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 CHQA201100118Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LEFT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02.SDR CHQA201100054Air Duct · contaminatedSHORTLY AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED THAT A LARGE AMOUNT OF WATER SPILLED OUT OF THE GALLEY CART AND RAN BACK INTO THE FLOOR AIR CONDITIONING INLET AT ROW 3. SHORTLY AFTER, THERE WAS A SMALL AMOUNT OF SMOKE REPORTED IN THE CABIN ALONG WITH A LSDR CHQA201100055O-Ring · tornCREW REPORTED THAT DURING CRUISE REPORTED A BLEED 2 LEAK MESSAGE IN ICING CONDITIONS ACCOMPANIED BY A BURNT RUBBER ODOR. THE AIRCRAFT DIVERTED TO KBTV AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LEAK AT JOINT 19 BEHIND THE CARGO COMPARTMENT SIDE WALL. SDR CHQA201100053Light · inoperativeDURING INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100051Controller · inoperativeCREW REPORTED, AFTER TAKEOFF WERE UNABLE TO CONTROL THE CABIN ALTITUDE IN MANUAL MODE WHILE THE AUTO MODE WAS ON DEFERRAL. IT WAS REPORTED THAT THE CABIN ALTITUDE WAS CLIMBING AT APPROXIMATELY THE SAME RATE AS THE AIRCRAFT AT ALL SETTINGS. THE AIRCRAFT RETURSDR CHQA201100050Check Valve · damagedFLT CREW REPORTED WHILE CLIMBING THROUGH FL270, RECEIVED A "CABIN" AURAL WARNING. NO RELATED EICAS MESSAGES DISPLAYED. CABIN PRESSURE INDICATED OVER 10,000FT & REPORTED TO BE CLIMBING TO 11,000FT. MEMORY ITEMS FOLLOWED & ACFT BEGAN DESCENT TO 10,000FT & DECSDR CHQA201100048Switch · intermittentFLIGHT CREW REPORTED A BLEED 1 VALVE CLOSED MESSAGE SHORTLY AFTER TAKEOFF AND RETURNED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 BLEED PUSH BUTTON AND THE E1 FAN AIR VALVE FILTER AS A PRECAUTION, WITH NO FURTHER DEFECTS BEING NOTED DURSDR CHQA201100049Wire · brokenDURING INSPECTION THE NR 1 FLOOR PROXIMITY EMERGENCY LIGHT WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REPLACED THE NR 1 FLOOR PROXIMITY LIGHT STRIP WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100047Controller · failedFLIGHT CREW REPORTED A PRESSURIZATION AUTO FAIL MESSAGE WHILE CLIMBING THROUGH FL270. CREW ALSO REPORTED THAT THE CABIN ALTITUDE WAS ALSO CLIMBING. THE PASSENGER OXYGEN GENERATORS WERE DEPLOYED AND THE AIRCRAFT DESCENDED TO FL100. THE AIRCRAFT LANDED IN MKESDR CHQA201100075Doubler · crackedDURING INSPECTION A CRACK WAS FOUND ON THE INTERNAL DOUBLER ON THE AFT BOTTOM CORNER OF THE MAIN PASSENGER DOOR. THE INTERNAL DOUBLER ON THE AFT BOTTOM CORNER OF THE MAIN PASSENGER DOOR WAS REPAIRED IAW ETD 2011-145/02468.SDR CHQA201100076Fitting · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE AFT STEP FITTING ASSEMBLY. THE MAIN PASSENGER DOOR STRUCTURE AFT STEP FITTING WAS REPLACED.SDR CHQA201100077Fitting · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD STEP FITTING ASSEMBLY. THE MAIN PASSENGER DOOR STRUCTURE FORWARD STEP FITTING ASSEMBLY WAS REPLACED.SDR CHQA201100078Profile · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD U PROFILE. THE MAIN PASSENGER DOOR STRUCTURE FORWARD SIDE "U" PROFILE WAS REPLACED.SDR CHQA201100081Channel · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD BOTTOM CORNER CHANNEL. THE MAIN PASSENGER DOOR STRUCTURE FORWARD BOTTOM CORNER CHANNEL WAS REPLACED.SDR CHQA201100082Rib · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD SUPPORT ASSEMBLY BOTTOM RIB. THE MAIN PASSENGER DOOR STRUCTURE FORWARD SUPPORT ASSEMBLY BOTTOM RIB WAS REPLACED.SDR CHQA201100083Angle · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD ANGLE ON AFT SIDE OF BOTTOM RIB. THE MAIN PASSENGER DOOR STRUCTURE FORWARD ANGLE ON AFT SIDE OF BOTTOM RIB WAS REPLACED.SDR CHQA201100084Rib · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM RIB. THE MAIN PASSENGER DOOR BOTTOM RIB WAS REPLACED.SDR CHQA201100085Door Frame · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM FRAME 1. THE MAIN PASSENGER DOOR STRUCTURE BOTTOM FRAME 1 WAS REPLACED.SDR CHQA201100086Door Frame · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM FRAME 2. THE MAIN PASSENGER DOOR STRUCTURE BOTTOM FRAME 2 WAS REPLACED.SDR CHQA201100087Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE AFT SUPPORT ASSEMBLY ON BOTTOM RIB. THE MAIN PASSENGER DOOR STRUCTURE AFT SUPPORT ASSEMBLY ON BOTTOM RIB WAS REPLACED.SDR CHQA201100088Angle · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE ANGLE BETWEEN FRAME 2 AND BOTTOM RIB. THE MAIN PASSENGER DOOR STRUCTURE ANGLE BETWEEN FRAME 2 AND BOTTOM RIB WERE REPLACED.SDR CHQA201100089Fitting · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE AFT FITTING ON BOTTOM RIB. THE MAIN PASSENGER DOOR STRUCTURE AFT FITTING ON BOTTOM RIB WAS REPLACED.SDR CHQA201100090Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON EXISTING REPAIR ON LEFT OMEGA BEAM FLANGE AT FRAME 20. THE REPAIR WAS REPLACED ON THE LEFT OMEGA BEAM FLANGE IAW SRM 53-00-10.SDR CHQA201100091Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE RIGHT OMEGA BEAM FLANGE AT FRAME 25. THE CABIN FLOOR STRUCTURE RIGHT OMEGA BEAM LOWER FLANGE AT FRAME 25 WAS REPAIRED IAW ETD2011-145/02427.SDR CHQA201100092Reinforcement · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR AFT SURROUND STRUCTURE. THE THICKNESS MEASUREMENT DONE BY UT IAW NDI MANUAL P.22 (F) ON REWORKED AREA FOUND THE MINIMUM MATERIAL THICKNESS REMAINING AT 0.022 INCHES. HFEC DONE ON THE AREA FOUND NO CRASDR CHQA201100079Channel · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD CHANNEL SPLICE. THE MAIN PASSENGER DOOR STRUCTURE FORWARD CHANNEL SPLICE WAS REPLACED.SDR CHQA201100080Casting · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE OPEN HANDLE BACK CASTING. THE MAIN PASSENGER DOOR OPEN HANDLE BACK CASTING WAS REPLACED.SDR CHQA201100097Skin · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR SURROUND LOWER PORTION AT FRAME NR 20. A THICKNESS MEASUREMENT WAS DONE BY UT IAW NDI MANUAL, INTRODUCTION P 22 (F). MINIMUM MATERIAL REMAINING IS 0.66 INCHES. A HIGH FREQUENCY EDDY CURRENT INSPECTIOSDR CHQA201100098Door Frame · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR SURROUND LOWER PORTION AT FRAME NR 22. A THICKNESS MEASUREMENT WAS DONE BY UT IAW NDI MANUAL, INTRODUCTION P 22 (F). MINIMUM MATERIAL REMAINING IS 0.22 INCHES. A HIGH FREQUENCY EDDY CURRENT INSPECTIOSDR CHQA201100095Window Frame · damagedDURING INSPECTION THE TOP WINDSHIELD CUTOUT STRUCTURE WAS FOUND TO BE DAMAGED AT THE LEFT FAIRING ATTACHMENT BRACKET. EDDY CURRENT INSPECTION CARRIED OUT ON LEFT BLEND IAW NDI MANUAL, INTRODUCTION P 17, NO CRACK FOUND. THE TOP WINDSHIELD CUT OUT STRUCTURE AT SDR CHQA201100096Window Frame · damagedDURING INSPECTION THE TOP WINDSHIELD CUT OUT STRUCTURE WAS FOUND TO BE DAMAGED AT THE RIGHT FAIRING ATTACHMENT BRACKET. EDDY CURRENT INSPECTION CARRIED OUT ON LEFT BLEND IAW NDI MANUAL, INTRODUCTION P 17, NO CRACK FOUND. THE TOP WINDSHIELD CUTOUT STRUCTURE ASDR CHQA201100093Angle · crackedDURING INSPECTION THE RIGHT OUTBOARD ANGLE THAT JOINS THE OMEGA BEAM AND THE WING STUB UPPER SKIN WAS FOUND TO BE CRACKED. THE RIGHT OUTBOARD ANGLE WAS REPAIRED IAW SRM 53-23-02.SDR CHQA201100094Angle · crackedDURING INSPECTION THE RIGHT INBOARD ANGLE THAT JOINS THE OMEGA BEAM AND THE WING STUB UPPER SKIN WAS FOUND TO BE CRACKED. THE RIGHT INBOARD ANGLE WAS REPAIRED IAW SRM 53-23-02.SDR CHQA201100043Light · inoperativeDURING INSPECTION, THE RIGHT EXIT ROW EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT EXIT ROW EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100044Battery Pack · inoperativeFLT 5045, DURING INSPECTION, BOTH THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100045Light · inoperativeDURING INSPECTION, THE NR 3 FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 3 FLOOR PROXIMITY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100046Light · inoperativeDURING INSPECTION THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100041Connector · corrodedCREW REPORTED THAT AFTER TAKEOFF THE THRUST MODE WOULD NOT CHANGE FROM TAKEOFF MODE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CORROSION ON CONNECTOR P0885. THE CORROSION WAS CLEANED AND THE CONNECTOR WAS RE-CONNECTED. OPERASDR CHQA201100042Inverter · inoperativeDURING INSPECTION, THE FORWARD OVERWING EXIT LOCATOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER FOR THE FORWARD OVERWING EXIT LIGHT LOCATOR. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100040Engine · malfunctionedCREW REPORTED THAT AFTER LEVELING OFF AT 23,000FT, REPORTED SMELLING A BURNING OIL/ELECTRICAL ODOR. THE CAPTAIN AND FIRST OFFICER DONNED OXYGEN MASKS AND PROCEEDED TO DIVERT TO IND. THE ODOR WAS CONTAINED MAINLY TO COCKPIT BUT FLIGHT ATTENDANT DID REPORT A SSDR CHQA201100119Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE ANGLE THAT JOINS THE OMEGA BEAM AND THE WING STUB SKIN ON THE RIGHT HAD SIDE. MAINTENANCE REPAIRED THE ANGLE AT THE RIGHT OMEGA BEAM AT THE WING STUB SKIN IAW SRM 53-23-02. THE ANGLE WAS FABRICATED LOCALLY IAW ETD201SDR CHQA201100120Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE ANGLE THAT JOINS THE OMEGA BEAM AND THE WING STUB SKIN ON THE RIGHT HAD SIDE. MAINTENANCE REPAIRED THE ANGLE AT THE RIGHT OMEGA BEAM AT THE WING STUB SKIN IAW SRM 53-23-02. THE ANGLE WAS FABRICATED LOCALLY IAW ETD20SDR CHQA201100114Skin · damagedDURING INSPECTION DAMAGE FROM A LIGHTNING STRIKE WAS FOUND ON CENTER FUSELAGE SKIN, SECTION II, AT FRAME 26, BETWEEN STRINGERS 4L AND 5L. MAINTENANCE PERFORMED AN EDDY CURRENT INSPECTION ON THE CUT-OUT IAW ETD2010-145-00077 AND NO CRACKS WERE FOUND. THE LIGHSDR CHQA201100121Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON AN EXISTING REPAIR ON THE LEFT OMEGA BEAM FLANGE AT FRAME 25. THE LEFT OMEGA BEAM FLANGE AT FRAME 25 CORROSION REPAIR WAS REPLACED IAW SRM 53-00-10.SDR CHQA201100038Connector · brokenDURING INSPECTION THE NR 1 EMERGENCY LIGHT PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE REMOVABLE SPLICE CONNECTOR ON THE NR 1 FLOOR PROXIMITY LIGHT WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100039Light · inoperativeDURING INSPECTION, THE NR 4 PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 PROXIMITY LIGHT STRIP AND OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100036Fire Loop · failedCREW REPORTED AN E1 FIRE DETECT FAIL MESSAGE IN FLIGHT. THE AIRCRAFT CONTINUED TO DCA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE E1 FIRE DETECTION LOOP WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100037Connector · looseCREW REPORTED THAT ON APPROACH WHEN THE LANDING GEAR WAS SELECTED DOWN, THERE WAS A RED NOSE LANDING GEAR INDICATION AND A LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS. THE GEAR WAS RETRACTED AGAIN AND THEN EXTENDED WITH NO FURTHER DIFFICULTIES. THE AIRCRAFTSDR V0XR20110211012Profile · corrodedLEFT OTBD PROFILE AT FR 61 IS CORRODED OUT OF LIMITS. R & R LT OTBD PROFILE AT FR 61 IAW SRM 51-10-02, 51-40-02, 51-21-04, 51-21-05.SDR V0XR20110211013Shroud · wornLT OTBD FLAP INBD AND OTBD FLAP DRIVERS ARE WORN OUT. R & R LT OTBD FLAP INBD AND O/D FLAP DRIVER SHROUDS IAW AMM 25-50-00. (PN'S 145-68246-001 AND 145-68249-001).
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