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.

SDR V0XR201002120001Gusset · corrodedCTR GUSSET Y.0.0 FROM FRM 19-23 IS CORRODED BEYOND LIMITS. R & R GUSSET.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002120002Gusset · corrodedGUSSET BETWEEN FRM 16-17 TO FRM 18 AND LY 479 TO Y 0.0 IS CORRODED BEYOND LIMITS. R & R GUSSET.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002120003Angle · corrodedANGLE UNDER PAX DOOR SILL FRM 16-17 IS CORRODED BEYOND LIMITS. R & R ANGLE.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002120004Angle · corrodedANGLE UNDER PAX DOOR SILL FRM 16-17 IS CORRODED BEYOND LIMITS. R & R ANGLE.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002120005Angle · corrodedANGLE FROM FRM 18 LY 479.0 - RY 780.0 CORRODED BEYOND LIMITS. R & R ANGLE.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002120006Floor Support · corrodedANGLE FROM FRM 20 AND Y 0.0 UNDER FLOORBOARD CARBON FIBER SUPPORT IS CORRODED BEYOND LIMITS. R & R ANGLE.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002120007Support · corrodedSUPPORT FROM FRM 18-20 AND Y 0.0 IS CORRODED BEYOND LIMITS. R & R SUPPORT.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002120008Sill · corrodedRT SILL FROM FRM 23-29 IS CORRODED BEYOND LIMITS. R & R SILL.Feb 12, 2010 · N806HK · Emb EMB145ER · Fuselage Miscellaneous StructureSDR V0XR201002120009Doubler · corrodedDOUBLER RY 479 AND FRM 20-22 IS CORRODED BEYOND LIMITS. R & R DOUBLER.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002120010Doubler · corrodedDOUBLER RY 479 AND FRM 20-22 IS CORRODED BEYOND LIMITS. R & R DOUBLER.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002120011Floor Support · corrodedDIGITAL PLATE ON LT OMEGA BEAM FROM FRM 18-23 IS CORRODED BEYOND LIMITS. R & R DIGITAL PLATE.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002120012Gusset · corrodedGUSSET YL 479.0 FROM FRM 30-36 IS CORRODED BEYOND LIMITS. R & R GUSSET.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002120013Channel · corrodedCTR HAT CHANNEL BEAM AT Y 0.0 FROM FRM 16-25 IS CORRODED BEYOND LIMITS. R & R BEAM.Feb 12, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR CHQA201000035Battery · dischargedDURING INSPECTION BOTH THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY IAW EMB MM 33-50-04, OPS CHECK GOOD.Feb 12, 2010 · N292SK · Emb EMB145LR · Emergency LightingSDR V0XR201002110001Beam · corrodedBEAM AT FRM 17 LY479-LY480 IS CORRODED BEYOND LIMITS. R & R BEAM.Feb 11, 2010 · N806HK · Emb EMB145EP · Fuselage Main, StructureSDR V0XR201002110002Floor Support · corrodedLT PROFILE BETWEEN LY479-LY780 AT FRM 61 IS CORRODED BEYOND LIMITS. R & R PROFILE.Feb 11, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002110001ABeam · corrodedBEAM BETWEEN LY479-LY780 AT FRM 17 IS CORRODED BEYOND LIMITS. R AND R BEAM.Feb 11, 2010 · N806HK · Emb EMB145EP · Fuselage Main, StructureSDR V0XR201002110003Beam · corrodedBEAM AT FRM LY479-LY 780 IS CORRODED BEYOND LIMITS. R & R BEAM.Feb 11, 2010 · N806HK · Emb EMB145EP · Fuselage Main, StructureSDR V0XR201002110004Gusset · corrodedLT OMEGA BEAM GUSSET FROM FRM 23-29 IS CORRODED BEYOND LIMITS. R & R GUSSET.Feb 11, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR CHQA201000034Battery Pack · dischargedDURING INSPECTION THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND LAMP WITH NO FURTHER DEFECTS NOTED.Feb 11, 2010 · N294SK · Emb EMB145LR · Emergency LightingSDR V0XRSill · corrodedLT SILL AT LY-780.0 FROM FRM 59-61 IS CORRODED BEYOND LIMITS. R & R SILL.Feb 10, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002100001Sill · corrodedLT SILL AT LY-780.0 FROM FRM 59-61 IS CORRODED BEYOND LIMITS. R & R SILL.Feb 10, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002100003Sill · corrodedRT SILL FRM 29-35 IS CORRODED BEYOND LIMITS. R & REPLACED SILL.Feb 10, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002100002Sill · corrodedFWD SERVICE DOOR SILL FRM 19-20 IS CORRODED BEYOND LIMITS. R & R SILL.Feb 10, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002100005Sill · corrodedRT SILL AT RY-780.0 FROM FRM 59-61 IS CORRODED BEYOND LIMITS. R & REPLACED SILL.Feb 10, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002100006Doubler · corrodedLT LOWER PARTITIAL AT FRAME 61 IS CORRODED BEYOND LIMITS. R & R LT DOUBLER FWD PARTITIAL.Feb 10, 2010 · N806HK · Emb EMB145EP · Fuselage Main, StructureSDR V0XR201002100007Gusset · corrodedCTR GUSSET AT Y-0.0 FROM FRM 59-61 IS CORRODED BEYOND LIMITS. R & R CTR GUSSET.Feb 10, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002100004Sill · corrodedLT SILL AT LY-780.0 FROM FRM 61-65 IS CORRODED BEYOND LIMITS. R & R SILL.Feb 10, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR CHQA201000033Light · inoperativeDURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOP DURING TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10, OPS CHECK GOOD.Feb 10, 2010 · N294SK · Emb EMB145LR · Emergency LightingSDR SIMA201004205Carbon Seal · leakingON FLIGHT 4225 ON ROTATION, CREW REPORTED SMOKE IN COCKPIT AND CABIN. CREW DECLARED AN EMERGENCY AND RETURNED TO GRB WITHOUT INCIDENT. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 0 CARBON SEAL ASSEMBLY IAW R & R MM 72-25-25-000-801 AND 72Feb 10, 2010 · N625AE · Emb EMB145LR · Turbine Engine Oil SystemSDR V0XR1002090001BSill · corrodedAFT SERVICE DOOR SILL AT FRM 22-23 IS CORRODED BEYOND LIMITS. R & R SILL.Feb 9, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201002090001Sill · corrodedLT SILL AT FRM 29-35 IS CORRODED BEYOND LIMITS. R & R SILL.Feb 9, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR CHQA201000032Battery Pack · dischargedDURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE INOP WHEN TESTED. MAINTENANCE REPLACED THE NR 4 EMERGENCY BATTERY PER AMM 33-50-04, OPS CHECK GOOD.Feb 9, 2010 · N562RP · Emb EMB145LR · Emergency LightingSDR V0XR201002080001Sill · corrodedLT SILL FROM FRM 18-23 IS CORRODED BEYOND LIMITS. R & R SILL.Feb 8, 2010 · N806HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR CHQA201000029Windshield · delaminatedAIRCRAFT RETURNED TO FIELD DUE TO THE FIRST OFFICER'S WINDSHIELD DELAMINATING. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD IAW ERJ 145 AMM 56-10-01.Feb 8, 2010 · N270SK · Emb EMB145LR · Flight Compartment WindowsSDR CHQA201000030Battery Pack · inoperativeDURING INSPECTION THE NR 1 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE 31 EMERGENCY LIGHT BATTERY PACK IAW EMB-145 AMM 33-50-04.Feb 8, 2010 · N269SK · Emb EMB145LR · Emergency LightingSDR CHQA201000031Battery Pack · inoperativeDURING INSPECTION THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 4 BATTERY PACK, BUT AFTER INSTALLATION OF THE NEW BATTERY PACK, THE OVERWING EMERGENCY LIGHTS WERE STILL INOP. THE BATTERY WAS REPLACED AGAIN WITH NO FUFeb 8, 2010 · N269SK · Emb EMB145LR · Emergency LightingSDR CHQA201000028Seal · detachedDURING CLIMB THE CREW REPORTED THAT THE UPPER HUMP SEAL ON THE FIRST OFFICER'S WINDSHIELD WAS FLAPPING ABOVE 200KTS. IT WAS DECIDED TO RETURN TO ORF WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE SEAL AND COMPLIED WITH TEMPORARY REPAIRFeb 7, 2010 · N577RP · Emb EMB145LR · Flight Compartment WindowsSDR CHQA201000048Trunnion · crackedDURING THE INSPECTION OF THE AFT UPPER TRUNNION ON THE RIGHT MAIN LANDING GEAR, A CRACK WAS FOUND ON THE TRUNNION FITTING AT THE AFT SPAR ATTACH POINT. THE CRACK PENETRATED THE ENTIRE LENGTH OF THE AFT SIDE TO THE RADIUS. NDT INSPECTION