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 SIMA200434204Floorbeam · corrodedDURING AN IMBV INSPECTION FOUND THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED A SECTION OF GALLEY AREA FORWARD DIGITAL. FABRICATED 2 REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200434208Stringer · gougedDURING AN IMBV INSPECTION STRINGER 19R WAS FOUND GOUGED FWD OF FRAME 53. BLENDED THE GOUGED AREA AND PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FAB 2 SHIMS AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K)SDR SIMA200434210Stringer · gougedDURING AN IMBV INSPECTION, STRINGER 19L WAS FOUND GOUGED FORWARD OF FRAME 53. BLENDED THE GOUGED AREA AND PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED 2 SHIMS AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K)SDR SIMA200433603Battery Pack · dischargedDURING PRE-FLIGHT, THE EMERGENCY LIGHTS DID NOT WORK DURING TEST FROM FLIGHT ATTENDANT PANEL. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK AND POWER SUPPLY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502113) (K)SDR SIMA200433401Control Unit · failedCREW REPORTED MAIN AND BACKUP PITCH TRIM FAILURE. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200501201)SDR SIMA200434207Sill · corrodedDURING AN IMBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE EXISTING SERVICE DOOR CENTER AND INSTALLED NEW SERVICEABLE SILL IAW SRM. (K)SDR SIMA200433604Control Unit · failedCREW REPORTED MAIN AND BACKUP PITCH TRIM FAILURE. MAINTENANCE COMPLIED WITH ENT AND FAULT ISOLATION MANUAL AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200434203Floor Support · corrodedDURING MBV INSPECTION THE CENTER OMEGA BEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED EXTERNAL ANGLE, SHIMS AND FILLER. REPAIR DONE IAW SRM. (K)SDR SIMA200434205Floor Support · corrodedDURING A MBV INSPECTION THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED EXTERNAL ANGLE, FILLER, SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200432909Cap · corrodedDURING AN MBV INSPECTION THE RT NOSE GEAR LEG BEARING CAP WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED BEARING CAP IAW AMM. THE AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501182)SDR SIMA200432910Fitting · corrodedDURING AN MBV INSPECTION THE LT AND RT NOSE GEAR LEG BEARING TRACKS FOUND CORRODED. MAINTENANCE REMOVED CORROSION AND REINSTALLED BEARING CAPS IAW AMM, SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501182)SDR SIMA200432908Sill · corrodedDURING A CPCP INSPECTION, THE SILL OF THE FORWARD SERVICE DOOR FOUND SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE SILL IAW SRM. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CHQA000588Engine · unserviceableON ADVANCING THRUST LEVERS, CREW FELT A VIBRATION COMING FROM NR 2 ENGINE, AT THE SAME TIME A TRIPLE CHIME OF "E2 LOW N1". TAKEOFF ABORTED JUST BEFORE 80 KNOTS & TAXIED A SHORT DISTANCE TO J INTERSECTION. AFTER TAKEOFF ABORTED TRIPLE CHIME MESSAGE WENT AWAY SDR CA041122006Turbine · failed(CAN) ON TAKEOFF ROLL, RT ENGINE PERFORMED AN UNCOMMANDED IN FLIGHT SHUT DOWN AT 80 KNOTS. PRELIMINARY REPORT REVEAL A CRACK TURBINE CASE AND LP STAGE 3 BLADE FAILURE. THE FAN BLADES WORE A HUGE GROOVE IN THE FAN CASE. ENGINE EN ROUTE TO ROLLS ROYCE CANADA SDR SIMA200432801Control Unit · failedDURING CRUISE FLIGHT THE CREW REPORTED PITCH TRIM .5 INOPERATIVE. MASTER WARNING WHEN A/P DISCONNECTED MOMENTARILLY. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVSDR SIMA200434206Floor Support · corrodedCORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY PERFORMING A CUTOUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM.(K)SDR SIMA200432903Floor Support · corrodedDURING AN MBV INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY PERFORMING A CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER SHIMS. REPAIR DONE IAW SRM.SDR SIMA200432904Floorbeam · corrodedDURING A MBV INSPECTION, CORROSION WAS FOUND ON THE GALLEY CENTER FLOORBEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (SW21200501183)SDR SIMA200432905Floor Support · corrodedDURING AN MBV INSPECTION CORROSION WAS FOUND ON A PREVIOUS REPAIR TO THE LT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND INSPECTION THE UNDERLYING BEAM, NO DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, SHIMS ND PLATE. REPAIR DONE IAW SRM. (SW2SDR SIMA200432703Switch · leakingCREW REPORTED AIRCRAFT HAD HYDRAULIC SYSTEM 2 FAIL IN FLIGHT. THEY FOLLOWED THE AOM AND CONTINUED AND PERFORMED AN EMERGENCY LANDING. AIRCRAFT LANDED SAFELY WITH NO OTHER INCIDENTS. FOUND NR 2 HYDRAULIC SYSTEM SWITCH LEAKING REPLACED SWITCH. FOUND NR 2 EDMSDR RAIA00411019Engine · malfunctionedORD - SMOKE IN CABIN AREA. MAINTENANCE REMOVED AND REPLACED NUMBER 1 ENGINE.SDR SIMA200432702Smoke Detector · malfunctionedEICAS LAVATORY SMOKE INDICATION DURING CLIMB OUT. INSPECTED LAVATORY FOUND NO EVIDENCE OF SMOKE. REPLACED LAVATORY SMOKE DETECTOR IAW AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200501195)SDR SIM2005F00004Skin · dentedDURING A MBV INSPECTION, ACCESS DOOR 123BL WAS FOUND DENTED. PERFORMED NDT INSPECTION NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER AND INSTALLED. REPAIR DONE IAW SRM. (SW21200501184)SDR SIMA200432901Sill · corrodedDURING A MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL. REPAIR DONE IAW SRM.SDR SIM2005F00003Sill · corrodedDURING A MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL. REPAIR DONE IAW SRM. (SW21200501184)SDR SIMA200432201Battery · dischargedEMERGENCY FLOOR LIGHT ON LT SIDE (FIRST 6 ROWS) DID NOT ILLUMINATE DURING TEST. REPLACED BATTERY POWER SUPPLY 2 IAW AMM. OPERATIONAL CHECK GOOD. (SW21200502112) (K)SDR SIMA200432101Engine · malfunctionedUNCOMMANDED SHUTDOWN ON ENGINE NR 1 ON CLIMBOUT. REPLACED NR 1 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200432206Skin · damagedDAMAGE ON THE AFT LOWER FUSELAGE BETWEEN FRAMES 65 AND 66 AT STRINGER 211. PERFORMED A CUTOUT OF THE DAMAGED AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM.SDR SIMA200432205Skin · damagedDAMAGE ON AFT LOWER FUSELAGE AT FRAME 68 AND STRINGER 21L. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM.(K)SDR CHQA000584Wire Harness · chafedDURING CLIMB OUT ON FLIGHT 3441 FROM LGA TO IND, "RUD HDOV PROT FAIL", "BLD VLV 2 FAIL", AND "BLEED 2 VLV CLOSED" MESSAGES APPEARED ON EICAS. WITHIN TEN SECONDS THE NR 2 ENGINE SHUTDOWN AND "ENG 2 OUT" MESSAGE APPEARED ON EICAS. THE CREW ATTEMPTED AN APU ASSSDR SIMA200431702Smoke · detectedDURING DECENT, CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT FOR ABOUT 30 SECONDS WITH PAINT SMOKE BEING SEEN FOLLOWED QRH PROCEDURES. THERE WERE NO ALARMS, WARNING MESSAGES OR SMOKE IN CABIN. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFTSDR RAIA00411013Engine · unknownPIT - ATTCS NO MARGIN, LEFT ENGINE. MAINTENANCE DID A GROUND POWER RUN ON BOTH ENGINES AND COULD NOT DUPLICATE.SDR SIMA200432212Mount · damagedIMBV- THE APU COWLING LT LOWER MOUNT FRAME WAS FOUND TO BE CRACKED. REMOVED DAMAGED MOUNT FRAME. INSTALLED NEW MOUNT IAW SRM. (SW21200501189)SDR SIMA200431701Brake · malfunctionedDURING APPROACH TO LGA WHEN CREW SELECTED FLAPS THE FLAPS FROZE WOULD NOT MOVE FROM 0 DEGREES. MAINTENANCE REMOVED AND REPLACED THE LT AND RT FLAP TRANSMISSION BRAKES IAW MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECSDR SIMA200432208Floor Support · corrodedIMBV - LT OMEGA BEAM AT FRAME 24 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501181)SDR SIMA200431506Floor Support · corrodedDURING AN IMBV INSPECTION THE LT OMEGA BEAM BETWEEN FRAME 20 AND 22 WAS FOUND CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A FILLER AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW21200501161)SDR CA041122008Compressor · damaged(CAN) UNCOMMANDED IN-FLIGHT SHUTDOWN. IN CLIMB MODE AT 10,000 FT, FLIGHT CREW HEARD A LOUD BANG AND THE NR 1 ENGINE SHUTDOWN. MINOR FINDINGS ON MCD'S. LP WILL ROTATE, HP WILL NOT ROTATE. CMC DOWNLOAD SHOWED HP VIBRATION EXCEEDANCE OF 1.7 IPS FOR 11SECONDS.SDR SIMA200432204Floor Support · corrodedTHE CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AND INSTALLED AN EXTERNAL DOUBLER. REPAIR DONE IAW SRM. (SW21200501189)SDR SIMA200432209Floor Support · corrodedIMBV - RT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW 21200501181)SDR SIMA200431505Floor Support · corrodedDURING AN IMBV INSPECTION, A PREVIOUS AIR ON THE LT BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE PREVIOUS REPAIR AT FRAME 20. FABRICATED AN EXTERNAL ANGLE, FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM. (SW21200501161)SDR SIMA200432211Floorbeam · corrodedTHE GALLEY AREA FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE GALLEY AREA FWD DIGITAL. INSTALLED THE NEW DIGITAL IAW SRM.SDR SIMA200431504Floor Support · corrodedDURING AN IMBV INSPECTION THE LT SIDE OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY CUTTING OUT A SECTION OF THE FORWARD DIDITAL. FABRICATED A DOUBLE. REPAIR DONE IAW SRM.SDR SIMA200431008Battery Pack · dischargedDURING PREFLIGHT, CREW FOUND THE EMERGENCY LIGHTS AFT OF ROW 12 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER PACK IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200431508Floor Support · corrodedDURING AN IMBV INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW2120051190)SDR SIMA200431502Floor Support · corrodedDURING AN IMBV INSPECTION THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED CORROSION BY MAKING CUTOUT. FABRICATED A FILLER, 2 SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM.SDR SIMA200431507Floor Support · corrodedDURING AN IMBV INSPECTION THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 32 AND 43. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND AN EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW21200501161)SDR SIMA200432207Sill · corrodedIMBV - CARGO DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. INSTALLED NEW CARGO DOOR CUT OUT LOWER SILL IAW SRM AND CPM. (SW21200501181)SDR SIMA200432210Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED CORRODED CENTER DOOR SILL. INSTALLED NEW SILL IAW SRM.SDR SIMA200431503Floor Support · corrodedDURING AN IMBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND CORRODED. REMOVED THE CORRODED GALLEY CENTER HAT BEAM. INSTALLED NEW HAT BEAM IAW SRM. (SW21200501161)SDR RAIA00411002Bleed Valve · stickingPIT - ATTCS HAS NO MARGIN. MAINTENANCE INSPECTED ENGINE COMPRESSOR BLEED SYSTEM. FOUND LOWER COMPRESSOR AIR BLEED VALVE TO BE STICKING. CLEANED VALVE.
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