Beech 99

Service difficulty reports · 294

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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 = '99'
  ORDER BY difficulty_date DESC"

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SDR CA060425019Skin · crackedVISUAL INSPECTION INDICATED A CRACK ON LT ENGINE NACELLE IB SKIN JUST FORWARD OF WING LEADING EDGE. CRACK RAN VERTICALLY JUST AFT OF IB NACELLE INSPECTION PANEL. A RIVET THAT ATTACHES THE NACELLE FILLET STRIP TO THE WING WAS INCLUDED IN THE CRACK. THERE WASApr 25, 2006 · Beech 99 · Nacelle/Pylon, Plate/SkinSDR CA060317001Actuator · failed(CAN) ON DEPARTURE, A LOUD BANG WAS HEARD AFTER GEAR WAS SELECTED UP, LANDING GEAR (IN TRANSIT) LIGHT REMAINED ON. GEAR WAS CYCLED, NO FURTHER NOISES WERE HEARD, (IN TRANSIT) LIGHT REMAINED ON. PASSENGER SEATED IN REAR ADVISED PILOT, RT MLG WAS NOT RETRACTING.Mar 14, 2006 · Beech 99 · Landing Gear ActuatorSDR CA060126001Torque Tube · cracked(CAN) DURING THE 100 HR INSPECTION THE TAIL CONE WAS REMOVED TO INSPECT THE TORQUE TUBES IAW INSPECTION PACKAGE. THE LT TORQUE TUBE WAS FOUND CRACKED AROUND HALF THE TUBE BRACE. IT HAD BEEN 100 HRS SINCE THE LAST INSPECTION. THE PN OF THE BRACKET IS 115-6100Jan 25, 2006 · Beech 99 · Elevator StructureSDR CA060124001Pinion Gear · broken(CAN) THE GEAR ACTUATOR WAS REMOVED FROM THE AIRCRAFT FOR A RELUBE AND END PLAY CHECK IAW AD72-10-04R2 PART B AND C. WHEN IT WAS CLEANED UP THE MECHANIC NOTICED THAT SEVERAL OF THE TEETH ON THE PINION GEAR WERE BROKEN OFF. THERE WAS NO OBVIOUS REASON FOR FAIJan 21, 2006 · Beech 99 · Landing Gear ActuatorSDR 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 CA051122001Nut · mismanufacturedTHE CREW WENT TO INSTALL A WING BOLT RETAINING NUT ON THE AIRCRAFT. IT WAS NOTICED THAT THE NUT WAS MISSING ONE OF THE TWO PLASTIC LOCKING DEVICES. IT APPEARS THE PLASTIC WAS NEVER INSTALLED IN ONE HOLE. THIS IS THE SECOND NUT THAT WAS FOUND WITH PROBLEMS. Nov 21, 2005 · Beech 99 · Wing StructureSDR 2005FA0001570Wire · chafedAC EXPERIENCED A FALSE FIRE WARNING ON THE LT ENGINE ENROUTE. WHILE FLYING THROUGH HEAVY PRECIPITATION. THE PILOT VISUALLY CHECKED THE ENGINE AND MONITORED ALL RELATED INSTRUMENTS AND SYSTEMS TO VERIFY NORMAL INDICATIONS THUS CONCLUDING THE INDICATION WAS FANov 21, 2005 · N192WA · Beech 99 · Fire Protection System WiringSDR 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 2005FA0001571Rib · crackedLT ELEVATOR WAS FOUND CRACKED BEHIND ELEVATOR BALANCE WEIGHT AT THE OB END OF THE ELEVATOR. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE BALANCE WEIGHT WAS MODIFIED TO INCREASE THE WEIGHT. THE ADDED WEIGHT WAS DETERMINED TO BE INSTALLED BECAUSE THE Oct 11, 2005 · N95WA · Beech 99 · AileronsSDR CA050726004Case · crackedDURING A SCHEDULED HOT SECTION INSPECTION, A CRACK WAS FOUND IN THE CASE WHERE THE FUEL NOZZLE SUPPORT IS LOCATED AT THE FIVE O`CLOCK POSITION. THE CRACK WAS RUNNING FROM THE EDGE OF THE NOZZLE DOUBLER PLATE TOWARDS THE RT IGNITER WELD.Jul 24, 2005 · Beech 99 · Turbine Engine Combustion SectionSDR YDA2005F00001Cover · burnedTHE RT ENGINE WAS REPORTED TO BE THROWING SPARKS OUT THE LOWER PORTION OF THE COWL. UPON INVESTIGATION, THE STARTER GEN WAS FOUND TO HAE BURN SPOTS ON THE BRUSH BAND COVER. THE STARTER GEN WAS REMOVED AND A SERVICEABLE STARTER GEN WAS INSTALLED. UPON FURTHEJul 18, 2005 · N14MV · Beech 99 · Starter-GeneratorSDR CA050628002Engine · shutdown(CAN) A LOSS OF OIL PRESSURE WAS NOTED BY THE FLIGHT CREW WHO ELECTED TO SHUT THE ENGINE DOWN ONCE THE OIL PRESSURE APPROACHED LOWER LIMITS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED FINE BLACK PARTICLES, CARBON IN THE OIL AND DETERMINED TJun 24, 2005 · Beech 99 · Engine (Turbine/Turboprop)SDR CA050620004Relay · intermittent(CAN) THE BEECH 99 WAS ON ITS TAKEOFF ROLL WHEN FIRST ONE THEN THE SECOND GENERATOR FAILED. THE LIGHTS IN THE COCKPIT BRIGHTENED SUDDENLY JUST BEFORE THE GENERATORS FAILED. WHEN MAINTENANCE TROUBLESHOT THE PROBLEM THEY INITIALLY COULD NOT FIND ANY THING WRONJun 15, 2005 · Beech 99 · DC Generating SystemSDR TIM2005F00005Fire Detector · contaminatedFIRE DETECTOR GAVE A FALSE FIRE WARNING IN FLIGHT. MOISTURE WAS PROBABLE CAUSE. AFTER TAXI, THE FIRE WARNING LIGHT EXTINGUISHES. NO OTHER PROBLEMS WITH THE SYSTEM. (K)Apr 19, 2005 · N14MV · Beech 99 · Fire DetectionSDR CA050323007Engine · failed(CAN) ON TAKE-OFF ROLL, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION ACCOMPANIED BY HIGH/INCREASING TURBINE TEMPERATURE. THE PILOT ABORTED TAKE-OFF AND SECURED THE ENGINE. SUBSEQUENT INSPECTION REVEALLED HOT SECTION DISTRESS.Feb 14, 2005 · Beech 99 · Engine (Turbine/Turboprop)SDR CA041115004Generator · intermittent(CAN) ON CLIMB OUT THE PILOT OBSERVED THAT ONLY ONE GENERATOR WAS ACCEPTING LOAD. DECIDED TO RETURN TO DEPARTURE AERODROME WITHOUT CARRYING OUT ANY CONFIRMATION CHECKS. A SUBSEQUENT MAINTENANCE INSPECTION DETERMINED THAT AT LIGHT ELECTRICAL LOADS BOTH GENERANov 11, 2004 · Beech 99 · DC Generator-AlternatorSDR KCQ2005F00001Actuator · crackedFOUND TOP CAP TO BE CRACKED AROUND CIRCUMFERENCE OF INTERIOR BORE. (GL13200503455) (K)Nov 