200King Air · 250

Parts most often named Windshield (130) · Windscreen (5) · Window (4) · Retainer (1)

DURING TAKEOFF FROM KBIL TO KHLN, THE CREW OBSERVED THE LEFT WINDSHIELD CRACK. THE CREW RETURNED TO KBIL WITHOUT INCIDENT.

AIRCRAFT WAS IN CRUISE FLIGHT AT 16,000 FT ENROUTE KBZN FROM KBIL WHEN THE RIGHT (COPILOT) WINDSHIELD SHATTERED. AT THAT TIME, THE FLIGHT CREW RETURNED TO KBIL AND LANDED WITHOUT INCIDENT.

DURING APPROACH TO KELP THE PILOTS WINDSHIELD SUFFERED A BIRD STRIKE WHICH SHATTERED THE OUTER PANE OF THE WINDSHIELD. NO LOSS OF PRESSURIZATION WAS NOTED OR LOSS OF FLIGHT CHARACTERISTICS. AIRCRAFT LANDED SAFELY AT KELP.

Parts most often named Motor (17) · Switch (7) · Landing Gear (7) · Drag Brace (4)

LANDING GEAR FAILED TO EXTEND NORMALLY. WAS ABLE TO EXTEND THE GEAR USING ABNORMAL PROCEDURE. LANDED WITHOUT EVENT. SUSPECT DOWN LIMIT SWITCH. SUPPLEMENTAL INFORMATION

PILOT DID NOT RECEIVE NOSE DOWN AND LOCKED LIGHT ON APPROACH, ATTEMPTED EMERGENCY EXTENSION, NO CHANGE. FLEW BY TOWER AND VERIFIED THAT NOSE GEAR WAS NOT EXTENDED. LANDED AT MWC WITH MAIN GEAR EXTENDED AND NOSE RETRACTED. MECHANICS NOTED THAT NLG RETRACT CHAIN BETWEEN GEARBOX AND CROSSOVER WAS BROKEN CAUSING FAILURE OF GEAR TO EXTEND.

LT MAIN GEAR EXTENDED IN FLIGHT WHILE ENROUTE. AIRCRAFT LANDED AT DESTINATION WITH NO DAMAGE. UPON POST LANDING WALKAROUND, CREW DISCOVERED LEFT MAIN GEAR LOCK LINK ASSEMBLY HAD FAILED IN-FLIGHT. THE ASSEMBLY WAS FOUND TO MISSING THE SPRING, BUSHING, AND ASSOCIATED HARDWARE. THE CLEVIS ENDS WERE STILL ATTACHED. FAILURE OF THE BOLT (P/N 101-810177-3) OCCURRED AT THE END OF THE THREADED SECTION AT THE SHANK.

Parts most often named Engine (92) · Compressor (1) · Seal Ring (1) · Bleed Valve (1)

RIGHT AFTER LIFTOFF, THERE WAS A LOUD POPPING SOUND COMING FROM THE LEFT ENGINE WITH FLAMES EMITTING FROM THE EXHAUST. COMMENCED A PRECAUTIONARY ENGINE SHUTDOWN, FEATHERED THE PROPELLER AND RETURNED TO THE FIELD FOR A SINGLE ENGINE LANDING. TAXIED BACK TO THE BLOCK.

ON FIANL APPROACH TO LANDING PILOT GOAT A NUMBER 1 ENGINE FUEL PRESSURE LIGHT ON QUICKLY FOLLOWED BY THE SAME ENGINE RILLING BACK AND SHUTTING OFF. AT THIS POINT THE PILOT WAS ON FINAL SO THE PILOT CONTINUED TO LAND AND WAS ABLE TO TAXI BACK.

(CAN) DURING THE CLIMB THROUGH FL230, THE CREW NOTICED A RT ENGINE POWER SURGE. TORQUE INDICATIONS WERE OBSERVED DEVIATING BY APPROXIMATELY 1500 FOOT-POUNDS WITH FLAMES EMANATING FROM THE EXHAUST STACK. THE POWER SETTING WAS REDUCED, THE ENGINE CONTINUED TO SURGE. SHORTLY THEREAFTER CONTROL AUTHORITY WAS RESTORED AND THE ENGINE WAS MAINTAINED AT MINIMUM POWER SETTING. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED UNEVENTFULLY. TROUBLESHOOTING IS ON-GOING.

Parts most often named Fire Detector (40) · Detector (9) · Fire Warning (4) · Fire Loop (3)

DURING CRUISE FLIGHT LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED, DETERMINED NO FIRE EXISTED, LANDED AIRCRAFT OAKLAND IAP. MAINTENANCE DETERMINED FIRE DETECTOR WAS MALFUNCTIONING REPLACED THE LOWER NR 1 ENGINE FIREWALL DETECTOR SYSTEM OPERATIONAL TESTS SATISFACTORY.

