Weatherly 620B

Service difficulty reports · 16

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 aircraft_model_key = '620B'
  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 CA150527006Control Cable · frayed(CAN) DURING ITS ANNUAL INSPECTION, THE LT RUDDER CABLE ASSEMBLY WAS FOUND WORN & FRAYED ON THE AFT PULLEY. THE RT RUDDER CABLE WAS FOUND TO BE WORN OUT & FRAYED AS WELL. CABLES REMOVED & TO BE REPLACED WITH NEW UNITS. BOTH LT & RT RUDDER CABLE ASSEMBLIES AMay 22, 2015 · Wthrly 620B · Rudder Control SystemSDR CA141015007Attach Angle · loose(CAN) WHILE CARRYING OUT AN ANNUAL INSPECTION, ALL RIVETS THOUGH THE HORIZONTAL STABILIZER ATTACH ANGLES (LONGERONS) AND DIRECTLY ADJACENT TO ALL FOUR STABILIZER ATTACH BLOCKS, WERE FOUND TO BE LOOSE AND SMOKING.Oct 15, 2014 · Wthrly 620B · Elevator Tab, Attach FittingsSDR CA141015006Rib · cracked(CAN) ANNUAL INSPECTION REVEALED CRACKS IN THE MAJORITY OF BOTH THE LH AND RH WING LEADING EDGE NOSE RIBS, CRACKS EMANATE FROM THE AFT PORTION OF THE UPPER AND LOWER FLANGES OF THE RIBS.Oct 15, 2014 · Wthrly 620B · Wing, Rib/BulkheadSDR CA100730007Blade · separatedPROPELLER RECEIVED FROM CUSTOMER WITH APPROX 5" OF BLADE MISSING FROM NR2 BLADE TIP (S/N H89522). PROPELLER DISMANTLED, CLEANED, CLAMPS AND HUB SPIDER MPI INSPECTED, BLADES LPI INSPECTED (IAW MFG), ALL BEARINGS REPLACED DUE TO CORROSION AND DENTING, BLADE REPJul 30, 2010 · Wthrly 620B · Propeller Blade SectionSDR 2010FA0000208Rib · crackedMOST L/E RIBS CRACKED AT UPPER AND LOWER AFT CORNERS WHERE ATTACHED TO FWD HINGED HALF. 50 PERCENT TO LT WING RIBS WERE CRACKED AS WERE 90 PERCENT OF RT WING RIBS. THESE RIBS REQUIRED REPAIR AND REINFORCEMENT. OTHER ACFT MAY REQUIRE SIMILAR ACTION.Feb 8, 2010 · N9024F · Wthrly 620B · Wing, Rib/BulkheadSDR HNJ2008F00000Spar · crackedLT AILERON SPAR CRACKED AT CENTER AND OB HINGE BRACKET ATTACH POINTS. POSSIBLY DUE TO TWISTING EFFECT OF AILERON ACTUATOR INSTALLED AT EXTREME IB END OF AILERON. (K)Feb 4, 2008 · N9024F · Wthrly 620B · AileronsSDR 2005FA0000782Cylinder Head · separatedDURING SPRAYING OPERATION, THE AIRCRAFT WAS CLIMBING INTO A RT TURN. THE PILOT HEARD A LOUD BANG, AND THE ENGINE BEGAN RUNNING EXTREMELY ROUGH. THE AIRCRAFT MADE A FORCED LANDING. INSPECTION OF THE ENGINE FOUND THE NR 2 CYLINDER HEAD SEPARATED FROM THE SLEEMay 11, 2005 · N9026F · Wthrly 620B · Reciprocating Engine Cylinder SectionSDR 2002FA0000423Bulkhead · crackedDURING ANNUAL INSPECTION FOUND FUSELAGE BELLY PAN BULKHEAD (PN 50351-101) CRACKED UPPER LEFT AND RIGHT CORNER. THIS AREA IS HARD TO SEE WITHOUT FLASHLIGHT AND MIRROR. ALSO FOUND TAIL CONE BULKHEADS (PN 50351-105) AND (PN 50351-133) CRACKED AND TABS WHERE BUMar 25, 2002 · N90275 · Wthrly 620B · Fuselage