# Service difficulty reports: Laser 200

A list on [Laser 200](https://openairdocs.org/model/laser-200.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 11 · 521 reports

- [SDR 2026FA0000014](https://openairdocs.org/sdr/2026FA0000014.md): Blade · broken · Jan 5, 2026 · N990JT · Gulstm 200 · Turbine Section
  > CREW HEARD A LOUD POP AND #1 ENGINE VIBRATION WENT INTO YELLOW ON INDICATOR. CREW SHUT DOWN ENGINE WITH NO FURTHER INCIDENT. HAD ENGINE BORESCOPED AND FOUND A HPT 2 BLADE HAD BROKEN
- [SDR 9JLA 202506250001](https://openairdocs.org/sdr/9JLA%20202506250001.md): Control Panel · failed · Jun 25, 2025 · N200QA · Gulstm 200 · Auto Flight System
  > YAW DAMP FAIL
- [SDR 2025FA0000066](https://openairdocs.org/sdr/2025FA0000066.md): Cable · broken · Jan 29, 2025 · N383JP · Gulstm 200 · Landing Gear System
  > DURING A PHASE 4 INSPECTION ON OUR KING AIR 200 N383JP, IT WAS DISCOVERED THAT THE MANUAL GEAR DOWN ACTUATION LEVER WOULD NOT OPERATE. UPON INSPECTION, IT WAS DETERMINED THAT THE ACTUATING LEVER CABLE GOING FROM THE ACTUATION LEVER TO THE LANDING GEAR GEARBOX
- [SDR QMLA2024072920093](https://openairdocs.org/sdr/QMLA2024072920093.md): Spacer · out of limits · Jul 25, 2024 · N969MA · Gulstm 200 · Power Lever
  > THROTTLE LINKAGE SPACER OUT OF POSITION CAUSED THE PROPELLER TO TRY TO GO INTO BETO RANGE EARLY DURING FINAL APPROACH TO RWY 18R AT KLRD. SPACER WAS LATER ADJUSTED PROPERLY, GROUND ENGINE RUN WAS NORMAL. ACFT RETURNED TO SERVICE 26 JULY 24.
- [SDR 2023FA0000856](https://openairdocs.org/sdr/2023FA0000856.md): Unknown · unknown · Dec 30, 2023 · N162GB · Gulstm 200 · Empennage Structure
  > DURING G200 ECS ZONAL INSPECTION SEVERAL FASTENERS FOUND DISCOLORED WITH POSSIBLE EVIDENCE OF ARCING IN ECS COMPARTMENT AT STN;14783MM,FRAME 51 (FWD. BEAM PYLON CAP) PN 4AS3177202-001
- [SDR JGVR202306062001](https://openairdocs.org/sdr/JGVR202306062001.md): Rod · damaged · Jun 6, 2023 · N199DF · Gulstm 200 · Elevator Control System
  > GULFSTREAM G200 S/N 128: DISCOVERED ELEVATOR UP TRAVEL WAS SHORT APPROXIMATELY 2 DEGREES OF MOVEMENT. THE SPRING ROD WAS DISCONNECTED AND ELEVATORS WERE FOUND TO FULLY MOVE THROUGH RANGE OF TRAVEL. UPON REMOVAL OF AFFECTED SPRING ROD THE SMALL END FELL OUT OF
- [SDR 2023FA0000266](https://openairdocs.org/sdr/2023FA0000266.md): Switch · failed · May 17, 2023 · N773KS · Gulstm 200 · Engine Thrust Reverser
  > THE LH T/R WAS PLACED ON MMEL BY A LETTER FROM GULFSTREAM. GULFSTREAM AND NORDAM DOES NOT HAVE STOCK ON THE SWITCH NEEDED TO FIX THE T/R SYSTEM.
