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 CHQA201100132Skin · dentedDURING INSPECTION, A DENT WAS FOUND ON THE CENTER FUSELAGE 1 SKIN BETWEEN FRAMES 19 AND 20 THAT WAS BEYOND LIMITS. THE DENT MEASURED 3 INCHES WIDE, BY 2.8 INCHES LONG AND 0.064 INCHES DEEP. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED WITH NO CRACSDR CHQA201100133Tire · separatedAFTER TAKEOFF, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MSG. AFTER FOLLOWING THE QRH, IT WAS DECIDED TO RETURN TO ORD WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. DURING POST FLIGHT INSPECTION, THE RIGHT INBOARD TIRE WAS FOUND TO HAVE LOST ITS TREAD WSDR CHQA201100146Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE DOOR SURROUND STRUCTURE LOWER BEAM. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE DOOR SURROUND LOWER BEAM WITH NO FURTHER DEFECTS NOTED. THE CARGO FLOOR STRUCTURE DOOR SURROUND STRUCTURE SDR CHQA201100147Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CABIN FLOOR CENTER FUSELAGE I ANGLE UNDER CARBON POST AT FRAME 18 ON LEFT OMEGA BEAM ANGLE. MAINTENANCE REPLACED THE CENTER FUSELAGE UNDER CARBON POST FRAME 18 ON LEFT OMEGA BEAM WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100130O-Ring · tornCREW REPORTED A BLEED 1 LEAK MESSAGE ON CLIMBOUT WITH A BLEED 1 CLOSED MESSAGE AT THE SAME TIME. THE MESSAGE REMAINED ON UNTIL CROSS BLEED WAS CLOSED AND BLEED 1 PUSH BUTTON WAS DESELECTED AND THE AIRCRAFT DIVERTED TO KCMH WHERE IT LANDED WITHOUT INCIDENT. MSDR CHQA201100131Spar · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LEFT WING SPAR I TOP FLANGE CRACKED THRU AT RIB 19. THE CRACK WAS 2.745 INCHES LONG AND 0.001 INCHES WIDE THRU THE MATERIAL. THE DAMAGED AREA WAS REMOVED AND A REINFORCING PATCH WAS INSTALLED PER TI-145-11-095.SDR CHQA201100135Channel · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE CENTER FUSELAGE 1 SERVICE DOOR CHANNEL. THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I SERVICE DOOR CHANNEL WAS REPLACED.SDR CHQA201100134Rib · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM CENTER RIB. MAINTENANCE REPLACED THE MAIN PASSENGER DOOR STRUCTURE BOTTOM CENTER RIB.SDR CHQA201100127Brake Sys · malfunctionedCREW REPORTED THAT DURING THE LANDING ROLL OUT, THE BRAKES INITIALLY WORKED NORMALLY, BUT WHILE DECELERATING FROM 90KTS TO 50KTS, THE BRAKES WERE INEFFECTIVE. REPORTED THAT THERE WAS STILL RESISTANCE IN THE PEDALS, BUT NO BRAKING FORCE WAS APPLIED. ONCE BELOSDR CHQA201100128Skin · damagedWHILE MOVING THE JET BRIDGE FROM THE AIRCRAFT, THE JET BRIDGE MADE CONTACT AIRCRAFT DAMAGING THE FORWARD FUSELAGE, AOA VANE, TAT SENSOR, ICE DETECTOR, AND THE PITOT PROBE. AOA VANE, TAT SENSOR, ICE DETECTOR AND PITOT PROBE WERE REPLACED AND A TEMPORARY REPAIRSDR CHQA201100126Outflow Valve · inoperativeCREW REPORTED THAT DURING DESCENT FROM FL320 TO FL240 CABIN ALTITUDE STARTED INCREASING. THE CREW DECLARED AN EMERGENCY AND INCREASED THERE DESCENT RATE. THE AIRCRAFT LANDED KCLT WITHOUT INCIDENT. MAINTENANCE FOUND THE MANUAL PRESSURIZATION MODE TO BE OPERASDR CHQA201100125O-Ring · leakingCREW REPORTED THAT DURING CLIMB, IN ICING CONDITIONS, RECEIVED A "BLEED 1 LEAK" MESSAGE. THE MESSAGE WENT AWAY AFTER