INDICATED CRACK THROUFeb 7, 2010 · N278SK · Emb EMB145LR · Main Landing Gear Attach SectionSDR CHQA201000026Light · inoperativeDURING INSPECTION THE RIGHT AND LEFT AFT EMERGENCY EXIT WINDOW LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BULBS IN THE RIGHT AND LEFT AFT EMERGENCY EXIT WINDOW LIGHT BULBS WITH NO FURTHER DEFECTS NOTED.Feb 2, 2010 · N562RP · Emb EMB145LR · Emergency LightingSDR CHQA201000027Fuse · openDURING INSPECTION, THE 3 LAST FLOOR PROXIMITY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSES IN THE NR 4 EMERGENCY LIGHT BATTERY IAW AMM 20-13-08 WITH NO FURTHER DEFECTS NOTED.Feb 2, 2010 · N562RP · Emb EMB145LR · Emergency LightingSDR CHQA201000024Unknown · malfunctionedDURING CLIMBOUT, THE CREW RECEIVED A RUDDER SYS 1-2 INOP MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE MESSAGE CLEARED AND AS A RESULT THE CREW RECEIVED AUTO-PILOT AND YAW DAMPER FAIL MESSAGES ON EICAS. THE CREW REDUCED ALTITUDE DUE TO NOW BEING NON-RVSM ANFeb 1, 2010 · N284SK · Emb EMB145LR · Rudder Control SystemSDR CHQA201000025Strut · overservicedWHILE GETTING VECTORS FOR APPROACH THE CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON EICAS WHEN THE GEAR WAS EXTENDED. THE QRH WAS FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR STRUT FULLY EXTENDED UPON INSPECTION. Feb 1, 2010 · N377SK · Emb EMB135KL · Nose/Tail Landing Gear Strut/AxleSDR CHQA201000023Connector · dirtyAFTER TAKEOFF THE CREW RETRACTED THE LANDING GEAR AND RECEIVED A LANDING GEAR DISAGREE EICAS MESSAGE. THE LEFT MAIN GEAR WAS NOT INDICATING RETRACTED. THE QRH WAS FOLLOWED AND THE GEAR WAS CYCLED AND CONTINUED TO INDICATE THAT IT WAS NOT RETRACTED. THE AIRCJan 31, 2010 · N374SK · Emb EMB135KL · Landing Gear System WiringSDR CHQA201000020Fuse · openDURING INSPECTION THE LEFT AND RIGHT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE ALONG WITH THE COCKPIT EMERGENCY FLOOD LIGHT. MAINTENANCE FOUND AN OPEN FUSE AT THE NR 1 BATTERY PACK FOR THE EMERGENCY LIGHTS. THE FUSE WAS REPLACED IN THE BATTERY PER EMB CMJan 30, 2010 · N269SK · Emb EMB145LR · Emergency LightingSDR CHQA201000021Light · inoperativeDURING INSPECTION THE AFT MOST SECTION OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOP. MAINTENANCE REPLACED THE AFT MOST SECTION OF EMERGENCY FLOOR LIGHTING WITH NO OTHER DEFECTS NOTED.Jan 30, 2010 · N269SK · Emb EMB145LR · Emergency LightingSDR CHQA201000022Fuse · openDURING INSPECTION THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOP. MAINTENANCE FOUND THE FUSE IN THE NR 4 EMERGENCY LIGHT POWER SUPPLY OPEN. THE FUSE WAS REPLACED IN THE NR 4 POWER SUPPLY IAW EMB 145 CMM 25-60-03 WITH NO FURTHER DEFECTS NOTED.Jan 30, 2010 · N269SK · Emb EMB145LR · Emergency LightingSDR CHQA201000019Wire Harness · damagedTHE FLIGHT CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF ALONG WITH A TAKEOFF CONFIG WARNING. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DOWNLOADED THE CMC AND FOUND MESSAGES FOR LGEU FAIL 1X, NOSE LG PROX SWJan 28, 2010 · N377SK · Emb EMB135KL · Landing Gear System WiringSDR CHQA201000018Relay · faultyDURING CRUISE THE FLIGHT ATTENDANT REPORTED THAT THE CABIN OXYGEN MASKS HAD DROPPED ALONG WITH THE CABIN LIGHTING GOING OUT. THE CREW REPORTED THE CABIN PRESSURE WAS STEADY AT 5,000FT, AND THE CABIN LIGHTING WAS TURNED BACK ON IMMEDIATELY WITH NO FURTHER DIFFJan 27, 2010 · N382SK · Emb EMB135KL · Passenger Oxygen SystemSDR CHQA201000017Light · malfunctionedDURING INSPECTION, THE VERTICAL EMERGENCY EXIT LIGHT AFT OF THE RIGHT OVERWING EMERGENCY EXIT WAS FOUND TO BE INOP. THE POWER WAS RESET AND THE LIGHT OPERATED NORMALLY IAW EMB 140 MM 33-50-00-0.Jan 26, 2010 · N380SK · Emb EMB135KL · Emergency Lighting
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