N651AE

Service difficulty reports · 214

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N651AE' AND registry_match = 'registration'
  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 SIMA200829604Sill · corrodedDURING MBV INSPECTION FOUND FORWARD SERVICE DOOR SILL TO BE CORRODED. REPAIRED SILL BY REMOVING CORROSION AND INSTALLING A DOUBLER IAW EMB SRM 53-21-10 FIGURE 204. AIRCRAFT RETURNED TO SERVICE.Oct 20, 2008 · N651AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200829603Floor Support · corrodedDURING IMBV INSPECTION FOUND LEFT OMEGA BEAM TO BE CORRODED JUST FORWARD OF FRAME 29. REPAIRED OMEGA BEAM BY CUTTING OUT DAMAGED AREA AND INSTALLING A DOUBLER IAW IMB SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.Oct 20, 2008 · N651AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200716911Charger · failedLEFT OVERWING AND AFT CABIN EMERGENCY LIGHTS STAYED ILLUMINATED. REMOVED AND REPLACED BATTERY CHARGER IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.Jun 17, 2007 · N651AE · Emb EMB145LR · Emergency LightingSDR SIMA200709201Carbon Seal · failedNUMBER 2 ENGINE OIL QUANTITY DROPPED TO 4 QUARTS, OIL PRESSURE STARTED TO DROP. CREW SHUTDOWN ENGINE. DIVERTED TO CID. POSTFLIGHT INSPECTION REVEALED OIL ON NUMBER 2 ENGINE COWL. REMOVED AND REPLACED NUMBER 4 GENERATOR AND CARBON SEAL ASSEMBLY PER EMB AMM Apr 1, 2007 · N651AE · Emb EMB145LR · Turbine Engine Oil SystemSDR SIMA200633103Floor Support · corrodedFOUND LEFT OMEGA BEAM AT FRAME 20 CORRODED. REMOVED PREVIOUS REPAIR. FABRICATED DOUBLER, CLEANED AND TREATED AND INSTALLED REPAIR DOUBLER. RESTORED PROTECTIVE FINISH IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.Nov 17, 2006 · N651AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200633101Repair · corrodedPREVIOUS REPAIR ON LEFT OMEGA BEAM AT FRAME 20 CORRODED. REMOVED PREVIOUS REPAIR. FABRICATED REPAIR DOUBLERS, CLEANED, TREATED AND INSTALLED REPAIR DOUBLERS AND RESTORED PREVIOUS FINISH IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.Nov 17, 2006 · N651AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 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)Dec 8, 2004 · N651AE · Emb EMB145LR · Emergency LightingSDR 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)Dec 4, 2004 · N651AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 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)Dec 4, 2004 · N651AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200434218Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED ATHE CORRODED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW SRM. (K)Dec 2, 2004 · N651AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 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)Nov 30, 2004 · N651AE · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR 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)Nov 30, 2004 · N651AE · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR SIMA200323601Ecu · malfunctionedLRD - FLT 3453 - DURING APPROACH, CREW REPORTED THE FLAPS WOULD NOT DEPLOY. FOLLOWED AOM PROCEDURES AND LANDED WITHOUT FLAPS WITH NO OTHER PROBLEMS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONROL UNIT IAW EMB MM. OPS CHECK WAS GOOD ANDAug 19, 2003 · N651AE · Emb EMB145LR · Trailing Edge Flap Control SystemSDR SIMA200218411Skin · dentedABI - FOUND DENT ON FUSELAGE UNDER RIGHT ENGINE FRAME 65, 66, 57, STRINGER 14R. DENT WAS REPAIRED IAW EO NR EM-53MR-391 PART A. (M)Jul 1, 2002 · N651AE · Emb EMB145LR · Fuselage Main, Plate/Skin
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