Beech B300

Service difficulty reports · 598

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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 = 'B300'
  ORDER BY difficulty_date DESC"

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SDR CA070423009Cross Tie · cracked(CAN) THE INTERIOR WAS REMOVED FOR REFURBISHMENT. MAINTENANCE DISCOVERED A CRACK IN THE CROSS TIE, A STRUCTURAL MEMBER AROUND THE EMERGENCY EXIT ON THE LT SIDE OF THE AIRCRAFT. CONTACTED MFG FOR A REPAIR. (TC NR 20070423009)Apr 22, 2007 · Beech B300 · Fuselage Internal Mounting StructureSDR CA070329009Wire · chafed(CAN) 5 AMP ANNUNCIATOR INDICATION (CB4) POPPED IN FLIGHT AND THE CREW LOST THE GREEN AND WHITE ANNUNCIATOR LIGHTS. THE CREW ATTEMPTED TO RESET THE 5 AMP CIRCUIT BREAKER, BUT COULD NOT BE RESET. PROBLEM WAS IN FOUND ON WIRE PIN D WIRE NR Q62A20 ON THE RT FUELMar 29, 2007 · Beech B300 · Fuel System WiringSDR PAI52007S4508Condition Lever · loosePILOT NOTED RT ENGINE CONDITION LEVER CONTROL FELT LOOSE AND IDLE N1 SPEED LOW. UPON INSPECTION, MAINTENANCE FOUND ALL SCREWS ATTACHING CONDITION LEVER TO QUADRANT LOOSE TO THE POINT OF ALMOST FALLING OUT.Mar 22, 2007 · N507EB · Beech B300 · Engine ControlsSDR CA070322001Panel · cracked(CAN) PANEL IS INSTALLED ON RT IB SIDE OF NACELLE. IT COVERS THE FUEL FIREWALL SHUTOFF VALVE. THE PANEL IS MANUFACTURED WITH A BULGE TO ACCOMMODATE THE VALVE. IN THIS INSTALLATION THE VALVE CONNECTOR PLUG CHAFFED AGAINST THE PANEL CAUSING A STRESS RISER RESULMar 21, 2007 · Beech B300 · Nacelle/Pylon, Plate/SkinSDR CA070226005Plate · failed(CAN) DISCOVERED DOOR MAKING NOISE WHEN RAISING OR LOWERING DOOR. INVESTIGATED FOR LOOSE HARDWARE INSIDE DOOR AND DETERMINED PIN AND ROLLER ASSY MIGRATED OUT OF LOWER AFT LATCH ASSY. THE DEFECTIVE PART IN QUESTION IS THE PLATE P/N 101-430032-7. THE PLATE IS THFeb 8, 2007 · Beech B300 · Passenger/Crew DoorsSDR HUN2007F00000Brake Assy · malfunctionedPILOT REPORTED A RECURRING PROBLEM WITH SPONGY BRAKES. THE LT MASTER CYLINDER HAD BEEN REPLACED AND SYSTEM HAD BEEN BLED SEVERAL TIMES. WE CHECKED BRAKES AND FOUND AIR IN LT SYSTEM. CHECKED TORQUE ON ALL (B-NUTS) IAW KA300 SERIES MM, CHAPTER 20-06-00, SECTIJan 17, 2007 · N92TH · Beech B300 · Landing Gear Brake SystemSDR LX5R200600003Wire Harness · shortedUPON TAKEOFF ROLL, THE CREW GOT THE AUTO FEATHER OFF LIGHT AND THE MASTER CAUTION LIGHT. THE CREW THEN OPTED TO ABORT TAKEOFF ROLL AND RETURN TO RAMP WITHOUT INCIDENT. UPON RETURNING TO RAMP, THE CREW NOTICED THAT THE AUTO FEATHER CRICUIT BREAKER HAD POPPED,Nov 15, 2006 · N961LL · Beech B300 · Propeller/Propulsor System WiringSDR LX5R200600002Wire Harness · shortedUPON TAKEOFF ROLL THE CREW GOT THE AUTOFEATHER OFF LIGHT AND THE MASTER CAUTION LIGHT. THE CREW THEN OPTED TO ABORT TAKEOFF ROLL AND RETURN TO RAMP WITHOUT