Beech 200

Service difficulty reports · 521

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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 = '200'
  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 DXTA201304185359Landing Gear · malfunctionedAFTER TAKEOFF, WITH NORMAL MLG RETRACTION, RT MLG RED CROSS HATCH UNSAFE LIGHT ILLUMINATED. LT MLG AND NLG RETRACTED NORMALLY. DEPARTED AIRFIELD WITH SNOW ON TAXI WAYS. DELAYED MLG RETRACTION AFTER TAKEOFF WITH RESPECT TO FIELD CONDITIONS. COMPLETED MLG DOEApr 17, 2013 · N719QS · Gulstm 200 · Landing Gear Retraction/Extension SystemSDR DXTA2013041805358Uplock · out of adjustAFTER TAKEOFF, RETRACTED GEAR AND RECEIVED A GEAR UNSAFE INDICATION ON LT MLG. RED HASHES. RETURNED TO DPARTURE & WHEN MLG WAS SELECTED DOWN, RECEIVED THREE GREEN. PERFORMED UPLOCK ADJUSTMENT, PERFORMED MAXIMUM RETRACTION PRESSURE CHECK AND FOUND LT AFT Apr 17, 2013 · N731QS · Gulstm 200 · Landing Gear Retraction/Extension SystemSDR DXTA201304015344Actuator · malfunctionedELEVATOR FEEL FAIL ILLUMINATED TWO TIMES DURING FLIGHT. REMAINING ON FOR 30-60 SECONDS EACH TIME. R & R Q FEEL SERVO ACTUATOR IAW CMP 273014. PERFORMED STALL PROTECTION AND Q FEEL ACTUATOR ADJUSTMENT TEST IAW CMP 273030. NO DEFECTS NOTED.Mar 29, 2013 · N701QS · Gulstm 200 · Elevator Control SystemSDR DXTA2013031905320Proximity Switch · faultedON GEAR RETRACTION, GEAR RETRACTED NORMALLY, WITH WHITE UP MESSAGES. AFTER ABOUT 30 SECONDS A YELLOW GEAR IN TRANSIT MESSAGE APPEARED ON THE RT MAIN GEAR, FOLLOWED CLOSELY BY A RED GEAR STUCK IN TRANSIT MESSAGE. PUT GEAR DOWN, RECEIVED THREE GREEN AND EXTENDEMar 18, 2013 · N738QS · Gulstm 200 · Landing Gear Retraction/Extension SystemSDR DXTA2013022805300Receptacle · failedCABIN MONITORS CIRCUIT BREAKER POPPED. LIGHT ACRID ODOR WAS NOTED IN CABIN. CABIN MONITORS CIRCUIT BREAKER WILL NOT RESET. REMOVED DEFECTIVE LT NR 2 CABIN SEAT MONITOR BASE RECEPTICLE. INSTALLED REPAIRED RECEPTICLE. PERFORMED OPS CHECK AND TESTED NORMAL. NOFeb 27, 2013 · N725QS · Gulstm 200 · Electrical Power System WiringSDR DXTA2013021405287Steering Sys · inoperativeNOSE WHEEL STEERING INOPERATIVE. TOOK SEVERAL TRIES TO ENGAGE. ONCE ENGAGED, IT WAS PULLING RIGHT. IN THE RT TURN, IT FAIL COMPLETELY FULL RIGHT. COMPLIED WITH NOSE STEERING TROUBLESHOOTING. DURING OPS CHECK, FOUND STEERING TO LT TRAVELS TO FULL DEFLECTIOFeb 14, 2013 · N743QS · Gulstm 200 · Landing Gear Steering SystemSDR DXTA2013021405286Generator · inoperativeNOSE WHEEL STEERING INOPERATIVE. TOOK SEVERAL