Allison AE-3007A1
Service difficulty reports · 321
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 = 'AE3007A1' 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 = 'AE3007A1' 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 C2XA11IA059Engine · vibrationIAH - FLIGHT 2482 IAH-GPT, THE CREW REPORTED ENGINE TWO VIBRATION IN AMBER FOR 2-3 SECONDS DURING CLIMB, AND AFTER POWERING BACK THE VIBE RETURNED TO GREEN RANGE, RETURNED AIRCRAFT TO CLIMB POWER AND VIBRATION STABILIZED BETWEEN 2.0 AND 2.4 IPS. THE AIRCRAFT SDR SIMA201104502Carbon Seal · failedON FLIGHT 4079 AFTER ROTATION LAVATORY SMOKE MESSAGE PRESENTED ON EICAS AND THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO YUL WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPSDR V0XR201012280004Floor Support · damaged(V0XR) FLOOR SUPPORT BEAM DAMAGED BEYOND LIMITS. R & R BEAM. W/C 1112SDR C2XA10CL188Switch · faultyTHE CREW REPORTED A BLD NR2 LOW TEMP MESSAGE IN ICING CONDITIONS. THE ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MX REPLACED THE NR2 BLEED PUSHBUTTON SWITCH. OPS CHECKS WERE GOOD.SDR C2XA10CL187Unknown · odorTHE CREW REPORTED A SLIGHT ODOR IN THE CABIN AFTER NR1 ENGINE START AND PACK 2 COMING ON LINE. THE ACFT RETURNED TO THE GATE. MX INSPECTED AND RAN BOTH ENGINES AND APU. NO DEFECTS WERE FOUND.SDR V0XR201011220002Sill · corroded(V0XR) RT SILL AT FRAME 41-48 IS CORRODED BEYOND LIMITS. R & R RT SILL. W/C 1067SDR V0XR2010110900004Sill · corroded(V0XR) SILL AFT OF SERVICE DOOR IS CORRODED BEYOND LIMITS. R & R SILL.SDR V0XR2010110900005Gusset · corroded(V0XR) GUSSET FROM FRAMES 20-23 ON CTR OMEGA BEAM IS CORRODED BEYOND LIMITS. R & R GUSSET.SDR V0XR2010110900009Sill · corroded(V0XR) LEFT SILL FROM FRAMES 42-48 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1089SDR JO0M08102800001AHand Rail · brokenDURING PASSENGER DEPLANING THE FWD MAIN DOOR STAIR HANDRAIL SEPARATED AT THE UPPER ATTACH BOLTS OF THE UPPER END FITTING ATTACHMENT.SDR V0XR210111050001Floor Support · corroded(V0XR) CTR OMEGA BEAM BETWEEN FRAMES 19-23 IS CORRODED BEYOND LIMITS. R & R CTR OMEGA BEAM.SDR V0XR210111050002Floor Support · corroded(V0XR) RT OMEGA BEAM BETWEEN FRAMES 19-23 IS CORRODED BEYOND LIMITS. R & R RT OMEGA BEAM.SDR V0XR210111050004Floor Support · corroded(V0XR) SUPPORT BETWEEN FRAMES 19-20 ON OMEGA BEAM IS CORRODED BEYOND LIMITS. R & R SUPPORT.SDR V0XR210111050005Sill · corroded(V0XR) LT SILL BETWEEN FRAMES 13-29 IS CORRODED BEYOND LIMITS. R & R LT SILL.SDR V0XR210111050006Sill · corroded(V0XR) LT SILL BETWEEN FRAMES 61-65 IS CORRODED BEYOND LIMITS. R & R LT SILL. W/C 2084SDR SIMA201028501Carbon Seal · faultyON FLIGHT 3355 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN ON THE TAKEOFF ROLL. THE CAPTAIN ELECTED TO ABORT. SMOKE BEGAN TO