THE BLEED 1 VALVE CLOSED. THE CREW RETURNED TO KLGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE O-RING AT THE LEFT WING ROOT. OPESDR CHQA201100123Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE TOP OF THE THE OMEGA BEAM FROM FR19 TO FR23. MAINTENANCE REPLACED THE OMEGA BEAM IAW EMB140 SRM 51-40-02.SDR CHQA201100109Switch · out of positionCREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE CREW RECEIVED "LANDING GEAR LEVER DISAGREE" WARNING MESSAGE ON THE EICAS. CYCLED THE GEAR PER THE QUICK REFERENCE HANDBOOK, ALL THREE GEAR WERE STILL SHOWING DOWN AND LOCKED. THE CREW SDR CHQA201100124Beam · corrodedDURING INSPECTION LEVEL 3 CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I MIDDLE BEAM BETWEEN FRAME 17 AND 25. THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I MIDDLE BEAM BETWEEN FRAME 17 AND 25 WAS REPLACED, THE NEW PART WAS INSTALLED WITH A SSDR CHQA201100099Unknown · noisyCREW REPORTED THAT DURING FLIGHT THERE WAS A LOUD NOISE COMING FROM THE NOSE OF THE PLANE. REPORTED THAT IT SOUNDED AS IF THE NOSE LANDING GEAR DOORS WERE NOT FULLY CLOSED. MAINTENANCE PERFORMED A DETAILED VISUAL INSPECTION OF THE NOSE GEAR DOOR ASSEMBLIES ASDR CHQA201100100Connector · corrodedCREW REPORTED THAT THE NOSE LANDING GEAR DOORS STAYED OPEN AFTER TAKEOFF. MAINTENANCE PLACED THE AIRCRAFT ON JACKS AND PERFORMED MULTIPLE GEAR SWINGS WITH NO DEFECTS NOTED OF THE EXTENSION AND RETRACTION SYSTEM. NOTED THAT THE NOSE LANDING GEAR DOORS WERE CYSDR CHQA201100129Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON AN EXISTING REPAIR OF THE LEFT OMEGA BEAM AT FRAME 20. MAINTENANCE REPLACED THE EXISTING REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 IAW SRM 53-00-10 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100072Carbon Seal · wornCREW REPORTED THAT UPON TAKEOFF, AT APPROXIMATELY 400 FEET, CREW BECAME AWARE OF SMOKE IN THE COCKPIT AND CABIN. AFTER LEVELING OFF AT 4000 FEET, THE SMOKE RAPIDLY DISSIPATED AND WENT AWAY WITH POWER REDUCTION AND THE RECIRCULATION FANS TURNED OFF. CREW DECLSDR CHQA201100073Unknown · noisyCREW REPORTED THAT AFTER RAISING THE LANDING GEAR DURING TAKEOFF, THERE WAS A LOUD WIND NOISE COMING FROM THE NOSE WHEEL COMPARTMENT. ALL GEAR INDICATIONS INDICATED THAT THE GEAR WAS UP AND LOCKED. THE CREW RECYCLED THE LANDING GEAR AND THE SOUND WAS STILL ASDR CHQA201100074Sealant · damagedCREW REPORTED THAT DURING CRUISE HEARD A STRANGE NOISE IN THE COCKPIT. THE CREW DIVERTED TO KCLE AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AERODYNAMIC SEALANT ABOVE THE FIRST OFFICER'S WINDSHIELD LOOSE AND FLUTTERING ON THE WINDSHIELD. REMOVED THE SDR CHQA201100070Check Valve · missingFLIGHT CREW REPORTED THAT ON CLIMBOUT, THE CABIN ALTITUDE WAS CLIMBING ALONG WITH THE AIRCRAFT ALTITUDE. I AUTO MODE THE CABIN ALTITUDE CLIMBED TO 7800FT SWITCHING TO MANUAL MODE HAD NO EFFECT AND THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MSDR CHQA201100071Electronic Unit · failedFLIGHT CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON ROTATION AND HAD TO USE THE DOWNLOCK OVERRIDE BUTTON TO GET THE LANDING GEAR RETRACTED. AFTER GEAR RETRACTION, THE LANDING GEAR AIR/GROUND FAIL MESSAGE REMAINED