- [SDR 9JLA2023052219508](https://openairdocs.org/sdr/9JLA2023052219508.md): Antenna · defective · Apr 18, 2023 · N991RL · Gulstm 200 · Communications System
  > THE FLIGHT CREW REPORTED THAT THE #2 COMM WOULD NOT TRANSMIT IN FLIGHT. THE MAINTENANCE PROVIDER REMOVED THE FAULTY VHF COMM 2 ANTENNA AND INSTALLED AN OVERHAULED ANTENNA. OPS CHECKS OK, AND THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR 9JLA2023041437810](https://openairdocs.org/sdr/9JLA2023041437810.md): Battery Pack · overheated · Apr 1, 2023 · N1221Q · Gulstm 200 · Battery/Charger System
  > THE FLIGHT CREW REPORTED THAT THE EMERGENCY BATTERY OVERHEAT EICAS MESSAGE DISPLAYED DURING THE FLIGHT. TEMP EXCEEDED 140 DEGREES. THE FLIGHT CREW RAN THE QRH AND SWITCHED OFF EMERGENCY BATTERY SWITCH. THE FLIGHT CONTINUED TO THE DESTINATION. THE MAINTENANCE T
- [SDR 1JAA20230324001](https://openairdocs.org/sdr/1JAA20230324001.md): Pump · leaking · Mar 24, 2023 · N119PS · Gulstm 200 · Turbine Engine Oil System
  > DURING CLIMB AFTER TAKEOFF, AIRCRAFT FILLED WITH SMOKE. CREW DAWNED OXYGEN MASKS, DECLARED AN EMERGENCY, AND RETURNED TO DEPARTURE AIRPORT PBI. TROUBLESHOOTING DETERMINED AN OIL PUMP SEAL FAILURE ON THE RH ENGINE TO BE AT FAULT.
- [SDR 2023F00031](https://openairdocs.org/sdr/2023F00031.md): Connector · corroded · Jan 16, 2023 · N573PT · Gulstm 200 · Fire Protection System Wiring
  > EMERGENCY BATTERY OVERHEAT INDICATION IN FLIGHT.
- [SDR 9JLA2023012637802](https://openairdocs.org/sdr/9JLA2023012637802.md): Outflow Valve · failed · Jan 6, 2023 · N1221Q · Gulstm 200 · Pressure Regulator/Outflow Valve
  > THE FLIGHT CREW REPORTED THAT THE AUTO PRESSURIZATION FAILED AFTER LANDING. THE MAINTENANCE TEAM DETERMINED THAT THE OUTFLOW VALVE FAILED. A REPAIRED UNIT WAS INSTALLED. OPS/LEAK CHECKS WERE PERFORMED AND FOUND TO BE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO
- [SDR 9JLA2022122940057](https://openairdocs.org/sdr/9JLA2022122940057.md): Overheat Sensor · defective · Dec 11, 2022 · N159JH · Gulstm 200 · Overheat Detection
  > THE FLIGHT CREW REPORTED THAT PRIOR TO START OF ENGINES RECEIVING A LEFT HOT BATTERY INDICATION. THE BASE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE LEFT MAIN BATTERY TEMP SENSOR WAS DEFECTIVE. THE BATTERY TEMP SENSOR WAS REMOVED AND REPLACED WITH A NEW
- [SDR 2022FA0000552](https://openairdocs.org/sdr/2022FA0000552.md): Connector · shorted · Sep 19, 2022 · N430S · Gulstm 200 · Electrical Power System Wiring
  > DURING FLIGHT FROM KVNY TO MMGM, WHILE DESCENDING FOR LANDING, SMOKE WAS DETECTED IN THE CABIN: INVESTIGATION REVEALED THAT THE RIGHT AFT FACING SEAT FRAME WAS CONTACTING A CONNECTOR INSTALLED IN THE LOWER RIGHT SIDEWALL (FS 206). THE RIGHT AFT FACING SEAT WAS
- [SDR 2022F00339](https://openairdocs.org/sdr/2022F00339.md): Hydraulic Line · leaking · Sep 9, 2022 · N119PS · Gulstm 200 · Hydraulic Fluid Servicing
