Keystone Helicopter S-92A
Service difficulty reports · 324
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 = 'S92A' 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 = 'S92A' 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 AMCR200700003Brake Assy · bindingDURING WHEEL CHANGE (LT OB) COULD NOT REMOVE THE WHEEL OFF OF AXLE. FOUND ONE OF THE CENTER STATORS (A35579) OF THE BRAKE ASSY TO BE PROTRUDING OUT OF THE PACK. THE STATOR CUT INTO THE WHEEL PREVENTING THE REMOVAL. WE DID NOT TEARDOWN THE BRAKE BUT SUSPECT EITSDR HEEA116019Detector · malfunctionedNR 2 ENGINE FIRE LIGHT ILLUMINATED FOR APPROX 2 SECONDS DURING IFR CLIMBOUT FIVE MINUTES AFTER TAKEOFF. REPLACED FLAME DETECTOR AND ALSO REPLACED HARNESS 92552-04112-041.SDR HEEA114154Control Panel · failedUPON APPROACH TO GC902 DURING BEFORE LANDING CHECK, GEAR WOULD NOT EXTEND. RETURNED TO HUM AND USED EMERGENCY BLOW DOWN. TROUBLESHOOTING REVEALED CONTACTS BETWEEN PINS A AND B OF LANDING GEAR CONTROL PANEL MAINTAINING CONTINUITY WHEN GEAR LEVER IS PLACED INSDR HEEA113586Fire Detector · malfunctionedENROUTE FROM MC778 TO HBP NR 2 ENGINE FIRE LIGHT CAME ON. REDUCED POWER BELOW 1200 LBS PER HR. FUEL FLOW AND LIGHT WENT OUT. INCREASED POWER AND LIGHT CAME BACK ON. REVIEWED ENGINE FIRE CHECKLIST AND REDUCED NR 2 ENGINE TO IDLE FOR OEI LANDING AT GRAND ISSDR CA070123007Cone · split(CAN) ON 06 JAN 07, THE TAIL ROTOR HEAD WAS IN PROCESS OF BEING REPLACED WHEN IT WAS NOTICED THAT THE IB SET OF SPLIT CONES WHICH CENTER AND SUPPORT THE TAIL ROTOR HUB LOADS WERE MISSING. FURTHER INVESTIGATION FOUND THAT WHEN THIS TAIL GEARBOX WAS INSTALLED 59SDR CA070115006Gearbox · malfunctioned(CAN) MAIN GEARBOX HAD SEVERAL OCCURENCES OF OIL PRESSURE DROPPING TO THE PRECAUTIONARY RANGE IN OPERATION. (TC NR 20070115006)SDR HEEA111740Fuel Filter · unknownNR 2 ENGINE FUEL PRESSURE LIGHT INTERMITTENT IN FLIGHT, RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL FILTER AND PRESSURE SWITCH 3066T64P01.SDR CA061023002Hinge Fitting · cracked(CAN) THE FOLLOWING INFORMATION REFERS TO CHC HELICOPTERS INTERNATIONAL GROUND OCCURRENCE REPORT ,WHICH WAS SUBMITTED BY OUR BASE IN MALAYSIA: "ON CARRYING OUT 50 HOUR INSPECTION ON PASSENGER DOOR AND HINGES, FOUND FORWARD UPPER HINGE CRACKED. CRACK WAS RUNNINSDR HEEA111385Seal · leakingOIL PRESSURE WAS NORMAL AFTER TAKEOFF, ABOUT 35 MIN IN CRUISE FLIGHT, NR 2 ENGINE OIL PRESSURE HAD DROPPED TO 55 PSI, THEN ON ARRIVAL, NR 2 ENGINE OIL PRESSURE WAS BETWEEN 47 AND 50 PSI. REPLACED G AXIS SEAL.SDR CA061002002Engine · failed(CAN) THE FOLLOWING REPORT REFERS TO FLT OCCURRENCE REPORT NR 06-00894. THE AIRCRAFT WAS OPERATING FOR CUSTOMER ON AN OFFSHORE FLIGHT. AT APPROX 09.58 WHILE ON SHORT FINAL APPROACH (IN VMC), 2 POPS WERE HEARD BY THE CREW. A MISSED APPROACH WAS INITIATED, AND DSDR HEEA110993Seal · failedIN CRUISE NR 1 ENGINE OIL PRESSURE DECREASED TO 28 PSI, CHECK LIST COMPLIED WITH AND RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE AXIS G SEAL AND MATING RING PN 4045T77P02.SDR HEEA110979Wire · damagedSHORTLY AFTER TAKEOFF