Beech 200

Service difficulty reports · 521

Newest first. General aviation reporting is voluntary.

Query with SQL
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 DXTA200803056Connector · contaminatedAFTER TAKEOFF, RT MLG WOULD NOT RETRACT WHEN GEAR WAS SELECTED UP.May 12, 2008 · N752QS · Gulstm 200 · Landing Gear System WiringSDR DXTA200803042Engine · vibrationCLIMBING THROUGH 12,000 FEET HEARD A LOUD BANG, THE RIGHT ENGINE, VIB INDICATOR TURNED YELLOW AND CLIMBED ABOVE THE 3RD TICK MARK ON THE RIGHT ENGINE. THE ENG LOST SOME OIL PRESSURE BUT STAYED IN THE GREEN. ALL OTHER PARAMETERS STAYED IN THE GREEN. ENG HAD May 4, 2008 · N723QS · Gulstm 200 · Engine (Turbine/Turboprop)SDR DXTA200803024Display · malfunctionedCO-PILOT'S MFD WENT IN-OP IN FLT WITH A BURNING SMELL. REMOVED DISPLAY & INSTALLED PER CMP 342304 GAC SAV W/O 142032 SQUAWK 6.1 OPS CHECK GOOD NO DEFECTS NOTED.Apr 25, 2008 · N719QS · Gulstm 200 · Central DisplaySDR DXTA200803006Actuator · out of adjustSLATS FAILED TO RETRACT SLAT UNBALANCED AND FLAP/SLAT MAINT CAS MESSAGES PRESENT. ADJUSTED RT NR 2 SLAT BALLSCREW ACTUATOR OK TO CONTINUE SERVICE. NO DEFECTS NOTED.Apr 20, 2008 · N712QS · Gulstm 200 · Leading Edge Slat ActuatorSDR DXTA200802998Engine · overservicedSHORTLY AFTER ROTATION THERE WAS AND OVERWHELMING ODOR SIMILAR TO BURNED RUBBER. INSPECTED LT & RT ENGINES FOR ABNORMAL CONDITIONS, INSPECTED ECS SYS, FOUND NO DEFECTS. TECHS PERFORMED ENGINES RUN. AN ODOR LIKE BURNED OIL FROM LT ENGINE AT BOTH LOW & HIGH POWEApr 14, 2008 · N708QS · Gulstm 200 · Turbine Engine Oil SystemSDR DXTA200802991Brake Assy · weakMAIN BRAKES REQUIRE EXCESSIVE PRESSURE ON TOE BRAKES TO SLOW OR STOP ACFT. REMOVED AND REPLACED NR 2 BRAKE REF MM 32-40-21 REF CMP 324302 COMPLIED WITH BRAKE BLEED AND OPS CHECK REF CMP 324005 AND 324017.Apr 12, 2008 · N731QS · Gulstm 200 · Landing Gear Brake SystemSDR DXTA200802986Actuator · malfunctionedAFTER TAKEOFF ELEVATOR FEEL FAIL MESSAGE CAME ON. REMOVED DEFECTIVE Q-FEEL ACTUATOR AND INSTALLED NEW Q-FEEL ACTUATOR P/N 4012-0000-000 S/N IL-217 ALL WORK DONE IAW MM 27-30-10.Apr 7, 2008 · N708QS · Gulstm 200 · Central WarningSDR DXTA20082986Warning Message · illuminatedAFTER TAKEOFF, ELEVATOR FEEL FAIL MESSAGE CAME ON.Apr 7, 2008 · N708QS · Gulstm 200 · Central WarningSDR DXTA200802970Slat · malfunctionedON DEPARTURE, GOT FLAP/SLAT MAINT MESSAGE. SLATS DID NOT COME ALL THE WAY UP. PERFORMED FUNCTIONAL TEST OF THE FLAP/SLAT CONTROL AND DRIVE SYS WITH NO DEFECTS NOTED AT THIS TIME. ALL WORK COMPLETED IAW CMP 275101.Mar 30, 2008 · N707QS · Gulstm 200 · Leading Edge Slat Control SystemSDR DXTA20082970Slat System · malfunctionedON DEPARTURE, GOT FLAP / SLAT MAINT MESSAGE. SLATS DID NOT COME ALL THE WAY UP. PERFORMED FUNCTIONAL TEST OF