Beech 400A

Service difficulty reports · 1,397

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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 = '400A'
  ORDER BY difficulty_date DESC"

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SDR 2026FA0000630Tire · blownACFT BLEW THE LEFT MAIN TIRE WHILE TAXIING TO THE HANGAR AFTER LANDING. AIRCRAFT LANDED WITH NO ISSUES. AIRCRAFT WAS ABLE TO TAXI OFF THE RUNWAY AND STARTED TO HEAD TOWARDS THE HANGAR. IT TAXIED ABOUT 300 YARDS ON TAXIWAY H BEFORE IT TURN OFF ONTO TAXIWAY E. WAug 7, 2026 · N473FL · Beech 400A · TireSDR OEJA202606080001Control Valve · stickingON TAKE OFF THE AIRCRAFT WAS CLIMING AND THE CREW HEARD A POPPPING NOISE AND THE CABIN BEGAN TO DROP, SO THE TURNED AROUND WENT BACK TO THE AIRPORT. THEY NOTIFED MAINTENANCE , PERFORMED SOME ENGINE RUNS AND THE AIRCRAFT PRESSURIZED ON THE GROUND , AIRCRAFT RETJun 4, 2026 · N75TG · Beech 400A · Hydraulic System, MainSDR 2026F00028Line · rupturedBLEED AIR DUCT FAIL ANNUCIATOR ILLUMINATED DURING CLIMB. CREW RETURNED TO THE AIRPORT. MX UNABLE TO FIND LEAK ON THE GROUND DURING RUNS. ANOTHER FLIGHT TO CONFIRM CONDITION. ANNUCIATOR ILLUMINATED AGAIN DURING CLIMB. CREW RETURNED TO THE AIRPORT. MX FOUNMar 14, 2026 · N82QD · Beech 400A · Pneumatic Distribution SystemSDR CVGA20260218003Bulb · inoperativeDURING APPROACH, AFTER EXTENDING THE LANDING GEAR, THE RIGHT LANDING GEAR SAFE LIGHT DID NOT ILLUMINATE. EMERGENCY DECLARED. UPON INSPECTION OF RT LG SAFE LIGHT FOUND LIGHT BULB TO BE BURNED OUT. REMOVED AND REPLACED THE RT LG SAFE LIGHT BULB WITH PN 327 FROFeb 16, 2026 · N452TM · Beech 400A · Landing Gear Position and WarningSDR CVGA20260216002Strut · overservicedON LANDING, REVERSERS WOULD NOT DEPLOY. BELOW 60 K LOST BRAKES. USED EMERGENCY BRAKES TO STOP ACFT. AFTER TAXIING OFF RUNWAY, PLACED BRAKES IN ANTI SKID OFF POSITION. BRAKES WERE RESTORED. AIRSPEED INDICATOR SPEED LOW BAR WAS VISUAL. AFTER ACFT PARKED MAIN WHFeb 13, 2026 · N453TM · Beech 400A · Main Landing Gear Strut/Axle/TruckSDR 2025F00291Button · wornDISCOVERED DURING PREFLIGHT, THE MAIN CABIN DOOR HANDLE WILL NOT STOW IN THE CLOSED POSITION. REMOVED HANDLE AND INTERIOR DOOR PANEL. FOUND THE HANDLE AND THE PUSH BUTTON TO BE WORN. ABLE TO TURN BOTH UNITS 180 DEGREES FOR USE UNTIL NEW PARTS ARRIVED. DOORDec 24, 2025 · N82QD · Beech 400A · Passenger/Crew DoorsSDR 3N0A2025121800284Windshield · delaminatedTHE RIGHT WINDSHIELD SHOWED SIGNS OF DELAMINATION SHORTLY AFTER DEPARTING PWN. AFTER LANDING AT BNA A PICTURE WAS SENT TO DIR. OF MAINTENANCE AND TRIP SUPPORT, AND WE WERE ADVISED TO CONTINUE THE FLIGHT BACK TO BASE, AT FL 360 WE HEARD A LOUD CRACKING NOISE, Dec 13, 2025 · N661WD · Beech 400A · Flight Compartment WindowsSDR CVGA20251114002Switch · faultyFLAP