  > RH HYDRAULIC SYSTEM FAILURE IN FLIGHT. CAS MESSAGES DISPLAYED INCLUDED R HYDR PRESS LOW, RH HYDR FLUID LOW, AUX PUMP CAME ON, THEN ALSO SHOWED LOW PRESSURE AND FLUID. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A HIGH PRESSURE PIN HO
- [SDR 2022F00350](https://openairdocs.org/sdr/2022F00350.md): None · none · Sep 6, 2022 · N573PT · Gulstm 200 · Oil Servicing
  > SMOKE IN THE CABIN DURING CLIMB. CREW DECLARED EMERGENCY AND RETURNED TO DEPARTING AIRPORT KTMB. MECHANIC NOTICED OIL ACCUMULATING ON RH ENGINE INLET. PRATT & WHITNEY IN PARTNERSHIP WITH WEST STAR TROUBLESHOT TO ENGINE OIL OVER-SERVICE. MECHANICAL DIFFICULTY R
- [SDR 2022F00349](https://openairdocs.org/sdr/2022F00349.md): None · none · Aug 31, 2022 · N573PT · Gulstm 200 · Oil Servicing
  > SMOKE IN THE CABIN DURING CLIMB. CREW DECLARED EMERGENCY AND RETURNED TO DEPARTING AIRPORT KTMB. MECHANIC NOTICED OIL ACCUMULATING ON RH ENGINE INLET. PRATT & WHITNEY IN PARTNERSHIP WITH WEST STAR TROUBLESHOT TO ENGINE OIL OVER-SERVICE. MECHANICAL DIFFICULTY R
- [SDR 2022F00139](https://openairdocs.org/sdr/2022F00139.md): Tire · debonded · Mar 13, 2022 · N427LM · Gulstm 200 · Tire
  > DURING PRE-FLIGHT THE CREW OF N427LM NOTICED THE FOLLOWING. 1. A SECTION OF TREAD SEPARATED FROM THE NUMBER 3 TIRE. 2. DAMAGE TO A CFRP PANEL ON THE LOWER SURFACE OF THE WING AS A RESULT.
- [SDR 9JLA202202178028](https://openairdocs.org/sdr/9JLA202202178028.md): Flex Hose · leaking · Feb 14, 2022 · N104SG · Gulstm 200 · Engine Fuel and Control
  > THE FLIGHT CREW REPORTED THE LEFT ENGINE ROLLED BACK 20 TO 25% AFTER THE INITIAL POWER REDUCTION BEFORE RELIGHTING. THIS OCCURRED AT THE YOP OF DECENT AROUND 36000 FT. THE FLIGHT CREW ALSO STATED THAT THE AIRCRAFT SHUTTERED DURING THIS EVENT. AFTER RELIGHT THE
- [SDR 2022FA0000031](https://openairdocs.org/sdr/2022FA0000031.md): None · none · Jan 16, 2022 · N55SR · Gulstm 200 · Landing Gear Brake System
  > UPON LANDING, BOTH LEFT MAIN TIRE ASSEMBLIES WERE NOTES AS LOCKED UP AND NOT TURNING. MAINTENANCE DETERMINED THAT THE BRAKES HAD FROZEN UP FROM ICE. BOTH BRAKE ASSEMBLIES WERE THAWED AND BOTH LEFT MAIN GEAR TIRES WERE REPLACED TO REMEDY THE DEFECT. NO OTHE
- [SDR 9JLA2021121731656](https://openairdocs.org/sdr/9JLA2021121731656.md): Audio Control · inoperative · Dec 11, 2021 · N1PK · Gulstm 200 · Audio Integrating System
  > THE FLIGHT CREW REPORTED THE CO-PILOTS AUDIO PANEL COMMUNICATION INOPERATIVE WITH PILOT SIDE. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE CO-PILOTS SIDE REQUIRED REPAIRS. THE REPAIRED UNIT WAS REINSTALLED AND OPS CHECKS WERE SATISFACTORY. THE AIRCRAFT
- [SDR 9JLA2021120831654](https://openairdocs.org/sdr/9JLA2021120831654.md): Audio Control · intermittent · Dec 5, 2021 · N1PK · Gulstm 200 · Communications System
  > THE FLIGHT CREW REPORTED THE COPILOTS AUDIO PANEL VOLUME COULD NOT BE CONTROLLED, DEFAULTED TO FULL VOLUME. THE MAINTENANCE TEAM DETERMINED THE CO-PILOTS AUDIO CONTROL PANEL WAS DEFECTIVE. THE AUDIO CONTROL PANEL WAS REMOVED AND REPLACED WITH A REPAIRED UNIT.
