Allison AE-3007A
Service difficulty reports · 3,309
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 = 'AE3007A' 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 = 'AE3007A' 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 CHQA20120601181Unknown · odorCREW REPORTED BURNING ODOR AT 22,000 FT. ODOR LASTED FOR APPROXIMATELY 15 SECONDS AND THEN DISSIPATED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED FAULT ISOLATION MANUAL TASK 72-00-00-810-814. NO DEFECTS WERE NOTED AT THAT TIME.SDR CHQA20120531178Fan · failedCREW REPORTED THAT THERE WAS A BURNING RUBBER ODOR IN THE COCKPIT AND FORWARD CABIN DURING FLIGHT. THE ODOR DISSIPATED AND RETURNED ON DESCENT. AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REPLACED THE NUMBER ONE RECIRCULATION FAN. OPS CHECKSDR CHQA20120530189CHSkin · dentedDURING INSPECTION, A DENT WAS FOUND IN THE RIGHT SIDE ELEVATOR UPPER SKIN. THE RIGHT ELEVATOR WAS REPAIRED IN ACCORDANCE WITH SRM 55-20-01.SDR CHQA20120529188Frame · crackedDURING INSPECTION, FRAME 23 WAS FOUND TO BE CRACKED AT THE RIGHT SILL. A SPLICE REPAIR PART WAS FABRICATED AND THE DAMAGED SECTION ON FRAME 23 WAS REPLACED IN ACCORDANCE WITH ETD2012-145-007840.SDR CHQA20120527182Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS FOUND ON FRAME 65 SHEAR TIE. MAINTENANCE REPLACED THE SHEAR TIE AT FRAME 65 IN ACCORDANCE WITH ETD 2012-145-007624.SDR CHQA20120516171Frame · crackedDURING INSPECTION, FRAME 66 WAS FOUND TO BE CRACKED UNDER THE LOWER BEAM. FRAME 66, UNDER THE LOWER BEAM, WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-007135.SDR CHQA20120516172Beam · corrodedDURING INSPECTION, THE CENTER FUSELAGE I RIGHT BEAM AT FRAME 22 WAS FOUND TO BE CORRODED. THE CENTER FUSELAGE RIGHT BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120515158Light · inoperativeMAINTENANCE REPORTED THAT AFTER THE EMERGENCY LIGHTS WERE RECHARGED, THE LAST EMERGENCY LIGHT FLOOR PROXIMITY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE LAST STRIP ON THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO SDR CHQA20120515159Battery · dischargedMAINTENANCE REPORTED THAT THE EMERGENCY LIGHTS WILL ONLY OPERATE FOR A FEW SECONDS AND THEN BECOME INOPERATIVE. MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120515160Battery · dischargedMAINTENANCE REPORTED THAT THE EMERGENCY LIGHTS WILL ONLY OPERATE FOR A FEW SECONDS AND THEN BECOME INOPERATIVE. MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120515161Battery · dischargedMAINTENANCE REPORTED THAT THE EMERGENCY LIGHTS WILL ONLY OPERATE FOR A FEW SECONDS AND THEN BECOME INOPERATIVE. MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120515162Battery · dischargedMAINTENANCE REPORTED THAT THE EMERGENCY LIGHTS WILL ONLY OPERATE FOR A FEW SECONDS AND THEN BECOME INOPERATIVE. MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120514167Beam · corrodedDURING INSPECTION, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120514168Floor Support · corrodedDURING INSPECTION, THE CENTER FUSELAGE I LEFT INBOARD OMEGA BEAM HAD AN EXISTING REPAIR THAT WAS FOUND TO BE CORRODED AT FRAME 20. THE CENTER FUSELAGE I LEFT INBOARD OMEGA BEAM AT FRAME 20 WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20120514169Frame · crackedDURING INSPECTION, THE LEFT FRAME 10 WAS FOUND TO BE CRACKED. THE LEFT FRAME 10 WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120514170Frame · crackedDURING INSPECTION, THE RIGHT FRAME 10 WAS FOUND TO BE CRACKED. THE RIGHT FRAME 10 WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120514174Shear Plate · corrodedDURING INSPECTION, THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE FOUND TO BE CORRODED. THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE