Allison AE-3007A1/2
Service difficulty reports · 289
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 = 'AE3007A12' 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 = 'AE3007A12' 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 CHQA20130112027Floorbeam · corrodedDURING INSPECTION, THE LEFT INBOARD FLOORBEAM FLOORBOARD SUPPORT WAS FOUND TO BE CORRODED AT CROSSBEAM MEMBER FRAME 24, Y479. THE CORRODED SECTION OF THE FLOORBEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130112028Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND AT STRINGER 21R AT FRAME 10 THROUGH FRAME 11. THE STRINGER 21R AT FRAME 10 THROUGH FRAME 11 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR SIMA20130110001Engine · power lossON FLIGHT 3422 THE CREW ABORTED TAKEOFF DUE TO GREATER 80 KNOTS TAKEOFF POWER LOSS ON NR 2 ENGINE AND LOSS OF NR 2 ITT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET FADEC 2A AND 2B, CLEAN CONNECTOR CHECK CORROSION ON CONNECTOR PER ROLLS ROYCE FIM 77-21-00-81SDR CHQA20130109009O-Ring · leakingCREW REPORTED THAT THEY RECEIVED A BLEED 1 LEAK MESSAGE DURING FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE O-RINGS AT JOINTS 17, 19, 23, AND 26 IN THE BLEED SYSTEM. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DESDR CHQA20130109010Cover · missingCREW REPORTED THAT DURING FLIGHT, THE AIRCRAFT WOULD NOT PRESSURIZE IN AUTOMATIC OR MANUAL MODES. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE EXTERNAL GROUND CONNECTION VALVE COVER TO BE MISSING AND DEFERRED THE ITEM. THE DSDR SIMA20130109038Frame · corrodedLT ENGINE FRAME FLANGE CORRODED OUT OF LIMITS. R & R LT ENGINE IAW WC 71-000-00.SDR SIMA20130107006Acm · faultyON FLIGHT 2977 THE CREW REPORTED AN OCCASIONAL STRONG OIL SMELL APPARENT IN THE COCKPIT AND GALLEY AREA AND OCCURS AT RANDOM TIMES AND DOES NOT SEEM ASSOCIATED WITH ANT PARTICULAR THRUST OR BLEED SETTINGS. THE PILOT STATED HE BELIEVES THE SMELL TO BE COMING FSDR CHQA20130107008Light · inoperativeDURING INSPECTION, THE EMERGENCY LIGHT FLOOR PROXIMITY STRIPS WERE FOUND TO BE INOPERATIVE AT ROW 8. MAINTENANCE REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT ROW 8. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130107014Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR CLIP AT FRAME 67 BETWEEN STINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130107015Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR CLIP AT FRAME 24 BETWEEN STRINGER 15R AND 16R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130107016Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN SHEAR CLIP AT FRAME 24 BETWEEN STRINGER 16R AND 17R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130107017Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130107018Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130107019Handle · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE COCKPIT GRAB HANDLE STRUCTURE. THE COCKPIT GRAB HANDLE STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-000584.SDR CHQA20121229003Valve · faultyCREW REPORTED, DURING FLIGHT THEY RECEIVED A BLEED 1 LOW TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FAN AIR VALVE THERMOSTAT AND THE FAN AIR VALVE. OPERATIONAL CHECKS WERE GOOD WSDR CHQA20121229004Thermostat · faultyCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 LOW TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FAN AIR VALVE THERMOSTAT AND THE FAN AIR VALVE. OPERATIONAL CHECKS WERE GOSDR CHQA20121228001Controller · faultyCREW REPORTED THAT ON DESCENT AN ELECTRICAL BURNING SMELL WAS PRESENT IN THE COCKPIT. THE CREW DESELECTED THE WINDSHIELD HEAT FOR BOTH WINDSHIELDS AND THE SMELL DISSIPATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD ONE HEAT CSDR CHQA20121228002Light · inoperativeDURING INSPECTION, THE LEFT NUMBER 4 FLOOR PROXIMITY EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT NUMBER 4 FLOOR PROXIMITY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121226478Engine · leakingCREW REPORTED, RECEIVED A LAVATORY SMOKE INDICATION ON CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NUMBER 1 ENGINE. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121222477Plug · damagedCREW REPORTED, RECEIVED A LAVATORY SMOKE INDICATION ON CLIMBOUT. THE FLIGHT ATTENDANT CONFIRMED A HAZY PRESENCE IN THE REAR OF THE CABIN AND THE CREW RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ISOLATED THE SMELL TO ENGINE 1 AND THESDR CHQA20121215476Light · inoperativeDURING INSPECTION, THE FLOOR PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE. THE FLOOR PROXIMITY LIGHT STRIP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121210469Ecu · faultyCREW REPORTED, FLAP FAIL MESSAGE ON APPROACH TO KRHI. THE CREW RETURNED TO FIELD IN KMKE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP ELECTRONIC CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121210458Profile · corrodedDURING INSPECTION, THE SERVICE DOOR LOWER AFT CORNER WAS FOUND TO BE CORRODED AT THE DOOR TRIM ATTACH POINT. THE AREA WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-017580. PART INFORMATION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT.SDR CHQA20121209459Ecu · faultyCREW REPORTED, RECEIVED A FLAP FAIL MESSAGE AFTER GEAR RETRACTION. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE FLAPS AND A FLAP LOW SPEED MESSAGE APPEARED. THE ITEM WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 12/10/2012 BY RSDR CHQA20121207470Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RAMP ANGLE FRAME 20 AT THE CENTER OMEGA BEAM. THE ANGLE AT FRAME 20 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-03.SDR CHQA20121207471Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SILL AT FRAME 20 TO FRAME 21. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-00.SDR CHQA20121207472Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE GUSSET AT LEFT OMEGA FRAME 59. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121207473Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE GUSSET AT RIGHT OMEGA FRAME 61. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND SRM 51-20-03.SDR CHQA20121207474Threshold · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR THRESHOLD BEAM AT THE SCREW HOLES. THE SERVICE DOOR THRESHOLD WAS REPLACED IN ACCORDANCE WITH SRM 53-21-02.SDR CHQA20121207475Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT THRESHOLD BEAM. THE THRESHOLD BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121206455Frame · bentDURING INSPECTION, FRAME 72 WAS FOUND TO BE BENT BETWEEN RIGHT STRINGER 14R AND 15R. THE DAMAGED AREA WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.SDR CHQA20121206564Rib · damagedDURING INSPECTION, THE LEFT ELEVATOR INTERNAL RIB AT STATION YH-1310 HAS TWO DAMAGED HOLES. THE DAMAGED AREA WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-017677.SDR CHQA20121205456Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND AROUND THE NUT PLATES AND FASTENER ON THE RIGHT OMEGA BEAM TOP GUSSET PLATE AT FRAME 59 TO THE COMPOSITE FLOOR. THE GUSSET PLATE WAS REPLACED IN ACCORDANCE WITH ETD 2012-145-017227-A.SDR CHQA20121205457Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE NUT PLATES ON THE CENTER OMEGA BEAM TOP GUSSET PLATE AT FRAME 59 TO THE COMPOSITE FLOOR CROSS BEAM. THE GUSSET WAS REPLACED IN ACCORDANCE WITH ETD 2012-145-017227. PART INFORMATION WILL BE SUBMITTED AS A SUPPLEMESDR CHQA20121205451Engine · leakingCREW REPORTED THAT THEY RECEIVED A LAVATORY SMOKE INDICATION ON CLIMBOUT. THEY REPORTED NO VISIBLE SMOKE WAS PRESENT, HOWEVER AN ODOR WAS PRESENT IN THE CABIN. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TASDR CHQA20121204450Battery · dischargedDURING INSPECTION, THE NUMBER 2 EMERGENCY BATTERY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121203468Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 BETWEEN STRINGERS 20L AND 21L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121202449Skin · damagedCREW REPORTED A LIGHTNING STRIKE ON CLIMBOUT. THE CREW DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. DURING THE LIGHTNING STRIKE INSPECTION, MAINTENANCE FOUND BURN MARKS BETWEEN STRINGERS 2L AND 3L, BETWEEN FRAMES 56 AND 57. MAINTENANCE REPAIRED THE AREA IN SDR CHQA20121130462Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 53 THROUGH FRAME 58. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121129460Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT TRACK AT FRAME 47 THROUGH FRAME 52. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121129461Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT TRACK AT FRAME 23 THROUGH FRAME 30. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121129463Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 42. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121129464Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT INBOARD SEAT TRACK AT FRAME 36 THROUGH FRAME 45. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121129465Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 47 THROUGH FRAME 52. THE SEAT TRACK WAS REPLACED IN ACORDANCE WITH AMM 53-01-06.SDR CHQA20121129466Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT INBOARD SEAT TRACK AT FRAME 30 THROUGH FRAME 36. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121129467Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 59. THE LEFT OMEGA BEAM GUSSET AT FRAME 59 WAS REPLACED IN ACCORDANCE WITH 51-40-02.SDR CHQA20121125452Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR ENTRY BEAM AFT OF THE NUT PLATE. THE CORROSION WAS BLENDED IN ACCORDANCE WITH SRM 51-10-03 AND A PREVIOUS REPAIR WAS FOUND TO HAVE COVERED THE DAMAGED AREA PER SRM 53-21-02.SDR CHQA20121125453Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM JUST FORWARD OF THE "Z" PROFILE AT FRAME 23. THE BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-10.SDR SIMA20121115003Carbon Seal · unserviceableDURING MAINTENANCE DETERMINED THAT AN OIL SMELL APPEARED TO BE COMING FROM THE NR 2 ENGINE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE ZERO CARBON SEAL IAW RRMM 72-25-25 PERFORMED ENGINE RUNS IAW RRMM 72-00-00 AND ETN EM -72-SDR SIMA20121108003Engine · malfunctionedON FLIGHT 2838, ADVANCED THE THRUST LEVERS TO THE DETENT FOR NORMAL CLIMB THRUST, E1 IMMEDIATELY BEGAN TO SPOOL DOWN UNCOMMANDED. EICAS MESSAGE E1 OUT APPEARED WITH NO OTHER ASSOCIATED MESSAGES. RAN THE APPROPRIATE EMERGENCY PROCEDURES. ADVISED ATC OF THE E
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