- [SDR 9JLA2021120831653](https://openairdocs.org/sdr/9JLA2021120831653.md): Detector · faulty · Nov 29, 2021 · N1PK · Gulstm 200 · Ice/Rain Protection System
  > THE FLIGHT CREW REPORTED THE LEFT ICE DETECT FAIL AND SIDE WINDOW HEAT EICAS MESSAGES POSTED. THE MAINTENANCE TEAM DETERMINED A LEFT ICE DETECTOR FAULT. THE DETECTOR WAS REMOVED AND REPLACED WITH A REPAIRED UNIT. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT W
- [SDR 1JAA20211120003](https://openairdocs.org/sdr/1JAA20211120003.md): None · broken · Nov 20, 2021 · N176QF · Gulstm 200 · Window/Windshield System
  > PER PILOT REPORT: DURING CLIMB(THRU FL360) LEFT SIDE WINDOW SHATTERED. CREW REQUESTED DESCENT, COMPLIED WITH CHECKLISTS AND DIVERTED TO ROC.
- [SDR 9JLA2021110320693](https://openairdocs.org/sdr/9JLA2021110320693.md): Igniter Box · defective · Oct 31, 2021 · N415PR · Gulstm 200 · Ignition Power Supply
  > THE FLIGHT CREW REPORTED RECEIVING A "RIGHT FADEC MINOR" MESSAGE. THE MAINTENANCE TEAM DETERMINED THE RIGHT NO2 ENGINE IGNITOR BOX WAS DEFECTIVE. THE UNIT WAS REMOVED AND REPLACED WITH AN OVERHAULED IGNITOR. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RE
- [SDR 1JAA20210825001](https://openairdocs.org/sdr/1JAA20210825001.md): Circuit Breaker · failed · Aug 21, 2021 · N176QF · Gulstm 200 · Electrical Power System Wiring
  > 75 AMP EMERGENCY BATTERY CIRCUIT BREAKER ON COCKPIT OVERHEAD PANEL POPPED. THIS CAUSED LOSS OF POWER TO SYSTEMS TO INCLUDE PRESSURIZATION CONTROL. NO SIGNS OF ARCING OR OVER HEATING PRESENT. VENDOR INSPECTED 75 AMP BATT CIRCUIT BREAKER LOCATED ON COCKPIT OVER
- [SDR 9JLA2021072829576](https://openairdocs.org/sdr/9JLA2021072829576.md): Computer · defective · Jul 8, 2021 · N856T · Gulstm 200 · Navigation System
  > WHILE THE FLIGHT CREW WAS ATTEMPTING TO UPLOAD THE CURRENT VERSION OF THE NAV DATABASE, THE UPLOAD TERMINATED WITH POWER INTERRUPT DETECTED. MESSAGE ON CDU RED FMS1 MESSAGE ON BOTH HSI AND ADI. THE MAINTENANCE TEAM DETERMINED THE FLIGHT MANAGEMENT COMPUTER WAS
- [SDR 9JLA2021052728324](https://openairdocs.org/sdr/9JLA2021052728324.md): Hydraulic System · false indication · May 25, 2021 · N104SG · Gulstm 200 · Hydraulic System, Main
  > THE FLIGHT CREW REPORTED THAT THE RIGHT HYDRAULIC QUANTITY DECREASED 1% PER 15 MINUTES. NORMAL 98% AFTER SHUTDOWN. A "LOW HYDRAULIC QUANTITY" REFILL EICAS MESSAGE. THE MAINTENANCE VENDOR SERVICED THE LEFT AND RIGHT HYDRAULIC SYSTEM AS PER THE AMM. NO SERVICING
- [SDR 9JLA2021051828322](https://openairdocs.org/sdr/9JLA2021051828322.md): Uplock Switch · defective · May 1, 2021 · N104SG · Gulstm 200 · Landing Gear Retraction/Extension System
  > THE FLIGHT CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION A GEAR UNSAFE INDICATION AFTER SUCCESSFUL RETRACTION. THEY RECYCLED THE LANDING GEAR WITH NO IMPROVEMENT. AFTER RUNNING THE CHECKLIST THE CREW ELECTED TO DIVERT BACK TO KPBI FOR LANDING AND REPAIR
- [SDR CWQA20210412001](https://openairdocs.org/sdr/CWQA20210412001.md): Carbon Seal · leaking · Apr 12, 2021 · N441JW · Gulstm 200 · Turbine Engine Compressor Section
  > DURING TAKE OFF CREW NOTICED OIL SMELL AND WHITE SMOKE IN COCKPIT. CHECKLIST FOLLOWED AND UNEVENTFUL LANDING PERFORMED. MAINTENANCE EVALUATION FOUND #1 ENGINE #2 BEARING CARBON SEAL FAILED BY EVIDENCE OF OIL RESIDUE IN BLEED LINES. REMOVED AND REPLACED #1 E
- [SDR 9JLA2021033029571](https://openairdocs.org/sdr/9JLA2021033029571.md): O-Ring · leaking · Mar 18, 2021 · N856T · Gulstm 200 · Air Distribution System
  > THE FLIGHT CREW REPORTED A BLEED AIR LEAK IN THE ACM BAY DURING FLIGHT. THE MAINTENANCE VENDOR REPLACED THE O-RINGS ON BOTH ENDS OF THE LOW LIMIT BLEED DUCT ASSYS WERE REPLACED WITH NEW O-RINGS.