ASYM LIGHT CAME ON AFTER SELECTING FLAPS 20 POSITION. FAULT COULD NOT BE DUPLICATED UPON ARRIVAL TO AIRCRAFT. MCC ELECTED TO REPLACE THE FLAP FOLLOW UP SWITCH. REMOVED FLAP FOLLOW UP SWITCH P/N 45AS61015-23 S/N 08A432AND INSTALLED AN OVERHAULED FLAP FOLLONov 10, 2025 · N492TM · Beech 400A · Trailing Edge Flap Control SystemSDR W39A202505140355Windshield · crackedRH WINDSHIELD CRACKED DESCENDING THROUGH FL 220 , CREW DETERMINED THAT IT WAS THE OUTER ACRILIC PLY, CREW COMPLIED WITH THE ABNORMAL PROCEDURE , PRESSURIZATION WAS NORMAL, CREW CONTINUE WITH THE FLIGHT TO SUAApr 10, 2025 · N127EJ · Beech 400A · Flight Compartment WindowsSDR CVGA20250407002Brake Assy · malfunctionedDURING TAXI OUT BRAKES WERE MOMENTARILY LOST ON BOTH SIDES LH & RH BRAKE PEDALS. (ONCE ON THE LEFT SIDE AND ONCE ON THE RIGHT SIDE BRAKE PEDALS)Apr 3, 2025 · N829HM · Beech 400A · Landing Gear Brake SystemSDR CVGA20250303001Diode · failedSMOKE CAME FROM DASH AREA WHEN ENG SYNC LIGHT IS ON - REMOVED AND REPLACED CR119 DIODE WITH NEW DIODE, P/N 1N4007, ON ENGINE FUEL SYNCH ANNUN CIRCUIT IAW BE400 AMM 20-20-02. OPS CHECK GOOD.REMOVED AND REPLACED RH GLARESHIELD INDICATOR PANEL P/N 45AS88843-49 S/Feb 25, 2025 · N496TM · Beech 400A · Instrument System WiringSDR CVGA20250219005Cabin Pressure · inoperativeON TAKEOFF AND CLIMB OUT AIRPLANE NOT PRESSURIZING. CYCLED PRESS SOURCE KNOBS WITH NO CHANGE- EMERGENCY DECLARED.Feb 15, 2025 · N465TM · Beech 400A · Cabin Pressure Control SystemSDR CVGA20250218004Controller · failedPITCH TRIM MOTOR FAILURE - EMERGENCY DECLARED - REMOVED RH PITCH TRIM CONTROLLER P/N 76621-4 S/N 2392. INSTALLED SERVICEABLE PITCH TRIM CONTROLLER P/N 76621-4 S/N 2722. OPS CHECK PITCH TRIM I/A/W BEECH 400 AMM CH 27-40-00, OPS CHECK SATISFACTORY.Feb 13, 2025 · N452TM · Beech 400A · Elevator Tab Control SystemSDR CVGA20250129006Brake · failedLEFT BREAK FAILED DURING TAXING. PERFORMED FUNCTIONAL TESTING MANUAL BRAKE SYSTEM AND POWER BRAKE SYSTEM IAW 400A AMM 32-40-00. PERFORMED POWER BRAKE BLEEDING IAW 400A AMM 32-40-00. NO DEFECTS NOTED. GAUGE ID# TL-00509, DUE 10/22/2025, GAUGE ID# TL-00503, DUE Jan 27, 2025 · N465TM · Beech 400A · Landing Gear Brake SystemSDR CVGA20250110004Brake Sys · failedBRAKE FAILURE WHILE TAXI TO TAKEOFF. COMPLETED FULL ANTISKID BRAKE TEST PRIOR TO FAIL. SIC CHECKED HIS BRAKES SUCCESSFULLY AND RETURNED CONTROLS, FELT LIKE BRAKE TEST. USED EMERGENCY TO STOP BEFORE RUNWAY BUT CROSSED LINE.Jan 8, 2025 · N675UP · Beech 400A · Landing Gear Brake SystemSDR CVGA20241205002Connector · faultedDURING HIGH SPEED TAXI CHECK AT 75 KTS BOTH BRAKES LOCKED AND BOTH TIRES DEFLATED. - REPLACED BOTH RH & LH MAIN BRAKE ASSEMBLIES WITH OVERHAULED IAW 400A MM 32-40-00. LH BRAKE ASSEMBLY PN OFF/ON: 5010614, SN OFF: NOV95-345, SN ON: JUN06-1336. RH