TRIES TO ENGAGE. ONCE ENGAGED IT WAS PULLING RIGHT. IN THE RIGHT TURN TO RETURN TO THE FBO, IT FAILED COMPLETELY, FULL RIGHT.Feb 14, 2013 · N743QS · Gulstm 200 · Landing Gear Steering SystemSDR DXTA2013020605272Unknown · vibrationFIVE SECONDS AFTER APPLICATION OF TAKEOFF POWER, MULTIPLE LOUD NOISES WITH THE ENTIRE ACFT SHAKING AND VIBRATIONS WHERE FELT.Feb 5, 2013 · N703QS · Gulstm 200 · Standard Practices/StructuresSDR DXTA2013020405270Unknown · unknownLEFT LANDING GEAR INDICATOR WOULD NOT INDICATE UP AND LOCKED. EVEN AFTER FOLLOWING PROCEDURES IN QRH. WHEN GEAR SELECTED DOWN THE GEAR INDICATORS WERE DOWN AND LOCKED. INSPECTED THE UPLOCK SWITCHES, NO DEFECTS NOTED. ADJUSTMENT OF SWITCHES ARE GOOD. PERFORFeb 1, 2013 · N703QS · Gulstm 200 · Landing Gear Retraction/Extension SystemSDR DXTA2013020405269Pdu · failedDURING DESCENT AT APPROX 13,000 FEET, ATTEMPTED TO EXTEND THE FLAPS TO 20 THE SLAT/FLAP MAINT MESSAGE CAME ON AND THEY STOPPED AT 18 DEGREES. RECYCLED THE FLAPS AND THE MESSAGE CAME ON AGAIN AND FLAPS STOPPED AT 6 DEGREES. RECYCLED FLAPS AGAIN, THIS TIME THEFeb 1, 2013 · N731QS · Gulstm 200 · Trailing Edge Flap Control SystemSDR 9JLA2013020104423Actuator · leakingTHE CREW REPORTED AFTER TAKEOFF, DURING THE CLIMBOUT, RECEIVED A LT LOW HYD QTY CAS MESSAGE. THE CREW STATED THAT THEY COMPLETED THE CHECKLIST IN THE POH AND SHORTLY AFTER THAT THE LT HYD PRESSURE BEGAN TO FLUCTUATE BETWEEN ZERO AND 2800 PSI. THE CREW DIVERTJan 17, 2013 · N2HL · Gulstm 200 · Elevator Control SystemSDR 9JLA2013030504421Inverter · defectiveCREW REPORTED THAT THE AC OUTLETS IN THE CABIN WERE INOPERATIVE. REMOVED THE DEFECTIVE AC INVERTER, SN 294 AND INSTALLED A REPAIRED UNIT. FAILED AFTER 7.6 HRS OF OPERATIONS .Jan 2, 2013 · N2HL · Gulstm 200 · AC InverterSDR 9JLA2013020504421Inverter · failedTHE CREW REPORTED THAT THE CABIN AC OUTLETS ARE INOPERATIVE. THE INVERTER FAILED AFTER ONLY 8 HRS OF OPERATION. THE DEFECTIVE INVERTER PN SS-200, SN 294 WAS REMOVED. A REPAIRED INVERTER WAS INSTALLED. REF: MM 24-21-01.Jan 2, 2013 · N2HL · Gulstm 200 · AC InverterSDR DXTA2012122105213Wire Harness · dirtyAFTER DEPARTING, CYCLED LANDING GEAR UP AND THE NOSE GEAR SHOWED STUCK IN TRANSIT. FOLLOWED THE CHECKLIST AND CYCLED GEAR DOWN AGAIN AND BACK UP BUT NOSE GEAR STUCK INTRANSIT CAME BACK ON AGAIN. CONTINUED CHECKLIST AND PUT GEAR HANDLE BACK DOWN RECEIVED THDec 21, 2012 · N718QS · Gulstm 200 · Landing Gear System WiringSDR DXTA2012120305199Unknown · odorELECTRICAL ODOR EMENATED FROM WHAT SEEMED LIKE THE