Kiwi Technologies K1200
Service difficulty reports · 68
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 = 'K1200' 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.
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 = 'K1200' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 96ZZZX5040Droop Stop · bentDROOP STOP ON RT SIDE HUB WAS BENT BY PILOT WHEN ATTEMPTING TO INSTALL TEETER LOCKS DURING ACFT TY-DOWN PROCEDURE. CREW CHIEF HAD REPAIRED STOP, BUT STOP WAS TWEAKED FORE AND AFT AS WELL AS UP AND DOWN. STOP HUNG UP DURING COAST DOWN AND R/S ROTOR BLADES CHASDR 96ZZZX5039Engine · oil ventingENGINE WAS VENTING OIL OVERBOARD FROM LARGE VENT LINE CONNECTED TO N1 GEARBOX. ALL POSSIBLE STEPS TO CORRECT WERE NOT SUCCESSFUL. ENGINE WAS REPLACED AUGUST 29, 1996.SDR CA960826066Pump Body · cracked(CAN) PUMP WAS REMOVED TO FACILITATE TRANSMISSION REPLACEMENT WHEN PUMP MOUNTING FLANGE WAS FOUND CRACKED APPROXIMATELY 1 INCH ACROSS THE THINNEST PORTION OF THE FLANGE ADJACENT TO THE 1 O'CLOCK MOUNT HOLESDR CA960716007Blade · cracked(CAN) DURING HELI LOGGING OPERATION THE PILOT NOTICED INCREASED RIGHT PEDAL REQUIRED TO MAINTAIN POSITION. WHEN IT BECAME OBVIOUS THAT WIND CONDITIONS WERE NOT RESPONSIBLE THE HELICOPTER LANDED WHERE IT WAS FOUND THAT THE BLADE HAD A 10" CRACK CHORDWISE ACROSSSDR CA960412013Blade · cracked(CAN) BLADES ARE MATCHED PAIRS. BLADE 1 - CHORDWISE CRACKS 10 INCHES LONG AT STN. 19 AND 75. BLADE 2 DIAGONAL CRACK AT STN. 15. CRACKS COULD NOT BEEN SEEN WITH BLADES AT REST AND UNDER OWN WEIGHT. FUTURE INSPECTIONS WILL BE WITH BLADE TIP SUPPORT.SDR GMAL9501025Seal Housing · crackedCIRCUMFERENCE CRACK OF OUTPUT GEARSHAFT SEAL HOUSING IN STEP-DOWN RADIUS OF HOUSING, 2:00 O'CLOCK TO 6:00 O'CLOCK POSITIONS. THIS SEAL RETAINER WAS REPLACED BY LYCOMING AT TOTAL TIME 583.6 ENGINE HOURS. (X)SDR GMAL9501024Seal Housing · crackedCIRCUMFERENCE CRACK OF OUTPUT GEARSHAFT SEAL HOUSING IN STEP-DOWN RADIUS OF HOUSING, LEFT AND RIGHT SIDES. (X)SDR GMAL9501023Fan · failedFAN MOTOR BEARINGS WORN. FAN WILL NOT ROTATE. FAN WAS INSTALLED AT A/C TT 560.8 HOURS ON 8-10-95. PREVIOUS FAN WAS REPLACED FOR SAME PROBLEM. TOTAL TIME, AIRCRAFT, 560.8 HOURS. (X)SDR GMAL9501022Seal Housing · crackedCIRCUMFERENCE CRACK OF OUTPUT GEAR SHAFT HOUSING IN STEP-DOWN RADIUS OF HOUSING, LEFT AND RIGHT SIDES 2:00 O'CLOCK TO 5:00 O'CLOCK AND 7:00 O'CLOCK TO 10:00 O'CLOCK POSITIONS. (X)SDR GMAL9501021Governor · defectivePILOT REPORTED GOVERNOR DECAY FROM 104 PERCENT NR DOWN TO 97 PERCENT NR DURING HOVER. PROBLEM INTERMITTENT EVERY 3 TO 4 TURNS DURING LOGGING OPERATIONS. (X)SDR GMAL951207Blade · crackedMAIN ROTOR BLADE CRACKED. CRACK LOCATED AT STA 109.5, CORDWISE, TOP 10.25 INCHES LONG, 4.5 INCHES AFT OF LEADING EDGE. ONLY 10 HOURS OF FERRY FLIGHT SINCE LAST INSPECTION. AIRCRAFT TOTAL TIME 985 HOURS. (X)SDR GMAL9509142Blade · crackedMAIN ROTOR BLADE FOUND CRACKED, CRACK LOCATED BETWEEN STA 172 AND STA 180, CORDWISE ON BOTTOM OF BLADE AT 13 INCHES LONG, 5 INCHES FROM LEADING EDGE. ONLY 4 HOURS OF FLIGHT SINCE LAST INSPECTION. AIRCRAFT TOTAL TIME 566 HOURS, 3 BLADES FOUND CRACKED AT SAME SDR GMAL9601252Blade · crackedMAIN ROTOR BLADE CRACKED. LOCATION UNKNOWN AT THIS TIME. BLADE RETURNED TO MANUFACTURER. (X)SDR 95ZZZX7039Airframe · crackedHELICOPTER USED IN LOGGING OPERATION. DURING DAILY INSPECTION, SHEET METAL CRACK ABOUT 3 INCHES IN LENGTH WAS DISCOVERED ON THE STRUCTURAL SUPPORT FOR THE LEFT FORWARD TRANSMISSION MOUNT PAD. THE CRACK IS RADIATING OUTWARD FROM A RIVET. SUSPECT CAUSE, IMPROPSDR GMAL9509143Blade · crackedMAIN ROTOR BLADE FOUND CRACKED. CRACK LOCATED AT STA 172 AND STA 180, CORDWISE ON BOTTOM OF BLADE AT 13 INCHES LONG, 5 INCHES FROM LEADING EDGE. ONLY 4 HOURS OF FLIGHT SINCE LAST INSPECTION. ACFT TOTAL TIME, 566 HOURS, 3 BLADES FOUND CRACKED AT SAME TIME. SDR GMAL9509141Blade · crackedMAIN ROTOR BLADE FOUND CRACKED. CRACK LOCATED AT STA 174, CORDWISE ON BOTTOM OF BLADE AT 10 INCHES LONG, 5 INCHES AFT OF LEADING EDGE. ONLY 4 HOURS OF FLIGHT SINCE LAST INSPECTION. AIRCRAFT TOTAL TIME 566 HOURS. THREE BLADES FOUND CRACKED AT SAME TIME. (XSDR 95ZZZX6245Drive Shaft · defectiveTA-7 FUEL CONTROL, TIP SEAL PUMP EQUIPPED, WAS FOUND TO HAVE WORN SPLINES. PUMP SECONDARY FUEL FLOW REDUCED TO ZERO PPH. PRIMARY PUMP FLOW REMAINED FULLY FUNCTIONAL. DRIVE SHAFT AND MATING PUMP GEAR SET WERE REPLACED WHILE CONTROL WAS RETURNED REPAIRED.SDR GMAL9601251Blade · crackedMAIN ROTOR BLADE CRACKED. CRACK AT BLADE STA 124, 2.9345 INCHES LONG. (X)
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