INCIDENT. UPON RETURNING TO RAMP THE CREW NOTICED THAT THE AUTOFEATHER CIRCUIT BREAKER HAD POPPED, IT WANov 15, 2006 · N961LL · Beech B300 · Propeller/Propulsor System WiringSDR DEBA391MT1106Switch · intermittentWHEN THE LANDING GEAR WAS EXTENDED, THE LT GREEN LIGHT DID NOT ILLUMINATE. THE PRESS TO TEST WAS TRIED AND THE BULB ILLUMINATED. CREW CYCLED GEAR 2 OR 3 MORE TIMES. A FEW SECONDS AFTER THE LAST TIME IT WAS EXTENDED, THE GREEN LIGHT ILLUMINATED. THE AIRCRAFT LANov 6, 2006 · N391MT · Beech B300 · Landing Gear Position and WarningSDR 2006FA0000968Starter Gen · wornIN FLIGHT THE LT SIDE STARTER/GEN AFT BEARING AT THE COOLING FAN FAILED AND THE GENERATOR FAILED. THE AC RETURNED TO ITS DEPARTURE TERMINAL WITHOUT INCIDENT. THE STARTER/GEN WAS REPLACED AND THE CHARGING AND ELECTRICAL SYSTEM OPS, CHECKED GOOD. NO KNOWN CAUSep 19, 2006 · N200VC · Beech B300 · Starter-GeneratorSDR CA060821005Bypass Valve · failed(CAN) RT OIL TEMPERATURE REACHED THE REDLINE WHEN CLIMBING THROUGH 25000 FT. POWER REDUCED AND A/C DESENDED TO 20000 FT. OIL TEMP RETURNED TO NORMAL. ENG POWER SETTING RETURNED TO NORMAL, NO FURTHER FAULT. NR 2 ENGINE OIL COOLER THRMOSTATIC BYPASS VALVE REPAug 12, 2006 · Beech B300 · Engine Oil CoolerSDR TT197941Motor · wornELECTRIC LANDING GEAR EXTENSION FAILED INFLIGHT. NORMAL LANDING ACCOMPLISHED USING MANUAL GEAR EXTENSION. LANDING GEAR MOTOR BRUSHES FOUND WORN EXCESSIVELY, COMMUTATOR PITTED. OVERHAULED MOTOR INSTALLED, NEW FILTER INSTALLED. GEAR RETRACTION CHECKS PERFORMAug 11, 2006 · N5626Y · Beech B300 · Landing Gear Retraction/Extension SystemSDR 2006FA0000825Turnbuckle · mismanufacturedWHEN THE PART WAS MFG, THE SAFETY SLOT DID NOT LIME UP WITH THE END SLOTS. THIS DID NOT CAUSE A PROBLEM EITHER OPERATIONALLY, OR IN THE PROCESS OF SAFETYING THE TURNBUCKLE. (K)Aug 4, 2006 · N8YN · Beech B300 · Elevator Control SystemSDR CA060705008Motor · malfunctioned(CAN) DURING APPROACH LANDING GEAR WOULD NOT EXTEND NORMALLY AND 2 AMP CONTROL CIRCUIT BREAKER HAD OPENED. LANDING GEAR WAS LOWERED USING MANUAL SYSTEM AND UNEVENTFUL LANDING CARRIED OUT. MAINTENANCE FOUND 60 AMP LANDING GEAR CIRCUIT BREAKER OPEN (IN LH WING).Jun 28, 2006 · Beech B300 · Landing Gear Retraction/Extension SystemSDR 2006FA0000376Windshield · crackedFLIGHT CREW REPORTED CO-PILOTS WINDSHIELD RAPIDLY FAILED IN CRUISE FLIGHT, INNER LAYER (SPIDER WEBBED) OVER ENTIRE INTERIOR SURFACE. DELAMINATIONS NOTED SPREADING FROM BOTH IB CORNERS UPON REMOVAL. TECH INSTALLING REPLACEMENT WINDSHIELD NOTED PREVIOUS INSTALMar 30, 2006 · N37TD · Beech B300 · Flight Compartment WindowsSDR CA060301007Nut Plate · damagedAIRCRAFT WAS ON APPROACH. POSITIVE NOSE GEAR DOWN LOCK WAS NOT INDICATING USING THE NORMAL SYSTEM. EMERGENCY GEAR DOWN WAS REQUIRED TO HAVE POSITIVE DOWN AND LOCK INDICATION. NOSE LANDING