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 CHQA201000081Solenoid Valve · faultyCREW REPORTED THAT DURING CLIMBOUT A VIBRATION AND LOW RUMBLE COULD BE HEARD AND FELT. AFTER LEVELING OFF, THE AIRCRAFT WOULD NOT ACCELERATE PAST 0.70 MACH IN CLIMB MODE. THE AIRCRAFT DIVERTED TO SDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSSDR CHQA201000079Solenoid Valve · faultyCREW RETURNED TO FIELD DUE TO A RUMBLING NOISE FROM THE NOSE LANDING GEAR AREA AFTER GEAR RETRACTION. THE AIRCRAFT WAS FERRIED TO SDF FOR FURTHER TROUBLESHOOTING. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOOR SOLENOID, ALL THREE HYDRAULIC MANIFOLD FILTERS,SDR CHQA201000078Landing Gear · malfunctionedON DEPARTURE THE CREW REPORTED THAT IT TOOK THE NOSE LANDING GEAR ALMOST 1 MINUTE TO RETRACT AFTER SELECTING THE GEAR UP. A LANDING GEAR DISAGREE MESSAGE WAS ALSO REPORTED. THE AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FIM SDR CHQA201000077Pump · leakingAIRCRAFT DIVERTED TO KGSO DUE TO A HYDRAULIC SYSTEM 1 LOW QUANTITY MESSAGE IN FLIGHT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE ENGINE 1 ENGINE DRIVEN PUMP LEAKING. THE ENGINE DRIVEN PUMP WAS REPLACED AND THE SYSTEM SERVICESDR CHQA201000076Duct · disconnectedAFTER TAKEOFF THE CREW REPORTED THAT THE AIRCRAFT DID NOT SHOW EVIDENCE OF PRESSURIZING. THE CABIN RATE FOLLOWED THE AIRCRAFT'S RATE FOR THE FLIGHT'S DURATION, AS DID CABIN/AIRCRAFT ALTITUDE. THE CREW REPORTED THAT WITH PACK 1 ON MEL, PACK 2 HAD INSUFFICIENTSDR CHQA201000075Battery Pack · dischargedDURING INSPECTION, ALL FOUR EMERGENCY LIGHT BATTERY PACKS WERE FOUND TO BE DISCHARGED. ALL FOUR EMERGENCY LIGHT BATTERIES WERE REPLACED WITH NO FURTHER DEFECTS NOTED. BATTERY NR 2: P/N: RPS1-B, S/N: 16905, TSN: 20686, CSN: 17308, TSR: 368; BATTERY NR 3: P/N:SDR CHQA201000074Wire · brokenDURING INSPECTION A PROXIMITY LIGHT STRIP WIRE LEAD WAS FOUND BROKEN. MAINTENANCE REPAIRED THE BROKEN WIRE ON THE EMERGENCY LIGHT FLOOR PROXIMITY STRIP IAW EMB SWPM 20-21-00 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000073Inverter · defectiveDURING INSPECTION THE LAST TWO ROWS OF EMERGENCY FLOOR LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE FOUND MULTIPLE FUSES IN BATTERY NR 4 BLOWN AND INVERTER NR 6 PRODUCING A HIGH PITCHED WHINE. THE NR 4 BATTERY PACK AND NR 6 INVERTER WERE REPLACED WITH NO FURTHSDR CHQA201000072Wire · brokenCREW REPORTED A BLEED 2 LEAK MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BROKEN WIRE ON THE TEMP SENSOR NEAR THE ENGINE START GROUND PNEUMATIC CONNECTION. THE WIRE WAS INTERMITTENTLY GROUNDING OUT ANDSDR CHQA201000071Air Duct · crackedCREW REPORTED A BLEED SYSTEM 2 LEAK MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE BLEED SYSTEM AND FOUND THE Y-DUCT IN THE NR 2 PYLON CRACKED. THE Y-DUCT WAS REPLACED WITH NO FURTHER DEFECTS NOTEDSDR SIMA201009504Carbon Seal · leakingON FLIGHT 4336 THE CREW REPORTED A STRONG OILY ODOR IN THE COCKPIT DURING FLIGHT AND THE STRONGEST ODOR OCCURRING DURING TAKEOFF ALT-TO -1 PACKS ON. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE NUMSDR CHQA201000069Light · malfunctionedCREW REPORTED THAT THE EMERGENCY LIGHTS WERE FLASHING ON AND OFF INTERMITTENTLY. MAINTENANCE RESET THE EMERGENCY LIGHTS IAW EMB AMM 35-50-00.SDR CHQA201000070Relay · intermittentCREW REPORTED THAT THE EMERGENCY LIGHTS WERE TURNING ON AND OFF INTERMITTENTLY. MAINTENANCE REPLACED RELAY K0275 PER AMM 20-10-02, OPS CHECK OF EMERGENCY LIGHTS WAS NORMAL.SDR V0XR201003300001Seat Track · corrodedRT LOWER SEAT TRACK BETWEEN FR 47-52 CTR FUSELAGE III IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2155.SDR CHQA201000068Battery Pack · dischargedDURING INSPECTION, BOTH OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04 WITH NO FURTHER DEFECTS NOTED.SDR V0XR201003390002Seat Track · corrodedRT LOWER SEAT TRACK BETWEEN FR 47-52 CTR FUSELAGE II IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2155.SDR V0XR201003390003Seat Track · corrodedRT LOWER SEAT TRACK BETWEEN FR 36-47 CTR FUSELAGE III IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2159.SDR CHQA201000065Coupler · inoperativeDURING APPROACH INTO CVG, THE LOCALIZER INDICATED RED X'S ON PFD 1, 2 & STANDBY. THE AIRCRAFT RETURNED TO SDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE VOR/LOC ANTENNA COUPLER-DIVIDER PER EMB 145 AMM 34-32-12, OPS CHECK GOOD. MAINTENANCE ALSO RESDR CHQA201000066Windshield · crackedDURING FLIGHT THE FIRST OFFICER'S WINDSHIELD CRACKED. THE AIRCRAFT RETURNED TO DCA AND LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD IAW EMB AMM 56-10-01, OPS AND LEAK CHECK GOOD.SDR CHQA201000067Inverter · weakDURING INSPECTION, THE RIGHT EMERGENCY EXIT LIGHT WAS FOUND TO BE DIM WHEN ILLUMINATED. MAINTENANCE REPLACED THE NR 5 EMERGENCY LIGHT DC/AC INVERTER IAW EMB 140 AMM 33-50-11.SDR CHQA201000064Control System · out of adjustDURING THE CLIMB CHECKLIST, THE CREW NOTICED THAT THE CABIN PRESSURE HAD NOT STARTED TO CLIMB. IT CONTINUED TO READ 0 FPM ON CLIMB RATE. AFTER REACHING 20,000FT THE INDICATION WAS STILL ZERO AND THE CREW ELECTED TO RETURN TO FIELD. THE AIRCRAFT LANDED BACK SDR CHQA201000063Connector · disconnectedDURING INSPECTION THE LEFT AFT FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN CONNECTION. THE LEFT AFT FLOOR PROXIMITY LIGHT CONNECTOR WAS RECONNECTED IAW EMB SWPM 20-21-00, NO FURTHER DEFECTS NOTED.SDR V0XR201003260009Floor Support · corrodedLT OTBD FWD DIGITAL FR 14-17 IS CORRODED BEYOND LIMITS. R & R DIGITAL. W/C 2102SDR CHQA201000061Brake Sys · malfunctionedCREW REPORTED THAT ON GEAR EXTENSION, "BRK OUTBD INOP" MESSAGE