BRAKE ASSEMBLYNov 27, 2024 · N419TM · Beech 400A · Landing Gear System WiringSDR CVGA20241016003Landing Gear · faultedWHEN SELECTING LANDING GEAR DOWN, NONE OF THE THREE GREEN LANDING GEAR SAFE LIGHTS ILLUMINATED. THE RED GEAR-HANDLE IN-TRANSIT LIGHT ILLUMINATED NORMALLY. EMERGENCY DELCARED. INSPECTED SQUAT SWITCHES FOR SECURITY AND EASE OF MOVEMENT, CLEANED AND INSPECTED CONOct 13, 2024 · N452TM · Beech 400A · Landing Gear Retraction/Extension SystemSDR V7PA202402270001Pressure Valve · failedCREW REPORTED A LH ENGINE FIRE WARNING IN FLIGHT WHILE CLIMBING THRU 12,000 FEET.. PULLED THROTTLE TO IDLE AND WARNING STOPPED. CREW DECLARED EMERGENCY AND RETURNED TO TTN. MAINTENANCE PERSONNEL TROUBLESHOT THE DISCREPANCY AND FOUND THE LH ENGINE PRESSURE SHSep 12, 2024 · N75TG · Beech 400A · Pneumatic Distribution SystemSDR 2024FA0000705Duct · out of positionBLLED AIR DUCT FAIL CAUTION LIGHT ILLUMINATED ON CLIMB OUT PASSING FL250.Sep 6, 2024 · N317PC · Beech 400A · Engine Bleed Air SystemSDR W39A2024092310001Windshield · crackedRH WINDSHIELD CRACKED DESCENDING THROUGH FL 210, 62NM OUT OF KILM, CREW COMPLIED WITH THE ABNORMAL PROCEDURE, PRESSURIZATION WAS NORMAL, AND THEN CONTINUED WITH APPROACH TO RWY 35 AND LANDED NORMALLY WITH NO FURTHER ISSUES.Sep 2, 2024 · N106KH · Beech 400A · Flight Compartment WindowsSDR CVGA20240904004Pressure Switch · faultyCABIN PRESSURE LO ANNUNCIATOR ILLUMINATED IN FLIGHT AT FL320 CABIN ALTITUDE WAS OVER 9000FT AND CLIMBING. BY FL350 WARNING LIGHT CAME ON PERFORMED EMER DESCENT LIGHT EXTINGUISHED AT 8000 FT. FERRIED AIRCRAFT FROM KJAX TO KFLL FOR REPAIRS. REMOVED CABIN LOW PREAug 31, 2024 · N929AG · Beech 400A · Cabin Pressure Control SystemSDR CVGA20240812002Thrust Reverser · malfunctionedLEFT AND RIGHT TR ARM LIGHTS CAME ON RIGHT AFTER T/O AND REMAINED ON AFTER STOWED. LANDING GEAR WOULD NOT GO UP LOCK WAS DOWN. AFTER MANUALLY RELEASING LOCK GEAR WENT UP. TCAS FAIL WAS ALSO FLASHING THE ENTIRE TIME. ALL THE WIRING CHECKS TO BOTH LT & RT LANDINAug 9, 2024 · N477TM · Beech 400A · Engine Thrust ReverserSDR CVGA20240729003Unknown · unknownLOST HEADING INFORMATION ON SDU, CDU, MFD - AIRPLANE DIDN'T KNOW WHERE IT WAS IN RELATION TO AIRPORT OR GUIDANCE. TROUBLESHOT AS REQUIRED WITH FSR. PERFORMED AHRS TEST IAW BEECHCRAFT 400 AMM 34-20-01. OPS CHECK GOOD. PERFORMED FMS INTITIALIZATION IAW COLLINS AJul 26, 2024 · N491TM · Beech 400A · Navigation SystemSDR CVGA20240725002Brake Sys · failedAFTER LANDING ON TAXIWAY MAIN BRAKES FAILED. HAD TO USE EMERGENCY BRAKE TO STOP.Jul 21, 2024 · N929AG · Beech 400A · Landing Gear Brake SystemSDR OEJA2024070300486Solenoid Valve · failedCLIMBING OUT OF TEB IN THE MID 30S THE AIRCRAFT WAS UNABLE TO MAINTAIN ADDITIONAL CABIN PRESSURE. THE CREW LEVELED OFF AND ASSESSED THE