THE FLAP/SLAT CONTROL AND DRIVE SYSTEM WITH NO DEFECTS NOTED AT THIS TIME. ALL WORK COMPLETED IAW CMP 275101.Mar 30, 2008 · N707QS · Gulstm 200 · Leading Edge Slat Control SystemSDR DXTA200802966Fseu · inoperativeLEAVING, AFTER GEAR RETRACTION, SELECTED FLAPS TOP 0 DEG AND FLAPS WOULD NOT RETRACT FROM 20 DEG. REMOVED ORIGINAL FSECU AND INSTALLED INSPECTED UNIT. PERFORMED SATISFACTORY RIG AND OPS CHECK OF FLAP SLAT SYSTEM. FOR ALL WORK REF MM 27-51-00, 27-50-05 AND 27-Mar 27, 2008 · N708QS · Gulstm 200 · Trailing Edge Flap Control SystemSDR DXTA20082966Control Unit · inoperativeLEAVING TQPF AFTER GEAR RETRACTION, SELECTED FLAPS TOP 0 DEG AND FLAPS WOULD NOT RETRACT FROM 20 DEG. REMOVED ORIGINAL FSECU AND INSTALLED INSPECTED UNIT. PERFORMED SATISFACTORY RIG AND OPS CHECK OF FLAP SLAT SYSTEM. FOR ALL WORK REF MM 27-51-00, 27-50-05 ANDMar 27, 2008 · N708QS · Gulstm 200 · Trailing Edge Flap Control SystemSDR DXTA20082955Fuse · failedAFTER ENGINE START (BOTH ENGINES STARTED) WITH ECS SELECTOR STILL IN (RAM), APU FIRE WARNING MESSAGE ILLUMINATED. T/S FOUND BLOWN FUSE 405. REPLACED FUSE WITH NEW PART. OPS CHECK GOOD. IAW MM 26-10-25.Mar 21, 2008 · N755QS · Gulstm 200 · Fire DetectionSDR DXTA20082944Autopilot Sys · failedAUTO PILOT PITCH FAILED. PERFORMED HORIZONTAL STABILIZER TRIM SYSTEM INTERFERENCE TEST, TRAVEL TEST, AND FUNCTIONAL TEST I.A.W. G200 M.M. 27-40-00. OPS CHECK GOOD.Mar 16, 2008 · N719QS · Gulstm 200 · Autopilot SystemSDR DXTA20082943Warning Light · illuminatedON TAKEOFF ROLL AT APPROX 60 KIAS, WE GOT A L. BLEED PRESS/TEMP HI CAS. PERFORMED APU & ENGINE RUNS WITH BLEEDAIR SELECTED ON BOTH ENGINES WITH NO DEFECTS NOTED. THEN PERFORMED BLEED AIR SELECTED ON APU WITH NO DEFECTS NOTED AT THIS TIME WITH ENGINES & APU RUMar 16, 2008 · N702QS · Gulstm 200 · Central WarningSDR DXTA20082940Circuit Breaker · trippedCLIMBING THROUGH FL 3111 I HEARD A CB POP, FOLLOWED BY NUMEROUS EICAS CAUTION AND WARNING MESSAGES. TROUBLESHOT SYSTEM, FOUND CB135P EMERGENCY BUSS BATTERY CB (60 AMP) TO BE DEFECTIVE. REPLACED CB135P AND PERFORMED GCU OPERATIONAL TEST AND DC LOAD SHEDDING OPMar 15, 2008 · N708QS · Gulstm 200 · Electrical Power SystemSDR DXTA20082934Brake · weakBRAKES ARE VERY SOFT AND WONT GRAB ON LANDING ROLLOUT UNTIL ABOUT 30 KNOTS (BOTH CAPTAIN AND PILOT SIDES). BLED BRAKES AFTER INSPECTION FOUND BRAKES WERE WITHIN TOLERANCE. NO AIR NOTED AT THIS TIME. WORK DONE IAW MM 32-40-20.Mar 12, 2008 · N703QS · Gulstm 200 · Landing Gear Brake SystemSDR DXTA20082925Adapter · dirtyON APPROACH TO ASE, SELECTED GEAR DOWN AND GOT RED HASH MARKS ON NOSE GEAR. TROUBLESHOT SYSTEM FOUND ON VISUAL INSPECTION OF NOSE GEAR TOW ADAPTOR WOULD NOT SPIN TO THE DOWN POSITION. REMOVED TOW ADAPTOR, CLEANED DEBRIS, LUBED, INSTALLED, OPS CHECK