5, 2004 · N799CZ · Beech 99 · Landing Gear ActuatorSDR KCQ2005F00000Motor · burnedPILOT REPORTED SMOKE IN COCKPIT DURING FLIGHT AND MADE EMERGENCY LANDING. FOUND GEAR MOTOR TO BE BURNED UP, HAVING CYCLED EXCESSIVELY. MATTER STILL UNDER INVESTIGATION, APPROX 3900 HOURS SINC REPAIR OF GEAR MOTOR. (GL13200503454) (K)Nov 5, 2004 · N299CZ · Beech 99 · Landing Gear ActuatorSDR CA041104007Support · cracked(CAN) DURING ROUTINE INSPECTION THE SUPPORT BRACKET FOR THE STEERING IN THE UPPER LT CORNER WAS FOUND CRACKED.Nov 3, 2004 · Beech 99 · Steering UnitSDR CA041029001Elt · inoperative(CAN) APPROXIMATELY 3 HOURS AFTER LANDING, ATC INFORMED THE COMPANY THAT THEY HAD A STRONG ELT SIGNAL. AFTER CHECKING ALL AIRCRAFT IT WAS NOTICED THAT THE ELT ON THIS AIRCRAFT WAS ACITVATED. THE SWITCH WAS IN THE ARM POSITION AND THE INDICATOR LIGHT WAS ON. Oct 28, 2004 · Beech 99 · Emergency Locator BeaconSDR CA040929004Scoop · departed(CAN) ON APPROACH TO AIRPORT THE LT OIL SCOOP DEPARTED THE AIRCRAFT. THE SECURING FASTENERS WERE FOUND STILL ATTACHED TO THE BOTTOM OF THE NACELLE. PIECES OF FIBERGLASS WERE STILL UNDER THE HARDWARE. THERE WAS SLIGHT SHEET METAL DAMAGE TO THE BOTTOM OF THE Sep 25, 2004 · Beech 99 · Engine Oil CoolerSDR CA040927007Door · inoperative(CAN) ON APPROACH, AT 20 MILES OUT AND 2500 FT ASL THE CABIN DOOR OPENED. FLIGHT SERVICES WAS INFORMED AND THE AIRCRAFT LANDED UNEVENTFULLY. THE COPILOT CLOSED THE DOOR AFTER LANDING. THE DOOR AND SURROUND WERE INSPECTED NO DAMAGE FOUND.Sep 24, 2004 · Beech 99 · Passenger/Crew DoorsSDR CA040723007Switch · stuck(CAN) ON CLIMB THE PILOT REPORTED THE GEAR IN TRANSIT LIGHT WAS ON. LANDING GEAR WAS EXTENDED WITH NO DIFFICULTIES AND MAINTENNACE WAS CONTACTED. AIRCRAFT RETURNED TO BASE. AIRCRAFT WAS PUT ON JACKS AND THE RT POWER LEVER 70 PERCENT SWITCH WAS FOUND STUCK. Jul 22, 2004 · Beech 99 · Power LeverSDR CA040517003Fitting · cracked(CAN) DURING A ROUTINE DETAILED INSPECTION, MAINTENANCE DISCOVERED A CRACK IN THE LT UPPER FORWARD WING FITTING OF THE WING CENTER SECTION. NDT, USING LPI AND EDDY CURRENT CONFIRMED THIS AS A CRACK. THIS AIRCRAFT HAS FLOWN 513.9 SINCE LAST NDT IAW MFG SIRM. May 15, 2004 · Beech 99 · Fuselage Main, Attach FittingsSDR CA040513008Spring · damaged(CAN) ON TAKE OFF ROLL, PWR SET TO 1290 FT LBS. AFTER ROTATION NOTICED TORQUE INCREASING ON RT ENG. FO ATTEMPTED TO REDUCE PWR BUT PWR LEVER WOULD NOT MOVE. TORQUE INCREASED TO APPROX 1500 FT LBS FOR ABOUT 90 SECONDS. AFTER REACHING SAFE ALTITUDE RT ENG SHMay 12, 2004 · Beech 99 · Power LeverSDR CA040220003Switch · contaminated(CAN) LANDING GEAR FAILED TO EXTEND WHEN SELECTED. APPROXIMATELY 1-5 MINUTES GEAR EXTENDING WITH NO ADDITIONAL CREW ACTIONS. AIRCRAFT RETURNED TO MAINTENANCE BASE. AIRCRAFT EXPOSED TO -30 DEGREES COLD SOAK FOR APPROXIMATELY 3 HOURS. AIRCRAFT PREVIOUS OPERATED Feb 11, 2004 · Beech 99 · Landing Gear SelectorSDR CA040220002Altimeter · failed(CAN) CAPTAIN'S ALTIMETER ERROR OF APPROXIMATELY 1,000 FEET CHECKED OK PRIOR TO DEPARTURE. NOT SURE WHEN FAILURE OCCURRED, BUT NOTICED ERROR AT LEVEL CRUISE. MAINTENANCE CONFIRMED NO STATIC SYSTEM LEAKS.Feb 11, 2004 · Beech 99 · Altimeter, Barometric/EncoderSDR CA031224003Engine · making metal(CAN) ENGINE S/N PCE40252 WAS SENT FOR METAL IN OIL. ENGINE WAS DISSASSEMBLED AND IT WAS FOUND THAT THE NR 2 BEARING ROLLER CAGE SILVER PLATE HAD FLAKED OFF. MFG HAS A SIL NR PT6A-106 ON THIS CONDITION. THIS ENGINE WAS REPAIRED IAW MFG LATEST SPECIFICATIONS ANov 24, 2003 · Beech 99 · Engine (Turbine/Turboprop)SDR CA031120006Latch · unsecure(CAN) NOTICED BAGGAGE DOOR LITE ON AFTER TAKEOFF, RETURNED TO BASE FOUND LATCH UNDONE. LATCH CLOSED. AIRCRAFT RETURNED TO SERVICE.Nov 20, 2003 · Beech 99 · Cargo/Baggage DoorsSDR 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 CA031027004Controller · malfunctioned(CAN) TAKE-OFF WAS REJECTED IN YXY DUE TO AUTO FEATHER FAILING TO ARM ON THE RIGHT SIDE A/C GROUND RUN TESTED-NORMAL-NO FAULT FOUND A/C RELEASED FOR RETURN TO SERVICEOct 9, 2003 · Beech 99 · Propeller Controlling SystemSDR CA030825012Hose · ruptured(CAN) TIME ON HOSE UNKNOWN ALTHOUGH DATA PLATE ON IT INDICATES 13 YEARS OLD. LANDING GEAR WAS SELECTED UP AND ONLY 2 MAIN GREEN LIGHTS CAME ON. THERE WAS ALSO A STRONG ODRO OF HYD FLUID. PILOT SELECTED DOWN AND THE NOSE GEAR LIGHT DID NOT COME ON. PILOT THAug 10, 2003 · Beech 99 · Landing Gear Retraction/Extension SystemSDR CA030731018Wire · chafed(CAN) SHORTLY AFTER TAKE OFF FROM FORT SMITH THE OIL PRESSURE INDICATION ON THE LT ENGINE DROPPED TO ZERO AND THE OIL PRESSURE LIGHT CAME ON. A PRECAUTIONARY SHUTDOWN WAS CARRIED OUT AND THE A/C RETURNED TO FORT SMITH. ON INVESTIGATION IT WAS DISCOVERED THAT Jul 30, 2003 · Beech 99 · Nacelle/Pylon System WiringSDR CA030716005Actuator · fractured(CAN) RT GEAR WOULD NOT RETRACT ON TAKE OFF.AIRCRAFT RETURNED TO BLOCKS AND RT MAIN GEAR ACTUATOR RELACED. RAM WAS FRACTURED ON THE FIRST THREAD OF RAM TO HOLD PISTON IN PLACE.Jul 10, 2003 · Beech 99 · Landing Gear ActuatorSDR CA030212003Rod End · damaged(CAN) PILOT REPORTED THAT ON DESCENT THAT HE COULD NOT ACHIEVE ANYTHING LESS THAN 1000 