GEAR INSPECTION WAS CARRIED OUT OF THE GREEN LIGHT INDICATOR SWITCHESFeb 24, 2006 · Beech B300 · Landing Gear Retraction/Extension SystemSDR 2006FA0000233Switch · out of toleranceDURING INITIAL 12 MONTH TEST OF CABIN OXYGEN SYSTEM FOUND BAROMETRIC SWITCH OPERATING OUT OF SPECIFIED MM TOLERANCE. REPLACED WITH NEW SUPERSEDING PN 10138402843 SWITCH SUPPLIED BY RAPID, TESTS PASSED SUCCESSFULLY. SUSPECT NEW 101384028-29 SEITCH ASSY MAY HAFeb 24, 2006 · N100BE · Beech B300 · Passenger Oxygen SystemSDR 2006FA0000232Switch · out of toleranceDURING INITIAL 12 MONTH TEST OF CABIN ALTITUDE WARNING SYS FOUND BAROMETRIC SWITCH OPERATING OUT OF SPECIFIED MM TOLERANCE. REPLACED SWITCH WITH NEW SUPERSEDING (PN 101-38402845) SWITCH ASSY FROM STOCK, NEW SWITCH ALSO TESTED OUT OF SERVICE LIMITS. REPLACED Feb 23, 2006 · N100BE · Beech B300 · Cabin Pressure Control SystemSDR 2005FA0001649Brake · draggingON TAKEOFF ROLL, BRAKES APPEARED TO BE DRAGGING. CREW DECIDED TO ABORT TAKEOFF W/O INCIDENT AND TAXIED BACK TO GATE. MAINT JACKED AC AND CHECKED BRAKES. BRAKES APPEARED TO BE DRAGGING AND NOT RELEASING ALL THE WAY. THESE ARE UNMODIFIED BRAKES (W/O STAINLESS Dec 19, 2005 · N981LL · Beech B300 · BrakeSDR CA051213006Hose · burstDURING DAILY INSPECTION, THE AME FOUND THE LT BRAKE DEICE HOSE (P/N 101-380015-9) BURST NEAR UNION (P/N 832-12D).Dec 13, 2005 · Beech B300 · Ice DetectionSDR CA051222004Spar · corrodedA/C IN FOR 5 YR WING BOLT REPLACEMENT AND MAIN SPAR LWR FITTING VISUAL INSPECT. LWR FWD LT WING BOLT DIFFICULT TO REMOVE AND UPON REMOVAL MODERATE CORROSION WAS OBSERVED IN BOLT BORES. LOOKING AT BOLT BORES FROM FRONT, GREATEST CORROSION APPEARED TO BE AFT ADec 9, 2005 · Beech B300 · Wing SparSDR CA051202008Angle · crackedWHEN COMPLYING WITH SPECIAL INSPECTION ON CABIN DOOR, DISCOVERED CRACKED CABIN DOOR SILL ANGLE AT TOP OF DOOR. ADVISED TO HAVE A SPARE PART ON HAND BEFORE DOING INSPECTION. PART WAS CRACKED ALONG WIDTH OF THE ANGLE RUNNING FORE AND AFT FROM AFT END OF THE DNov 9, 2005 · Beech B300 · Passenger/Crew DoorsSDR 2005FA0000848Control Cable · brokenPERFORMING A PHASE 1 INSPECTION, IT IS REQUIRED TO PERFORM A FUNCTIONAL CHECK OF THE PASSENGER OXYGEN SYSTEM. THE TEE HANDLE CONTROL WAS PULLED TO MANUALLY DEPLOY AND FLOW THE PASSENGER OXYGEN MASKS. THE MASKS DID NOT DEPLOY AND THERE WAS NO OXYGEN FLOW. FUJun 7, 2005 · N6117C · Beech B300 · Passenger Oxygen SystemSDR 2005FA0001000Skin · delaminatedDURING A POST FLIGHT CHECK, A MECHANIC NOTICED A BULGE ON THE UNDERSIDE OF THE IB LEADING EDGE OF THE LT WING. UPON FURTHER INVESTIGATION, A DELAMINATION AREA OF APPROXIMATELY 22 INCHES X 10 INCHES WAS FOUND. AFTER REMOVAL OF THE LEADING EDGE AND CLOSER EXAJun 6, 2005 · N991LL · Beech B300 · Leading Edge DevicesSDR 2005FA0000823Bearing · seizedPILOT REPORTED RT ENGINE