LEFT ENGINE FIRE ANNUNCIATOR CAME ON IN FLIGHT. MECHANICS INSPECTED AND TESTED THE SYSTEM IAW THE KING AIR 200 MM SECTIONS 26-10-00 AND 26-10-01. ALL CHECKS WERE SATISFACTORY. NO DEFECTS NOTED AT THIS TIME.

DURING CLIMB THE L ENG FIRE LIGHT ILLUMINATED. RETURNED TO 4A9 ON A PRECAUTION DUE TO NOT BEING ABLE TO VERIFY IF THE ENG WAS ON FIRE. AFTER INSPECTION AND GROUND TEST IT WAS DETERMINED THE SYSTEM WAS WORKING CORRECTLY AND THAT THE L ENG FIRE LIGHT WAS PROBABLY CAUSED FROM THE SUNLIGHT ENTERING THE COWLING.

Parts most often named Actuator (31) · Nut (7) · Motor (5) · Bearing (5)

RH MLG ACTUATOR CRACKED THE END CAP WHERE THE ACTUATOR SHAFT COMES OUT. BEECHCRAFT PART NUMBER OF ACTUATOR IS 101-388014-1.

DURING A CONTROLLED APPROACH WHEN THE LANDING GEAR WAS SELECTED DOWN THE GEAR UNSAFE LIGHT ILLUMINATED AND LANDING GEAR FAILED TO EXTEND. THE GEAR HANDLE WAS PLACED BACK IN THE RETRACTED POSITION AND THE GEAR UNSAFE LIGHT STAYED ILLUMINATED. THE PILOT COMPLIED WITH EMERGENCY EXTENSION PROCEDURES WITH RESULTS OF RIGHT MAIN, LEFT MAIN, AND NOSE GEAR DOWN AND LOCKED GREEN LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT.

RIGHT MAIN GEAR FAILED TO RETRACT ON TAKE-OFF CLIMB. MANUALLY EXTENDED. RETURNED TO LAND UNEVENTFULLY. FOUND RIGHT MAIN GEAR ACTUATOR BINDING. REPLACED ACTUATOR ALONG WITH GEAR MOTOR AND GEARBOX.

Parts most often named Channel (6) · Bolt (4) · Handle (3) · Support (3)

PIN ATTACHING FOWARD DOOR HOOK ON UPPER MAIN DOOR LOCKING MECHANISM SHEARED ALLOWING HOOK TO COME LOOSE ALLOWING ENOUGH MOVEMENT IN THE MAIN CABIN DOOR IN FLIGHT TO CAUSE A SIGNIFICANT PRESSURIZATION LOSS.

MAIN ENTRY DOOR SKIN CRACKED NEAR DOOR HANDLE. REMOVED AIR-STAIR DOOR FROM AIRCRAFT. REPAIRED CRACK IAW TEXTRON AVIATION STANDARD REPAIR DR# SR-KA-ATA52-40125 AND TEXTRON STRUCTURES DEVIATION LETTER# DQ53723M1. REINSTALLED AIR-STAIR DOOR AND CHECKED DOOR RIGGING. OPS CHECK OK. REF BEECH B200CGT AMM CH. 52-30-09. SEE FAA 337 THIS DATE.

AFTER TAKE OFF FROM LAS VEGAS, NM, WE HAD A RAPID DECOMPRESSION AT FL260 WITH AIRFLOW HEARD AT THE CABIN DOOR FOLLOWED BY CABIN ALT HI ANNUNCIATOR AND MASTER WARNING. WE DONNED OUR O2 MASKS AND DESCENDED TO 15K' AND DIVERTED TO ABQ. MAINTENANCE FOUND PASSENGER DOOR SEAL DAMAGED. REPLACED DOOR SEAL, OPS CHECK GOOD.

Parts most often named Switch (14) · Downlock Switch (11) · Uplock Switch (6) · Squat Switch (5)

RIGHT LANDING GEAR DOWN LIGHT DIDN’T ILLUMINATE, APPROPRIATE CHECKLIST WAS PREFORMED, EMERGENCY GEAR EXTENSION WAS INEFFECTIVE AND THE AIRCRAFT WAS LANDED AS PRESCRIBED IN THE CHECKLIST

THE NOSEWHEEL GEAR DOWN INDICATOR LIGHT FAILED TO ILLUMINATE. THE ACTUAL NOSEWHEEL HAD COME DOWN AND LOCKED, BUT WITH NO INDICATION TO THE PILOT OF ITS STATUS, AND EMERGENCY WAS DECLARED. THE PLANE LANDED WITHOUT INCIDENT.