GOOD. CMar 8, 2008 · N752QS · Gulstm 200 · Nose/Tail Landing GearSDR DXTA20082916Actuator · leakingAFTER TAKEOFF AND ON SPEED, RETRACTED KRUEGERS FROM FLAPS UP POSITION TO KRUEGER/SLATS UP POSITION. THE KRUEGER UNBAL CAS MSG ILLUMINATED WITH KRUEGER POINTER INDICATOR YELLOW. FOUND THE RT KRUEGER ACTUATOR TO BE LEAKING. REMOVED ACTUATOR AND REPLACED WITH INMar 5, 2008 · N706QS · Gulstm 200 · Leading Edge Slat Control SystemSDR DXTA20082887Control Unit · inoperativeON DEPARTURE, RECEIVED (KRUEGER IMBALANCE) CAS MESSAGE. REMOVED AND REPLACED FLAP/SLAT ELECTRIC CONTROL UNIT. PERFORMED FUNCTIONAL TEST WITH NO DEFECTS NOTED. ALL WORK DONE IAW MM CHAPTER 27-51-45 AND CHAPTER 27-52-00. (SQK NR 1.4)Feb 18, 2008 · N706QS · Gulstm 200 · Leading Edge Slat Control SystemSDR DXTA20082872Tire · failedUPON LANDING, THE RT MAIN TIRES BLEW AND DISINTEGRATED AND DAMAGED THE RIMS AND GEAR DOOR. REPLACED ALL 4 MLG WHEEL ASSEMBLIES IAW THE G200 CMP'S NR`S 324201, 324202, 324203 AND 324204.Feb 13, 2008 · N723QS · Gulstm 200 · TireSDR DXTA200802858Fuse · failedAPU FIRE CAS MESSAGE ILLUMINATED ALONG WITH FIRE BELL ENROUTE AT FL380. RT FIRE BOTTLE WAS DISCHARGED INTO APU. FIRE INDICATION REMAINED ON, DIVERTED. AFTER SHUTTING DOWN AND EXITING AC, NO SMOKE, FLAMES OR SOOT WERE VISIBLE IN THE AREA OF THE APU BUT THE APU Feb 10, 2008 · N729QS · Gulstm 200 · Fire DetectionSDR DXTA200802844Air Duct · contaminatedWITH THE APU ON THE COCKPIT FILLED WITH JET FUEL FUMES STRONG ENOUGH TO BURN YOUR EYES. FOUND AIR COND. DUCTS UNDER CABIN FLOOR TO BE FUEL SOAKED. REMOVED FUEL SOAKED DUCTS AND INSTALLED INSPECTED DUCTS, LEAK AND OPS CHECKED OK. IAW G200 MM 25-00-00. NO ODOR Feb 7, 2008 · N707QS · Gulstm 200 · Air Distribution SystemSDR DXTA200802840Switch · inoperativeDURING T/O ROLL WITH THROTTLES AT T/O DETENT THE BLEED PRESS/TEMP HIGH MSG ILLUMINATED. THE T/O WAS ABORTED. M2B- REMOVED FWD OVERTEMP SWITCH P/N 641180-1 S/N 0245 AND INSTALLED NEW FWD OVERTEMP SWITCH P/N 641180-1 S/N 0368. REMOVED AFT OVERTEMP SWITCH P/N 641Feb 5, 2008 · N728QS · Gulstm 200 · Air Distribution SystemSDR DXTA200802800Control Unit · malfunctionedSLATS FAILED TO RETRACT, CAS MSG: SLAT UNBALANCED, SLAT FLAP MAINTAIN. FLAPS/SLATS FUNCTIONAL TEST GOOD. PERFORMED FSECU BITE CHECK. NO FAULTS FOUND.Jan 26, 2008 · N712QS · Gulstm 200 · Leading Edge Slat Control SystemSDR DXTA200802776Connector · defectiveAFTER TAKEOFF AT MLG AMBER AND RED HASHES FLASHED ON AND OFF THRU ENTIRE FLIGHT. REPLACED RT MLG CONNECTOR 44G1 USING CONNECTOR P/N D38999/24WB98SN. BACKSHELL P/N TX1240AB90-1006A1 AND BOOT 202S132-25S. WORK IAW ENG ORDER DOC 4AS8104002 A013REV. PERFORMED RTJan 21, 2008 · N752QS · Gulstm 200 · Landing Gear System WiringSDR DXTA200810073297Actuator · inoperativeAFTER TAKEOFF