OVERHEAD PANEL. FOUND NO EVIDENCE OF OVERHEATING OR SHORTING. OPERATED ELECTRICALS, NO EVIDENCE OF AN ELECTRICAL ODOR. OPERATED THE AIR CONDITIONING SYS AND THERE WAS NO EVIDENCE OF AN ELECTRICAL ODOR. CDec 1, 2012 · N749QS · Gulstm 200 · Air Distribution SystemSDR DXTA2012110105162Seal · leakingCLIMBING THRU 38000 FT TO 39000, RECEIVED A RT ENGINE LOW OIL PRESS INDICATION. RAN CHECK LIST AND SHUTDOWN ENGINE IAW CHECK LIST. CHECKED OIL PRESSURE, IT WAS 0. LANDING WAS UNEVENTFUL ON POST FLIGHT NOTICED OIL LEAKING FROM THE ENGINE COWLING AREA. FOOct 31, 2012 · N725QS · Gulstm 200 · Engine Oil Indicating SystemSDR DXTA2012110105126Oil System · leakingCLIMBING THRU 38,000 FEET TO 39,000, RECEIVED A RT ENGINE LOW OIL PRESSURE INDICATION. RAN CHECK LIST AND SHUTDOWN THE ENGINE IAW CHECK LIST. CHECKED ENGINE OIL PRESSURE IT WAS 0. LANDING WAS UNEVENTFUL ON POST FLIGHT NOTICED OIL LEAKING FROM THE ENGINE COOct 31, 2012 · N726QS · Gulstm 200 · Turbine Engine Oil SystemSDR DXTA2012102205157Wire · overheatedENROUTE, DETECTED SMOKE IN COCKPIT AT 14,000 FT. A MINUTE OR SO LATER SMOKE STARTED EMANATING FROM THE UPPER RT CORNER OF THE CO-PILOT'S SIDE WINDSHIELD. DECLARED EMERGENCY AND RAN CHECKLISTS, TURNED WINDSHIELD HEATS OFF. SMOKE SUBSIDED THEN DISSIPATED ABOUOct 20, 2012 · N752QS · Gulstm 200 · Ice/Rain Protection System WiringSDR DXTA2012101905154Damper · malfunctionedMED DAMPER ARM IS CONTACTING WEB 330 LT SIDE AT FS 5728 WL 200. ENLARGED EXISTING CUTOUT IN RIB 330 LT SIDE, AT FS5728/WL 200 TO CLEAR MED DAMPER ARM IAW WO CS304901. NO CRACKS NOTED.Oct 18, 2012 · N727QS · Gulstm 200 · Passenger/Crew DoorsSDR DXTA2012101905152Switch · out of adjustDURING TAXI AT SLOW SPEEDS, LESS THAN 10 KNOTS, WHILE APPLYING CONSTANT PRESSURE TO THE BRAKES, THE BRAKES FAILED. WHEN TOE BRAKES WERE RELEASED, MOMENTARILY BRAKES RETURNED TO NORMAL. PERFORMED MULTIPLE TIMES ALL A VERY SLOW SPEEDS, MOST OF THE TIME WHILE MOct 17, 2012 · N724QS · Gulstm 200 · Landing Gear Position and WarningSDR DXTA2012100805138Brake · burnedPERFORMED A NORMAL LANDING. DID NOT BREAK HARD AND DID NOT NOTICE ANY SIGNIFICANT ISSUES WHILE BREAKING. AFTER STOPPING, SAW A LOT OF SMOKE FROM THE NR 2 BRAKE ASSY. THE SMOKE STEADILY INCREASED FOR ABOUT 20 MIN. FIRE DEPT SCOPED THE LT ASSEMBLY AT 229 DEG Oct 6, 2012 · N723QS · Gulstm 200 · Landing Gear Brake SystemSDR DXTA2012090405114Valve · malfunctionedON LANDING, HAD TO APPLY MUCH MORE FORCE THAN NORMAL TO GET ANY EFFECTIVENESS OUT OF THE BRAKES. SLOWING THROUGH 80 KIAS THE BRAKES