SURGING, SMOKE FROM EXHAUST SIMULTANEOUSLY WITH RT GENERATOR GOING OFF LINE IN CRUISE FLIGHT. FOUND RT STARTER/ GENERATOR ANTI-DRIVE (BRUSH END) BEARING SEIZED, INPUT SHAFT INTACT. REPLACED STARTER/GENERATOR AND EXAMINED OIL FILTER May 26, 2005 · N350TT · Beech B300 · Starter-GeneratorSDR 2005FA0000654Control Cable · looseDURING SCHEDULED INSPECTION, FOUND CABLE QUADRANT FOR AUTOPILOT RUDDER SERVO LOOSE ON RUDDER TORQUE SHAFT ASSY. REPLACED LOOSE RIVETS W/NEXT SIZE LARGER RIVETS INSTALLED WET W/EA 9309 STRUCTURAL ADHESIVE IAW TECH SUPPORT RECOMMENDATIONS. RECOMMEND THIS AREAApr 23, 2005 · N768WT · Beech B300 · Rudder Control SystemSDR 2005FA0000653Screw · wrong partDURING SCHEDULED INSPECTION FOUND SCREWS ATTACHING AFT LOWER EDGES OF FORWARD WING ROOT FAIRINGS TO UNDERSIDE WING ROOT FAIRINGS TO BE OF EXCESSIVE LENGTH. SCREW TIPS HAD GOUGED LT AND RT LOWER FUSELAGE SKINS AT THE APPROXIMATE FS 166.300 LOCATION TO 0.020 INApr 22, 2005 · N768WT · Beech B300 · FastenersSDR 2005FA0000181Bearing · failedSHAFT BEARING AT THE COOLING FAN END OF THE S/G CAME APART. THIS CAUSE THIS END OF THE COMMUTATOR TO MOVE SIDE TO SIDE AND THE COOLING FUN RUBBED INTO THE HOUSING. (K)Feb 6, 2005 · N893MC · Beech B300 · Starter-GeneratorSDR 2005FA0000193Retainer · misinstalledDURING INSP OF ENG INERTIAL VANE CONTROL SYS, IT WAS FOUND THAT RETAINER PLATE, PN 101-910114-35 THAT LOCKS INTO A GROOVE ON SHAFT, PN 101910114129, FOR AFT INTERIAL VANE, WAS NOT INSTALLED CORRECTLY. WHEN RETAINER PLATE IS CORRECTLY INSTALLED IN GROOVE ON SHFeb 4, 2005 · N5XM · Beech B300 · Air Intake Anti/De-Ice SystemSDR 2005FA0000012Governor · malfunctionedDURING NORMAL GROUND RUN-UP. THE AIRCRAFT PROPELLER AUTO-FEATHER SYSTEM WAS OPERATIONALLY CHECKED. BOTH LT AND TR PROPELLER SWITCHES WERE SELECTED AND BOTH PROPELLERS FEATHERED CORRECTLY. WHEN THE SWITCHES WERE RELEASED THE LT PROPELLER DID NOT COME OUT OF Dec 6, 2004 · N981LL · Beech B300 · Propeller Controlling SystemSDR MGO2004F00000Screw · chafedWHILE COMPLYING WITH TIME SCHEDULE REPLACEMENT OF THE EMERGENCY EXIT LIGHT BATTERIES, FOUND THAT THE BATTERIES HAD LEAKED ACID AND CORRODED THE BATTERY HOLDERS. FOUND THE BATTERY HOLDER SCREWS HAD CHAFFED THROUGH THE BATTERY SIDE LABEL AND SHORTED BATTERY TO Sep 9, 2004 · N300TM · Beech B300 · Emergency LightingSDR 2004FA0000704Hydraulic System · contaminatedDURING THE INITIAL PHASE 1 AND 2 INSPECTION BEING COMPLETED ON AC, ROUTINE INSPECTION OF HYDRAULIC SYS COMPONENTS REVEALED THAT THE HYDRAULIC SYS FILTER HAD RETAINED A LARGE AMOUNT OF RED PLASTIC MATERIAL AND THE (GEAR DOWN) PORT SCREEN WAS FOUND TO BE ALMOST Sep 8, 2004 · N74TF · Beech B300 · Hydraulic System, MainSDR 4101Tire · groovedPROBLEM FOUND DURING NORMAL WORN TIRE REPLACEMENT. CORD (WIRE LIKE MATERIAL) WAS NOT DEEP ENOUGH IN THE RUBBER OF THE TIRE