REPAIRED IN ACCORDANCE WITH ETD 2012-145-006943.SDR CHQA20120514175Shear Plate · corrodedDURING INSPECTION, THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE FOUND TO BE CORRODED. THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE REPAIRED IN ACCORDANCE WITH ETD 2012-145-006943.SDR CHQA20120514176Skin · burnedDURING INSPECTION, A SKIN BURN FROM A LIGHTNING STRIKE WAS FOUND ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 24 AND FRAME 25 AT STRINGER 18R. THE RIGHT FUSELAGE SKIN BETWEEN FRAME 24 AND FRAME 25 AT STRINGER 18R WAS REPAIRED IN ACCORDANCE WITH SRM 53-22-01.SDR CHQA20120514177Skin · damagedDURING INSPECTION, A SKIN BURN FROM A LIGHTNING STRIKE WAS FOUND ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 30 AND FRAME 31 AT STRINGER 16R. THE RIGHT FUSELAGE SKIN BETWEEN FRAME 30 AND FRAME 31 AT STRINGER 16R WAS REPAIRED IN ACCORDANCE WITH SRM 53-22-01.SDR CHQA20120513163Floor Support · crackedDURING INSPECTION, THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA20120513164Floor Support · crackedDURING INSPECTION, THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA20120513165Floor Support · crackedDURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA20120513166Floor Support · crackedDURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA20120511148Light · inoperativeDURING INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE RIGHT OVERWING EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120510147Hydraulic System · lowCREW REPORTED THAT THEY RECEIVED A HYDRAULIC 1 LOW QUANTITY MESSAGE IN FLIGHT. AFTER RECEIVING THE MESSAGE THEY RECEIVED A HYDRAULIC SYSTEM 1 FAIL MESSAGE. THE CREW PERFORMED AN ABNORMAL FREE FALL LANDING GEAR EXTENSION DUE TO THE HYDRAULIC SYSTEM 1 FAILURESDR ASOA20120509098Mount · crackedNR 1 ENGINE FWD LOWER MOUNT BRACKET IS CRACKED. R & R BRACKET.SDR CHQA20120508144Valve · missingCREW REPORTED THAT THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT IN AUTO MODE OR IN MANUAL MODE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE EXTERIOR GROUND AIR CONNECTION VALVE FLAPPER MISSING. THE GROUND AIR CONNECTION VALVSDR CHQA20120508146Control Panel · faultyCREW REPORTED THAT THE FLIGHT ATTENDANT COULD NOT CONTROL THE EMERGENCY LIGHTS FROM THE FLIGHT ATTENDANT PANEL, THE LIGHTS WORKED PROPERLY FROM THE COCKPIT. MAINTENANCE REPLACED THE PASSENGER LIGHT CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHERSDR CHQA20120508145Light · inoperativeMAINTENANCE REPORTED THAT THE ROW 12 EMERGENCY LIGHT FLOOR STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE DEFERRED THE FLOOR STRIP. THE DEFERRAL WAS CLEARED BY REPLACING THE FLOOR LIGHTING STRIP AT ROW 12. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTSDR CHQA20120506143Light · inoperativeCREW REPORTED THAT THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT THE EMERGENCY EXIT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120504156Skin · damagedDURING INSPECTION, THE RUDDER I PROTRACTOR SKIN AT THE ATTACHING NUT PLATE WAS FOUND TO BE DAMAGED. THE RUDDER I SKIN AT PROTRACTOR ATTACHING NUT PLATE WAS REPAIRED IN ACCORDANCE WITH SRM 55-40-01.SDR CHQA20120503150Angle · corrodedDURING INSPECTION, THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR SURROUND STRUCTURE WERE FOUND TO BE CORRODED. THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR SURROUND STRUCTURE WERE REPAIRED IN ACCORDANCE WITH ETD 2012-145-006382 REVISION A.SDR CHQA20120503151Angle · corrodedDURING INSPECTION, THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR SURROUND STRUCTURE WERE FOUND TO BE CORRODED. THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR SURROUND STRUCTURE WERE