APPEARED ON EICAS. CREW FOLLOWED QRH AND REPORTED THAT ON LANDING ROLL OUT IT FELT LIKE BRAKES WERE ONLY HALF AS EFFECTIVE. ON TAXI A "BRK OVERHEAT" MESSAGE WAS REPORTED AND MFD INDICATED THE OUTSDR CHQA201000062Light · inoperativeDURING INSPECTION, THE FLOOR EMERGENCY LIGHT BETWEEN ROWS 7 AND 9 WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE FLOOR EMERGENCY LIGHT STRIP BETWEEN ROWS 7 AND 9 IAW E135 AMM 33-50-12, OPS CHECK GOOD.SDR CHQA201000060Battery Pack · dischargedDURING INSPECTION THE NR 4 EMERGENCY LIGHT BATTERY WAS INOP WHEN TESTED. MAINTENANCE REPLACED THE NR 4 BATTERY IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD.SDR CHQA201000059Wire · brokenDURING INSPECTION FLOOR 241DF AISLE FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REPLACED THE FLOOR 241DF FLOOR PROX LIGHT STRIP IAW EMB 145 AMM 33-50-20. OPS CHECK GOOD.SDR C2XA10RI042Fadec · defectiveFLIGHT 2882 - FLIGHT CREW REPORTED PARTIAL LOSS OF POWER ON ENGINE 1, 2 TIMES IN FLIGHT. DURING CRUISE, N1 WENT DOWN TO 67 PERCENT, IGN A AND B CAME ON AND RESTORED POWER ALSO ENGINE 1 SHORT DISPATCH ON EICAS. EWR MX REMOVED FADEC 1A AND 1B AND PERFORMED OPESDR C2XA10RI043Fadec · defectiveFLIGHT 2882 - FLIGHT CREW REPORTED PARTIAL LOSS OF POWER ON ENGINE 1, 2 TIMES IN FLIGHT. DURING CRUISE, N1 WENT DOWN TO 67 PERCENT, IGN A AND B CAME ON AND RESTORED POWER ALSO ENGINE 1 SHORT DISPATCH ON EICAS. EWR MX REMOVED FADEC 1A AND 1B AND PERFORMED OPESDR CHQA201000058Static Inverter · failedWHILE EN ROUTE FROM SDF TO LGA THE CREW RECEIVED A 115 VAC OFF BUS MESSAGE ON EICAS. THIS FAILURE DISABLED THE WIND SHEAR ALERTING SYSTEM AND BECAUSE OF WIND SHEAR IN THE LGA AREA, THE AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACESDR CHQA201000057Bushing · wornAFTER REACHING V1 ON TAKEOFF THE CREW REPORTED THE YOKE REQUIRED EXCESSIVE FORCE TO COMMAND THE ELEVATOR. THE AIRCRAFT ROTATED AND ONCE AIRBORNE THE ELEVATOR CONTINUED TO FEEL STIFF. THE CREW DECLARED AN EMERGENCY AND REQUESTED TO DIVERT TO KJFK. AS THE AIRSDR DXTA2010031504033Control Handle · malfunctionedLANDING GEAR HANDLE WOULD NOT ALLOW FOR GEAR RETRACTION AFTER TAKEOFF. REMOVED FAULTY LANDING GEAR CONTROL HANDLE. INSTALLED REPAIRED LANDING GEAR CONTROL HANDLE. PERFORMED OPS CHECK GOOD IAW MM 32-30-01.SDR CHQA201000056Coupler · inoperativeAIRCRAFT DIVERTED TO KCMH DUE TO AN OPEN ILS MEL AND THE WEATHER CONDITIONS IN KDCA THAT REQUIRED AND ILS APPROACH. MAINTENANCE TROUBLESHOT THE FAULT AND FOUND THE MARKER BEACON AND GLIDE SLOPE SYSTEMS TO BE OPERATING NORMALLY AND ONLY THE LOCALIZER TO BE MALSDR CHQA201000054Battery Pack · dischargedDURING INSPECTION THE NR 1 EMERGENCY LIGHT PANEL AND THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WERE INOP DURING TESTING. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK IAW EMB 145 AMM 33-50-04 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000055Battery Pack · dischargedDURING INSPECTION THE AFT EXTERIOR EMERGENCY LIGHTS AND THE NR 4 EMERGENCY LIGHT CEILING PANEL WERE INOP WHEN TESTED. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK IAW EMB 145 AMM 33-50-04 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000052Rmu · frozenAIRCRAFT RETURNED TO FIELD DUE TO RMU NR 1 REVERTING TO PREVIOUSLY ENTERED FREQUENCY IN STANDBY MODE AND RMU NR 2 FREEZING DURING CLIMBOUT. MAINTENANCE REPLACED THE NR 2 RMU WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000053Light · inoperativeDURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS INOP. MAINTENANCE RELAMPED THE FIXTURE IAW EMB 145 AMM 33-50-09, OPS CHECK GOOD.SDR DJFA2010006Acm · seizedON DESCENT CREW REPORTED SMOKE IN THE COCKPIT FOLLOWED BY A BURNING SMELL. ACFT LANDED SAFELY. MX FOUND THE AFT ACM FAILED AND PRODUCING SMOKE. THE ACM WAS REPLACED.SDR V0XR201003040003Support Angle · corrodedOTBD RT SILL SUPPORT ANGLE FROM LY 479.0 AT FRM 18.5 IS CORRODED BEYOND LIMITS. R & R SUPPORT ANGLE.SDR CHQA201000050Inu · inoperativeDURING DESCENT INTO BNA THE CREW REPORTED NAV 1 AND 2 BOTH FAILED AND THE RMU NAV 1 AND 2 BOXES INDICATED DASHES. THE AIRCRAFT DIVERTED TO SDF WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH NAV 1 AND 2 UNITS WITH NO FURTHER DEFECTS NOTED. (NAV SDR CHQA201000051Unknown · malfunctionedCREW RECEIVED ATT: CAGE MESSAGE ON ISIS IN FLIGHT. IN STABLE FLIGHT THE CREW TRIED TO RESET PER QRH AND FAILED TO GET ATT 10'S FLAG AND RETURNED TO FIELD. MAINTENANCE TROUBLESHOT THE FAULT PER FIM 34-01-00-810-809-A AND FOUND IT TO BE A TRANSITORY CONDITIONSDR V0XR201003010001Sill · corrodedSILL ON SERVICE IS CORRODED BEYOND LIMITS. R & R SILL.SDR V0XR201003010002Floor Support · corrodedLT FWD DIGITAL AT FRM 15-17.5 IS CORRODED BEYOND LIMITS. R & R DIGITAL.SDR V0XR201003010003Floor Support · corrodedCTR PORTION OF FWD DIGITAL AT FRM 15-17.5 IS CORRODED BEYOND LIMITS. R & R DIGITAL.SDR V0XR201003010004Floor Support · corrodedRT PORTION OF FWD DIGITAL AT FRM 15-17.5 IS CORRODED BEYOND LIMITS. R & R DIGITAL.SDR V0XR201003010005Sill · corrodedLT SILL FROM FRM 18-23 IS CORRODED BEYOND LIMITS. R & R LT SILL.SDR V0XR201003010006Floor Support · corrodedFLOOR ANGLE UNDER PASSENGER DOOR ARE CORRODED BEYOND LIMITS. R & R FLOOR ANGLE.SDR V0XR201003010007Gusset · corrodedLT GUSSET AT LY - 479.0 FROM FRM 59-61 IS CORRODED BEYOND LIMITS. R & R LT GUSSET.SDR V0XR201003010008Gusset · corrodedCTR GUSSET AT YO.O FROM FRM 59-61 IS CORRODED BEYOND LIMITS. R & R CTR GUSSET.SDR V0XR201003010009Gusset · corrodedRT GUSSET AT RY 479.0 FROM FRM 59-61 IS CORRODED BEYOND LIMITS. R & R RT GUSSET.
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