SEAT AREA WHICH LEFT A GROOVE (MIRROR IMAGE OF THE CORD) IN THE NR 4 MAIN WHEEL RIMS (INNER AND OUTER HALVES). THE GROOVES COVERED A THAug 16, 2004 · N350NY · Beech B300 · TireSDR 2724Tire · defectivePROBLEM FOUND DURING NORMAL WORN TIRE REPLACEMENT. CORD (WIRE LIKE MATERIAL) WAS NOT DEEP ENOUGH IN THE RUBBER OF THE TIRE SEAT AREA WHICH LEFT A GROOVE (MIRROR IMAGE OF THE CORD) IN THE NR 3 MAIN WHEEL RIMS (INNER AND OUTER HALVES). THE GROOVES COVERED MOREAug 16, 2004 · N350NY · Beech B300 · TireSDR 2004F00104Control Column · inoperativeDURING A PHASE INSPECTION A SQUEAK WAS NOTED DURING MOVEMENT OF FLIGHT CONTROL COLUMN. INVESTIGATION REVEALED. LOOSE RIVETS BETWEEN THE CONTROL T COLUMN AND BEARING PLATES AT THE POINT WHERE THE CONTROL COLUMN ATTACHES TO THE AIR FRAME AND PIVOTS. MFG ISSUEMar 22, 2004 · N552TP · Beech B300 · Control Column SectionSDR E812004F00001Tube · chafedPILOT REPORTED LT ENGINE BLEED AIR WARNING ANNUNCIATOR ILLUMINATED. DURING TROUBLESHOOTING, FOUND CHAFED LT ENGINE BLEED AIR WARNING EVA TUBING UNDER NR 1R CABIN SEAT AREA. SMALL AIR LEAK FROM AREA CHAFING ON ADJACENT STRUCTURE. SPLICED REPAIRED TUBING AFTEDec 22, 2003 · N447TF · Beech B300 · Engine Bleed Air SystemSDR 2004F00054Skin · debondedLEFT IB LEADING EDGE WING PANEL WAS REMOVED TO REPLACE THE DE-ICE BOOT AND IT WAS DISCOVERED THAT SUBSTANTIAL DEBONDING OF THE LOWER HALF OF THIS PANEL HAD OCCURRED. THERE WAS NO APPARENT DAMAGE TO THE OUTSIDE SKIN THAT WOULD EXPLAIN THIS AND ITS UNLIKELY THADec 19, 2003 · N904MC · Beech B300 · Wing, Plate/SkinSDR 2003FA0001261Line · leakingPILOT REPORTED RT BLEED AIR LINE FAIL ANNUNCIATOR CAME ON, CLIMBING THROUGH FL 260. INVESTIGATED AND TROUBLESHOT IAW MM 26-11-00. FOUND SMALL HOLE IN BLEED AIR WARNING EVA TUBING IN FORWARD RT CABIN UNDERFLOOR AREA. NO BLEED AIR LEAKS NOTED ADJACENT TO AREANov 28, 2003 · N447TF · Beech B300 · Engine Bleed Air SystemSDR 2003FA0001161Servo · bindingINVESTIGATED PILOT COMPLAINT OF AILERON CONTROLS BINDING. NOTED BINDING/BANGING TYPE SOUNDS UNDER CENTER CABIN FLOOR. FOUND NOISES AND BINDING NOT PRESENT WITH AILERON SERVO REMOVED FROM CAPSTAN, RETURNED WHEN AILERON SERVO REINSTALLED. ALSO NOTED NOISES/BOct 31, 2003 · N447TF · Beech B300 · Autopilot SystemSDR LX52003F00002Power Supply · odorTHE POWER SUPPLY EMITTED A FOUL ODOR THAT WAS NOTICED THROUGH OUT AIRCRAFT AND THEN UNIT FAILED.Oct 1, 2003 · N991LL · Beech B300 · Electrical Power SystemSDR 2003FA0000813Bolt · seizedDURING INSPECTION FOUND BOLT ON NOSE WHEEL DRAG LEG SEIZED IN BUSHING AS THE RESULT OF IMPROPER LUBRICATION. THIS SEEMS TO BE DUE TO A RESENT LUBE POINT DESIGN CHANGE. THE OLD BOLT WAS HOLLOW ALLOWING GREASE TO BE DELIVERED TO THE INNER BUSHING. THE NEW BOLJul 1, 2003 · N583AT · Beech B300 · Wheel/Ski/FloatSDR 2003FA0000812Bolt · seizedDURING