Beechcraft-Hawker BH-125-400A
Service difficulty reports · 22
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 = 'BH125400A' 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 = 'BH125400A' 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 CA110315014Hinge Fitting · cracked(CAN) DURING ACCOMPLISHMENT OF AD 80-12-10 R1/SB 57-55 THE LEFT OUTBOARD HINGE UPPER LUG WAS FOUND TO BE CRACKED.SDR ET72009F00000Cabin Pressure · failedAPPROX 8-10 MINUTES INTO FLIGHT, HEARD A LOUD "POP" COME FROM THE REAR OF THE ACFT. FELT DISCOMFORT IN OUR EARS, LOOKED AT THE PRESSURIZATION GUAGES AND NOTICED THE CABIN VSI WAS CLIMBING OVER 6000 FPM AND THE CABIN ALTITUDE WAS CLIMBING RAPIDLY. ALL OXYGEN SDR DXTA200810173310Controller · inoperativeAT 14000' AND AT 280 KTS WITH AP/FD SELECTED TO LEFT SIDE, RIGHT SIDE ONLY AP PITCH TRIM FAIL LIGHT CAME ON. DISENGAGED AP, NO TRIMMING WAS REQUIRED, AND LIGHT WENT OUT. RE-ENGAGED AP AND SAME THING HAPPENED. REMOVED NR 2 FCC-4007, INSTALLED OVERHAULED FCC-4SDR 2006FA0000082Switch · pilot errorPILOT MISTAKENLY TRIPPED THE APU FIRE EXTINGUISHER SWITCH INSTEAD OF THE APU START SWITCH. BOTH SWITCHES ARE OF THE SAME STYLE, ARE LOCATED CLOSE TOGETHER AND BOTH HAVE THE SAME STYLE OF RED GUARDED SWITCHES. (K)SDR BTA2004F00001Control Valve · incorrectREJECTED TAKEOFF, UNUSUAL BLEED AIR NOISE IN COCKPIT WHEN THROTTLES WERE ADVANCED FOR TAKE-OFF. TAKE-OFF ABORTED BEFORE 60 KNOTS, DISCOVERED COCKPIT WINDOW DEMISTER CONTROL VALVE IN FULL OPEN POSITION, REPOSITIONED CONTROL HANDLE TO NORMAL POSITION. SUBSEQUESDR 20010517CW008Apu · malfunctionedINTERRUPTION TO A FLIGHT, UPON ARRIVAL , START ATTEMPT OF APU AFTER FIRST ATTEMPT FAILED TO LIGHT, CAUSED A FIRE IN EXHAUST PIPE. APU FIRE BOTTLE WAS EXPENDED, FIRE EXTINGUISHED, FIRE DEPARTMENT SPRAYED PKP WHICH REQUIRED INSPECTION AND APU AND APU FIRE BOTTSDR 99ZZZX1167Pump · failedON FLIGHT FROM CAE TO SDL, AIRCRAFT INSTRUMENTS INDICATED THE RIGHT-HAND HYDRAULIC PUMP FAILED. THE CREW LANDED AT LIT AND INSPECTED RIGHT ENGINE. HYDRAULIC FLUID NOTICED ON THE ENGINE NACELLE. MAINTENANCE INSPECTION SHOWED THAT THE NR 2 HYDRAULIC PUMP HAD SDR 98ZZZX4010Cooling Turbine · failedAIRCRAFT TOTAL TIME 6,992.5 HOURS. AIRCRAFT WAS IN CLIMB TO 10,000 FEET WHEN VIBRATIONS AND ODOR WERE NOTICED IN COCKPIT AND CABIN. RETURNED TO AIRPORT AND FOUND MAIN BEARINGS HAD FAILED ON COOLING TURBINE. MANUFACTURER HAS NO OVERHAUL PERIOD FOR THIS UNIT.SDR 98ZZZX3451Valve · failedAFTER APPROXIMATELY 2 HOURS OF CRUISE FLIGHT, AUXILIARY HEAT WAS SELECTED TO WARM COCKPIT. AFTER SYSTEM WAS TURNED ON FOR APPROXIMATELY 3 SECONDS, SMOKE AND EXCESSIVE HEAT WERE NOTED IN CABIN AND COCKPIT. SELECTING DECREASE OR (COLD) HAD NO EFFECT. RAN CHECSDR 98ZZZX20Valve · failedAFTER TAKEOFF, VALVE FAILED IN OPEN POSITION. THIS CAUSED EXCESSIVE HOT BLEED AIR TO REACH COCKPIT. PRESSURIZATION WAS DIFFICULT TO CONTROL AND PILOTS WERE SUBJECTED TO EXTREME HEAT. AIRCRAFT HAD TO DESCEND AND LAND AS SOON AS POSSIBLE. ONLY BY SHUTTING DOSDR 97ZZZX3445Wheel