N577W

Service difficulty reports · 27

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 = 'N577W' 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 XGNA20240223002Rib · cracked1 5/8-INCH CRACK ORIGINATING FROM THE FORWARD END OF LOWER FLANGE OF THE AFT INBOARD RIB. CRACK EXTENDS BEYOND THE FIRST RIVET OF FLANGE THEN SPLITS INTO 2 CRACKS WITH ONE ALMOST TO THE SECOND RIVET AND THE SECOND MOVING TOWARD THE RADIUS OF THE BEND IN THE FLFeb 19, 2024 · N577W · Beech 58 · Horizontal Stabilizer, Spar/RibSDR XGNA20240219001Rib · cracked2 3/16-INCH CRACK IN AFT END OF LOWER FLANGE OF INBOARD FORWARD RIB. CRACKED THROUGH FIRST 3 RIVETS THEN, INTO RADIUS OF FLANGE JUST STARTING UPWARD INTO THE WEB OF RIB.Feb 19, 2024 · N577W · Beech 58 · Horizontal Stabilizer, Spar/RibSDR XGNA202402150005Rib · crackedTWO CRACKS IN INBOARD FORWARD RIB OF LEFT HORIZONTAL STABILIZER AT STA 00.000. .25-INCH CRACK ORIGINATING FROM THE EDGE OF THE UPPER AFT FLANGE INTO THE FIRST RIVET. 2.5-INCH CRACK ORIGINATING FROM THE EDGE OF THE LOWER AFT FLANGE THROUGH THE FIRST 3 RIVETS, JFeb 14, 2024 · N577W · Beech 58 · Horizontal Stabilizer, Spar/RibSDR XGNA2024021500006Channel · cracked.25-INCH CRACK INTO FIRST RIVET IN LOWER FLANGE OF FRONT SPAR CHANNEL AT HORIZONTAL STABILIZER STA 00.000.Feb 14, 2024 · N577W · Beech 58 · Horizontal Stabilizer StructureSDR XGNA202402150004Rib · crackedCRACK 1.0 INCH IN LENGTH IN FORWARD LOWER FLANGE OF AFT INBOARD RIB AT HORIZONTAL STABILIZER STA 00.000. CRACK FROM AFT END OF FLANGE THROUGH THE FIRST RIVET AND THEN SPLITTING OFF INTO 2 CRACKS WITH THE MAIN CRACK ALMOST INTO THE SECOND RIVET AND THE OTHER CRFeb 14, 2024 · N577W · Beech 58 · Horizontal Stabilizer, Spar/RibSDR XGNA2021052500012Spar · crackedDURING A VISUAL INSPECTION REQUIRED BY AD 90-08-14 SPAR CARRY THRU INSPECTION CRACKS WERE FOUND RADIATING FROM THE OUTBOARD UPPER HUCKBOLT HOLE OUTWARD ON THE FORWARD AND AFT SIDES OF THE LEFT HAND FORWARD SPAR. THESE CRACKS WERE FOUND ABOVE THE INSPECTION AREFeb 15, 2021 · N577W · Beech 58 · Fuselage Main, StructureSDR XGN2013F00002Fitting · crackedTHIS MOUNT IS RIVETED ONTO THE REAR SPAR, IT IS WHERE THE LG MOUNTS INSIDE THE LT WING AFT SIDE. THE BOLT THAT GOES THRU THE LG MOUNT GOES INTO THIS FITTING ON THE SPAR. THE FITTING IS CRACKED HORIZONTALLY JUST ABOVE THE BOLT PASS THROUGH ON THE VERTICAL LEGNov 15, 2013 · N577W · Beech 58 · Wing, Landing Gear Attach FittingsSDR XGN2007F00015Cylinder · crackedCYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)Oct 23, 2006 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2007F00007Cylinder Head · crackedCYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)Oct 23, 2006 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2007F00012Cylinder · crackedCYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)Sep 21, 2006 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2007F00011Cylinder · crackedCYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)Sep 21, 2006 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2007F00009Cylinder Head · crackedCYLINDER HEAD CRACKED IN EXHAUST AREA. (K)Sep 21, 2006 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2007F00005Cylinder Head · crackedCYLINDER HEAD CRACKED INTHE EXHAUST AREA. (K)Sep 21, 2006 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2006F00050Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HR INSPECTION. WE ARE USING A SOAP SOLUTION TO DETECTED CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HRS. 3 CRACKED CYLINDER WEREMay 4, 2006 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2006F00049Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HR INSPECTION. WE ARE USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HRS. 3 CRACKED CYLINDER WERE FMay 4, 2006 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2006F00044Cylinder · crackedFOUND CYLINDER HEAD CRACKED IN THE EXHAUST SIDE DURING A 50 HR INSPECTION. THIS IS AN ON GOING PROBLEM WITH THE CYLINDERS. (K)Oct 11, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2005F00014Cylinder · crackedFOUND CYLINDER HEAD CRACKED IN THE EXHAUST SIDE DURING A 50 HOUR INSPECTION. THIS IS AN ON GOING PROBLEM WITH THE ECI CYLINDER. (K)Oct 11, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2006F00048Cylinder · crackedFOUND CRACKED CYLINDER HEAD AT 50 HR INSPECTION. DUE TO THE FREQUENCY OF THE NUMBER OF CYLINDERS WE ARE FINDING CRACKED, WE DO A COMPRESSION CHECK EACH 50 HRS. (K)Oct 5, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2006F00045Cylinder · crackedCYLINDER HEAD CRACKS FOUND AT 50 HR INSPECTION. DUE TO THE FREQUENCY OF THE NR OF CYLINDERS WE ARE FINDING CRACKED, WE DO A COMPRESSION CHECK EACH 50 HOURS. (K)Sep 6, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2005F00005Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HOUR INSPECTION. WE ARE USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HOURS. 3 CRACKED CYLINDERS WMay 4, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2005F00004Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HOUR INSPECTION. WE ARE USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HOURS. 3 CRACKED CYLINDERS WMay 4, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2005F00003Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HOUR INSPECTION. ARE USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HOURS. 3 CRACKED CYLINDERS WEREMay 4, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2006F00047Cylinder · crackedCYLINDER HEAD CRACKED, FOUND DURING 100 HR INSPECTION. THIS IS AN ON GOING PROBLEM THAT WE ARE FINDING IN OUT FLEET OF AIRCRAFT. (K)Apr 26, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2006F00046Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HR INSPECTION. USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. DOING COMPRESSION CHECKS EACH 50 HRS. 3 CRACKED CYLINDERS WERE FOUND ON THE Apr 26, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2005F00002Cylinder Head · crackedCYLINDER HEAD CRACKED. FOUND DURING 100 HR INSPECTION. THIS IS AN ONGOING PROBLEM THAT WE ARE FINDING IN OUR FLEET OF AIRCRAFT. (K)Apr 26, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR 98ZZZX148Cylinder · failedDURING A FLIGHT JUST AFTER TAKEOFF, PILOT REPORTED THE ENGINE PERIODICALLY LOST POWER AND VIBRATED. UPON LANDING, PILOT ALSO NOTICED A CONSIDERABLE AMOUNT OF OIL ON THE NACELLE. UPON INVESTIGATION, DISCOVERED THE NR 6 CYLINDER PUSH ROD WAS BENT AND PUSH ROD Dec 12, 1997 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR 96ZZZM986Drive Gear · strippedUPON LANDING GEAR ACTUATION, LANDING GEAR CYCLE SLOWER THAN NORMAL AND GRINDING NOISE HEARD. UPON REMOVED OF LANDING GEAR MOTOR, P/N 1514818, STRIPPED OF ALL TEETH EXCEPT FOR 2 OR 3 TEETH REMAINING.May 22, 1996 · N577W · Beech 58 · Landing Gear Retraction/Extension System
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