- [SDR 9JLA2021030929568](https://openairdocs.org/sdr/9JLA2021030929568.md): Attach Bracket · broken · Feb 26, 2021 · N856T · Gulstm 200 · Fuselage Main, Attach Fittings
  > THE FLIGHT CREW NOTED DURING THE PREFLIGHT THE LEADING EDGE OF THE RIGHT STRAKE LOOSE. THE MAINTENANCE VENDOR GAINED ACCESS AND FOUND THE RIGHT STRAKE FORWARD BRACKET AT STATION 16024.0 BROKEN. BRACKET P/N 7AS3170520-026. A NEW ATTACHMENT BRACKET WAS INSTALLE
- [SDR E0YA2021011300002](https://openairdocs.org/sdr/E0YA2021011300002.md): Bottle · empty · Jan 12, 2021 · N710RH · Gulstm 200 · Landing Gear Retraction/Extension System
  > DURING SERVICE CHECKS, TECHNICIAN NOTICED LANDING GEAR EMERGENCY EXTENSION BOTTLE GAUGE READING ZERO. UPON SERVICING, NOTICED THE NITROGEN WAS NOT FILLING AND IMMEDIATELY LEAKING OUT. FURTHER TROUBLESHOOTING REVEALED THE UNION THAT SCREWS INTO THE BOTTLE HAD
- [SDR CVGA20200706001](https://openairdocs.org/sdr/CVGA20200706001.md): Control Cable · out of tolerance · Jun 30, 2020 · N180LD · Gulstm 200 · Elevator Control System
  > WHILE AT ALTITUDE (41,000FT) ELEVATOR (E) AMBER, THEN RED ILLUMINATED ON PFD, FOLLOWED BY AN OSCILLATING PITCH UP (APPX 3-5 DEGREES) AUTOPILOT WAS ENGAGED DURING THIS EVENT AND WAS DISCONNECTED. AN ELECTRIC SMOKE ODOR WAS THEN DETECTED BY BOTH CREW MEMBERS AS
- [SDR CJPA202006250001](https://openairdocs.org/sdr/CJPA202006250001.md): Circuit Breaker · broken · Jun 21, 2020 · N159JH · Gulstm 200 · Electrical Power System
  > BETWEEN DBLSS AND HRPER AT FL340 THE CAS INDICATED MULTIPLE ISSUES WITH RED WARNING AND AMBER CAUTION MESSAGES. A/P DISENGAGED AND NEITHER PRIMARY OR SECONDARY TRIM APPEARED OPERATIVE. AURAL WARNING SYSTEM INDICATED AN OVERSPEED CONDITION DUE TO THE MACH TRIM
- [SDR Y9PA2020020620](https://openairdocs.org/sdr/Y9PA2020020620.md): Drain Valve · leaking · Feb 4, 2020 · N999MC · Gulstm 200 · Potable Water System
  > AFTER FLIGHT CREW SQUAWKED PORTABLE WATER TANK LEAKING INTO BILGE WATER OBSERVED DRIPPING FROM FWD FUSELAGE DRAIN HOLE. UPON INSPECTION BY TECHNICIANS DISCOVERED THAT THE FILL DRAIN VALVE (PN DO5A00, SN 2553, DATED 10/99, MANUFACTURED BY C3406 GKN WESTLAND-SIT
- [SDR V0JA201910210006](https://openairdocs.org/sdr/V0JA201910210006.md): Sensor · faulted · Oct 16, 2019 · N165PB · Gulstm 200 · Battery/Charger System
  > RH MAIN BATTERY OVERHEAT MESSAGE. INSPECTION FOUND BATTERY TEMP SENSOR FAULTY.
