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 SIMA200535510Floor Support · corrodedDURING CPCP INSPECTION, FOUND CARBON CROSS MEMBER AT FRAME 24-25 CENTER OMEGA BEAM ATTACHMENT IS CORRODED. REPAIRED OMEGA BEAM BY INSTALLING AN EXTERNAL DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200535508Floor Support · corrodedDURING CPCP INSPECTION FOUND OMEGA BEAM DOUBLER AT FRAME 20 IS CORRODED. REPLACED DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200535507Floor Support · corrodedDURING CPCP INSPECTION FOUND CENTER HAT BEAM UPPER PROFILE HAS SPOTS OF CORROSION FROM FRAMES 19 TO 23. REPLACED GUSSET IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200534501Charger · inoperativeDISC FLOOR PROXIMITY LIGHTS COME ON BY THEMSELVES AND WOULD NOT EXTINGUISH. REPLACED NR 3 BATTERY CHARGER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)SDR CHQA200500206Light · inoperativeEMERGENCY LIGHT ON RT FUSELAGE OUT. RELAMPED EMERGENCY COURTESY LIGHT ON RT WING. OPS CHECK GOOD IAW MM 33-50-09.SDR F05012Lamp · burned outTHE AIRCRAFT WAS RUN IN CAE LAST NIGHT AND THE CREW FOUND THAT THE AFT CABIN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP.SDR CA051209003Engine · malfunctioned(CAN) A/C WAS IN ROUTE TO DESTINATION, WHEN 20 MINUTES INTO THE FLIGHT, THE CAPTAIN NOTICED THAT EICAS INDICATIONS FLICKERED OFF THEN ON. LT ENGINE THEN SHUTDOWN UNCOMMANDED AND CREW RECEIVED NUMEROUS EICAS MESSAGES. (TC NR 20051209003)SDR MASA200500979Carbon Seal · leakingASH 2829 MGM. SHUTDOWN THE ENGINE DUE TO THE LOST OF ENGINE OIL PRESSURE AND THE LOST OF ENGINE OIL. MAINTENANCE REPLACED NR 2 GENERATOR AND NR 2 GENERATOR CARBON SEAL.SDR CHQA200500207Engine · making metalE2 OIL IMPENDING BYPASS MESSAGE DURING CRUISE. OIL QUANTITY DROPPED TO 6 QUARTS, OIL TEMPERATURE WAS OPERATING AROUND 12.5 THEN WENT INTO RED. MOVED LEVERS ACCORDINGLY TO KEEP IN GREEN. LATER IN DESCENT, MOVED TO IDLE AND ENGINE 2 LOW OIL PRESSURE MESSAGE RSDR SIMA200533602Floor Support · corrodedTHE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKEING A CUTOUT. PREPARED A DOUBLER, FILLER, PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR CHQA200500202Battery Pack · inoperativeSEVERAL EMERGENCY EXIT LIGHTS ARE INOP IN THE AFT CABIN. REMOVED AND REPLACED AFT FLOOR EMERGENCY EXIT LIGHT BATTERY PACK IAW 145 AMM 33-50-04. OPS CHECK GOOD.SDR SIMA200533603Fitting · wornTHE LT AILERON OB HINGE POINT BEARING HOLE WAS FOUND TO BE WORN BEYOND MANUAL LIMITS. REMOVED DAMAGED HINGE FITTING. LOCATED AND DRILLED IN NEW FITTING. APPLIED ALODINE AND PRIMER TO ALL BARE SURFACE. REPAIR DONE IAW SRM. (K)SDR CHQA200500201Bulb · burned outRT OVERHEAD AFT EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED THE RT WING AFT EMERGENCY EXIT LIGHT BULB IAW 140 MM 33-50-09. OPS CHECK GOOD.SDR SIMA200532901Carbon Seal · leakingDFW - FLT 3749 - DURING TAKEOFF, RECEIVED LAVATORY SMOKE MASTER WARNING ON EICAS AND LAVATORY SMOKE DETECTOR ALARM WAS ACTIVATED. FOUND 0 CARBON LEAKING. REPLACED NR 2 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200532903Floor Support · corrodedTHE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 27. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200532902Stringer · chafedSTRINGER 19R WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED AND TREATED THE CHAFED AREA WITH EA934. FABRICATED A REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200532904Floor Support · corrodedTHE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 27. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200532905Stringer · chafedSTRINGER 19L WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED THE CHAFED AREA AND APPLIED EA 934. FRABRICATED A REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200532906Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL AND INSTALLED NEW CENTER SILL IAW SRM AND CPM. (K)SDR SIMA200532511Relay · failedAFTER TAKEOFF, RECEIVED EICAS MESSAGE (SPOILER FAIL) ACCOMPAINED BY (OPN) INDICATION IN SPOILERS. REMOVED AND REPLACED LANDING GEAR DOWN LOCK RELAY K0030 AND K0031. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K)SDR SIMA200532510Skin · puncturedSKIN PUNCTURE ON RT FUSELAGE BETWEEN FRAMES 22A/23 AND STRINGER 15R. PERFORMED CUT OUT OF THE SKIN TO REMOVE THE DAMAGE. FABRICATED FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)SDR SIMA200532201Structure · ground damageAIRCRAFT WAS STRUCK BY JETBRIDGE CAUSING DAMAGE TO PASSENGER ENTRY DOOR. AIRCRAFT WAS FERRIED TO MAINTENANCE. DOOR REPAIRED WITH AN EXTERNAL DOUBLER AT DAMAGE CORNER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200532202Warning Light · false activationDURING LANDING FLARE EICAS MESSAGE RUDDER SYSTEM ONE AND 2 INOPERATIVE. NO RUDDER CONTROL DURING REMAINDER OF LANDING OR DURING TAXI. PERFORMED OPERATIONAL CHECK OF THE RUDDER SYSTEM WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (K)SDR SIMA200532506Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING AND INSTALLED SERVICEABLE SILL IAW SRM. (K)SDR SIMA200532501Floor Support · corrodedTHE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUT OUT SECTION OF BEAM TO REMOVE CORROSION. PREPARED A DOUBLER, FILLER, SHIMS AND A PLATE. REPAIR DONE IAW SRM. (K)SDR SIMA200532908Floor Support · corrodedDURING INSP, FOUND LT OMEGA BEAM AT FRAME 20 LT, CORRODED. REPAIRED OMEGA BEAM BY INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200532907Sill · corrodedDURING INSPECTION FOUND SERVICE DOOR CENTER SILL CORRODED. REPAIRED SERVICE DOOR SILL BY INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR FDK2005F00003Smoke · detected(REF: FO5011 - CNTRL NR 100129) THE CREW NOTED SMOKE IN THE CABIN AFTER APU START UP ON THE GROUND DURING PREFLIGHT INSPECTION. MAINTENANCE INSPECTED THE PLANE AND DETERMINED THAT THE APU WAS NOT RUNNING DURING DE-ICING AND INGESTED THE STRAY FLUID CAUSING TSDR SIMA200532505Sill · corrodedTHE BAGGAGE DOOR SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND INSTALLED SERVICEABLE SILL IAW SRM. (K)SDR SIMA200532504Handle · crackedA CRACK WAS DISCOVERED ON THE PASSENGER DOOR INNER HANDLE BRACKET. STOP DRILLED THE CRACK ON THE PAX DOOR HANDLE BRACKET. FABRICATED A REINFORCEMENT ANGLE. REPAIR DONE IAW SRM. (K)SDR SIMA200532502Support · damagedTHE APU COWLING RT LOWER MOUNTING SUPPORT AREA WAS FOUND DAMAGED. FABRICATED A REINFORCEMENT DOUBLER. REPAIR DONE IAW SRM. (K)SDR SIMA200532507Floor Support · corrodedTHE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200532509Floor Support · corrodedTHE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING CUTOUT. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR RAIA00511007Connector · looseEMERGENCY LIGHTS OUT AT FWD CABIN DECK AND AT ROWS 8-12. MAINTENANCE RE-SET CONNECTOR AT LIGHT INVERTER.SDR CHQA20050191Light · brokenFORWARD FLOOR PROXIMITY LIGHT IS BROKEN. REMOVED AND REPLACED PROXIMITY STRIP IAW MM 33-50-12.SDR SIMA200532503Sill · corrodedTHE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LOWER SILL. INSTALLED SERVICEABLE SILL IAW SRM. (K)SDR C2XA05BT078Heat Shield · brokenDURING ROUTINE CHECK MAINTENANCE FOUND THE NR 1 ENGINE REAR TURBINE BEARING SUPPORT HEAT SHIELD BROKEN, DAMAGED TWO REAR TURBINE BEARING SUPPORT STRUTS/PYLONS (P/N 23077731). THE 11 O`CLOCK POSITION STRUT HAD BEEN CUT 0.25 INCHES THROUGH AND THE 1 O`CLOCK POSSDR SIMA200532508Floor Support · corrodedA PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED AHT PREVIOUS REPAIR. PREPARED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)SDR SIMA200531101Cradle · brokenFLIGHT ATTENDANT FLASHLIGHT OVER ROW 13 WILL NOT STAY IN FLASHLIGHT CRADLE. REPLACED FLASHLIGHT CRADLE ASSY IAW SRM. AC RETURNED TO SERVICE. (K)SDR 2005FA0001529Tire · leakingTHE TIRE WAS REMOVED FROM THE AIRCRAFT FOR A SLOW LEAK. THE WEEP HOLES IN THE SIDEWALL OF THE TIRE WERE BUBBLING WHEN CHECKED WITH LEAK DETECTOR FLUID. (K)SDR SIMA200531103Inverter · inoperativeTHE CENTER FLOOR EMERGENCY LIGHT STRIPS WERE FAILED TO TEST. REPLACED THE DC/AC INVERTER ASSY. OPS CHECK GOOD. AC RETURNED TO SERVICE. (K)SDR SIMA200530405Warning Light · false activationLAVATORY SMOKE EICAS MESSAGE ILLUMINATED AFTER TAKEOFF. FOUND BLUE WATER SPILL ON BLEED DUCT IN LAVATORY. CLEANED BLUE WATER SPILL AND PERFORMED OPERATIONAL CHECK OF AIR CONDITIONING SYSTEM. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. ACSDR SIMA200530404Light · failedEMERGENCY EXIT FLOOR STRIP AT GALLEY WILL NOT ILLUMINATE. REPLACED NR 1 EXIT DOOR EMERGENCY LIGHT, FLOOR PROXIMITY STRIP IAW MM. OPS CHECK GOOD. AC RETURNED TO SERVICE. (K)SDR DXTA200501038Float Valve · failedIN FLIGHT ,WING TANK OFULL R AMBER CAS MESSAGE ILLUMINATED AT FL290 SHORTLY AFTER LEVELING OFF. THE APPROPIATE CHECKLIST WAS COMPLETED FUEL VENTED OUT OF R WING FOR 3 MINUTES (LOST 150 LBS).THEN MESSAGE WENT OUT 2 MINUTES LATER (TOTAL FUEL 4900 LBS/L TANK 235SDR SIMA200530401Skin · corrodedDURING INSPECTION OF FUSELAGE SKIN BETWEEN FRAMES 21 AND 22 AND STRINGERS 19R AND 191., WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF CORRODED AREA. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)SDR SIMA200530402Beam · corrodedDURING INSPECTION OF FUSELAGE CENTER BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF CORRODED AREA. FABRICATED A DOUBLER, FILLER AND 2 SHIM. REPAIR DONE IAW SRM. (K)SDR SIMA200530108Flap System · stuckCREW REPORTED AFTER TAKEOFF DURING FLAP RETRACTION THEY RECEIVED A FLAP FAIL MESSAGE. REPLACED RT FLAP TRANSMISSION BRAKE. OPERATIONAL CHECK GOOD, AC RETURNED TO SERVICE. (K)SDR C2XA05CL089Carbon Seal · failedCLE FLIGHT 2201 - THE CREW REPORTED DURING CLIMB AND DESCENT THERE WAS A OIL ODOR IN THE COCKPIT AND CABIN. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. SUPPLEMENT THE NR 4 CARBON SEAL WAS FOUND TO BE THE CAUSE OF OIL ODOR.SDR CA051125004Turbine Blades · failed(CAN) DURING A FLIGHT THE ENGINE EXPERIENCED AN ITT OVERTEMP OF 1045 DEGREES C FOR 36 SECONDS. THIS RESULTED IN AN UN-COMMANDED IN FLIGHT SHUTDOWN. ENGINE DISASSEMBLY AT MFG REVEALED AN HPT1 BLADE FAILURE FROM THE ROOT.SDR C2XA05IA118Turbine Blades · failedIAH - FLIGHT 2010, THE CREW REPORTED AN UNCOMMANDED ENGINE SHUT DOWN IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS
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