SITUATION, AND AFTER SOME TROUBLE SHOOTING ELECTED THAT THE FLIGHT WAS UNABLE TO CONTINUE TO AUSTIN AT THAT POINT IN TIME.Jul 3, 2024 · N436FL · Beech 400A · Passenger/Crew DoorsSDR CVGA20240628002Brake Assy · failedLOST BRAKES ON TAXI. COMPLETE BRAKE VALVE ON BOTH SIDES. DEPLOYED NITROGEN EMERGENCY BRAKES.Jun 25, 2024 · N929AG · Beech 400A · Landing Gear Brake SystemSDR CVGA20240530002Pump · low pressureON FINAL APPROACH INTO IAD, THE LH PUMP PRESS LO AND THE HYD LEVEL LO LIGHTS ILLUMINATED THE HYD PRESS GAUGE INDICATED NORMAL SYSTEM PRESS. AFTER LANDING BRAKING WAS NORMAL INITIALLY THEN FAILED TOTALLY. APPLIED EMERGENCY NITROGEN BRAKES TO STOP A/O. ENGINE HYMay 26, 2024 · N492TM · Beech 400A · Hydraulic Pump (Electric/Engine), MainSDR CVGA20240530001Fire Loop · chafedLH ENG FIRE PUSH SWITCHLIGHT ILLUMINATED AND FIRE BELL SOUNDED AT 400' AGL TAKE OFF THRUST SET, BROUGHT LEFT ENGINE THRUST LEVER BACK TO IDLE, LIGHT EXTINGUISHED AFTER APPROX 10 SECONDS. FOUND FIRE LOOP TO BE DAMAGED ON THE LH ENGINE FROM RUBBING AGAINST BLEEDMay 26, 2024 · N449TM · Beech 400A · Smoke DetectionSDR OEJA2024032600001Warning Light · illuminatedAT CRUISE AND 41,000 AGL A NO RIGHT ENGINE NO DISPACT LIGHT CAME ON AND WOULD NOT EXTINGUISH , RAN THE QRH CHECK LIST AND IT ADVISED US TO LAND AS SOON AS PRACTICAL , SO THE KVNY WAS CHOSEN TO LAND AT, NO OTHER ISSUES , MAINTENANCE WAS ADVISED OF THE SITUATIOMar 23, 2024 · N473FL · Beech 400A · Central WarningSDR CVGA20240322001Frame · crackedMULTIPLE CRACKS WERE FOUND AROUND FASTENER HOLES AT FS330 WHILE PERFORMING BLEED AIR TUBING INSPECTION. PERFORMED REPAIR TO LH FUSELAGE FRAME #330 IAW DOCUMENT #MROS-87927 REV IR. NO ADDITIONAL ADDED INSPECTION REQUIREMENTS WILL BE NECESSARY OUTSIDE OF THE INSMar 15, 2024 · N497TM · Beech 400A · Fuselage Main, FrameSDR CVGA20240319001Switch · defectiveON TAKEOFF HAD AN UN-COMMANDED ROLL TRIM TO THE LEFT AT FULL DEFLECTION. INITIALLY WE WERE UNABLE TO CORRECT THE TRIM TO NORMAL. EVENTUALLY WE WERE ABLE TO NEUTRALIZE THE ROLL TRIM. EMERGENCY DECLARED. R&R PILOT YOLK HAT SWITCH WITH NEW. OPS CHECK GOOD WITH NOMar 14, 2024 · N672UP · Beech 400A · Rudder Tab Control SystemSDR 3CMA2024022300001Windshield · failedWHILE COMING FROM SDF LOUISVILLE KENTUCKY AT AN ALTITUDE OF 29000 FT ON DESCENT THE COPILOT'S WINDSHIELD SHATTERED. PILOT TOOK OVER AND ABOUT 2 MINUTES LATER THE PILOT'S WINDSHIELD ALSO SHATTERED. THEY CONTINUED THE FLIGHT INTO PIT WITH BOTH WINDSHIELDS SHATTEFeb 22, 2024 · N400MX · Beech 400A · Flight Compartment WindowsSDR CVGA20240124001Switch · intermittentLH MAIN GEAR DOWN GREEN LIGHT WOULD NOT ILLUMINATE WHEN GEAR DOWN SELECTED. LIGHT WOULD TEST. PERFORMED GEAR EMERGENCY EXTENSION PROCEDURE. LH GEAR DOWN LIGHT STILL DID NOT ILLUMINATE. LIGHT CAME ON AFTER SHUTDOWN