Bell 206B

Service difficulty reports · 1,564

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 = '206B'
  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 HEEA954563Wheel · sulfidationENGINE REMOVED DUE TO CYCLED 1ST THROUGH 4TH STAGE WHEELS. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: MILD SULFIDATION ON 50% OF TURBINE 1ST STAGE WHEELS BLADES. SCRAPPED 1ST STAGE WHEEL.Mar 22, 1995 · N2271V · Bell 206B · Turbine SectionSDR HEEA954544Adapter · seal leakingSEAL LEAKING. ALSO REPLACED HOUSING P/N 206-040-052-009 AND SEAL P/N 206-040-156-101 AS AN ASSEMBLY. SEE MMIR'S #4542 AND #4543 FOR OTHER PARTS REPLACED.Mar 16, 1995 · N2277A · Bell 206B · Main Rotor GearboxSDR HEEA954543Seal Assy · leakingSEAL LEAKING. ALSO REPLACED HOUSING P/N 206-040-052-009 AND ADAPTER P/N 206-040-048-003 AS AN ASSEMBLY. SEE MMIR'S #4542 AND #4544 FOR OTHER PARTS REPLACED.Mar 16, 1995 · N2277A · Bell 206B · Main Rotor GearboxSDR HEEA954542Housing · seal leakingSEAL LEAKING. ALSO REPLACED SEAL P/N 206-040-156-101 AND ADAPTER P/N 206-040-048-003 AS AN ASSEMBLY. SEE MMIR'S #4543 AND #4544 FOR OTHER PARTS REPLACED.Mar 16, 1995 · N2277A · Bell 206B · Main Rotor GearboxSDR 95ZZZX1926Line · crackedDURING NORMAL FLIGHT, NOTED THE TOT WAS HIGHER THAN NORMAL (45 DEGREES - 50 DEGREES). REPLACED CRACKED LINE FROM BLEED VALVE TO COMPRESSOR.Mar 15, 1995 · N2299U · Bell 206B · Engine Bleed Air SystemSDR HEEA954366Fin · separatedSEPARATED AT STINGER AND FIN OVERWEIGHT 17.1 LBS.Feb 14, 1995 · N2277A · Bell 206B · Vertical StabilizerSDR HEEA954319Transceiver · defectiveNO ACTIVITY FROM LIGHT AND LIGHT OPERATIONAL. NO ACTIVITY WHEN LANDING LIGHT CYCLED. FOUND UNIT INOPERATIVE. REPLACED OPEN TRANSISTOR Q415. REPAIRED. ALSO REPLACED CRACKED FACEPLATE, BAD PHOTOCELL V301, DETERIORATED RESISTOR R477 AND PUT HEATSINK BEHIND Q4Feb 6, 1995 · N2271V · Bell 206B · ATC Transponder SystemSDR 95ZZZX2539Hose Assy · corrodedINSPECTION FOUND MOISTURE IS TRAPPED BETWEEN FIRE SLEEVE AND ALUMINUM FITTING AND CAUSES CORROSION OF THE FITTING AND FIRE SLEEVE.Jan 31, 1995 · N35Q · Bell 206B · Powerplant SystemSDR 95ZZZX2538Hose Assy · corrodedINSPECTION FOUND MOISTURE IS TRAPPED BETWEEN FIRE SLEEVE AND ALUMINUM FITTINGS AND CAUSES CORROSION OF THE FITTING AND FIRE SLEEVE.Jan 31, 1995 · N35Q · Bell 206B · Powerplant SystemSDR 95ZZZX2537Hose Assy · corrodedINSPECTION FOUND MOISTURE IS TRAPPED BETWEEN FIRE SLEEVE AND ALUMINUM FITTINGS AND CAUSES CORROSION OF THE FITTINGS AND FIRE SLEEVE.Jan 31, 1995 · N35Q · Bell 206B · Powerplant SystemSDR 95ZZZX1053Bearing · crackedMECHANIC NOTED A CRACKED FEATHERING BEARING ON TAIL ROTOR BLADE DURING POST-FLIGHT INSPECTION. REPLACED BEARING AND SLEEVE, PN 206-010-765-001 AND PN 206-010-733-003, IAW WITH BHT C.R. & O. MM.Jan 27, 1995 · N125NH · Bell 206B · Tail Rotor BladesSDR HEEA954188Bearing · defectiveFEATHERING BEARING ONE EACH OUTBOARD DEFECTIVE, ONE EACH OUTBOARD WORN. PAINT PEELING FROM BLADES. ALSO REPLACED 4 EACH SLEEVES P/N 206-010-733-003. BLADES S/N CS-6053, T.T. 859:05, BLADES CS-6017, T.T. 859:05. BOTH BLADES WERE RECEIVED 2-1-94Jan 23, 1995 · N2275Q · Bell 206B · Tail Rotor BladesSDR HEEA954187Bearing · wornFEATHERING BEARING ONE EACH OUTBOARD DEFECTIVE, ONE EACH OUTBOARD WORN. PAINT PEELING FROM BLADES. ALSO REPLACED 4 EACH SLEEVES P/N 206-010-733-003. BLADES S/N CS-6053, T.T. 859:05, BLADES CS-6017, T.T. 859:05. BOTH BLADES WERE RECEIVED 2-1-94,Jan 23, 1995 · N2275Q · Bell 206B · Tail Rotor BladesSDR HEEA954234Templates · overtempOVERTEMP INDICATIONS. OPPOSITE SIDE OF DISC - 2 EACH TEMP PLATES OVERTEMP.Jan 12, 1995 · N3181J · Bell 206B · Main Rotor Drive System
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