DISSAPATE AFTER POWER TO IDLE AND TAXI TO GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE ASSEMBSDR SIMA201027701Carbon Seal · failedON FLIGHT 2827 DURING TAKEOFF THE CREW REPORTED, AIR CONDITIONING SMOKE IN THE COCKPIT. THE CAPTAIN ELECTED TO ABORT THE TAKEOFF. THE CREW PERFORMED CHECK LIST PROCDURES AND RETURNED TO THE GATE. NO FURTHER ANOMALIES; NO SMOKE NOTED DURING TAXI. THE AIRCRAFSDR SIMA201027101Engine · leakingON FLIGHT 4270 SHORTLY AFTER TAKEOFF (APPROX 1500FT ABOVE GROUND LEVEL) THE FLIGHT ATTENDANT INFORMED US THAT THERE WAS A SMALL AMOUNT OF SMOKE IN THE CABIN. AT ONE POINT IN THE CLIMB AND SUBSEQUENT LEVEL OFF THE AMOUNT OF SMOKE SIGNIFICANTLY INCREASED. ON DSDR SIMA201025803Carbon Seal · failedON FLIGHT 3332 THE CREW REPORTED THAT DURING TAKEOFF AND CLIMBOUT DETECTED A BURNING OIL ODOR IN THE COCKPIT. THE CREW ELECTED TO CONTINUE TO DESTINATION AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINSDR C2XA10TY110Engine · smokeTYS - A/C WAS FERRIED FROM ORD TO TYS WHERE THE NR 1 ENGINE WAS REMOVED AND THE AIR CONDITIONING DUCTS CLEANED. ALL WORK CW IAW THE ENGINE TASKCARD 6271001. ALSO EMB AMM TASK 21-20-100-805 OPS CHECK GOOD.SDR SIMA201021405Carbon Seal · leakingFOR FLIGHT 4322 DURING INSPECTION FOUND AN OIL SMELL IN THE COCKPIT WITH THE NUMBER 1 BLEED AND PACK ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE IAW 71-000-00. THE OPERATIONAL CHECK WAS GOOD. NO LEAKS NOTED. THE CAUSE OSDR SIMA201018301Carbon Seal · smokeON FLIGHT THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN FLIGHT AND NOTICED THE NR 1 ENGINE SMOKING AFTER SHUTDOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE IAW WC 71-000-00. THE OPESDR SIMA201015205Engine · faultyON FLIGHT 3444 THE CREW REPORTED AN ODOR IN THE COCKPIT DURING TAKEOFF WITH THE PACKS ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 1 ENGINE. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR V0XR201005030021Strip · cracked(V0XR) LT WING TO FUSELAGE FAIRING STRIP X=14967.0 - X=16143.5 IS CRACKED. R & R STRIP. W/C 2132.SDR RAIA2010041300001Engine · leakingWHILE IN CRUISE, THE CREW REPORTED THAT THE LAVATORY SMOKE DETECTOR WENT OFF AND THAT A STRONG SMELL WAS COMING FROM PACK NR 2. INITIALLY, THE NR 2 PACK WAS DEFERRED AND THE SMOKE DETECTOR WAS OPERATIONALLY CHECK GOOD. THE DEFERRAL WAS CORRECTED WHEN MAINTENSDR V0XR201004070003Threshold · corrodedANGLES UNDER PASSENGER DOOR THRESHOLD ARE CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1145.SDR C2XA10IA055Clamp · defectiveIAH - FLIGHT 2069 THE CREW REPORTED A BLEED ONE LEAK DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FORWARD CLAMP ON THE NUMBER ONE ENGINE BLEED VALVE. OPERATIONAL AND LEAK CHECKS WERE COMPLSDR C2XA10IA041Thermostat · inoperativeIAH - FLIGHT 2413 - THE CREW REPORTED A BLEED 1 LOW TEMP DURING ICING TEST. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE BLEED THERMOSTAT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE SDR C2XATYEngine · malfunctionedMSP - EWR ON CLIMBOUT THRU APPROX 14000 TO APPROX 24000 AN ACRID BURNING SMELL THOUGHT TO BE COMING FROM THE PACKS - COULD NOT ISOLATE WHICH PACK- SMELL THEN DISSIPATED BUT RETURNED ON DESCENT FROM MID 20'S TO APPROX 17000. A/C FERRIED FROM EWR TO TYS. TYS MSDR C2XA10TY018Engine · malfunctionedMSP - EWR ON CLIMBOUT THRU APPROX 14000 TO APPROX 24000 AN ACRID BURNING SMELL THOUGHT TO BE COMING FROM THE PACKS - COULD NOT ISOLATE WHICH PACK - SMELL THEN DISSIPATED BUT RETURNED ON DESCENT FROM MID 20'S TO APPROX 17000. A/C FERRIED FROM EWR TO TYS. TYS SDR SIMA201001203Engine · odorON FLIGHT 4100 THE CREW REPORTED A LAVATORY SMOKE WARNING ON INITIAL CLIMBOUT AND COCKPIT FUMES PRESISITED WITH ELECTRICAL SMELL IN FORWARD CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 1 LEFT HAND ENGINE AND OPERATIONAL CHECKSSDR SIMA20100402Carbon Seal · failedFLIGHT 3789, RIGHT AFTER TAKEOFF CREW REPORTED RECEIVING A LAVATORY SMOKE MESSAGE ON EICAS. FOLLOWED AOM PROCEDURES & REQUESTED CRASH, FIRE & RESCUE UPON LANDING. ELECTED TO RETURN TO FIELD & LANDED WITHOUT INCIDENT. AFTER LANDING, FIRE DEPARTMENT INFORMED SDR C2XA09229Engine · smokeFLIGHT 3060 - EWR - FLIGHT CREW REPORTED NR 1 ENGINE EMITTING AN UNUSUAL AMOUNT OF SMOKE AFTER BEING SHUTDOWN. EWR MX RAN ENGINE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. NO SMOKE NOTICED AFTER SHUTDOWN.SDR SIMA200935703Carbon Seal · leakingFLIGHT 2792 DURING THE CLIMBOUT THE CREW REPORTED AN EXHAUST TYPE ODOR IN THE COCKPIT. ODOR INTENSIFIED. BOTH COCKPIT CREW MEMBERS DONNED OXYGEN MASK & ELECTED TO RETURN TO DFW. PASSENGERS DID NOT REPORT DETECTING ANY EXHAUST ODORS. ACFT REMOVED FROM SERVISDR SIMA200931702Carbon Seal · faultyDURING FLIGHT 3225 ON TAKEOFF THE CREW REPORTED A LAVATORY SMOKE DETECTION MESSAGE AND SMOKE ODOR IN THE AFT CABIN. THE CREW ELECTED TO RETURN TO CID. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGSDR FDKA2009102800191Engine · malfunctionedFRL FLT 6216 CLT-HOT. RTF-EMERG DECLARED ENGINE 2 OUT EICAS. MX REPLACED ENGINE, OPS GOODSDR FDKA2009101400187Engine · malfunctionedFRL FLT 6143 MDT-CVG. DIVERTED TO IAD, DECLARED AN EMERGENCY DUE TO NR 1 ENGINE ITT SPIKE TO 914, LP/HP VIBE AND ENGINE AUTO SHUT DOWN. MX REMOVED AND REPLACED NR 1 ENGINE.SDR SIMA200927111Engine · malfunctionedON FLIGHT 4468, THE CREW REPORTED AN OIL SMELL IN THE COCKPIT MOST OF THE FLIGHT. THE FLIGHT ATTENDANT DID NOT NOTICE ANY SMELLS IN THE CABIN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE NR 1 IAW 71-000-00. OPERATIONAL CHECK GOOD.SDR SIMA20092709Engine · malfunctionedON FLIGHT 