GRABBED EXTREMELY HARD, BUT EVENLY. IT GRABBED AND RELEASED AS IF THE ANTI-SKID WAS WORKING, BUT MORE VIOLENTLY. AFTER PARKINGSep 1, 2012 · N724QS · Gulstm 200 · Landing Gear Brake SystemSDR DXTA2012082405105Probe · overheatedHEAVY SULFUR ODOR IN COCKPIT WITH APU OPERATING WITH AVIONICS ON. ODOR IS NOT ASSOCIATED WITH ENVIRONMENTAL SYS. NO VISIBILE SMOKE WAS NOTICED. FOUND "PROBE HEAT" SWITCH IN OVERRIDE POSITION. THIS SETTING DELIVERS FULL POWER TO ALL PROBES AND TAKES THE AOAAug 24, 2012 · N701QS · Gulstm 200 · Pitot/Static Anti-Ice SystemSDR DXTA2012082105101Switch · out of adjustTHE GEAR HANDLE IS STUCK IN THE DOWN POSITION. APPLIED ABOUT 50 POUNDS OF FORCE, THE GEAR HANDLE DID NOT MOVE. AFTER CHANGING THE FLIGHT CONTROLS, THE OTHER PILOT TRIED WITH SAME RESULTS. ADJUSTED WOW SWITCHES. PERFORMED A SATISFACTORY OPS CHECK OF THE LANDAug 21, 2012 · N725QS · Gulstm 200 · Landing Gear Position and WarningSDR 9JLA2012073104410Computer · defectiveTHE CREW REPORTED DURING TAXI OUT, "RT FQMC FAIL" MESSAGE ILLUMINATED ALONG WITH RT WING FUEL QTY "0". IT EXTINGUISHED AFTER ABOUT 5 SECONDS SHOWING NORMAL READINGS. SHORTLY THEREAFTER "RT FEED TANK LOW" MESSAGE ILLUMINATED AND FEED TANK SHOWED 120LBS. THIS TJul 20, 2012 · N2HL · Gulstm 200 · Fuel Quantity IndicatorSDR DXTA2012072305056Compressor · contaminatedDURING TAXI OUT, BOTH CREW MEMBERS NOTED LIGHT SMOKE FOLLOWED BY AN OIL ODOR. APU WAS SUPPLYING BLEED AIR FOR ECS AT THE TIME. APU WAS IMMEDIATELY SHUTDOWN, ECS SELECTED TO BOTH (ENGINES) POSITION ON PANEL CONDITIONS DID NOT IMPROVE. RETURNED TO RAMP, AND SJul 20, 2012 · N755QS · Gulstm 200 · APU Core EngineSDR LM1R20120731002Carbon Seal · failedAFTER TAKEOFF, CREW NOTICED BURNING ODOR AND MIST IN CABIN. PERFORMED EMERGENCY RETURN TO DEPARTURE. FOUND OIL STREAKING IN EXHAUST AND FOD IN COMPRESSOR SECTION. ON TEARDOWN, NR 2 BEARING CARBON SEAL WAS FOUND FRACTURED WITH FRAGMENTS OF THE SEAL HAVING MIGJul 18, 2012 · N749QS · Gulstm 200 · Turbine Engine Oil SystemSDR DXTA201207190553Engine · odorAFTER TAKEOFF, SMELLED A BURNING SMELL AND THERE WAS WHAT APPEARED TO BE A MIST IN THE CABIN. PERFORMED AN EMERGENCY RETURN TO DEPARTURE. INSPECTED RT ENGINE AND FOUND EVIDENCE OF OIL IN THE EXHAUST DUCT AND COWLS. INSPECTED ENGINE INLET WITH BORESCOPE IAW Jul 18, 2012 · N749QS · Gulstm 200 · Engine (Turbine/Turboprop)SDR BKEA20120716001Actuator · malfunctionedAIRCRAFT DEPARTED FROM VAN NUYS AIRPORT (KVNY) GEAR WAS RETRACTED. LEFT MAIN GEAR FAILED TO RETRACT AFTER TAKEOFF (RED