FOR THE REST OF THE FLIGHT. ON LANSDR CHQA201100069Controller · inoperativeCREW REPORTED THAT DURING CRUISE, THE CABIN PRESSURIZATION RATE STARTED TO CLIMB 2500FPM. THE CREW FOLLOWED THE QRH AND SWITCHED TO MANUAL MODE. MANUAL MODE WAS SLOW TO RESPOND. MAINTENANCE REPLACED THE DIGITAL PRESSURIZATION CONTROLLER. OPERATIONAL CHECKSSDR CHQA201100122Thermostat · inoperativeCREW REPORTED THAT DURING FLIGHT RECEIVED A BLEED 2 OVERTEMP MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND BLEED 2 WAS DESELECTED, AND RETURNED TO A NORMAL TEMPERATURE. ADDITIONAL WARNING MESSAGES FOR WING ANTI-ICE AND STAB ANTI-ICE FAIL WERE RSDR CHQA201100068Connector · corrodedCREW REPORTED THAT WHILE ON FINAL APPROACH INTO CAE, HAD WINDSHEAR WARNING DUE TO WEATHER AND ON GEAR RETRACTION, THE NOSE LANDING GEAR RETRACTED NORMALLY, BUT 30 SEC LATER THERE WAS A LANDING GEAR AIR/GROUND FAIL MESSAGE AND BOTH MAINS SHOWED IN TRANSIT. A MSDR CHQA201100066Battery · failedDURING INSPECTION THE NR 2 EMERGENCY LIGHT BATTERY WAS FOUND TO HAVE FAILED. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100067Light · inoperativeDURING INSPECTION THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100064Proximity Switch · corrodedDURING CLIMBOUT, THE FLIGHT CREW REPORTED THAT THEIR WAS AN INTERMITTENT LANDING GEAR AIR/GROUND FAIL MESSAGE DISPLAYING ON THE EICAS. THE CREW RETURNED TO KORD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR WOW PROXIMITY SWITCH CORRODESDR CHQA201100065Brake Sys · contaminatedCREW REPORTED THAT DURING TAXI THE RIGHT BRAKES PULSATED WHEN APPLIED. MAINTENANCE CYCLED THE RIGHT OUTBOARD BRAKE FUSE AND BLED ALL MAIN LANDING GEAR BRAKE ASSEMBLIES. MAINTENANCE PERFORMED OPERATIONAL AND TAXI CHECKS WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100063Seal · looseSHORTLY AFTER TAKEOFF, THE FLIGHT CREW REPORTED A NOISE COMING FROM JUST AFT OF THE CAPTAIN'S DV WINDOW. THEY COULD SEE SOMETHING SLAPPING THE FUSELAGE BUT COULD NOT IDENTIFY WHAT IT WAS SO THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENASDR CHQA201100108Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE FLOOR STRUCTURE CENTER FUSELAGE I MIDDLE OMEGA BEAM BETWEEN FRAME 19 AND 25. MAINTENANCE REPLACED THE FLOOR STRUCTURE CENTER FUSELAGE I MIDDLE OMEGA BEAM BETWEEN FRAME 19 AND 25 AND INSTALLED WITH A SOLID RIVET IAWSDR CHQA201100062Windshield · crackedDURING CLIMBOUT, THE FLIGHT CREW REPORTED THAT THE CAPTAIN'S WINDSHIELD OUTER PANE CRACKED. THE AIRCRAFT DIVERTED TO KCMH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAPTAIN'S WINDSHIELD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100107Angle · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE ENTRANCE FORWARD SIDE ANGLE. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE ENTRANCE FORWARD SIDE ANGLE AND INSTALLED WITH A SOLID RIVET IAW SRM 51-40-02.SDR CHQA201100060Warning System · false activationON DESCENT THE FLIGHT CREW REPORTED A FLAP FAIL MESSAGE WHEN ATTEMPTING TO DEPLOY FLAPS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE THE FAULT ON THE GROUND AND THE FLAPS WERE OPERATING NORMALLY AT THAT TIME. THE AIRCRAFT WAS TSDR CHQA201100061Velocity Sensor · faultyCREW REPORTED THAT DURING