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 CHQA20120930365Overheat Sensor · faultyCREW REPORTED, ON TAKEOFF RECEIVED A BRAKE OVERTEMP MESSAGE ON THE EICAS. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. FIRE RESCUE USED THERMAL IMAGING TO DETERMINE THE BRAKE TEMPERATURES AND IT WAS DETERMINED SDR CHQA20120930372Sill · damagedDURING INSPECTION, THE LEFT SILL 16L AT THE MAIN CABIN DOOR THRESHOLD HAD 16 HOLES THAT WERE ELONGATED AND REQUIRED REPAIR. THE DAMAGE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-013944ASDR CHQA20120929373Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND IN RIGHT SILL AT ANCHOR HOLES FRAME 22 TO FRAME 23. THE RIGHT SILL AT FRAME 22 TO FRAME 23 WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120929364Light · inoperativeDURING INSPECTION, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 3 AND 12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE OVERHEAD EMERGENCY LIGHTS AT ROWS 3 AND 12. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120929374Floor Support · corrodedDURING INSPECTION, CORROSION IN FLOORBOARD SUPPORT ANGLE AT RISER BETWEEN FRAMES 23 AND 24 CENTER OMEGA TO RIGHT SILL. THE FLOORBOARD SUPPORT ANGLE WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120929375Attach Bracket · corrodedDURING INSPECTION, CORROSION WAS FOUND AT FLOOR ATTACH BRACKETS PASSENGER DOOR THRESHOLD. THE FLOOR ATTACH BRACKETS WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120929376Attach Bracket · corrodedDURING INSPECTION, CORROSION WAS FOUND AT FLOOR ATTACH BRACKETS PASSENGER DOOR THRESHOLD. THE FLOOR ATTACH BRACKETS WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120927363Wire Harness · defectiveCREW REPORTED THAT COCKPIT READING LIGHT WENT OUT AND AN ELECTRICAL BURNING SMELL SOON APPEARED IN THE COCKPIT. MAINTENANCE ISOLATED THE BURNING SMELL TO THE FIRST OFFICER'S CHARTHOLDER LIGHT HARNESS AND DISCONNECTED THE HARNESS. THE ITEM IS CURRENTLY ON DEFSDR CHQA20120927370Shear Beam · crackedDURING INSPECTION, A CRACK WAS FOUND IN SHEAR FOOT FRAME 73 BETWEEN STRINGERS 8R AND 9R. THE SHEAR FOOT WAS REPAIRED IN ACCORDANCE WITH SRM 53-31-04.SDR CHQA20120926367Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND UNDER CROSS MEMBER LEFT OMEGA BEAM AT FRAME 24 AND 25. THE LEFT OMEGA BEAM AT FRAME 24 AND 25 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120926368Threshold · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR THRESHOLD BEAM SCREW HOLES. THE SERVICE DOOR THRESHOLD WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-02.SDR CHQA20120926369Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25. THE CENTER OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20120926371Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND IN FLOOR SUPPORT STRUCTURE BETWEEN FRAMES 22 AND 23 RIGHT OMEGA. THE FLOOR SUPPORT STRUCTURE WAS REPLACED IN ACCORDANCE WITH 51-40-02.SDR CHQA20120921354Light · inoperativeDURING INSPECTION, THE RIGHT LOWER FUSELAGE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT LOWER FUSELAGE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120920353Ballast · sparksCREW REPORTED THAT THE CEILING LIGHT OVER SEAT 1A WAS SPARKING. THE LIGHT BALLAST WAS PLACED ON MEL AND THE FINAL CORRECTIVE ACTION AND PART INFORMATION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT.SDR CHQA20120919360Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR STRUCTURE AROUND THE FASTENERS AT THE BOTTOM OF THE DOOR. THE SERVICE DOOR STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-013524.SDR CHQA20120919361Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR STRUCTURE AROUND THE FASTENERS AT THE BOTTOM OF THE DOOR. THE SERVICE DOOR STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-013524.SDR CHQA20120918362Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK SUPPORT AT FRAME 50. THE SEAT TRACK SUPPORT AT FRAME 50 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120917352Engine · failedCREW REPORTED THAT DURING FLIGHT THAT THE ENGINE 2 OIL PRESSURE DROPPED INTO THE AMBER RANGE AND THE ENGINE ITT ROSE INTO THE RED. THE CREW SHUT DOWN THE ENGINE IN FLIGHT, RAN THE CHECKLIST, AND DECLARED AN EMERGENCY. THE PASSENGER O2 MASKS WERE ALSO DEPLOYESDR CHQA20120916351Battery · dischargedDURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120915359Structure · bentDURING INSPECTION, THE RIGHT OUTBOARD LEADING EDGE WAS BENT AT THE OUTBOARD FRAME. THE RIGHT OUTBOARD LEADING EDGE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-013240A.SDR CHQA20120913350Light · malfunctionedCREW REPORTED THAT THE EMERGENCY LIGHTS AT ROWS 3, 4, 5, AND 6 WERE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT SYSTEM AND OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120912355Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE CARBON CROSSMEMBER CENTER OMEGA FRAME 27. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20120912356Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE CARBON CROSSMEMBER LEFT OMEGA INBOARD FLOORBOARD FLANGE BETWEEN FRAMES 24 AND 25. THE OMEGA BEAN WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20120912357Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND AT CARBON CROSSMEMBER CENTER OMEGA LEFT FLOORBOARD FLANGE BETWEEN FRAME 24 AND 25. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20120912358Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND AT CARBON CROSSMEMBER LEFT OMEGA AT FRAME 27. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20120911347Probe · inoperativeCREW REPORTED, RECEIVED A TAT 2 HEAT INOPERATIVE MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE TAT 2 PROBE. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120911349Structure · damagedDURING HEAVY MAINTENANCE, A PERMANENT REPAIR ON RUDDER II FASTENER WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-01759A. PART INFORMATION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT.SDR CHQA20120909309Inverter · inoperativeDURING INSPECTION, THE CENTER CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 6 DC TO AC INVERTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120907308Light · inoperativeDURING INSPECTION, THE EMERGENCY FLOOR LIGHTING STRIP AT THE OVERWING EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHTING STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120907331Skin · dentedDURING INSPECTION, A DENT WAS FOUND ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 13 AND FRAME 14 AND STRINGERS 10R AND 11R. THE DENT ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 13 AND FRAME 14 AND STRINGERS 10R AND 11R WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-02.SDR CHQA20120906307Carbon Seal · leakingCREW REPORTED THAT THEY RECEIVED A LAVATORY SMOKE INDICATION AFTER TAKE-OFF. CREW ALSO REPORTED THAT THERE WAS NO SMOKE OR ODOR PRESENT IN THE CABIN OR COCKPIT AND THE MESSAGE CLEARED BEFORE LANDING. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENTSDR CHQA20120906311Skin Splice · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 14 AND 16 AND STRINGERS 21L TO 20R. THE SKIN SPLICE WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-02.SDR CHQA20120906312Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON SHEAR CLIP AT FRAME 10 BETWEEN STRINGER 21R AND 20R. THE SHEAR CLIP AT FRAME 10 WAS REPLACED IN ACCORDANCE WITH SRM 53-12-04 AND 51-40-02.SDR CHQA20120906326Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 19 AND FRAME 21 AND STRINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012320A.SDR CHQA20120906327Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 16 AND FRAME 18 AND STRINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012320A DETAILS E AND F.SDR CHQA20120906328Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 11 AND FRAME 12 AND STRINGERS 21L AND 20L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-012394 REVISION B, DETAILS B AND C.SDR CHQA20120906329Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 10 AND FRAME 11 ON STRINGERS 21R AND 20R WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012394 REVISION B, DETAIL D.SDR CHQA20120806330Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 10 AND FRAME 11 ON STRINGERS 21L AND 20L WAS COMPLETED IN ACCORDANCE WITH ETD2012-145-012394 REVISION B, DETAIL E.SDR CHQA20120906336Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 12 AND FRAME 13 AND BETWEEN STINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012394 REVISION B, DETAIL H.SDR CHQA20120904305Light · malfunctionedCREW REPORTED THAT DURING PRE-FLIGHT INSPECTION, THE EMERGENCY LIGHT FLOOR STRIPS AT ROWS 4 THROUGH 6 WERE INOPERATIVE. THE ITEM WAS DEFERRED. THE DEFERRAL WAS CLEARED LATER IN THE DAY WHEN MAINTENANCE PERFORMED A SUCCESSFUL OPERATIONAL CHECK OF THE EMERGENCSDR CHQA20120904306Smoke Detector · false activationCREW REPORTED A LAVATORY SMOKE INDICATION ON THE EICAS. THE FLIGHT CREW FURTHER REPORTED THAT NO SMOKE WAS OBSERVED AND THERE WAS NO SMELL OF SMOKE IN THE CABIN OR COCKPIT. THE INDICATION CLEARED ITSELF AND THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE REPLACSDR CHQA20120904316Web · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 11 AND 12. THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 11 AND 12 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120904318Stanchion · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT STANCHION AT FRAMES 12 AND 13. THE RIGHT STANCHION BETWEEN FRAMES 12 AND 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120904319Stanchion · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT STANCHION AT FRAMES 11 AND 12. THE RIGHT STANCHION BETWEEN FRAMES 11 AND 12 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120904317Web · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 12 AND 13. THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 12 AND 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120904320Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R FROM FRAME 8 TO FRAME 13. THE STRINGER 21R AT FRAME 8 TO FRAME 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-20-02.SDR CHQA20120903345Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM AT FRAME 23. THE RIGHT OMEGA BEAM AT FRAME 23 WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-10.SDR CHQA20120831304Light · inoperativeDURING INSPECTION, THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE LEFT AFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR ASOA20120830084Floor Support · corrodedDURING C-CHECK LT OMEGA BEAM FRAME 29 HAS CORROSION (LOCAL LEVEL 2) AT CROSSBEAM ATTACHMENT POINT LWR FLANGE. MX PERFORMED REPAIR AND INSTALLED J-CHANNEL AT LT OMEGA BEAM FRAME 29 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
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