NR 2 ENGINE FIRE LIGHT AND AUDIO CAME ON AND WENT OFF AFTER 3 OR 4 SECONDS. MAINTENANCE REPAIRED INSULATION ON WIRE TO PIN C OF CONNECTOR TO THE OB FIRE DETECTOR.SDR HEEA109200Wire Harness · inoperativeDURING DESCENT TO LANDING, 9 MILES FROM HMA, NR 2 FIRE LIGHT CAME ON FOR ABOUT 3 SECONDS THEN WENT OFF. TWO MILES FROM LANDING, IT CAME ON AGAIN, THEN WENT OFF AFTER ABOUT 3 SECONDS. LANDED WITH NO PROBLEMS. REPAIRED WIRES IN HARNESS.SDR HEEA109090Bonding Jumper · looseAFTER DEPARTURE FROM HMA-BP HAD AFCS DEGRADE - AP1 & AP2 FAILED - WOULD NOT RESET. FOUND BONDING JUMPER LOOSE ON PITCH SAS ACTUATOR.SDR HEEA108876Wire Harness · malfunctionedDEPARTING LAFAYETTE FOR HOUMA NOTED NR 2 ENGINE FIRE WARNING LIGHT FLICKERING. RETURNED TO LAFAYETTE. MAINTENANCE REPLACED NR 2 ENGINE FIRE WARNING HARNESS.SDR HEEA108478Wire Harness · damagedJUST AFTER TAKEOFF NR 2 ENGINE FIRE LIGHT-AUDIO STARTED COMING ON AND OFF. IT DID THIS ABOUT 10 TIMES EVERY 30 SECONDS OR SO UNTIL WE LANDED AT LFT AND SHUTDOWN. REPLACED NR 2 ENGINE FIREWALL TO FLAME DETECTOR HARNESS.SDR HEEA108295Control Panel · inoperativeNR 2 FIRE LIGHT ILLUMINATED VERY BRIEFLY WITH THE FIRE AUDIO, A FEW SECONDS LATER CAME ON FOR A LONGER DURATION - APPROX. 10 SEC. BROUGHT NR 2 THROTTLE BACK TO IDLE AND PREPARED TO EXECUTE THE FIRE EMERGENCY PROCEDURE. JUST PRIOR TO PUSHING THE FIRE BUTTON,SDR CA060210007Engine · making metal(CAN) AFTER TAKE-OFF, ENGINE NR 2 CHIP LIGHT STARTED TO FLICKER. AC WAS TURNED AROUND TOWARDS PLACE OF DEPARTURE. EMERGENCY CHECKLIST WAS FOLLOWED, ENG NR 2 WAS BROUGHT BACK TO IDLE. DURING A LONG FINAL ON DESCENT, ENGINE WAS BROUGHT BACK ON LINE FOR LANDINGSDR HEEA107969Computer · malfunctionedDURING CRUISE AIRCRAFT STARTED UNCOMMANDED DESCENT WITH NOSE PITCH UP. ROTOR SPLIT HIGH TO 107. ESTABLISHED CONTROL. FOUND COLLECTIVE WANTED TO DRIVE FULL DOWN. DISENGAGED COLLECTIVE TRIM AND PROBLEM CEASED. SWAPPED FROM FD NR 1 TO FD NR 2 AND PROBLEM CESDR HEEA107895Trim Switch · shortedDURING CRUISE AIRCRAFT STARTED UNCOMMENTED DESCENT WITH NOSE PITCH UP. ROTOR SPLIT HIGH TO 107. ESTABLISHED CONTROL. FOUND COLLECTIVE WANTED TO DRIVE FULL DOWN. DISENGAGED COLLECTIVE TRIM AND PROBLEM CEASED. SWAPPED FROM FD#1 TO FD#2 AND PROBLEM CEASED THSDR HEEA107325Heat Exchanger · rupturedDURING CRUISE FLIGHT, THE NR 1 HYDRAULIC RESERVOIR LOW LIGHT ILLUMINATED, FOLLOWED BY OTHER ASSOCIATED LIGHTS CONFIRMING THE NR 1 HYDRAULIC SYSTEM FAILURE. MAINTENANCE FOUND THE HYDRAULIC SYSTEM HEAT EXCHANGER RUPTURED.SDR HEEA107335Line · rupturedNR 2 HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE FOUND NR 2 HYDRAULIC PUMP DISCHARGE HOSE HAD RUPTURED. REPLACED HOSE.SDR HEEA107354Selector Valve · failedDURING TAKEOFF, NR 1 ENGINE FAILED. RETURNED TO DEPARTURE. MAINTENANCE REPLACED FUEL SELECTOR VALVE.SDR HEEA107343Hose · leakingON FIRST FLIGHT OF DAY, IN CRUISE HYD SERVO ONE LIGHT FOLLOWED BY HYD PUMP ONE LIGHT AND ONE HYD PRESSURE WENT TO ZERO. FOUND PIN HOLE IN HOSE UNDER CLAMP. REPLACED HOSE AND CLAMP.
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