Main, BulkheadSDR 2002FA0000422Bulkhead · crackedDURING ANNUAL INSPECTION FOUND FUSELAGE BELLY PAN BULKHEAD (PN 50351-101) CRACKED UPPER LEFT AND RIGHT CORNER. THIS AREA IS HARD TO SEE WITHOUT FLASHLIGHT AND MIRROR. ALSO FOUND TAIL CONE BULKHEADS (PN 50351-105) AND (PN 50351-133) CRACKED AND TABS WHERE BULMar 25, 2002 · N90275 · Wthrly 620B · Fuselage Main, BulkheadSDR 2002FA0000421Bulkhead · crackedDURING ANNUAL INSPECTION FOUND FUSELAGE BELLY PAN BULKHEAD (PN 50351-101) CRACKED UPPER LEFT AND RIGHT CORNER. THIS AREA IS HARD TO SEE WITHOUT FLASHLIGHT AND MIRROR. ALSO FOUND TAIL CONE BULKHEADS (PN 50351-105) AND (PN 50351-133) CRACKED AND TABS WHERE BULMar 25, 2002 · N90275 · Wthrly 620B · Fuselage Main, BulkheadSDR TYW2002F00000Blade · failed11 INCHES SEPRATED FROM ONE PROPELLER BLADE DURING FLIGHT. AIRCRAFT WAS SPRAYING A CROP AND WAS IN A TURN WHEN BLADE TIP SEPARATED.Feb 7, 2002 · N90275 · Wthrly 620B · Propeller Blade SectionSDR 2001FA0000255Valve Spring · brokenENGINE BEGAN BACKFIRING AND POWER DECREASED, AIRCRAFT LANDED AS A RESULT OF RUNNING THROUGH A FENCE. FOUND NR 1 CYLINDER INTAKE VALVE SPRINGS BROKEN. REPLACED SPRINGS, OPERATION NORMAL. APPEARED TO BE SMALL RUST PITS IN BREAK AREAS.Jul 25, 2001 · N2035N · Wthrly 620B · Reciprocating Engine Cylinder SectionSDR AU001056Piston · wrong part(AUS) INCORRECT PISTONS FITTED TO NR 4 AND NR 7 CYLINDERS. THE PISTONS WERE UNDRILLED AND ARE ONLY USED IN NR 5 AND NR 6 CYLINDERS. THE ENGINE HAD BEEN OVERHAULED IN THEUSA. UNAPPROVED PART. (X)Oct 24, 2000 · Wthrly 620B · Reciprocating Engine Cylinder SectionSDR 20000925SH021Screw · looseCARBURETOR FLOAT FULCRUM SCREW WAS FOUND LOOSE ON ANNUAL INSPECTION. BRASS THREADS WERE FOUND WORN. REPLACED FULCRUM SCREW, PROPERLY INSTALLED NEW SCREW AND SAFTIED. BELIEVE SCREW WAS NOT PROPERLY INSTALLED BY MANUFACTURER. SUBMITTER RECOMMENDED AN AD OR SSep 25, 2000 · N90303 · Wthrly 620B · Fuel Control/Reciprocating EnginesSDR 20000925SH023Screw · looseCARBURETOR FLOAT FULCRUM SCREW VIBRATED LOOSE CAUSING FLOAT TO STICK. AIRCRAFT ENGINE BEGAN RUNNING ROUGH. AIRCRAFT SUCCESSFULLY RETURNED TO FIELD. FULCRUM SCREW BRASS THREADS WERE FOUND WORN CAUSING SCREW3 TO COME LOOSE. AIRCRAFT WAS NEW ON 12-6-96 AND NOSep 1, 1999 · N9025D · Wthrly 620B · Fuel Control/Reciprocating EnginesSDR 20000925SH022Screw · looseCARBURETOR FLOAT FULCRUM SCREW SAFETY WIRE VIBRATED THROUGH BACKING OUT FULCRUM SCREW FOR FLOAT. ENGINE QUIT RUNNING CAUSING FORCED LANDING. AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE. FULCRUM SHOWED CHATTER MARKS INDICATING FULCRUM SCREW WAS NOT PROPERLY SEATEDAug 8, 1999 · N197SK · Wthrly 620B · Fuel Control/Reciprocating Engines
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