GOT INDICATION ON RT MAIN GEAR TRANSIT (RED) NOT LOCKED UP. IAW CHECKLIST, SLOWED PLANE DOWN, LOWER GEAR GOT 3 GREEN. RAISED GEAR AGAIN, RT MAIN STAYED GREEN, LT AND NOSE UP AND LOCKED. ALSO GOT ANTI-SKID LIGHT THIS TIME WITH THE GEAR. FELT LIKE Jan 7, 2008 · N716QS · Gulstm 200 · Landing Gear ActuatorSDR DXTA200802747Squat Switch · malfunctionedGROUND AIR BRAKES DEPLOYED ON FINAL APPROACH WHEN THE SWITCH WAS ARMED. R & R LT MLG WOW SWITCH AND HARNESS IAW AMM 32-60-05. OPERATIONAL & FUNCTIONAL CHECK GOOD WITH NO FURTHER DEFECTS NOTED.Jan 4, 2008 · N749QS · Gulstm 200 · Landing Gear Position and WarningSDR DXTA200702677Control Valve · bypassingAC PULLS RT WITH NEUTRAL TILLER POSITION. NWS DISENGAGES WHEN ATTEMPTING FULL RT TURN. REMOVED AND REPLACED NOSEWHEEL STEERING CONTROL VALVE. AND ADJUSTED FEEDBACK MANIFOLD POTENTIOMETERS 1 AND 2 IAW GAC G200 AMM 32-50-00 AND 32-50-15.Dec 14, 2007 · N718QS · Gulstm 200 · Landing Gear Steering SystemSDR CA071128015Valve · malfunctioned(CAN) PILOT REPORTED PARK BRAKE SET AND INDICATED ON EICAS. STARTED RT ENGINE WITH THE CHOCKS REMOVED, READY FOR DEPARTURE. THE AIRCRAFT ROLL FWD AFTER THE ENGINE WAS STARTED. PILOT CHECKED THE INDICATION ON EICAS AND THE INDICATION WAS STILL ON EICAS PARK BRANov 26, 2007 · Gulstm 200 · Landing Gear Brake SystemSDR CA071127010Connector · contaminated(CAN) AIRCRAFT LANDED, PILOT REPORTED NO NOSE WHEEL STEERING. PARKED AIRCRAFT AT FBO. LATER A/C WAS TAKEN TO MFG. THE NOSE WHEELING SYSTEM WAS INSPECTED AND MOISTURE WAS FOUND IN THE FEEDBACK POTENTIOMETER CONNECTOR PLUG. CLEANED AND RECONNECTED CONNECTOR PLUGNov 23, 2007 · Gulstm 200 · Landing Gear System WiringSDR DXTA200702617Warning Light · illuminated"RT BLEED AIR LEAK" WOULD NOT EXTINGUISH INFLIGHT AND RT ENGINE SHUTDOWN INFLIGHT. "RT BLEED AIR LEAK" MESSAGE REMAINED ON AFTER ENGINE SHUTDOWN. R & R RT FWD & AFT LEAK DETECTION ELEMENTS IAW MM 21-61-60. OPS CHECKED SATISFACTORY.Nov 18, 2007 · N706QS · Gulstm 200 · Pneumatic Distribution SystemSDR DXTA200702614Skin · damagedDURING LANDING AND AFTER TOUCHDOWN, THE AIRCRAFT DEPARTED THE LT SIDE OF THE RUNWAY. DAMAGE NOTED ON THE LOWER IB SECTION OF THE RT WING, DAMAGE NOTED ON THE RT WING IB LEADING EDGE, AND DAMAGE NOTED ON THE RT KRUEGER FLAP.Nov 17, 2007 · N701QS · Gulstm 200 · Wing, Plate/SkinSDR CA071108006Actuator · failed(CAN) AFTER TAKEOFF THE CREW REPORTED THAT THE GEAR WAS SELECTED UP AND THE NOSE AND RT MAIN GEAR RETRACTED WITH NO FAULT, THE LT GEAR DID NOT RETRACT. THE CREW REPORTED THEY CYCLED THE GEAR DOWN AND THE (3) GREEN LIGHTS WAS ON EICAS INDICATING DOWN AND LOCK.Nov 7, 2007 · Gulstm 200 · Landing Gear ActuatorSDR DXTA200702588Starter Gen · inoperativeRT GENERATOR FAILED AFTER TAKEOFF POWER , R/T GEN WOULD NOT STAY RESET NOR