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 SIMA200435801Sill · corrodedDURING CPCP INSPECTION FOUND FORWARD CABIN LT SILL CORRODED. REMOVED AND REPLACED SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)SDR SIMA200435802Angle · corrodedDURING CPCP INSPECTION FOUND ANGLE CORRODED THROUGH AFT END. REMOVED AND REPLACED FORWARD CABIN FLOOR ANGLE WITH A NEW ANGLE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501) (K)SDR SIMA200435804Floorbeam · corrodedDURING CPCP INSPECTION, FOUND THE FLOOR DIGITAL CORRODED IN SEVERAL AREAS REMOVED AND REPLACED FLOOR DIGITAL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)SDR SIMA200435805Sill · corrodedDURING CPCP INSPECTION, FOUND THE FORWARD CABIN FLOOR RT SILL HAS CORROSION AROUND NUTPLATE. REMOVED AND REPLACED SILL ASSY IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)SDR SIMA200435812Skin · dentedDURING MBV INSPECTION, A DENT WAS FOUND AFT OF RADOME FRAME 1 AND STRINGER 13 R. REPLACED DAMAGED SECTION OF SKIN IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)SDR SIMA200435816Floorbeam · corrodedDURING AN MBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. BLENDED DIGITAL TO REMOVED CORROSION. FABRICATED A DOUBLER FOR REPAIR. REPAIR DONE IAW SRM. (SW21200501984) (K)SDR SIMA200435820Beam · corrodedDURING AN MBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER HAT BEAM. INSTALLED SERVICEABLE HAD BEAM IAW SRM. (SW21200501979) (K)SDR C2XA04RI018Engine · malfunctionedDURING FLIGHT AFTER ENGINE BLEEDS WERE SELECTED THE LAV SMOKE ALARM CAME ON ALONG WITH THE LAV SMOKE INDICATION ON THE EICAS. REMOVED AND REPLACED THE NR 1 ENGINE. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200435803Floor Support · corrodedDURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR OMEGA SHAPE CORRODED. REPAIRED FORWARD LT CABIN OMEGA SHAPE AT FRAME 20 CROSSBEAM ATTACH JUNCTION IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)SDR SIMA200435806Floor Support · corrodedDURING CPCP INSPECTION, FOUND THE SUPPORT CORRODED UPPER AFT END. REMOVED AND REPLACED FLOOR SUPPORT BETWEEN FRAME 19 AND FRAME 20 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200435807Angle · corrodedDURING CPCP INSPECTION, FOUND THE MAIN DOOR SILL ANGLES ARE CORRODED. REMOVED AND REPLACED MAIN DOOR SILL ANGLES IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)SDR SIMA200435808Sill · corrodedDURING CPCP INSPECTION, FOUND THE SERVICE DOOR SILL CORRODED AROUND NUTPLATES UPPER SURFACE. REMOVED AND REPLACED SERVICE DOOR SILL PLATE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)SDR SIMA200435811Doubler · corrodedDURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR DOUBLERS HAVE CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR DOUBLERS IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)SDR SIMA200435813Stringer · chafedDURING AN IMBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT BELLEY FAIRING CUTOUT. BLENDED THE CHAFED AREA. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE, 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501981) (K)SDR SIMA200435815Sill · corrodedDURING INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW SRM. (SW21200501979) (K)SDR SIMA200435819Stringer · chafedDURING AN IMBV INSPECTION STRINGER 19R WAS FOUND TO BE CHAFED AT AFT BELLY FAIRING CUT OUT. BLENDED THE CHAFED AREA. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE, 2 SHIMS. REPAIR DOEN IAW SRM. (SW21200501981) (K)SDR SIMA200435207Starter Gen · malfunctionedCREW REPORTED ELECTRICAL SMELL IN COCKPIT AFTER ATTEMPTED APU START WHICH FAILED. INSPECTED APU AND FOUND STARTER GENERATOR TO BE MAKING LOUD NOISES AND SPARKING ON START UP. MAINTENANCE REMOVED AND REPLACED THE STARTER/GENERATOR IAW MM. GROUND RUN WAS COMPSDR SIMA200435809Sill · corrodedDURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR SILL ASSEMBLY HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED FORWARD SILL ASSEMBLY IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)SDR SIMA200435810Gusset · corrodedDURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR GUSSET HAS CORROSION ON UPPER SURFACE. INSTALLED NEW GUSSET IAW SRM. AC RETURNED TO SERVICE. (SW21200501985) (K)SDR SIMA200429802Floorbeam · crackedDURING AN MBV INSPECTION A CRACK WAS DISCOVERED ON THE FORWARD DIGITAL AT FRAME 13. PERFORMED EDDY CURRENT INSPECTION TO DETERMINED THE LENGTH OF THE CRACK AND STOP DRILLED THE CARCK. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW STATEMENT IC2004/145-4832. SDR SIMA200435204Pressure Switch · failedDURING CLIMB, THE YAW DAMP FAILED FOLLOWED BY RUDDER SYS-1 INOPERATIVE. FOLLOWED BY THE RUDDER SYS-2 INOPERATIVE. AIRCRAFT WAS CONTROLLABLE AND RETURNED AS A PRECAUTION . MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER PRESSURE SWITCH IAW MM. OPS CHECK WASDR C2XA04CL126Engine · leakingCREW REPORTED A LAV SMOKE WARNING AFTER TAKEOFF. AIRCRAFT RETURNED TO EWR WITHOUT INCIDENT. REPLACED THE NR 2 ENGINE AND AIRCRAFT RETURNED TO SERVICE.SDR SIMA200434903Battery · dischargedDURING EMERGENCY LIGHT TEST ALL LIGHTS ILLUMINATE MOMENTARILY THEN ALL LIGHTS AFT OF ROW 7 DIM AND GO OUT. REPLACED NR1, NR2, NR3 AND NR4 BATTERY PACKS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. BATTERY PN 2013BR SN OFF NR1-B2425/ NR2-B2430 / NR3-B2433SDR SIMA200434904Skin · lightning strikeLIGHTNING STRIKE DAMAGE FOUND ON SKIN AT FRAME 20 BETWEEN STRINGERS 3L AND 4L. MAINTENANCE COMPLETED A PATCH REPAIR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501814) (K)SDR SIMA200435205Actuator · inoperativeCREW REPORTED DURING CLIMB, THE RUDDER TRIM JAMMED RT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE YAW TRIM ACTUATOR IAW MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200434902Control Unit · failedDUAL PITCH TRIM FAIL ON CLIMBOUT. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200501813) (K)SDR CHQA000593Carbon Seal · leakingFLIGHT 3192 DEPARTING SDF, DURING TAKEOFF ROLL, THE CREW HAD SMOKE IN THE COCKPIT AND ABORTED THE TAKEOFF. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE LEFT ENGINE "0" CARBON SEAL LEAKING. REMOVED AND REPLACED E1 0 CARBON SEAL. OPS CHECK GOOD.SDR SIMA200434504Power Supply · inoperativeDURING PRE-FLIGHT THE EMERGENCY LIGHTS FROM ROW NINE BACK WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPLY UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200435202Skin · dentedDURING AN MBV INSPECTION AND REPAIR OF A DENT DEFERRED UNDER TDMI NR 84053525 BETWEEN FRAMES 21 AND 22 AND BETWEEN STRINGERS 12L AND 13L. PERFORMED A CUTOUT OF THE DAMAGED SKIN AND TREATED THE BARE METAL EDGES. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIRSDR SIMA200435201Floor Support · corrodedDURING AN MBV INSPECTION OF AIRCRAFT. THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUTOUT A SECTION OF THE DAMAGED OMEGA BEAM AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR ANGLE .050 IN, REPAIR PLATE .125 IN, SHIMS AND A FILLER. REPAIR DONE IASDR SIMA200434503Connector · looseCREW REPORTED THE EMERGENCY LIGHTS AT SEAT 3BC AND GALLEY SERVICE DOOR ARE INOPERATIVE. MAINTENANCE FOUND CONNECTOR PLUG LOOSE ON BATTERY PACK RECONNECTED CONNECTOR PLUG. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501826) (K)SDR SIMA200435203Sill · corrodedDURING AN MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED, REMOVED EXISTING CENTER SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW SRM AND CORROSION PREVENTATIVE MANUAL.SDR SIMA200434501Bulb · inoperativeFA REPORTED A BURNING SMELL AT 16000 FT. DECLARED EMERGENCY AND RETURNED TO FIELD. THE FLIGHT ATTENDANT NOTICED AFTER LANDING THAT THE FORWARD OVERHEAD ENTRY LIGHT ABOVE HIS SEAT WAS BURNED OUT. CONTACTED MAINTENANCE, VERIFIED THAT THE BULBS WERE BURNED ANDSDR SIMA200434502Charger · inoperativeCREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS FROM ROW 8 THRU 12 DO NOT STAY ON WHEN TESTED THEY COME ON THEN IMMEDIATELY GO OUT. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICESDR SIMA200434202Relay · inoperativeICE CONDITION ANTI-ICE WARNING. ENGINE 2, FIRE DETECTION FAIL EICAS MESSAGE. REPLACED AIR GROUND RELAY AT LT RELAY SUPPORT B14. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.(K)SDR SIMA200434217Floor Support · corrodedTHE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER, FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM.(K)SDR SIMA200434221Floor Support · corrodedTHE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER AND INSTALLED. REPAIR DONE IAW SRM. (K)SDR C2XA04BT123Engine · smokeCREW REPORTED LAV SMOKE WARNING AFTER TAKEOFF. THIS OCCURRED 60 SECONDS AFTER TRANSITION FROM APU BLEED TO ENGINE BLEEDS. AIRCRAFT RETURNED TO NEWARK AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SMOKE SMELL WITH BLEEDS ON AFTER TAKEOFF POWER OBTAINED. APSDR SIMA200434102Control Unit · inoperativeON APPROACH, RECEIVED (FLAP FAIL) ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED AND LUBRICATED THE LT AND RT FLAP FLEX SHAFTS AND REPLACED NR 2 AND NR 3 FLAP ACTUATORS AND THE FLAP ELECTRONIC CONTRSDR SIMA200434218Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED ATHE CORRODED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW SRM. (K)SDR SIMA200434219Floor Support · corrodedTHE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND DOUBLER. REPAIR DONE IAW SRM.SDR SIM2005F00005Floor Support · corrodedTHE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND DOUBLER. REPAIR DONE IAW SRM.SDR SAAIEN440786Blade · fractured1ST STAGE HPC BLADE FOR NR 2 ENGINE FRACTURED DURING OPERATION, RESULTING IN UNCOMMANDED IN-FLIGHT SHUTDOWN. ONCE ENGINE DISASSEMBLED, BLADE REMNANT RETURNED TO ROLLS-ROYCE FOR ANALYSIS.SDR SIMA200434209Floor Support · corrodedDURING AN IMBV INSPECTION THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED CORROSION, FABRICATED A PLATE, FILLER, 2 SHIMS AND DOUBLER. REPAIR DONE IAW SRM. (K)SDR SIMA200434211Web · corrodedFOUND WEB AFT OF SERVICE DOOR AT RIB 22 AND 23, STR 15 HAS SMALL SPOTS OF CORROSION. REPLACED RIGHT AFT SERVICE DOOR WEB IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200434214Web · corrodedDURING CPCP INSPECTION, FOUND WEB AT FRAME 17 TO 20R FORWARD OF SERVICE DOOR HAS SPOTS OF CORROSION ON UPPER SURFACE. INSTALLED NEW WEB IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200434213Sill · corrodedDURING CPCP INSPECTION, FOUND SERVICE DOOR SILL IS CORRODED ON TOP SURFACE AROUND NUT PLATES. REPLACED SERVICE DOOR SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE.(K)SDR SIMA200434215Floor Support · corrodedDURING CPCP INSPECTION, FOUND OMEGA BEAM FRAME 20 LT, ABOVE STRINGERS 18-19L IS CORRODED AT CARBON CROSSBEAM. REPAIRED OMEGA BEAM IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200434212Gusset · corrodedDURING CPCP INSPECTION, FOUND GUSSET ON FLOORBEAM AT FRAME 20, ABOVE STRINGER 18L, HAS CORROSION. REPLACED GUSSET AT FR 20 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE.(K)SDR SIMA200434216Skin · corrodedA DENT 18 INCHES AFT OF THE PASSENGER DOOR WAS FOUND. REMOVED THE DAMAGED SKIN BY MAKING A CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)
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