- [SDR CWQA201908190001](https://openairdocs.org/sdr/CWQA201908190001.md): Battery · false indication · Aug 18, 2019 · N358TD · Gulstm 200 · Battery/Charger System
  > DURING CLIMB, CREW RECEIVED R/H BATTERY OVERHEAT YELLOW EICAS MESSAGE - 170 RED TEMPERATURE INDICATION. CHECK LIST FOLLOWED, EMERGENCY DECLARED, AND UNSCHEDULED LANDING PERFORMED WITHOUT INCIDENT. MAINTENANCE EVALUATION ISOLATED AS FALSE INDICATION ISSUE, BA
- [SDR 2019FA0000250](https://openairdocs.org/sdr/2019FA0000250.md): Bolt · defective · Aug 13, 2019 · N999MC · Gulstm 200 · Wheel/Ski/Float
  > MAIN WHEEL ASSEMBLY HAD ONE TIE BOLT FAILURE WHILE TOWING AIRCRAFT. THIS TIE BOLT BROKE TOWARDS THE CENTER WITH WHAT LOOKS LIKE A FATIGUE CRACK.
- [SDR IEYA2019FA0000165](https://openairdocs.org/sdr/IEYA2019FA0000165.md): Warning System · activated · May 26, 2019 · N860CB · Gulstm 200 · Engine Oil Pressure
  > AT 35,000', AIRCRAFT'S RED CAS MESSAGE L ENG OIL PRESS CAME ON. CREW RAN ASSOCIATED CHECKLIST, CHECKLIST CALLED OUT FOR PRECAUTIONARY ENGINE SHUTDOWN. THE CREW SHUT DOWN THE LEFT ENGINE PER THE CHECKLIST. LEFT ENGINE INDICATED 25 PSI OIL PRESSURE AND DROPPING
- [SDR Y9PA20190103191](https://openairdocs.org/sdr/Y9PA20190103191.md): Mount Bracket · broken · Jan 3, 2019 · N251LB · Gulstm 200 · Exterior Lighting
  > DURING A PRE-FLIGHT INSPECTION, THE MECHANIC DISCOVERED THAT THE RIGHT-WING NAVIGATION LIGHT WAS NOT ILLUMINATING. THE MECHANIC CHANGED THE LIGHT BUT THE LIGHT WAS STILL NOT ILLUMINATING. NEXT, THE MECHANIC CHECKED THE WIRE CONNECTIONS FOR THE LIGHT AND DID N
- [SDR Y9PA2018010319](https://openairdocs.org/sdr/Y9PA2018010319.md): Mount Bracket · broken · Jan 3, 2019 · N251LB · Gulstm 200 · Exterior Lighting
  > DURING A PRE-FLIGHT INSPECTION, THE MECHANIC DISCOVERED THAT THE RIGHT-WING NAVIGATION LIGHT WAS NOT ILLUMINATING. THE MECHANIC CHANGED THE LIGHT BUT THE LIGHT WAS STILL NOT ILLUMINATING. NEXT, THE MECHANIC CHECKED THE WIRE CONNECTIONS FOR THE LIGHT AND DID N
- [SDR IEYAN201812100001](https://openairdocs.org/sdr/IEYAN201812100001.md): Unknown · pressure loss · Dec 8, 2018 · N188AJ · Gulstm 200 · Cabin Pressure Control System
  > LOUD 'BANG FOLLOWED BY PRESSURIZATION LOSS AT 3000 - 4000 FPM. NO ASSOCIATED ANNUNCIATOR LIGHTS. OCCURRED AT 35,000'. AIRCRAFT WILL BE FERRIED TO GULFSTREAM DALLAS FOR REPAIR.