INDICATION) CYCLED GEAR THREE TIMES. ATC TOWER VERIFIED THAT LEFT MAIN GEAR APPEARED TO BE DOWN RETURNED AND LANDED AT KVNY.Jul 16, 2012 · N889MR · Gulstm 200 · Landing Gear ActuatorSDR 9JLA2012101904409Wire Harness · intermittentCREW REPORTED THE RT WING FUEL QUANITITY INTERMITTENTLY SHOWS DASHES ON THE INDICATOR. THE RT WING FUEL WIRE HARNESS WAS REMOVED AND A NEW HARNESS WAS INSTALLED. FUNCTIONAL CHECKED SATISFACTORY.Jul 15, 2012 · N2HL · Gulstm 200 · Fuel System WiringSDR DXTA2012080305074Web · gougedTHE MAIN ENTRY DOOR DAMPER LOWER ARM HAS BEEN CONTACTING WEB AT FS 5727 DURING NORMAL OPERATION OF MED, RESULTING IN GOUGES ON THE WEB AND A CRACK EMANATING FORWARD OT THE EDGE OF THE WEB. ARE REQUESTING AN ENGINEERING DISPO TO REPAIR THE WEB. IF A REPAIR DOJul 5, 2012 · N720QS · Gulstm 200 · Passenger/Crew DoorsSDR DXTA2012070605032Shutoff Valve · failedON TAKEOFF WITH T/O POWER SET, AT APPROX 400 FEET, WE HAD A CABIN DUCT OVERHEAT MESSAGE FOLLOWED BY COCKPIT DUCT OVERHEAT MESSAGE. IT WAS ASSOCIATED WITH EXTREMELY HOT TEMPS AND SMELL OF BURNING RUBBER. ELECTED TO RETURN TO FIELD. AFTER EXITING THE RUNWAY AJul 5, 2012 · N729QS · Gulstm 200 · Cabin Pressure Control SystemSDR DXTA2012062805021Eec · inoperativeIN FLIGHT, RECEIVED FADEC FAULTY ICAS MESSAGE AND EICAS COMPARITOR FAIL WITH YELLOW DASH LINES IN ITT. ABOUT 5 MINUTES LATER, FELT A LIGHT SHUTTER ASSOCIATED WITH THE ENGINE ROLLING BACK AND FAILED. AFTER ABOUT 30 SECONDS, ENGINE AUTO LIGHTED. NO ABNORMAL VJun 28, 2012 · N702QS · Gulstm 200 · Fuel Controlling SystemSDR DXTA2012060505017Proximity Switch · out of adjustON TAKEOFF, HAD A RED HASHED RT MAIN GEAR DIPLAY (GEAR HANDLE UP). CYCLED THE GEAR VIA THE CHECKLIST STILL HAD THE RED UNSAFE UP INDICATION. PUT GEAR HANDLE DOWN HAD GOOD SAFE GEAR INDICATION CONTINUED TO LANDING. ADJUSTED AFT UPLOCK PROX SWITCH ON THE RT GJun 25, 2012 · N740QS · Gulstm 200 · Landing Gear Position and WarningSDR DXTA2012062505017Indicator · intermittentON TAKEOFF, HAD A RED HASHED RT MAIN GEAR DIPLAY (GEAR HANDLE UP). CYCLED THE GEAR VIA THE CHECKLIST STILL HAD THE RED UNSAFE UP INDICATION. PUT GEAR HANDLE DOWN HAD GOOD SAFE GEAR INDICATION CONTINUED TO LANDING.Jun 25, 2012 · N740QS · Gulstm 200 · Landing Gear Position and WarningSDR DXTA2012060604992Pdu · failedDURING THE APPROACH, FLAPS STUCK AT 12 DEGREES. DIVERTED. ON LANDING, FAULT LIGHTS ILLUMINATED ON THE FSECU. (MOTOR, FAULT, ECU.) REMOVED FAULTY FLAP PDU AND INSTALLED REPAIRED FLAP PDU IAW CMP 275210. RAN FLAPS THRU 10 CYCLES WITH NO