REPAIRED IN ACCORDANCE WITH ETD 2012-145-006382 REVISION A.SDR CHQA20120503152Beam · corrodedDURING INSPECTION, THE LOWER BEAM ON THE CARGO DOOR SURROUND STRUCTURE WAS FOUND TO BE CORRODED. THE LOWER BEAM ON THE CARGO DOOR SURROUND STRUCTURE WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120503153Floor Support · crackedDURING INSPECTION, THE RIGHT OMEGA BEAM OUTBOARD ANGLE WAS FOUND TO BE CRACKED BETWEEN FRAME 47 AND FRAME 48. THE RIGHT OMEGA BEAM OUTBOARD ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA20120503154Angle · crackedDURING INSPECTION, THE LEFT OMEGA BEAM OUTBOARD ANGLE WAS FOUND TO BE CRACKED BETWEEN FRAME 47 AND FRAME 48. THE LEFT OMEGA BEAM OUTBOARD ANGLE BETWEEN FRAME 47 AND FRAME 48 WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA20120503155Support · crackedDURING INSPECTION, THE FORWARD RADIO ALTIMETER 2 BASE SUPPORT WAS FOUND TO BE CRACKED. THE FORWARD RADIO ALTIMETER 2 BASE SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120502141Valve · brokenCREW REPORTED THAT DURING FLIGHT, THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT WITH EITHER AUTO-PRESSURIZATION OR MANUAL PRESSURIZATION MODES. THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE FOUND THE EXTERIOR GROUND AIR CONNECTION VALVE FLAPPER MISSING. MAINTENSDR CHQA20120502149Frame · crackedDURING INSPECTION, THE RIGHT FRAME 10 WAS FOUND TO BE CRACKED. THE RIGHT FRAME 10 WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120428134Selector Switch · faultyCREW REPORTED, RECEIVED A BLEED 2 VALVE CLOSED MESSAGE IN FLIGHT. THE CREW FOLLOWED THE QUICK-REFERENCE HANDBOOK BUT THE VALVE WOULD NOT INDICATE OPEN. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED 2 PUSHBUTTON SSDR CHQA20120427133Battery · dischargedDURING INSPECTION, THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR ASOA20120426033REngine · leakingCREW REPORTED SMOKE IN COCKPIT & CABIN AFTER TAKEOFF, CLEARED AFTER SEVERAL MINUTES. AIR RETURN TO DEPARTURE WITHOUT INCIDENT. MX R & R NR 1 ENGINE IAW TASK CARD 6271001 AND IPC 72-00-00. OPS AND LEAK CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICESDR CHQA20120426142Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR FORWARD FRAME INTERNAL AT SECOND STOP FROM THE TOP. THE FORWARD FRAME ON THE PASSENGER DOOR WAS REPLACED IN ACCORDANCE WITH ETD 2012-145-006034.SDR CHQA20120424136Skin · dentedDURING INSPECTION, A DENT WAS FOUND ON CENTER FUSELAGE IV SKIN BETWEEN FRAME 59 AND FRAME 60, AND STRINGERS 12R AND 13R. THE CENTER FUSELAGE IV SKIN BETWEEN FRAME 59 AND FRAME 60, AND STRINGERS 12R AND 13R, WAS REPAIRED IN ACCORDANCE WITH SRM 53-24-01.SDR CHQA20120424132Battery · dischargedDURING INSPECTION, THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120424140Skin · debondedDURING INSPECTION, THE RIGHT INBOARD FLAP TRAILING EDGE AND LOWER SKIN WERE FOUND TO BE DISBOUND. MAINTENANCE REPAIRED THE RIGHT INBOARD FLAP TRAILING EDGE UPPER AND LOWER SKIN IN ACCORDANCE WITH ETD 2012-145-005883 REVISION B.SDR CHQA20120423131Duct · crackedCREW REPORTED, RECEIVED A BLEED 1 LEAK MESSAGE AFTER TAKEOFF. THE CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE T-DUCT JUST BELOW JOINT 17. OPERATIONAL AND LEAK CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120423137Angle · crackedDURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED. THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLES WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA20120423138Angle · crackedDURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED. THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLES WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02.
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