- [SDR 2018F00049](https://openairdocs.org/sdr/2018F00049.md): Unknown · smoke · Dec 6, 2017 · N403SL · Gulstm 200 · Air Distribution System
  > DURING TAKE OFF FROM KPBI AFTER ROTATION WE GOT A LOT OF SMOKE FOLLOWED BY A SMELL OF OIL IN THE COCKPIT AND CABIN. WE RETURNED TO KPBI AND LANDED WITH NO ISSUES.
- [SDR 2018F00048](https://openairdocs.org/sdr/2018F00048.md): Unknown · smoke · Nov 21, 2017 · N403SL · Gulstm 200 · Air Distribution System
  > ON DEPARTURE OUT OF PBI ABOUT 1000 FEET INFLIGHT WE STARTED SMELLING SOMETHING BURNING. SOON AFTER WE STARTED NOTICING A LOT OF SMOKE IN THE COCKPIT. IMMEDIATELY AFTER WE HAD AN EICAS MASSAGE APPEAR ( R ENGINE OIL FILTER. SO WE TURNED BACK TO THE AIRPORT IN PB
- [SDR W6JA2017111400017](https://openairdocs.org/sdr/W6JA2017111400017.md): Downlock Switch · out of rig · Nov 9, 2017 · N412AP · Gulstm 200 · Landing Gear Position and Warning
  > LEFT MAIN LANDING GEAR INDICATED UNSAFE ON SELECTION OF GEAR EXTENSION. RAN CHECKLIST, CYCLED GEAR, LANDED WITH LEFT MAIN GEAR UNSAFE INDICATION WITHOUT INCIDENT. GEAR INDICATION TURNED GREEN AT END OF ROLL OUT. MAIN LANDING GEAR DOWNLOCK SWITCH ADJUSTMENT WA
- [SDR W6JA20171030016](https://openairdocs.org/sdr/W6JA20171030016.md): Wire Harness · malfunctioned · Oct 30, 2017 · N52AJ · Gulstm 200 · Landing Gear System Wiring
  > LEFT GEAR WILL NOT FULLY RETRACT UPON GEAR RETRACTION SELECTION. THE LIGHT WILL INDICATE UP WHEN GEAR SELECTOR LEVER IS PULLED UP FURTHER. IN FLIGHT THE LEFT GEAR DOOR WILL GET A TRANSIT INDICATION IN FLIGHT OCCASIONALLY. REMOVED A FAILED LT WING HARNESS. IN
- [SDR BKEA201609210501](https://openairdocs.org/sdr/BKEA201609210501.md): Engine · vibration · Sep 20, 2017 · N889MR · Gulstm 200 · Engine (Turbine/Turboprop)
  > ACFT DEPARTED. UPON REACHING FL 370 I, THE PILOT, REDUCED THROTTLE POWER FOR CRUISE FLIGHT. AT THIS MOMENT THERE WAS A LOUD BANG AND A JERK HEARD AND FELT FROM THE FLIGHT CREW. IMMEDIATELY FOLLOWING THIS, THE EVM INDICATED MAJOR VIBRATIONS COMING FROM THE
- [SDR K95A201709190001](https://openairdocs.org/sdr/K95A201709190001.md): Elevator System · malfunctioned · Sep 15, 2017 · N648RR · Gulstm 200 · Elevator Control System
  > THE PIC CALLED MX CONTROL TO ADVISE THEY HAD NO CONTROL OF ELEVATORS WHILE AT CRUISE. QRH WAS FOLLOWED AND SLIGHT MOVEMENT OF THE LEFT YOKE ONLY WAS GAINED, BUT NOT FULL CONTROL FWD AND AFT (APPROX. 1IN FWD AND AFT). FLIGHT CREW NOTIFIED TOWER AND EMERGENCY L
- [SDR W6JA20170530014](https://openairdocs.org/sdr/W6JA20170530014.md): Switch · failed · May 26, 2017 · N882SG · Gulstm 200 · Rudder Tab Control System
  > WHILE DESCENDING THROUGH 15,000 FT AT 320 KIAS, THE RUDDER TRIM WENT INTO FULL DEFLECTION. REPLACED THE RUDDER TRIM SWITCH WITH UPGRADED PART.

Next page: https://openairdocs.org/model/laser-200/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/laser-200/reports

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