Half · crackedWHEEL HALF WAS TESTED FOR MILLION AIR; SALT LAKE CITY, UTAH IAW DUNOP 32-40-2(4) 6-28-84, FOUND CRACKED.SDR 97ZZZX2565Seal · tornMKE/LAX - CHARTER FLIGHT DIVERTED TO STL. P/R APPROXIMATELY 6 FEET OF THE 9 FEET RUBBER SEAL ON RT WING TO FUSELAGE FAIRING TORN OFF IN-FLIGHT. PILOTS REPORTED BY FLIGHT PHONE THAT ACFT DEVELOPED A MODERATE VIBRATION DURING FLIGHT. A PRECAUTIONARY OVERWEIGHSDR 32697125CKDuct · looseREAR BAY OVERHEAT LIGHT CAME ON IN FLIGHT. RE-INSTALLED ACM EXHAUST DUCT AND CLAMP. OPS CHECKED ON GROUND - GOOD. (X)SDR 96ZZZX5276Duct · crackedAIR CONDITIONING RAM AIR INTAKE TO REFRIGERATION UNIT INLET DUCT SEVERELY CRACKED ON LT AND RT SIDES LOWER AREA. RT SIDE LOWER CONNECTION PORT (CAPPED FOR THIS INSTALLATION) COMPLETELY SEPARATED FROM DUCT AND FOUND LAYING ON ELEVATOR FLIGHT CONTROL CABLES DURSDR 96ZZZX4334Tire · failedTIRE LOST 25 POUNDS PRESSURE OVERNIGHT. FOUND HOLE IN SIDEWALL. REPLACED TIRE WHICH HAD 199 LANDINGS. NORMAL USAGE GIVES 500 LANDINGS. TIRE SENT TO DUNLOP FOR EXAMINATION.SDR 96ZZZX4692Flap Vane · crackedTHE LT AND RT OTBD FLAP VANE SKINS AND VANE SPARS HAVE BEEN ALTERED FROM THE ORIGINAL. A RADIUS APPROX 1 INCH WIDE AND .6250 INCH DEEP HAS BEEN GROUND INTO THE FLAP VANES IN THE AREA OF THE OTBD FLAP HINGE. ONE RIVET HAS BEEN REMOVED. IT IS BELIEVED THIS 'SDR 96ZZZX4691Flap Vane · crackedTHE LT AND RT OTBD FLAP VANE SKINS AND VANE SPARS HAVE BEEN ALTERED FROM THE ORIGINAL. A RADIUS APPROX 1 INCH WIDE AND .6250 INCH DEEP HAS BEEN GROUND INTO THE FLAP VANES IN THE AREA OF THE OTBD FLAP HINGE. ONE RIVET HAS BEEN REMOVED. IT IS BELIEVED THIS 'SDR 96ZZZX3899Duct · crackedWHILE ACCOMPLISHING AIRFRAME INSPECTION, ONE OF THE INSPECTION REQUIREMENTS CALLED OUT TO INSPECT THE APU. WHILE CONDUCTING THE INSPECTION, NOTED A LARGE CRACK ABOVE THE RAM AIR DUCT DOOR. THE APU WAS REMOVED WHICH REVEALED THE CRACKED RAM AIR DUCT ASSY. THSDR 96ZZZX3048Duct · crackedWHILE ACCOMPLISHING 500-HOUR AIRFRAME INSPECTION, ONE OF THE INSPECTION REQUIREMENTS CALLED OUT TO INSPECT THE APU. DURING INSPECTION, LARGE PIECES OF METAL WERE FOUND BEHIND THE APU. APU REMOVED WHICH REVEALED THE CRACKED RAM AIR DUCT ASSY. THE RT SIDE OF SDR 96ZZZX2573Wheel Assy · brokenFOUND RT MLG OUTBOARD WHEEL BROKEN ON BRAKE SIDE OF ASSY. APPROXIMATELY 8 INCHES OF THE RIM HAD BROKEN OFF DURING LANDING. THIS CONDITION WAS FOUND DURING A POST-FLIGHT INSPECTION. LANDING WAS UNEVENTFUL AND NO DAMAGE OCCURRED IN THE AREA OF WING.SDR 95ZZZX6462Valve · failedHYDRAULIC FLUID FLOWED FROM RESERVOIR TO BLEED AIR SYSTEM THROUGH RT PRESSURE SOURCE LINE. SUSPECT HYDRAULIC FLUID FLOW INTO BLEED AIR SYSTEM CAUSED BY INITIAL FLOW OF AIR IN SYSTEM. NON-RETURN VALVE IN PRESSURE SOURCE LINE INSTALLED TO PREVENT THIS REVERSE SDR 95ZZZX3266Wheel Half · crackedINSPECTION FOUND A 1 INCH CRACK LOCATED IN THE RADIUS OF THE HUB ADJACENT TO THE PART NUMBER/SERIAL NUMBER. THIS PART WAS EDDY CURRENT TESTED IAW DUNLOP 32-40-02(4), REV. 41.
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