N608AE

Service difficulty reports not matched to an aircraft · 16

They name N608AE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

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 n_number = 'N608AE' AND registry_match IS NULL
  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 SIMA200207008Floorbeam · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY AREA FORWARD DIGITAL. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPLACEMENT STRAP, TWO DOUBLERS AND A SHIM. WORK DONE IAW EMB 145 SRM 145/1Mar 8, 2002 · N608AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200207201Stringer · chafedABI - DURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19R CHAFED. BLENDED CHAFE, FABRICATED TWO DOUBLERS ANGLE 14.5 INCH BY 1.5 INCH, .050 INCH THICK, AND FOUR SHIMS 4.5 INCH BY .75 INCH .080 INCH THICK IAW EMB 145 SRM 145/1142 REV 17 53-25-02, GST-063Mar 6, 2002 · N608AE · Emb EMB145 · Fuselage Main, Longeron/StringerSDR SIMA200207202Stringer · chafedDURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19L CHAFED. BLENDED CHAFE. FABRICATED TWO DOUBLER ANGLE 14.5 INCH BY 1.5 INCH, .050 INCH AND FOUR SHIMS 4.5 INCH BY .75 INCH, .080 INCH THICK IAW EMB 145 (SRM 145/1142 REV 17) 53-24-02, GST-0633/02, ETN Mar 6, 2002 · N608AE · Emb EMB145 · Fuselage Main, Longeron/StringerSDR SIMA200207009Floor Support · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY CENTER HAT BEAM. REMOVED CORRODED GALLEY CENTER HAT BEAM. INSTALLED NEW HAT BEAM IAW EMB 145 SRM/1142, REV 17, 51-20-03, 51-40-02, GST-0623/02, ITEM 7 SEP 0114/02 AND STANDARD SRM PRAMar 2, 2002 · N608AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200207001Doubler · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION, PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR, CORROSION LIMITED TO PREV REPAIR. FABRICATED A DOUBLER ANGLE AND FILLER. A PLATE AND TWO SHIMS. WORK DONE IAW EMB 145Feb 24, 2002 · N608AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208305Skin · corrodedABI - THIS IS A LEVEL 2 FINDING, CORROSION FOUND ALONG FUSELAGE SKIN EDGE JUST BELOW BATTERY COMPARTMENT ACCESS DOOR. BLENDED, INSPECTED DAMAGE AND IT WAS ACCEPTED AS IS IAW EMB GST 0623/02. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Main, Plate/SkinSDR SIMA200207203Sill · corrodedABI - RIGHT SILL BETWEEN FRAME 23 AND 29 HAS CORROSION. BLENDED OUT, PERFORMED NDT AND TREATED IAW EMB GST-0623/02. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200207204Frame · corrodedABI - RIGHT HAT BEAM AT FRAME 22 HAS CORROSION. BLENDED AND NDT'D AND TREATED HAT BEAM AT FRAME 22 IAW EMB GST 0623/02. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Main, FrameSDR SIMA200207205Structure · corrodedABI - GALLEY AREA AFT DIGITAL HAS CORROSION. BLENDED OUT, PERFORMED NDT, AND TREATED FOR CORROSION IAW EMB 145 CPM 51-21-03, 51-21-04, 51-21-05, 51-21-06. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Main, StructureSDR SIMA200207206Beam · corrodedABI - FOUND LEFT OMEGA BEAM BETWEEN FRAME 24 AND 25 HAS CORROSION. BLENDED AND PERFORMED NDT INSPECTION AND TREATED FOR CORROSION IAW EMB GST 0623/02. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Main, StructureSDR SIMA200207207Beam · corrodedABI - CENTER OMEGA BEAM BETWEEN FRAME 23 AND 25 HAS CORROSION. BLENDED, PERFORMED NDT AND TREATED FOR CORROSION IAW EMB GST-0623/02. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Main, StructureSDR SIMA0681Warning System · activatedGRR - FLT 4405 - ON TAKEOFF ROLL OF 90 KNOTS HAD EICAS MESSAGE OF REV DISAGREE, RETURNED TO GATE FOR MAINTENANCE. NOTE THE MESSAGE WENT AWAY VERY QUICK. INSPECTOR AND OPS CHECK IAW AMM. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. (M)Mar 9, 2001 · N608AE · Emb EMB145LR · Central WarningSDR SIMA200103601Actuator · malfunctionedSGF - FLT 3560 - ON TAKEOFF ROLL, HAD TR1 DISAGREE, ABORTED TAKEOFF AND RETURNED TO GATE. ENGINE 1 THRUST REVERSER PUT ON MEL AT THIS TIME. MAINTENANCE ADJUSTED UPPER AND LOWER T/R ACTUATORS ON NR 1 ENGINE IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETFeb 5, 2001 · N608AE · Emb EMB145LR · Engine Thrust ReverserSDR SIMA3602Pressure Switch · leakingDFW - FLT 3418 - AIRCRAFT LOST ALL HYDRAULIC 1 SYSTEM QTY AND PRESSURE. REPLACED NR 1 HYD SYSTEM PRESSURE SWITCH IAW AMM. OPS CHECK GOOD. (M)Dec 25, 2000 · N608AE · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR SIMA2665Engine · leakingORD - FLT 4249 - CREW ABORTED TAKEOFF FOR ENGINE NR 2 OIL PRESSURE WENT TO RED ON TAKEOFF ROLL. FERRY TO CMH. MAINTENANCE C/W ENGINEERING ORDERS EM-7900-010 AND EM-6900-011. INSTALLATION ON OIL PRESSURE RELIEF KIT AND SMART SENSOR (NEW PN 23073475A). OPERASep 22, 2000 · N608AE · Emb EMB145LR · Engine Oil Indicating SystemSDR SIMA2612Sign · malfunctionedMGM - FLT 3684 - SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESEATED CANNON PLUG FOR SERVICE DOOR LIGHT AND PERFORMED OPERATIONAL CHECK. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 17, 2000 · N608AE · Emb EMB145LR · Emergency Lighting
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