DURING TOW TO FBO. EMERGENCY DECLARED. TROUBLJan 17, 2024 · N418TM · Beech 400A · Landing Gear Position and WarningSDR 2024FA0000040Duct · crackedPILOT REPORTED GETTING THE "BL AIR DCT FAIL" LIGHT IN FLIGHT, DURING CRUISE OPERATION. DURING TROUBLESHOOTING, IT WAS NOTED THAT THE BLEED AIR TUBE THAT CONNECTED TO THE LEFT ENGINE WAS CRACKED ALL THE WAY AROUND IN THE PYLON AREA.Jan 16, 2024 · N880MG · Beech 400A · Engine Bleed Air SystemSDR CVGA20240118001Unknown · unknown"HSTAB ICE FAIL " ANNUNCIATION ILLUMINATED IMMEDIATELY AFTER SYSTEM ACTIVATION IN THE AIR. SYSTEM PASSED GROUND CHECK PRIOR TO TAKE OFF. EMERGENCY DECLARED.Jan 15, 2024 · N498TM · Beech 400A · Airfoil Anti/De-ice SystemSDR CVGA20231216001Unknown · unknownDURING CLIMB L AND R TR ARM LIGHTS BECAME ILLUMINATED WITHOUT THE MASTER CAUTION WARNING LIGHT. AN EMERGENCY WAS DECLARED. THE LEFT AND RIGHT THRUST REVERSERS WERE PLACED ON MEL.Dec 12, 2023 · N225SB · Beech 400A · Engine Thrust ReverserSDR CVGA20231211001Oxygen Bottle · emptyO2 NEEDS SERVICE FOR POSSIBLE LEAK. READS 0 ON GAUGE. REMOVED AND REPLACED O2 BOTTLE REF B400 AMM CH 35-11-00. OPS AND LEAK CHECK PASSED AT THIS TIME. NO DEFECTS NOTED. EMERGENCY WAS DECLARED.Dec 5, 2023 · N465TM · Beech 400A · Crew Oxygen SystemSDR OEJA202312050001Unknown · unknownON 12/3/2023 AT APX 2230 N420FL ENCOUNTERED A FLAP ASYM LIGHT ON APPROACH INTO MSP, THE FLAPS WERE LOCKED OUT AND DID NOT EXTEND. AFTER CYCLING THE FLAPS AND MAKING A 2ND ATTEMPT AT EXTENSION WE REQUESTED A DELAY VECTOR TO TROUBLESHOOT. AFTER COMPLETING QRH PRDec 3, 2023 · N420FL · Beech 400A · Trailing Edge Flap Control SystemSDR CVGA20231127001Light · failedNOSE AND RIGHT LANDING GEAR LIGHTS INDICATOR INOP. REPLACED NOSE AND RIGHT LANDING GEAR INDICATOR LAMPS. OPS CHECK GOOD. AN EMERGENCY WAS DECLARED.Nov 21, 2023 · N673UP · Beech 400A · Exterior LightingSDR CVGA20231027001Door Seal · failedCABIN PRESS LO ANNUNCIATOR ILLUMINATED IN FLIGHT APPROXIMATELY FL280. FOUND MAIN ENTRANCE DOOR WEATHER SEAL TO BE CUT AND FOLDED OVER. REMOVED SEAL AND INSTALLED NEW SEAL. PERFORMED SATISFACTORY OPS AND LEAK CHECK OF DOOR SEAL OPERATION. ALL WORK PERFORMED IN Oct 23, 2023 · N671UP · Beech 400A · Cabin Pressure Control SystemSDR CVGA20231016001Switch · faultyIMMEDIATELY AFTER TAKEOFF, AUTOPILOT OFF, ROLL TRIM RAN TOWARDS RIGHT WING DOWN. IT STOPPED WITH LEFT INDICATOR APPROXIMATELY 2 INDICATOR MARKS UP AND RIGHT INDICATOR APPROXIMATELY 21/2 INDICATOR MARKS DOWN. ACTUAL ROLL TRIM TAB POSITIONS MATCHED THE INDICATOOct 12, 2023 · N76GJ · Beech 400A · Aileron Control SystemSDR OEJA202310110001Door Seal · unknownDURING CLIMB OUT ENROUTE TO MONTEREY CA FROM PORTLAND OR THE CREW NOTICED THE CABIN A WAS NOT CLIMBING , SO THE CREW DECIDED TO RETURN TO PORTLAND FOR A SAFE LANDINGOct 