DEFECTS NOTED. OPSJun 6, 2012 · N748QS · Gulstm 200 · Trailing Edge Flap Control SystemSDR DXTA2012050404968Brake Assy · stiffUPON LANDING AND ROLL-OUT BRAKES WERE STIFF WITH INITIAL APPLICATION. BRAKES DID NOT GRAB. WITH MAX BRAKING EFFORT APPLIED ACFT SHOULD HAVE HAD A MORE POSITIVE DECELERATION. PERFORMED NORMAL BRAKE BLEEDING PROCEDURE. CHECKED BRAKE HYD PRESSURES, IAW NORMALMay 3, 2012 · N723QS · Gulstm 200 · Landing Gear Brake SystemSDR DXTA2012042504960Actuator · inoperativeAFTER LANDING GEAR RETRACTION, RT LANDING GEAR INDICATION DISPLAYED A RED ON THE ICAS DISPLAY. THERE WAS A NOTICABLE VIBRATION. REFERENCED QRH, PUT GEAR DOWN AND DISPLAYED THREE GREEN. LANDED NORMALLY. REMOVED RT MLG SIDEBRACE ACTUATOR AND INSTALLED IAW CMApr 24, 2012 · N755QS · Gulstm 200 · Landing Gear Retraction/Extension SystemSDR 9JLA2012032104403Actuator · defectiveTHE CREW REPORTED THAT THE TE FLAPS FAILED TO RETRACT FROM THE 12 DEGREE POSITION AFTER TAKEOFF. TROUBLESHOOTING IDENTIFIED THE RT NR 3 FLAP ACTUATOR AS DEFECTIVE. INSTALLED AN O/H UNIT. OPS CHECKED SATISFACTORY.Mar 16, 2012 · N2HL · Gulstm 200 · Trailing Edge Flap ActuatorSDR DXTA2012031604922Altimeter · inoperativeAFTER DEPARTURE AT APPROX 3000" IN CLIMB, RED GEAR NOT DOWN CAS MESSAGE CAME ON ALONG WITH GEAR HORN. BOTH RADAR ALTIMITERS FLUCUATED WITH A RANGE OF RA ALTITUTDES MUTIPLE TIMES, EVENTUALLY THE LT RA SHOWED 0 FOR THE REMAINDER OF THE FLIGHT WHILE THE RIGHT RAMar 15, 2012 · N730QS · Gulstm 200 · Ground Proximity SystemSDR DXTA2012031404919Receptacle · damagedON THE GROUND WITH APU RUNNING, POWERED UP THE PERSONAL VIDEO MONITORS TO DISPLAY THE AIRSHOW. AFTER ABOUT 3 TO 5 MINUTES, NOTICED THE MONITOR AT SEAT NR 2 POSITION FLICKERED, THEN WENT BLANK AND IT BEGAN TO EMANATE AN ELECTRICAL BURNING ODOR FROM CONNECTIONMar 13, 2012 · N726QS · Gulstm 200 · Communications System WiringSDR DXTA2012031204915Strut · damagedWHEN NLG RETRACTED, HEARD A LOUD THUMP. SOUNDED ALMOST LIKE A BASEBALL BAT HITTING A BASEBALL. AT THIS TIME RECEIVED BOTH RT AND LT PITOT HEAT AND TAT PROBE HEAT AMBER MESSAGES. MESSAGES WENT OUT WHEN PROBE HEAT SWITCH IS TO OVERIDE, BUT MESSAGES ILLUMINATE WMar 10, 2012 · N729QS · Gulstm 200 · Nose/Tail Landing Gear Strut/AxleSDR DXTA2012030504905Unknown · odorAFTER STARTING APU, A STRONG ELECTICAL BURNING ODOR DETECTED. APU TURNED TO RAM AIR, COULD NOT DETECT BURNING ODOR. SHUTDOWN ACFT. INSPECTED ACFT, NO DEFECTS NOTED.Mar 5, 2012 · N707QS · Gulstm 200 · Air Distribution SystemSDR DXTA2012030104893Selector Valve · inoperativeON GEAR EXTENSION, RECEIVED GREEN LIGHTS FOR THE LT MAIN AND NOSE GEAR BUT THE RT MAIN INDICATED YELLOW FOR APPROX 20 SECONDS FOLLOWED BY A RED "UNSAFE" INDICATION FOR ABOUT 30 SECONDS. ALSO SHOWED THE RT ANTI-SKID SYS INOPERATIVE. RT MAIN GEAR LIGHT THEN Feb 29, 2012 · N700QS · Gulstm 200 · Landing Gear Retraction/Extension SystemSDR 2012FA0000262Bolt · looseFLIGHT CREW DISCOVERED, DURING PREFLIGHT INSPECTION THAT THE RT ENGINE FAN DISK SPINNER ATTACH BOLT, PN 31B0162-01 HAD COME LOOSE FROM THE TIE ROD. RECORDS SEARCH REVEALED THAT THE FAN DISK HAD NOT BEEN REMOVED SINCE NEW. MX REPLACED BOLT AND LOCK WASHER WITFeb 28, 2012 · N200KN · Gulstm 200 · Fuel Controlling SystemSDR DXTA2012022004881Brake Sys · weakWHILE APPLYING BRAKES ON LANDING, REQUIRED CONSIDERABLY MORE PRESSURE ON THE PEDALS TO ACHIEVE DESIRED AMOUNT OF BRAKING. R & R NR 1 OTBD BRAKE ASSY WITH AN INSPECTED UNIT. BLED SYS, OPS CHECKED SATISFACTORY IAW CMP.Feb 19, 2012 · N706QS · Gulstm 200 · Landing Gear Brake SystemSDR DXTA2012021304873Landing Gear · malfunctionedAFTER TAKE OFF, RT MLG WOULD NOT LOCK IN THE UP POSITION. PERFORMED QRH PAGE EG-6 CHECK LIST. MEASURED UPLOCK ROLLER AND PROX SWITCH CLEARANCE. NO DEFECTS NOTED. CLEANED ALL CONNECTOR PLUGS AND VERIFIED LOCKING PRESSURE WITH NO DEFECT NOTED. PERFORMED LUBRFeb 10, 2012 · N716QS · Gulstm 200 · Landing Gear Retraction/Extension SystemSDR DXTA2012013004856Warning Light · illuminatedDURING CLIMB OUT, GEAR UP & LOCKED, SLATS & KRUEGERS OUT, RECEIVED AN "AUX HYD PUMP ON" MESSAGE EACH TIME, POWERED ABOVE MAX CRUISE. BETWEEN 8 & 10,000 & AIRSPEED BETWEEN 180 & 235. BROUGHT SLATS & KRUEGERS UP, COULD NOT REPRODUCE PROBLEM. SWAPPED LT & RT Jan 27, 2012 · N711QS · Gulstm 200 · Hydraulic System, MainSDR DXTA2012012704855Unknown · odorAFTER TAKEOFF ELECTRICAL ODOR IN CABIN. AFTER TURNING OFF CABIN/ GALLEY POWER NO CHANGE. NOTICED LIGHT HAZE IN CABIN MOVING FORWARD. SELECTED ECS TO RT, THEN LT NO CHANGES. SELECTED ECS RAM AND HAZE CLEARED. RAN ENGINES AT MAX CRUISE POWER FOR 20 MINUTES EAJan 26, 2012 · N719QS · Gulstm 200 · Air Distribution SystemSDR DXTA2012012604853Generator · burnedIN FLIGHT, THE LT GENERATOR INDICATED 201 AMPS AND THE RT GENERATOR INDICATED 137 AMPS. THIS IS TWICE THE NORMAL TOTAL LOAD FOR THE ACFT. THIS IS A REPEAT WRITE UP. ON APPROACH THERE WAS A FAINT "BURNED WIRE SMELL". WE TURNED OFF THE BAGGAGE HEAT AND CABIN Jan 23, 2012 · N722QS · Gulstm 200 · DC Generating System
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