HOLD AMP LOAD NOR VOLTS, TO ABORTED. REMOVED AND REPLACED RH STARTER GEN PER G200 MM 24-30-06. OPS CHECK GOOD PER G200 MM 24-30-00Nov 1, 2007 · N718QS · Gulstm 200 · Starter-GeneratorSDR DXTA200702570Thermal Switch · inoperativeJUST AFTER ENGINE RUN-UP GOT LINE PRESSURE HIGH/OVER TEMP WARNING ILLUMINATED. WHEN THROTTLES REDUCED TO IDLE, LIGHT WENT OUT. PERFORMED ENGINE RUN, NO DEFECTS NOTED. CHECKED HP PRSOV VALVES NR 1 & 2 ENGINE; PRESSURE FROM NR 1 ENG HP PRSOV VALVE 25 PSI AND NOct 24, 2007 · N702QS · Gulstm 200 · Pneumatic Indicating SystemSDR DXTA200702555Brake · wornNORMAL BRAKES INEFFECTIVE ON LANDING ROLLOUT. FOUND NR 1 BRAKE ASSY WORN. REMOVED AND REPLACED NR 1 BRAKE ASSY WITH REPAIRED UNIT IAW G-200 CMP CARD NR: 324301. PERFORMED NORMAL BRAKE SYSTEM BLEEDING IAW G-200 MM CHAPTER 32-40-20. OPS CHECK AND LEAK CHECK SATOct 19, 2007 · N703QS · Gulstm 200 · Landing Gear Brake SystemSDR CA071106001Windshield · broken(CAN) PILOT REPORTED RT WINDSHIELD CRACKED ON RETURN. C/O INSPECTION ON RT WINDSHIELD AND COULD NOT FAULT THE WINDSHIELD. THE AIRCRAFT WAS RELEASE FOR RETURN TO SERVICE. THE AIRCRAFT MADE (3) OTHER TRIPS. THE PILOTS REPORTED THE SAME CRACK ON THE RT WINDSHIELDOct 17, 2007 · Gulstm 200 · Flight Compartment WindowsSDR DXTA200702536Slat System · malfunctionedAFTER DEPARTURE AT APPROPRIATE SPEED, WE SELECTED SLATS UP, KRUEGERS RETRACTED SLATS WENT TO AN INTERMEDIATE POSITION. FLAP/SLAT OPS CHECK I/A/W G200 MM 27-51-45 NO DEFECTS NOTED.Oct 11, 2007 · N712QS · Gulstm 200 · Leading Edge Slat Control SystemSDR BKE2007F00000Drain Line · crackedWHILE FLYING AT FLIGHT LEVEL 370, THE PILOTS WERE NOT ABLE TO MOVE THE AILERON CONTROLS. THE AIRCRAFT DESCENDED TO A LOWER ALTITUDE AND THE AILERON CONTROLS FUNCTIONED NORMALLY. THE AIRCRAFT UPON RETURN TO HOME BASE WAS INSPECTED. IT WAS DETERMINED THAT WATSep 14, 2007 · N322AD · Gulstm 200 · Potable Water SystemSDR DXTA200702363Slat System · out of rigSLATS WOULD NOT RETRACT ALL THE WAY THEY ARE STUCK IN THE MIDDLE . SEVERAL FAULTS ON THE FSEU. [08-23-07] COMPLIED WITH RIGGING BOX FUNCTION CHECK AS OUTLINED IN GULFSTREAM G200 MM 27-50-05 & FOUND FLAP/SLAT SYSTEM TO FUNCTION NORMALLY ON GROUND AT THIS TIMJul 29, 2007 · N752QS · Gulstm 200 · Leading Edge Slat Control SystemSDR DXTA200702291Fire Loop · malfunctionedAPU FIRE INDICATION ON GROUND. BLEW BOTTLE INTO APU DURING CHECKLIST. RT FIRE BOTTLE IS EMPTY. [07-12-07] REMOVED TAIL CONE AND INSPECTED APU FOR DAMAGE. FOUND NO DAMAGE. REMOVED APU FIRE DETECT LOOP AND INSTALLED A NEW GAC FURNISHED BOTTLE. PERFORMED SATJun 23, 2007 · N728QS · Gulstm 200 · Fire DetectionSDR DXTA200702207Unknown · unknownAIRCRAFT WOULD NOT ROTATE WITH STICK FULL AFT. (M2B) PERFORMED HIGH ENERGY STOP INSPECTION REF MM 5-50-01, NO DEFECTS