FT POUNDS TORQUE ON THE LT ENGINE WHEN PULLING THE POWER LEVER BACK TO IDLE. PILOT LANDED AND SHUT ENGINE OFF AND TAXIED TO TERMINAL. MAINTENANCE FOUND ROD END FROZEN DUE Feb 10, 2003 · Beech 99 · Fuel Controlling SystemSDR CA030114005Blower · failed(CAN) AIRCRAFT WAS TAXING FROM TERMINAL TO RUNWAY WHEN SMOKE STARTED FILLING COCKPIT. ELECTRICAL COMPONENTS WERE TURNED OFF AND AIRCRAFT RETURNED TO TERMINAL. MAINTENANCE WAS CONTACTED AND FORWARD VENT BLOWER WAS REPLACED. GROUND CHECKED SERVICEABLE.Dec 31, 2002 · Beech 99 · Air Distribution FanSDR CA021218009Cap · fractured(CAN) AIRCRAFT SELECTED GEAR DOWN AND NO GREEN LIGHTS. CYCLED GEAR AND MAIN GEAR LIGHTS CAME ON. COULD NOT GET NOSE GEAR TO LOCK. EMERGENCY EXTENSION DID NOT GET NOSE GEAR LIGHT TO COME ON. AIRCRAFT LANDED WITH NOSE GEAR NOT LOCKED. NOSE GEAR COLLAPSED Dec 16, 2002 · Beech 99 · Landing Gear ActuatorSDR CA021205005Line · chafed(CAN) AIRCRAFT WAS INSPECTED FOR FUEL LEAK IN LT NACELLE AREA. PROBLEM WAS CAUSED BY A 'CHAFED' FUEL LINE. THE CHAFING WAS CAUSED BY A FUEL BOOST PUMP POWER WIRE THAT WAS ROUTED IN THE SAME HOLE AS THE FUEL LINE.THERE WAS NO PROTECTIVE MATERIAL BETWEEN THE Dec 3, 2002 · Beech 99 · Aircraft Fuel Distribution SystemSDR CA021031019Splice Plate · cracked(CAN) THE RT NACELLE I/B SPLICE PLATE CRACKED DUE TO HOLE'S ON UPPER SPAR BEING ELONGATED, THUS CAUSING PLATE TO WORK IN THAT AREA. PARENT STRUCTURE FAILED DUE TO SPLICE PLATE BEING CRACKED AND NACELLE LOADING TRANSFURED TO THAT AREA.Oct 31, 2002 · Beech 99 · Nacelle/Pylon, Main FrameSDR CA021001009Terminal · loose(CAN) ON DESCENT INTO FORT SMITH FROM FORT CHIPEWYAN, THE CREW NOTICED AN ELECTRICAL SMELL, FOLLOWED SHORTLY BY SMOKE.ALL ELECTRICAL POWER WAS TURNED OFF.ALL NON ESSENTIAL FUNCTIONS WERE TURNED OFF THEN POWER WAS TURNED BACK ON. THE SMELL REAPPEARED.POWER WASSep 30, 2002 · Beech 99 · Electrical Power System WiringSDR IUXR941LBearing · failedBEARING CAGE SEPARATED DURING ENGINE TEST. (S/N E967). BEARING RETURNED TO BEARING REFURB FACILITY. CURRENTLY PERFORMING ANALYSIS, EARLY INDICATION IS LATENT DEFECTS (CRACKS) IN CAGE.Sep 13, 2002 · Beech 99 · Turbine SectionSDR CA020628002Cap · cracked(CAN) PILOT SELECTED GEAR DOWN. GEAR CAME DOWN AND 3 GREEN WERE INDICATED. MOTOR KEEP RUNNING UNTIL C/B POPPED. AIRCRAFT LANDED WITHOUT INCIDENT. NOSE GEAR ACTUATOR REPLACED, GEAR SWINGS CARRIED OUT AND AIRCRAFT RELEASED TO SERVICE. END CAP FRACTURED.Jun 27, 2002 · Beech 99 · Landing Gear ActuatorSDR CA020415001Actuator · failed(CAN) AIRCRAFT DEPARTED BASE AND THE GEAR WOULD NOT RETRACT