N24BH, cancelled Jun 18, 2026

Service difficulty reports · 19

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N24BH' AND deregistration_id = 'N24BH-2026-06-18'
  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 TIMA20251226004Electrical Box · contaminatedWHILE IN CRUISE FLIGHT THE CIRCUIT BREAKER PANEL STARTED SMOKING. PILOT REQUESTED APPROACH FOR PRIORITY IN HELENA, MT. PILOT SAID THE SMOKE SHORTLY STOPPED AFTER 5 SECONDS. PILOT HAD A NORMAL LANDING IN KHLN AND CONTACTED MAINTENANCE. MAINTENANCE SAID THAT DE-Dec 23, 2025 · N24BH · Beech 99 · Light System WiringSDR TIMA20151015006Gear Set · strippedDURING CRUISE CLIMB AT APPROX 9000 FT, THE LT ENG SUDDENLY LOST ALL POWER. ACFT RETURNED TO DEPARTURE LOCATION & LANDED WITHOUT INCIDENT. INSPECTION REVEALED THE LT ENG HIGH PRESS FUEL PUMP GEAR SET SPLINE WAS STRIPPED RESULTING IN FUEL PUMP FAILURE.Oct 15, 2015 · N24BH · Beech 99 · Engine Fuel PumpSDR TIMA20140213005Rib · crackedINSPECTION REVEALED A CRACK IN THE RT ELEVATOR LE RIB. THE RIB WAS REPLACED WITH A NEW RIB.Feb 13, 2014 · N24BH · Beech 99 · Elevator, Spar/RibSDR TIMA201000002Cowling · openCOWL OPENED AFTER TAKEOFF. PILOT STATED THAT HE LATCHED THE COWL, BUT THERE IS NO WAY TO VISUALLY CONFIRM THAT THE LATCHES WERE CONNECTED. COWL WAS SUBSTANTIALLY DAMAGED BY BUFFETING.Jan 14, 2010 · N24BH · Beech 99 · Engine Cowling SystemSDR TIM2006F00001Skin · corrodedTHE SKIN ON THE UPPER LEADING EDGE OF THE RT AILERON WAS FOUND TO BE TEARING AFT. INVESTIGATION DETERMINED THAT THERE WAS SIGNIFICANT CORROSION ON THE INSIDE OF THE AILERON. (K)Jan 6, 2006 · N24BH · Beech 99 · AileronsSDR TIM2005F00011Ground Wire · corrodedLANDING GEAR FAILED TO EXTEND. INSPECTION FOUND A CORRODED GROUND WIRE. THE FAILURE WAS INTERMITTENT THIS CAUSED CONSIDERABLE TROUBLE IN THE TROUBLESHOOTING AND SEVERAL HOURS OF TIME TO REPAIR THE PROBLEM. (K)Nov 8, 2005 · N24BH · Beech 99 · Landing Gear System WiringSDR 2004F00035Door · departedLEFT ENGINE COWLING SIDE DOOR DEPARTED FROM AIRCRAFT DURING FLIGHT. INSPECTION REVEALED THAT THE CAUSE WAS MOST LIKELY, FAILURE TO SECURE DOOR PANEL PRIOR TO FLIGHT NM-SLC-FSDO. (M)Oct 27, 2003 · N24BH · Beech 99 · Nacelle/Pylon, Main FrameSDR 20000913SH020Turbine · lightning strikeTHE AIRCRAFT WAS BROUGHT INTO MAINTENANCE FOR A SCHEDULED INSPECTION. UPON INSPECTION OF THE LEFT ENGINE, A HOLE WAS FOUND IN THE POWER SECTION CASE. THE HOLE CAUSED DAMAGE TO EXTERNAL WIRING AND TRANSFER TUBES. SUBMITTER STATED CAUSED BY A LIGHTING STRIKE.Aug 28, 2000 · N24BH · Beech 99 · Turbine SectionSDR 20000808SH032Arm · wornNOSE STEERING WAS REPORTED TO BE LOOSE. INSPECTION REVEALED RUDDER PEDAL ARM PIVOT HOLES ELONGATED. REPLACED RUDDER ARM ASSY WITH NEW COMPONENT AND NEW HARDWARE AS NECESSARY. LACK OF LUBRICATION IN THIS AREA POSSIBLY ACCELERATED THE WEAR OF THE PIVOT HOLES.Jul 7, 2000 · N24BH · Beech 99 · Nose/Tail Landing GearSDR 20000808SH031Arm · looseNOSE STEERING REPORTED LOOSE AND INSPECTION REVEALED NOSE STEERING TORQUE ARM HOLE TO ACTUATOR ELONGATED. REPLACED NOSE STEERING TORQUE ARM WITH SERVICEABLE ARM. THE ELONGATION COULD HAVE BEEN PREVENTED WITH THE ADDITION OF SHIMS BETWEEN THE CLEVIS ARM AND TJul 7, 2000 · N24BH · Beech 99 · Nose/Tail Landing GearSDR 20000803SH010Vane · inaccurateA TREND HAS DEVELOPED INDICATING PROCEDURES, TECHNIQUES, OR WORKMANSHIP OF OVERHAULED VANE RINGS IS RESULTING IN PREMATURE FAILURE OF PN 3032651 WHICH RESULTS IN UNSATISFACTORY ENGINE PERFORMANCE AND POSSIBLE ENGINE FAILURE. (X)Jul 7, 2000 · N24BH · Beech 99 · Turbine SectionSDR 20000426SH027Fuel Line · crackedDISCOVERED FUEL LEAKING FROM LOWER COWL ON THE LEFT ENGINE ON A POST-FLIGHT INSP. INSP REVEALED THE FUEL LEAK SOURCE TO BE A HIGH PRESSURE FUEL LINE FROM THE FCU TO THE START FLOW CONTROL UNIT. THE SS LINE HAD A SMALL CRACK WHERE THE FERRULE WAS SECURED TO TMar 17, 2000 · N24BH · Beech 99 · Engine Fuel DistributionSDR 99ZZZX4113Pump · inoperableFUEL BOOST PUMP INOPERABLE.Oct 1, 1999 · N24BH · Beech 99 · Fuel Boost PumpSDR 99ZZZX4175Tire · damagedA NEW TIRE WITH 151 CYCLES INSTALLED ON 9-13-99. DURING INSPECTION, FOUND TIRE TREAD SPLIT AND SEPARATED THE SAME DIRECTION AS TIRE GROOVES.Sep 13, 1999 · N24BH · Beech 99 · TireSDR 99ZZZX3387Hinge · bentCREW DOOR LEAKS AIR IN-FLIGHT DUE TO SLIGHT MIS-ALIGNMENT ON FORWARD EDGE. PROBLEM FOUND TO BE BENT HINGE ON UPPER FORWARD SIDE. REPLACED HINGE AND INSPECTED AREA FOR HIDDEN DAMAGE. NO OTHER DISCREPANCIES TO REPORT. THE DESIGN OF THE HINGE IS SUCH THAT THIAug 10, 1999 · N24BH · Beech 99 · Passenger/Crew DoorsSDR 99ZZZX3006Fuel Cell · leakingPILOT REPORTED FUEL LEAKING FROM AREA OTHER THAN THE FUEL SUMPS IN THE VICINITY OF THE NACELLE. INSPECTION REVEALED VARIOUS SMALL LEAKS IN THE BLADDER OF THE CELL. THE CELL WAS REPLACED WITH A SERVICEABLE CELL AND AIRCRAFT TANK LINER RE-TAPED WITH CHAFE RESIJul 20, 1999 · N24BH · Beech 99 · Fuel StorageSDR 99ZZZX2219Motor · failedFLAPS WERE INOPERATIVE. MOTOR WINDINGS COOKED (BRUSHES WORN). REPLACED FLAP MOTOR AND GEARBOX AS AN ASSEMBLY. VERIFIED RIGGING OK. MOTOR INOPERATIVE DUE TO NORMAL WEAR.May 17, 1999 · N24BH · Beech 99 · Trailing Edge Flap ActuatorSDR 99ZZZX794Fuel Cell · leakingPILOT REPORTS RM FUEL LEAK, FUEL DRIPPING FROM GEAR DOOR. FUEL CELL REMOVED AND TESTED. REPLACED CELL.Jan 29, 1999 · N24BH · Beech 99 · Fuel StorageSDR 99ZZZX4Deicer · contaminatedPILOT REPORTED TO MAINTENANCE ICE REMAINING ON TAIL AFTER LANDING. (SPECIFICALLY, BOTH HORIZONTAL SURFACE DEICERS.) OPERATIONAL CHECK OF BOOTS BROKE ICE FORM SURFACE, HOWEVER, A CLOSER INSPECTION OF SURFACE DEICERS REVEALED MINOR HOLES IN LEADING EDGES. FURNov 18, 1998 · N24BH · Beech 99 · Airfoil Anti/De-ice System
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