034319.SDR CHQA20140423137Fitting · damagedDURING INSPECTION, THE LT AILERON ACTUATOR ATTACH LUG OTBD HAT BUSHING WAS FOUND TO BE MIGRATING AWAY FROM THE LUG. THE LT AILERON PCA FITTING WAS REPLACED IAW SRM 51-20-01 & SRM 51-40-02.SDR CHQA20140423138Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE CARGO DOOR FRAME JUST BELOW THE DOOR BUMPER PLATE. THE FRAME WAS REPAIRED IAW ETD 2014-145-034902.SDR CHQA20140423139Reinforcement · corrodedDURING INSPECTION, CORROSION WAS FOUND AROUND THE THE REINFORCEMENT FOR THE BOTTOM DOOR STOP INSIDE THE AFT STRUCTURE OF THE MAIN ENTRY DOOR. THE DOOR STOP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140423140Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE INNER STRUCTURE OF THE LOWER FWD AREA OF THE MAIN ENTRY DOOR. THE INNER STRUCTURE OF THE LOWER FWD AREA OF THE MAIN ENTRY DOOR WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140423141Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND & A CRACK WAS FOUND ON THE STRUCTURE UNDER THE MIDDLE FWD STAIR SUPPORT ON THE MAIN ENTRY DOOR. THE STRUCTURE UNDER THE MIDDLE FWD STAIR SUPPORT WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140423143Reinforcement · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE DOOR STOP REINFORCEMENT INSIDE OF THE FWD FRAME OF THE MAIN ENTRY DOOR. THE DOOR STOP REINFORCEMENT WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140423144Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE INNER STRUCTURE OF THE LOWER AFT CORNER OF THE MAIN ENTRY DOOR. THE LOWER AFT CORNER STRUCTURE OF THE LOWER MAIN ENTRY DOOR WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140422134Doubler · corrodedDURING INSPECTION, A PREVIOUS REPAIR DOUBLER ON THE LT FWD OMEGA BEAM FWD CAP AT FRAME 20 WAS FOUND TO BE CORRODED. THE REPAIR DOUBLER WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140422135Support · corrodedDURING INSPECTION, THE LT SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED AT FRAME 45. THE SEAT TRACK SUPPORT WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140921121Duct · crackedCREW REPORTED THAT THEY RECEIVED A BLEED 2 LEAK MSG DURING CLIMB OUT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. SECURED THE BLEED VLV, CLOSED & DEFERRED THE BLEED 2 SYS. THE DEFERRAL WAS CLEARED LATER THAT DAY WHEN THE DUCT FROM THE RT ENG BLEEDSDR ASOA20140419036Bolt · shearedDURING FLIGHT, AFTER A SERIES OF BUMPS OR WHAT SOUNDED LIKE A BACKFIRE. NR 2 ENGINE ITT SPIKED INTO THE RED FOLLOWED BY NR 2 ENGINE OUT. RESTART WAS SUCCESSFUL, FOLLOWED SHORTLY BY REPEAT OF UNCOMMANDED ENGINE SHUTDOWN. THE ACFT LANDED WITHOUT FURTHER INCIDESDR CHQA20140411110O-Ring · leakingCREW REPORTED THAT THEY RECEIVED A BLEED 1 LEAK MSG AFTER TAKEOFF. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. REPLACED THE O RING AT JOINT 3. OPERATIONAL & LEAK CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140411118Doubler · corrodedDURING INSPECTION, A PREVIOUS REPAIR DOUBLER ON THE RT OMEGA BEAM AT FRAME 61 WAS FOUND TO BE CORRODED. THE DOUBLER WAS REPLACED IAW ETD 2014-145-031092.SDR CHQA20140409112Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLE IN THE RT OMEGA BEAM AT FRAME 23. THE OMEGA BEAN WAS REPAIRED IAW ETD2014-145-030931 REVISION B.SDR CHQA20140407119Access Door · corrodedDURING INSPECTION, THE REAR ELECTRONIC DOOR WAS FOUND TO BE CRACKED BELOW THE HOLD OPEN HINGE BRACKET. THE DOOR WAS REPAIRED IAW ETD 2014-145-031377.SDR CHQA20140409120Skin · gougedDURING INSPECTION, THE FUSELAGE EXTERIOR SKIN WAS FOUND TO BE GOUGED INSIDE THE PYLON PANEL NR 414DB AT FRAME 67 & STRINGER 6LT. THE SKIN WAS REPAIRED IAW ETD 2014-145-031086.SDR CHQA20140331100Battery · dischargedDURING INSPECTION, THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140331099Electronic Unit · faultyCREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED A LG AIR & GND FAIL MSG & THAT THE LG DID NOT RETRACT. THE CREW ELECTED TO RETURN TO FIELD & LANDED WITHOUT INCIDENT. THE WEIGHT ON WHEELS PROXIMITY SWITCHES WERE INSPECTED WITH NO DEFECTS NOTED. THE ACFT WAS SDR CHQA20140329098Hydraulic System · low pressureCREW REPORTED THAT AFTER TAKEOFF, RECEIVED A HYD SYS 1 LOW QTY MSG DURING GEAR RETRACTION. RETURNED TO FIELD & LANDED WITHOUT INCIDENT.. SERVICED HYD SYS 1. FURTHER, INSPECTIONS WERE COMPLETED ON THE FLIGHT CONTROLS, THE BRAKE SYS, THE