NOTED. MEASURED ELEVATOR UP AND DOWN TRAVEL, TRAVEL NORMAL. ELEVATORS MOVED WITH EASE. PERFORMED ELEVATOR CONTROL SYSTEM TRAVEL TEST AND FOUNDMay 20, 2007 · N725QS · Gulstm 200 · Flight Control SystemSDR DXTA200702191Wire · brokenRT MLG RED INDICATION IN FLIGHT W/GEAR NOT SELECTED DOWN. IT OCCURRED DESCENDING THROUGH 9000 FT. AT 250 KIAS. ACCOMPANIED BY RED GEAR SPEED LIMIT INDICATIONS. M2B- FOUND A BROKEN WIRE AND WATER IN THE BACKSHELL OF WHEEL WELL DISCONNECT 44GJ1. RE-PINNED CONNEMay 13, 2007 · N718QS · Gulstm 200 · Landing Gear System WiringSDR DXTA200702184Proximity Switch · out of rigRIGHT MAIN LANDING GEAR RED INDICATION IN FLIGHT WITH GEAR NOT SELECTED DOWN. INDICATION APPEARED SLOWING BELOW 300 KTS. T/S PROBLEM NOTED RIGHT GEAR DOOR BOX SWITCH TO BE OUT OF RIG. ADJUSTED DOOR PROX SWITCH & PERFORMED OPS CHECK, WITH NO DEFECTS NOTED.May 10, 2007 · N718QS · Gulstm 200 · Landing Gear Position and WarningSDR DXTA200702149Monitor · inoperativeDURING POST FLIGHT, EVALUATING INOP VIDEO MONITOR SCREEN. SCREEN WAS MOVED TO VIP STATION TO DETERMINE IF MONITOR CONNECTOR WAS CONNECTED OR MONITOR ITSELF WAS INOPERATIVE. IMMEDIATELY AFTER MONITOR WAS PLUGGED IN AT VIP SEAT SMOKE WAS NOTED AT THE CONNECTIONApr 26, 2007 · N705QS · Gulstm 200 · Indicating/Recording SystemSDR DXTA200702137Unknown · odorACRID ELECTRICAL BURNING SMELL EMINATING FROM BEHIND LT PILOT SEAT IN COCKPIT. CHECKED ALL CB'S, NOTHING FOUND (POPPED). [4-27-07] PERFORMED ENG RUN AND APCS RUNS FOR COCKPIT SMELLS, RUNS SATISFACTORY. ACCESSED L/R RELAY PANEL FOUND SATISFACTORY. ACCESSED FWApr 24, 2007 · N701QS · Gulstm 200 · Air Distribution SystemSDR DXTA200702108Warning System · unknownLT ENG BLEED AIR LEAK, RED WARNING MESSAGES ILLUMINATED IN FLT-QUICK REF HANDBOOK PROCEDURES FOLLOWED IAW EH-3 BLEED AIR LEAK CHECKLIST. LT BLEED AIR LEAK REMAINED ON SO LT ENGINE SHUTDOWN IAW CHECKLIST. REMOVED DUCT COMING OFF PRSOU VALVE, REPLACED O-RINGS REApr 15, 2007 · N708QS · Gulstm 200 · Pneumatic Indicating SystemSDR DXTA200702086Fire Warning · unknownAT FL-380 APU FIRE WARNING ILLUMINATED, RAN QRH CHECKLIST FIRED APU FIRE BOTTLE INDICATION DID NOT GO OUT. LANDED AT NEAREST AIRPORT. REPLACED APU FIRE DETECTOR P/N 3001-148-450-9, S/N 86516 WITH INSPECTED DETECTOR P/N 3001-148; S/N 87592 IAW G200 AMM SECTIONApr 5, 2007 · N729QS · Gulstm 200 · Fire DetectionSDR DXTA200702061Actuator · intermittentSELECTED GEAR DOWN, THE RT MLG DID NOT SHOW DOWN & LOCKED WITH A RED INDICATION PRESENT. ON FINAL, CYCLED MLG 1 MORE TIME & INDICATION THE SAME. FLY BY TOWER & TOLD THAT THE MLG LOOKED TO BE NORMAL. ON DOWNWIND LEG AT 1500 FT AGL RED LIGHT WENT OUT & GREEN LIMar 31, 2007 · N706QS · Gulstm 200 · Landing Gear Actuator
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