INSPECTION FOUND BOLT ON NOSE WHEEL DRAG LEG SEIZED IN BUSHING AS THE RESULT OF IMPROPER LUBRICATION. THIS SEEMS TO BE DUE TO A RESENT LUBE POINT DESIGN CHANGE. THE OLD BOLT WAS HOLLOW ALLOWING GREASE TO BE DELIVERED TO THE INNER BUSHING. THE NEW BOLJul 1, 2003 · N434BW · Beech B300 · Wheel/Ski/FloatSDR B4Z2003F00000Bolt · missingON TAKEOFF ROLL, BOTH ENGINES WOULD NOT DEVELOP FULL POWER. AIRCRAFT TAXIED BACK TO RAMP. FURTHER INSPECTION BY TECH FOUND BOLT PN AN5-4A FROM LEFT SIDE OF PEDESTAL LYING ON FLOOR AFTER REMOVING LEFT PEDESTAL SIDE COVER. (ATTACHMENT)Apr 15, 2003 · N685BC · Beech B300 · Instrument PanelSDR LX52003F00001Valve · stickingTHERE IS A PERSISTANT PROBLEM WITH THIS SERIES BRAKE DEICE VALVE STICKING IN THE OPEN POSITION. THIS PROBLEM SEEMS TO BE GREATER DURING THE WINTER (EXTREME COLD) BUT IT DOES OCCUR AT ALL TIMES OF THE YEAR.Jan 24, 2003 · N981LL · Beech B300 · Ice DetectionSDR LX52003F00000Valve · stickingTHERE IS A PERSISTANT PROBLEM WITH THIS SERIES BRAKE DEICE VALVE STICKING IN THE OPEN POSITION. THIS PROBLEM SEEMS TO BE GREATER DURING THE WINTER (EXTREME COLD) BUT IT DOES OCCUR AT ALL TIMES OF THE YEAR.Jan 24, 2003 · N981LL · Beech B300 · Ice DetectionSDR MEA200301Windshield · failedA/C WAS ENROUTE AT FL260, WINDSHIELD ANTI-ICE WAS SELECTED ON AND WAS ON FOUR 1 1/2 HOURS WHEN A LOUD CRACK WAS HEARD AND THE PILOTS WINDSHIELD SHATTERED THE INNER PANE INTO PEA SIZED PIECES. CREW FOLLOWED AIRCRAFT ABNORMAL PROCEDURES AND DESCENDED BELOW 25,00Dec 27, 2002 · N593MA · Beech B300 · Flight Compartment WindowsSDR QC42002F00002Windshield · failedPILOT WINDSHIELD INNER PANE SHATTERED WHILE IN FLIGHT. THE OUTERPANE HELD WITH NO PROBLEM AND THE COPILOT WAS ABLE TO LAND THE PLANE SAFELY. INSPECTION OF THE WINDSHIELD AFTER REMOVAL SHOWED NO OBVIOUS DAMAGE OR CHIPS IN THE OUTER PANE THAT WOULD HAVE LEAD Oct 22, 2002 · N160AC · Beech B300 · Flight Compartment WindowsSDR PG22002F00000Switch · shortedPILOTS HEADING SYSTEM CONTINUOUSLY ROTATED COUNTER CLOCKWISE. TROUBLESHOT PROBLEM TO A2S2 IN THE CCU65 CONTROL UNIT. FOUND SPRING INTERNAL TO SWITCH SHORTED TO OPPOSITE TERMINAL. REPLACEMENT OF SWITCH CURED PROBLEM. A HEIGHT QUALITY SWITCH, OR INSULATION AOct 1, 2002 · N200VC · Beech B300 · Attitude Gyro and Indicating SystemSDR CGO2002F00002Plate · failedDURING FREON AIR CONDITIONING SYSTEM TROUBLESHOOTING, FOUND COMPRESSOR FAILED. UPON REMOVAL OF OLD UNIT FOR REPLACEMENT, FOUND PIVOT PLATE CRACKED COMPLETELY THROUGH.Sep 11, 2002 · N991LL · Beech B300 · Cabin Cooling SystemSDR JEM2002F00006Crossbeam · crackedCROSSBEAM IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSSBEAM ADJACENT TO THE AFT, LOWER CORNER OF THE EMERGENCY EXIT OPENING.Aug 16, 2002 · N711VN · Beech B300 · Fuselage Main, Structure
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