HYD SYS, THE SPOILERSDR CHQA20140328096Indicator · tumblesCREW REPORTED THAT THE ISIS ATTITUDE INDICATOR TUMBLED IN FLIGHT. THE ACFT DIVERTED & LANDED WITHOUT INCIDENT. RESET THE SYSTEM, OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140328097Indicator · tumblesCREW REPORTED THAT THE ISIS ATTITUDE INDICATOR TUMBLED IN FLIGHT. THE ACFT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. DEFERRED THE ISIS, THE DEFERRAL WAS CLEARED THAT EVENING BEFORE THE ACFT RESUMED FLIGHT BY REPLACING THE ISIS. OPERATIONAL CHECKS WERE GOSDR CHQA20140327094Unknown · odorCREW REPORTED THAT DURING FLIGHT THERE WAS A SMOKE SMELL IN THE COCKPIT & CABIN. THE CREW DIVERTED THE ACFT & DECLARED AN EMERGENCY. THE ACFT LANDED WITHOUT INCIDENT. FIRE DEPARTMENT PERSONNEL CHECKED THE AIRCRAFT & FOUND NO SIGNS OF FIRE OR HEAT. INSPECTESDR CHQA20140326095Light · inoperativeDURING INSPECTION, THE LT EXTERNAL OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED THE LT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140325106Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20. THE CTR OMEGA BEAM WAS REPAIRED IAW SRM 53-21-10.SDR CHQA20140324091Light · faultyDURING INSPECTION, THE 2ND EMERGENCY LIGHT FLOOR STRIP WAS FOUND TO BE FLICKERING. DEFERRED THE EMERGENCY LIGHT STRIP. THE EMERGENCY LIGHT IS CURRENTLY ON DEFERRAL & THE FINAL CORRECTIVE ACTION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT.SDR CHQA20140324092Proximity Switch · faultyCREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A LG AIR & GND FAIL MESSAGE & THAT THE LG WOULD NOT RETRACT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. THE ACFT WAS FOUND SAFE FOR FERRY FLIGHT & WAS FERRIED TO KCMH FOR REPAIR. REPLACED BOTH RT MLGSDR CHQA20140323090Light · inoperativeDURING INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE RT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140322103Stringer · chafedDURING INSPECTION, STRINGER 21 WAS FOUND TO BE CHAFED BETWEEN FRAME 20 & 21. THE STRINGER WAS REPAIRED IAW ETD 2014-145-025850-A.SDR CHQA20140322104Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 24 & STRINGERS 15R - 16R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140322105Doubler · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM DOUBLER AT Y=-479.0 AT FRAME 20. THE BEAM WAS REPAIRED IAW SRM 53-00-10.SDR CHQA20140322107Skin · gougedDURING INSPECTION, A GOUGE WAS FOUND ON THE RT NR 2 WING LE UPPER NOSE SKIN. THE RT NR 2 WING LE UPPER NOSE SKIN WAS REPAIRED IAW SRM 57-40-00.SDR CHQA20140318089Pump · malfunctionedCREW REPORTED THAT DURING FLIGHT, THEY RECEIVED A HYD SYS 2 FAIL MESSAGE. DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE HYD SYS 2 ENGINE DRIVEN PUMP. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140316086Battery · dischargedDURING INSPECTION THE NR 4 EMERGENCY LIGHT BATTERY WAS REPORTED TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140315085Battery · dischargedDURING INSPECTION THE NR 4 EMERGENCY LIGHT BATTERY WAS REPORTED TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140314084Switch · faultyCREW REPORTED THAT THEY RECEIVED A PITCH TRIM MAIN INOPERATIVE MSG IN FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX REPLACED THE AUTO PILOT DISCONNECT SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140312083Battery · dischargedDURING INSPECTION BOTH OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140310078Connector · unsecureDURING INSPECTION THE EMERGENCY LIGHT STRIP BETWEEN ROWS 6 - 7 WAS FOUND TO BE INOPERATIVE. MX SECURED THE PLUG ON THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140310079Wire · unsecureDURING INSPECTION THE EMERGENCY LIGHT STRIP BETWEEN ROWS 12 - 14 WAS FOUND TO BE INOPERATIVE. MX SECURED THE WIRE ON THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140309077Flap · malfunctionedCREW REPORTED THAT THEY RECEIVED A FLAP FAIL MSG DURING FLIGHT. THE CREW DECLARED AN EMERGENCY & LANDED AT THEIR INTENDED DESTINATION WITHOUT INCIDENT. MX RESET THE FLAP SYS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140308076Relay · failedCREW REPORTED THAT THEY RECEIVED A TAT 2 HEAT INOPERATIVE MSG DURING FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX REPLACED CURRENT SENSOR RELAY K0494. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
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