APPROACH WHEN THE FLAPS WERE SELECTED, RECEIVED A FAIL MESSAGE WITH THE FLAPS STILL AT ZERO. THE FLIGHT CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT FLAP VELOCITY SENSOR AND THESDR CHQA201100059Brake · failedCREW REPORTED THAT ON APPROACH THERE WAS A FLAP FAIL MESSAGE WHEN SELECTING FLAPS FROM 0-9. ON CALL MAINTENANCE COULD NOT DUPLICATE FAULT ON GROUND AND OPERATIONAL CHECKS WERE GOOD. LATER THAT DAY, DUE TO CMC MESSAGING, KSDF MAINTENANCE REPLACED THE RIGHT FLSDR C2XA11CL069Actuator · faultyIAD FLT 5821 THE CREW REPORTED A LAV SMOKE WARNING MESSAGE ON TAKEOFF. ALSO REPORTED A SMOKE SMELL. NO SMOKE WAS NOTED. THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE CVG ACTUATOR. OPERATIONAL SDR CHQA201100056Carbon Seal · leakingCREW REPORTED THAT AFTER TAKEOFF AT BETWEEN 600-700FT THERE WAS VISIBLE SMOKE IN THE CABIN FOLLOWED BY A LAVATORY SMOKE INDICATION ON EIACS. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN BOTH ENGINES AND BLEEDS WITH PACKS IN MULTISDR CHQA201100057Brake Sys · contaminatedCREW REPORTED THAT AFTER LANDING THE BRAKES WERE SLUGGISH AND THAT THE PEDALS HAD TO BE PUSHED ALL THE WAY TO THE FLOOR BEFORE THEY WERE EFFECTIVE. MAINTENANCE BLED ALL 4 BRAKE SYSTEMS. AIR WAS FOUND TO BE PRESENT IN THE INBOARD AND OUTBOARD BRAKE SYSTEMS. SDR CHQA201100058Unknown · odorCREW REPORTED THAT ON DESCENT, AFTER ANTI-ICE SYSTEM WAS ACTIVATED, THAT THERE WAS A BURNING SMELL IN THE COCKPIT. ON CALL MAINTENANCE INSPECTED THE ELECTRICAL AREA BEHIND THE CAPTAIN'S SEAT, AND PERFORMED OPERATIONAL CHECKS OF THE ANTI-ICING AND BLEED SYSTEMSDR CHQA201100101Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON AN EXISTING REPAIR ON THE LEFT OMEGA BEAM FLANGE AT FRAME 20. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM FLANGE AT FRAME 20 AND RE-INSTALLED IAW SRM 53-00-10.SDR CHQA201100102Beam · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CARGO DOOR SURROUND STRUCTURE LOWER BEAM. MAINTENANCE REPLACED THE CARGO DOOR SURROUND STRUCTURE LOWER BEAM IAW SRM 51-40-02.SDR CHQA201100103Floor Support · corrodedDURING INSPECTION THE CABIN FLOOR STRUCTURE LEFT OMEGA BEAM AFT ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE LEFT OMEGA BEAM AT FRAME 20 IAW SRM 51-40-02.SDR CHQA201100104Structure · corrodedDURING INSPECTION THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I PASSENGER DOOR U SHAPE WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I PASSENGER DOOR U SHAPE AND INSTALLED WITH A SOLID RIVET IAW SRM 51-40-02.SDR CHQA201100105Rib · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I AFT GALLEY RIB. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I AFT GALLEY RIB AND INSTALLED WITH A SOLID RIVET IAW SRM 51-40-02.SDR CHQA201100106Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I ANGLE MIDDLE SUPPORT. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I ANGLE MIDDLE SUPPORT AND INSTALLED WITH A SOLID RIVET IAW SRM 51-40-02.SDR CHQA201100115Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02.SDR CHQA201100116Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02.SDR CHQA201100117Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02.
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