7, 2023 · N436FL · Beech 400A · DoorsSDR CVGA20231002001Anti-Skid Sys · failedAFTER LANDING JUST BEFORE EXITING THE RUNWAY PIC BRAKE BRAKE PEDALS WENT ALL THE WAY TO THE FLOOR WITH NO BRAKE. EMER BRAKE WAS USED TO BRING A/C TO A STOP. PIC BRAKE WORKED NORMAL. REPLACED ANTI SKID CONTROL BOX.Sep 27, 2023 · N929AG · Beech 400A · Landing Gear Brake SystemSDR CVGA20230927001Transducer · faultyCOMING INTO PARKING, BRAKES ON BOTH SIDES WENT ALL THE WAY TO THE FLOOR AND WOULD NOT STOP. BRAKES WORKED BRIEFLY AND STOPPED THE AIRCRAFT. EMERGENCY BRAKE WAS USED TO ENSURE STOP. REMOVED AND REPLACED R/H WHEEL SPEED TRANSDUCER.Sep 23, 2023 · N929AG · Beech 400A · Landing Gear Brake SystemSDR CVGA20230918001Switch · failedSUDDEN LEFT YAW AND LEFT THROTTLE UN-COMMAND REDUCED TO IDLE. THE LEFT THRUST REVERSER HAD BEEN PREVIOUSLY PLACED ON MEL. CLEARED THE MEL ITEM BY REPLACING THE LH T/R STOW SWITCHES. CYCLED T/R SEVERAL TIMES. T/R OPERATION WAS SMOOTH AND CONSISTENT. ENSURED T/RSep 14, 2023 · N489TM · Beech 400A · Engine Thrust ReverserSDR CVGA20230915001Unknown · unknownLEFT THRUST REVERSER DEPLOY IN FLIGHT. FOUND THRUST REVERSER LH DEACTIVATION PROCEDURE PERFORMED ON 9/13/2023 WAS INCOMPLETE. CONNECTORS P427 AND P429 WERE STILL CONNECTED. DISCONNECTED P427 AND P429 REMOVING POWER FROM THE ISOLATION AND CONTROL VALVES. WORK PSep 14, 2023 · N489TM · Beech 400A · Engine Thrust ReverserSDR OEJA202308170001Control Box · failedDURING TAKE OFF ROLL AND ABOUT 60 KNOTS THE LEFT BLEED SOURCE CAUTION LIGHT CAME ON INDICATION BLEED AIR FAILURE , SO THE TAKE OFF WAS REJECTEDAug 16, 2023 · N490FL · Beech 400A · Cabin Temperature Control SystemSDR CVGA20230814001Unknown · unknownCLIMBING OUT OF SSI AT 14,000 FT WE NOTICED AN INCREASING FUEL IMBALANCE TOWARD THE RIGHT, FOLLOWED BY A ROLL SERVO WARNING (YELLOW A IN A BOX ON PFD). WE THEN NOTICED THAT THE LEFT ROLL TRIM INDICATOR WAS DEFLECTED DOWN MORE THAN 2 TIC MARKS BELOW BELOW NEUTRAug 10, 2023 · N76GJ · Beech 400A · Autopilot SystemSDR YQKA202308090001Starter Gen · misoverhauledSTARTER/GENERATOR ORDERED AND RECEIVED. UPON INSPECTION OF STARTER/ GENERATOR IT WAS FOUND THAT ONE OF THE FOUR BRUSH TERMINALS WAS LOOSE AND NOT MAKING PROPER CONTACT. FURTHER TROUBLE SHOOTING NOTED THAT THE MOUNTING SCREW WAS TIGHT BUT THE BRUSH HOLDER ATTAug 10, 2023 · N917E · Beech 400A · Starter-GeneratorSDR CVGA20230727001Unknown · unknownSMOKE FROM COPILOT'S SIDE CABIN TRAY TABLE AREA ALONG WITH EXCESSIVE HEAT FROM COCKPIT ON COPILOT'S SIDE. A/C CIRCUIT BREAKER WAS PULLED BY PREVIOUS CREW AND DEFERRED. COMPRESSOR CB WAS NOT PULLED. FOUND THAT THE WRONG CIRCUIT BREAKER WAS DEACTIVATED DURING THJul 23, 2023 · N671UP · Beech 400A · Cabin Temperature Control System
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