3355 DURING THE TAKEOFF AT ABOUT 40 KNOTS THE CREW REPORTED GRAYISH WHITE SMOKE IN THE COCKPIT THAT INCREASED RAPIDLY. THE CREW ELECTED TO ABORT THE TAKEOFF. SMOKE REMOVAL PROCEDURES WERE APPLIED WITH THE APU AND PACKS AND THE SMOKE CLEARED TO 84 PSDR SIMA200926602Carbon Seal · leakingFLIGHT 9803 - DURING THE INITIAL CLIMBOUT THE CREW REPORTED, SAW AND SMELLED OILY SMOKE IN THE COCKPIT AND CABIN. THE CREW ELECTED TO RETURN TO ORD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. ENGINE NUMBER 2 WAS REPLACED. UPON THE DSDR FDKA2009082400177Engine · damagedASH FLT 6106 GRR TO CVG. RTF DUE TO NR 1 ENGINE SHUT DOWN, OIL PRESSURE DROPPED TO ZERO. EMERGENCY DECLARED. CONTRACT MX FOUND ENGINE DIFFICULT TO TURN AND METAL IN THE EXHAUST. MX R2 NR 1 ENGINE OPS LEAKS GOOD.SDR C2XA09TY201Case · corrodedNR 2 ENG FAN CASE FWD FLANGE HAS CORROSION IN BOLT HOLES. REMOVED CORROSION FROM 12 HOLES BY REAMING IAW EC 7220-01066.SDR C2XA09IA185Metering Unit · malfunctionedMFE - FLIGHT 2627, THE CREW REPORTED THAT E2 WOULD NOT ADVANCE 85 PERCENT N2 OR 90 PERCENT N1 AND ITT WAS SPIKING ERRONEOUSLY BETWEEN 300-500 DEGREES, WITH AN EICAS CHECK MESSAGE ON MFD WITH BOTH IGNITERS ON FOR E2. THE ISSUE RESOLVED ITSELF AFTER TWO MINUTESSDR RAIA2009072100004Engine · malfunctionedDURING FLIGHT, THE CREW REPORTED HEARING A LOUD BANG. THE N1 REDUCED TO 33 PERCENT AND N2 INCREASED TO 105 PERCENT, ITT INCREASED THROUGH 980 DEGREES. CREW PERFORMED EMERGENCY SHUTDOWN OF THE NR 2 ENGINE AND DECLARED EMERGENCY WITH NO INCIDENT ON LANDING. MSDR SIMA200919501Fadec · defectiveDISC - AFTER LANDING GOT E1-2 NO DISP + RUD HDOV PROT FAIL. ALSO EN ROUTE FELT LEFT YAW. LOOKED AT ENG INSTRUMENTS AND SAW SOME FLUCTUATION. LATER, YAW AGAIN + LOST NR 1 ITT (AGAIN) AOM NR 1 PROCEDURE BROUGHT IT BACK. SAW N1 GO TO 68 PERCENT + ING AB + LOWSDR SIMA200916001Carbon Seal · wornON FLIGHT 4521 CREW REPORTED ON TAKEOFF CABIN AND COCKPIT FUMES WITH LAV SMOKE INDICATION ON EICAS. ACFT RETURNED TO DEPARTURE FOR AN UNDERWEIGHT LANDING. NO FIRE NOTED. WARNING EXTINGUISHED AFTER LEVEL OFF AT 4000 FEET. ACFT REMOVED FROM SERVICE. REMOVED ANSDR SIMA200916001SUPCarbon Seal · wornON FLIGHT 4521 CREW REPORTED ON TAKEOFF CABIN AND COCKPIT FUMES WITH LAV SMOKE INDICATION ON EICAS. ACFT RETURNED TO DEPARTURE FOR AN UNDERWEIGHT LANDING. NO FIRE NOTED. WARNING EXTINGUISHED AFTER LEVEL OFF AT 4000 FEET. ACFT REMOVED FROM SERVICE. REMOVEDSDR C2XA09CL075Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL074Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND DURING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL071Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND DURING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.
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