10/6/2022: [tail no. removed] LEFT KBIL @ APPROXIMATELY 2340 ENROUTE 1S3 (FORSYTH, MT). UPON REACHING CRUISE, THE PILOT OBSERVED THE "GEAR UNSAFE" LIGHT ILLUMINATED. AFTER A FEW MINUTES, THE LIGHT BECAME INTERMITTENT. THE CREW EXTENDED THE LANDING GEAR AND OBSERVED 3 GREEN LANDING GEAR "DOWN AND LOCKED" LIGHTS WITH NO "GEAR UNSAFE" LIGHT. THE CREW DECIDED TO RETURN TO KBIL AT THIS POINT. THE AIRCRAFT LANDED BACK AT KBIL @ APPROXIMATELY 0020 WITHOUT INCIDENT.

Parts most often named Fuel Control (26) · Fcu (12) · Bearing (2) · Seal (1)

(CAN) ON TAKEOFF ROLL, THE CREW EXPERIENCED A LACK OF TORQUE INCREASE ON THE RT ENGINE, AND ABORTED THE TAKEOFF. TROUBLESHOOTING WAS COMPLETED BY MAINTENANCE AND THE RH ENGINE FCU WAS FOUND TO BE IN NEED OF ADJUSTMENT/REPAIR OF THE ACCELERATION FUNCTION. THE FCU WAS REMOVED AND [S/N removed] AT APPROVED OVERHAUL SHOP TO CORRECT THE DEFECT. THE FCU WAS AT TSO 3679 AT THE TIME OF THE DEFECT.

(CAN) THE AIRCRAFT WAS IN LEVEL FLIGHT AT FL 280. THE RIGHT HAND ENGINE TORQUE FLUCTUATION WAS NOTED WHICH LED UP TO AN ENGINE FLAME OUT. DURING THE PROCESS TO SECURE THE ENGINE, ENGINE POWER WAS REGAINED. THE CREW ELECTED TO RETURN TO THE MAIN BASE OF OPERATION. DURING THE DECENT THERE WAS MORE SURGING BUT NO LOSS OF POWER. FCU WAS SENT FOR EVALUATION AND WAS FOUND TO BE OUT OF CALIBRATION. THE FCU WAS RECALIBRATED AND TESTED WITH ENGINE PERFORMING NORMALLY. THE AIRCRAFT WAS RETURNED TO [S/N removed].

INSTALLED NEW OVERHAULD FUEL CONTROL UNIT DURING MAINTENANCE. OVERHAULED UNIT THEN FAILED AFTER A FEW SUCCESSFUL ENGINE RUNS. THE SYMPTOMS OF FAILURE WERE SLUGGISH ACCELERATION ON THE FINAL SUCCESSFUL RUN, FOLLOWED BY MIN-FLOW STARTS, APPROXIMATELY 50 PERCENT [tail no. removed].

Parts most often named Door Sill (17) · Structure (5) · Intercostal (2) · Web (2)

(51267) THE UPPER AFT CORNER IS CRACKED FROM THE WELL NUT HOLE, ACROSS THE ENTIRE CARGO DOOR/ ENTRY DOOR CLOSURE APPROXIMATELY 1.40" IN LENGTH.

(24147) CRACKS IN THE LOWER AFT CORNER ENTRY DOOR SILL CLOSURE AREA. MULTIPLE CRACKS BEGINS AT FS 278.50 AND ENDS AT APPROXIMATELY FS 305.260.

(CAN) WHILE DOING A STRUCTURE INSPECTION, IT WAS NOTICED THAT THE CROSS TIE WAS CRACKED HALF WAY UP INBD AFT. THIS IS A HIGH TIME ACFT.

Parts most often named Frame (39) · Strap (1) · Unknown (1)

FRAME CRACKED AT LIGHTNING HOLE AT FS 187.383 JUST ABOVE STRINGER 10R. REPAIRED CRACK FS 187.383 ABOVE STRINGER 10R USING 0.071", 2024-T3 ALCLAD IAW SIRM 20-10-31.

FRAME CRACKED AT FS 256.250 AND STRINGER 13L, PN 50-420068-31. REPAIRED CRACKED FRAME AT FS 256.250 AND STRINGER 13L USING 2024-T3, 0.063" ALCLAD IAW SIRM 20-10-34.

(CAN) DURING FUSELAGE DETAILED INSP, THERE WAS A CRACK NOTED AT THE LWR END OF FRAME 207.125 WHERE A RELIEF HAD BEN CUT OUT FOR A STR DURING MFG. THE CRACK PROPOGATED FROM THE RADIUS OF THE RELIEF. REPAIR WAS CONDUCTED IAW WITH SIRM INSTRUCTIONS.