N625AE

Service difficulty reports · 168

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 = 'N625AE' 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 SIMA200220510Floorbeam · corrodedFOUND CORROSION ON GALLEY CENTER FLOORBEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FABRICATED A REPAIR DOUBLER AND FILLER. REPAIR DONE IAW SRM.Jul 19, 2002 · N625AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200220508Frame · dentedFOUND FRAME 71 DENTED AT STRINGER 16R IN CARGO COMPARTMENT. RECONTOURED DENT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (B8349)Jul 17, 2002 · N625AE · Emb EMB145LR · Fuselage Main, FrameSDR SIMA200220506Frame · dentedFOUND FRAME 72 DENTED AT STRINGERS 14 LT AND 15 LT IN CARGO COMPARTMENT. RECONTOURED DENT. FABRICATED A REPAIR DOUBLER USING CHANNEL FRAME. REPAIR DONE IAW SRM. (B8349)Jul 17, 2002 · N625AE · Emb EMB145LR · Fuselage Main, FrameSDR SIMA200220505Frame · dentedFOUND FRAME 72 DENTED AT STRINGERS 14 RT AND 16 RT IN CARGO COMPARTMENT. RECONTOURED DENT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (B8349)Jul 17, 2002 · N625AE · Emb EMB145LR · Fuselage Main, FrameSDR SIMA200220003Stringer · chafedABI - FOUND STRINGER 19R CHAFED. BLENDED CHAFED, FABRICATED AND INSTALLED A DOUBLER ANGLE, IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18 53-24-02, AEA ETN-51-020. (M)Jul 16, 2002 · N625AE · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR SIMA200220002Stringer · chafedFOUND STRINGER 19L CHAFED. BLENDED CHAFE, FABRICATED AND INSTALLED TWO DOUBLER ANGLES IAW EMB GST-2182/02, AEA ETN-51--020. (M)Jul 16, 2002 · N625AE · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR SIMA200220512Beam · damagedFOUND UNDOCUMENTED BLENDED AREAS ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED PREVIOUS REPAIR AND FABRICATED A DOUBLER, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW SRM. (B8349)Jul 13, 2002 · N625AE · Emb EMB145LR · Fuselage Main, StructureSDR SIMA200220513Sill · damagedFOUND NUMEROUS UNDOCUMENTED BLENDED AREAS ON SERVICE DOOR CENTER SILL. FILLED BLENDED AREAS WITH EPOXY RESIN, SANDED AREA SMOOTH. FABRICATED REPAIR DOUBLER. REPAIR DONE IAW SRM.Jul 12, 2002 · N625AE · Emb EMB145LR · Fuselage Main, StructureSDR SIMA200220503Windshield · corrodedFOUND PILOT WINDSHIELD CUTOUT LOWER STRIP HAS 6 CORRODED HOLES. REMOVED CORROSION BY REAMING HOLES 2 AND 4 TO ALLOWABLE LIMITS. REAMED HOLES 1 AND 4 TO .313 TO REMOVE CORROSION. FABRICATED TO FREEZE PLUGS. REPAIR DONE IAW SRM. (B8349)Jul 12, 2002 · N625AE · Emb EMB145LR · Fuselage Structure (General)SDR SIMA200219813Skin · dentedABI - DURING MBV INSPECTION MAINTENANCE FOUND A DENT 4 INCHES FORWARD OF FRAME 20 BELOW STRINGER 15L. PERFORMED EDDY CURRENT INSPECTION AND THICKNESS TEST AND FOUND NO DEFECTS. (M)Jul 6, 2002 · N625AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA200219812Skin · dentedABI - DURING MBV INSPECTION, FOUND A DENT 5.5 INCH AFT OF FRAME 19 BELOW STRINGERS 15L. PERFORMED EDDY CURRENT INSPECTION AND THICKNESS TEST AND FOUND NO DEFECTS. (M)Jul 6, 2002 · N625AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA200219811Skin · dentedABI - DURING MBV INSPECTION, MAINTENANCE FOUND A DENT BETWEEN FRAMES 17 AND 18 AND STRINGER 21-20L. PERFORMED EDDY CURRENT INSPECTION AND FOUND NO DEFECTS. DENT FOUND TO BE WITHIN EMB145 SRM 53-21-10, TABLE 102 LIMITS. (M)Jul 6, 2002 · N625AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA200219810Skin · dentedABI - DURING MBV INSPECTION MAINTENANCE FOUND A DENT 8 INCH AFT OF FRAME 20, BELOW STRINGER 11L. PERFORMED EDDY CURRENT INSPECTION AND FOUND NO DEFECTS. DENT ACCEPTED AS IS IAW EMB GST-2182/02, SURFACE PROTECTION RESTORED. (M)Jul 6, 2002 · N625AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA200219809Skin · dentedABI - DURING MBV MAINTENANCE, FOUND A DENT 3 INCH AFT OF FRAME 20, BELOW STRINGER 11L. PERFORMED EDDY CURRENT INSPECTION AND FOUND NO DEFECTS. DENT ACCEPTED AS IS IAW EMB GST-2182/02, SURFACE PROTECTION APPLIED. (M)Jul 6, 2002 · N625AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA200219808Skin · dentedABI - DURING MBV MAINTENANCE, FOUND DENT 3 INCHES FORWARD OF FRAME 20, BELOW STRINGERS 15L. PERFORMED EDDY CURRENT AND THICKNESS CHECK AND FOUND NO DEFECT. DENT TREATED FOR CORROSION AND ACCEPTED AS IS IAW EMB GST-2182/02. (M)Jul 6, 2002 · N625AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA1299Unknown · odorIND - FLT 4079 - WHEN CREW SELECTED APU BLEED AS BLEED SOURCE, THERE WAS A DEFINITE ODOR AND SMOKE IN CABIN. LAV SMOKE DETECTOR ACTIVATED. APU WAS MEL. 050-125D 49-2. FOUND APU OIL OVERSERVICED. DRAINED TO PROPER LEVEL. OPS CHECK GOOD. (X)May 8, 2000 · N625AE · Emb EMB145LR · Air Distribution SystemSDR SIMA1104Smoke Detector · malfunctionedCLE - FLT 4337 - BAGGAGE SMOKE LIGHT CAME ON IN FLIGHT. DISCHARGED BOTH FIRE BOTTLES AND DECLARED AN EMERGENCY. AIRCRAFT HAD NORMAL LANDING. INSPECTED CARGO AREA. NO EVIDENCE OF SMOKE OR FIRE DAMAGE. FOUND FORWARD SMOKE DETECTOR FAULTED. REMOVED AND REPLApr 19, 2000 · N625AE · Emb EMB145LR · Overheat DetectionSDR SIMA0711Controller · malfunctionedFLT 4239 - ORD - FLIGHT CREW NOTED ELECTRICAL SMELL ON APPROACH TO ORD. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER. OPS CHECK GOOD. (M)Mar 11, 2000 · N625AE · Emb EMB145LR · Integrated Flight System
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