WHEN THE GEAR HANDLE WAS SELECTED UP. AIRCRAFT RETURNED TO TO BASE. GEAR ACTUATOR WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE.Apr 8, 2002 · Beech 99 · Landing Gear ActuatorSDR CA020111001Switch · intermittent(CAN) PILOT SELECTED GEAR DOWN AND GOT NO NOSE GREEN LIGHT. PILOT WAS READY TO DO A EMERGENCY EXTENTION WHEN THE GREEN LIGHT CAME ON. MAINTENANCE REPLACED THE SWITCH AND RETURNED AIRCRAFT TO SERVICE.Jan 10, 2002 · Beech 99 · Landing Gear Position and WarningSDR TIM2002F00001Casting · crackedDURING A DETAILED INSPECTION OF THE INTERIOR AND STRUCTURE, CRACKS WERE FOUND EXTENDING FROM THE RIVETS HOLDING UNTPLATES USED TO SECURE THE RUDDER CONTROL BELLCRANK PIVOT CASTING. FURTHER INSPECTION REVEALED NO OTHER DISCREPANCIES. BEAM WAS REPLACED WITH NEDec 20, 2001 · N4381Y · Beech 99 · Rudder Control SystemSDR TIM2002F00000Bearing · wornTHE LEFT ELEVATOR PIVOT BEARING WAS FOUND TO BE LOOSE WHERE THE HORN PIVOTS ON THE INBOARD SIDE IN THE TAIL. THE BEARING AND BUSHING WERE REPLACED AND INSTALLED IAW MM. THIS APPEARS TO BE A FREQUENT DISCREPANCY WITH THE MFG AND COULD BE RELATED TO THE BLAST Dec 20, 2001 · N4381Y · Beech 99 · Elevator Control SystemSDR TIM2002F00002Actuator · leakingTHE AIRCRAFT HAD NEEDED INFREQUENT SERVICING OF THE HYD. FLUID RESERVOIR AND YET NO LEAKS HAD BEEN DISCOVERED. SINCE THE AMOUNT OF FLUID ADDED HAD NEVER BEEN AN ALARMING AMOUNT, THE AIRCRAFT HAD ALWAYS BEEN RETURNED TO SERVICE. THE LEAK OF HYD. FLUID WAS DISNov 26, 2001 · N14MV · Beech 99 · Landing Gear ActuatorSDR TIM2002F00003Inlet · burnedDURING A POST INSPECTION CHECK OF AIRCRAFT SYSTEMS, IT WAS DETERMINED THE LEFT ENGINE INLET DEICER WAS INOPERATIVE. A CLOSE INSPECTION OF THE SURFACE OF THE DEICER REVEALED IRREGULAR BULGING AND INDICATORS OF HIGH HEAT. THE DEICER WAS REPLACED AND THE REST OFNov 15, 2001 · N14MV · Beech 99 · Air Intake Anti/De-Ice SystemSDR CA011031027Wheel · cracked(CAN) WHEEL HALF WAS REMOVED DUE TO CUTS IN THE RUBBER. UNIT DISASSENBLED AND DYE PEN INSPECTED. CRACK INDICATIONS WERE FOUND ON THE INSIDE OF THE OUTER WHEEL HALF. UNIT SCRAPPED OUT PART TIME AND CYCLES ARE UNKNOWN.Oct 31, 2001 · Beech 99 · Wheel/Ski/FloatSDR CA011210009Drain Valve · broken(CAN) DURING THE LATTER PART OF A FLIGHT THE RT NACELLE WAS SHOWING A DECLINE IN DUEL CAPACITY ABOVE NORMAL. WHEN REACHING THE DESTINATION IT WAS DISCOVERED THAT FUEL WAS ESCAPING FROM THE RT FUEL MANIFOLD DRAIN. UPON FURTHER INVESTIGATION IT WAS FOUND THAT THOct 29, 2001 · Beech 99 · Engine Drains
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