Gulfstream Aerospace GVI
Service difficulty reports · 52
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 = 'GVI' 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.
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 = 'GVI' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2026FA0000647Line · leakingWHILE CARRYING OUT OXYGEN FOLLOW ONS, LARGE OXYGEN LEAK HEARD FROM BEHIND PSU. UPON DROPPING PSU, OXYGEN LINE FOUND TO NOT BE FULLY CONNECTED TO OXYGEN BOX. ONCE OXYGEN LINE WAS RECONNECTED TO OXYGEN BOX, OXYGEN BOX WAS FOUND TO HAVE A LARGE LEAK AND IS US.2.DSDR 2026FA0000530Mount · out of positionDURING LT PYLON ACCESS FOR ACB001, IT WAS NOTICED THAT THE LT ENIGNE UPPER AFT ENGINE MOUNT ANTI ROTATION DEVICE (FWD SIDE) WAS ROTATED OUT OF POSITION. WITH A SLIGHT MANIPULATION OF THE ENGINE MOUNT TVA (FWD SIDE) THE ANTI ROTATION DEVICE BECAME LOOSE WHICHSDR 2026FA0000243Wire Harness · exposedAIRCRAFT REPORTED SSPC 3327 - SIGN LIGHTS TRIPS INTERMITTENTLY AND HE SUSPECTED THE DEFECT TO BE BETWEEN THE LT AFT PSU AND AFT LAV LT PSU. CONTINUITY CHECKS WERE CARRIED OUT BETWEEN TB 931TJ3S AND CONNECTOR 794A1P1, INCLUDING LINE TO LINE AND CHECKS TO GROUNDSDR 2025FA0000788Actuator · warning messageEICAS MESSAGE NOTING RIGHT HAND ELEVATOR HYDRAULIC ACTUATOR FAILURE.SDR Y9PA2025111010000Flap · not reportedRIGHT HAND ON THIS AIRCRAFT WHILE THE ORIGINAL FLAP WAS REMOVED FOR REPAIR. NEEDED TO GROUND THE ACFT TO VERIFY THE FLAP. THEY STATED THE FLAP WAS NOT PROPERLY IDENTIFIED WHEN INSTALLED. THEY PROCEDDED TO SEND A MECHANIC TO THE AIRCRAFT TO VERIFY STATUS OF THESDR 2025F00252Attach Bracket · misinstalledLH ENGINE FIXED COWL FORWARD LOWER ATTACHMENT BRACKET INSTALLED INCORRECTLY (180 DEGREES/WRONG WAY AROUND).SDR 2025FA0000690Mec · smokeCREW MET ON ARRIVAL, LT AILERON MCE CONFIRMED TO HAVE STRONG BURNED ODUR AND SOOTING EVIDENT ABOVE UNIT AND ON ADJACENT STRUCTURE. WIRING HARNESS VISUALLY INSPECTED, NO DEFECTS APPARENT. EBHA CB'S INSPECTED IN TAIL COMPARTMENT. L AILERON BRAKER FOUND TO HAVE TSDR 2025FA0000696Warning Message · intermittentINTERMITTENT "L MAIN GEAR NOT UP" AMBER (CAUTION) CAS MESSAGE ALERT OCCURRED DURING CLIMB, APPROXIMATELY 8-10 MINS AFTER SUCCESSFUL GEAR RETRACTION. MESSAGE CLEARED FOLLOWING GEAR EXTENSION. THE DEFECT RECURRED INTERMITTENTLY, AGAIN AFTER 8-10 MINS DURING A SSDR 2025FA0000369Warning Message · illuminatedDURING CLIMB, PILOT RECEIVED A WARNING LIGHT LEFT HAND MAIN GEAR WAS NO LONGER UP AND STOWED. REVIEWED FLIGHT MANUAL AND FURTHER RECEIVED A SECOND WARNING RIGHT HAND MAIN GEAR WAS NO LONGER UP AND STOWED.SDR J7SA2025020700431Microwave Oven · faultedBURNING WIRE SMELL WHEN MICROWAVE OVEN IS IN USE. TESTED ON GROUND AFTER FLIGHT, SMALL AMOUNT OF SMOKE PRESENT. REPLACED DYNAMO MICROWAVE IAW G650 AMM 25-37-02. OPS CHECK GOOD.SDR 2024F00252Electrical Sys · faultedRIGHT POWER DISTRIBUTION BUS DC OVERHEAT AND EMERGENCY BUS FAULT DURING FLIGHT. FOUND LOOSE GROUND TERMINALS AT STUD 270GS6E / WIRES RELATED TO THE FOLLOWING SYSTEM R PDB DC FAN FAULTSDR 2024FA0000490Bellcrank · crackedCHECK FLIGHT CONTROL RIGGING, FULL FLAP GEAR DOWN RH AILERON 2 GRADUATIONS REQUIRED, CRUISE CLEAN LH WING OUTBOARD FLIGHT SPOILER SLIGHTLY UP. LEFT FLIGHT SPOILER BELL CRANK P/N 1159CM50209-5 (ASSY MFR 80378, 03-27- 2004) FOUND CRACKED AT BEARING LOCATION FORSDR J7SA2024051600399Windshield · arcedAIR TURN BACK DUE TO CREW NOTICED ARCHING IN THE LH WINDSCREEN AT FL410. SHORTLY AFTER, A SMELL OF BURNING ELECTRICAL WIRES WAS NOTICED AND THE LH WINDOW HEAT WAS DEACTIVATED. FOLLOWING THIS, A LOUD POP WAS HEARD, AND THE WINDSCREEN CRACKED. CREW FOLLOWED CHECSDR 2024FA0000278Windshield · crackedEN-ROUTE FROM KHOU TO KTEB THE CREW EXPERIENCED PILOT SIDE WINDSHIELD CRACKED. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO KTUL.SDR J7SA2024032100386Actuator · unserviceableBEGINNING INITIAL DESCENT INTO BOS, CREW RECEIVED AMBER RUDDER FAIL CAS. CREW CALLED MX TO CONFIRM ACFT IS ASC 135. MX CONFIRMED ACFT IS ASC 135. CREW RAN CHECKLIST, PERFORMED TWO UNSUCCESSFUL RESETS, LANDED WITHOUT INCIDENT. COMPLIED WITH AMM 27-20-00 SECTSDR J7SA2024032200387Bushing · missingDURING BLEEDING OF LH HYDRAULIC SYSTEM, CLUNKING NOISE HEARD UNDER COCKPIT ENTRY WAY FLOOR WHEN OPERATING ELEVATORS THROUGH FULL RANGE OF TRAVEL. BUSHINGS FOR PILOT AFT LAT/LONG CONTROL MODULE ASSEMBLY FOUND MISSING. INSTALLED NEW BUSHINGS AND HARDWARE IAW G65SDR 7P9A2024040100001Software · corruptedON APPROACH INTO EINN CREW EXPERIENCED A FAILURE OF THE EGPWS SYSTEM, THE SYSTEM INDICATED THAT THEY WERE FLYING BELOW TERRAIN DESPITE BEING AT 18,000 FT. DUE TO THE FAILURE RESULTING IN LOSS OF INSTRUMENT GUIDANCE FOR LANDING AND IMC CONDITIONS CREW ELECTED TSDR 2023FA0000788Unknown · unknownAIRCRAFT REPORTED THE FOLLOWING LEFT AILERON FAIL CAS MSG. 27156413LAL.OSCILLATION EVENT OCCURRED. DURING INVESTIGATION OF DEFECT ALL REU CONNECTORS FOUND CONTAMINATED WITH SUSPECTED DC4 FLUID. REPLACED EB MANIFOLD, HA MANIFOLD, EHSA MANIFOLD, REU'S 1 AND 3SDR 2023FA0000542Connector · unknownBACK IN 2016, GULFSTREAM ISSUED CB 126, WHICH HAD OPERATORS REPLACE THE RIGHT ENGINE HYDRAULIC PUMP DEPRESSURIZATION VALVE CONNECTOR DUE TO FAILURE OF THE CONNECTOR PER ROLLS ROYCE SB BR700-71-900578. IN ADDITION, GULFSTREAM ISSUED CB 127 TO INSPECT THE RIGHT SDR 7ORR202309150036Blade · fracturedHPT 1 BLADE RELEASE #2 ENGINE, AND SUBSEQUENT COLLATERAL DAMAGE TO TRAILING TURBINE STAGES; WHICH COULD RESULT IN ENGINE FAILURE AND SUBSEQUENT SINGLE ENGINE OPERATION. BORESCOPE INSPECTION WAS INITIATED AT THE BEHEST OF ROLLS-ROYCE DEUTSCHLAND LTD & CO KG ESCSDR CWQA20230712001Unknown · unknownDURING CRUISE SHORTLY AFTER LIGHT TURBULENCE, CREW RECEIVED TWO “STABILIZER CHANNEL FAIL” AND “STABILIZER FAILED” CAS MESSAGES, HOWEVER FLIGHT CONTROL SYNOPTIC SHOWED ALL FLIGHT CONTROL SURFACES OPERATING NORMALLY INCLUDING THE STAB. AT NO TIME DID THE AIRCRASDR 2023FA0000212Fire Bottle · cloggedAFTER REPLACING CABIN FIRE EXTINGUISHER (WATER) FOR HYDROSTATIC DUE DATE, WE ATTEMPTED TO TO USE THE WATER FIRE EXTINGUISHER THAT WAS COMING DUE FOR HYDROSTATIC TESTING AS A TRAINING AID. FOLLOWING THE INSTRUCTIONS PRINTED ON THE BOTTLE, AN ATTEMPT TO DISCHARGSDR J7SA2023040300355Unknown · unknownMICROWAVE EMITTED A STRONG ELECTRICAL BURNING SMELL WHILE IN USE. WHEN STOPPED, EVIDENCE OF BURNING (BLACK SOOT) WAS SEEN INSIDE THE MICROWAVE. REPLACED MICROWAVE OVEN IAW G650 OUTFITTING MAINTENANCE MANUAL 25-37-02. OPS CHECK GOOD.SDR 2023FA0000144Autothrottle Sys · missingDURING SCHEDULED MAINTENANCE ON 6243 AT GAC FAB WO SC23856.12.18, THROTTLE QUADRANT ASSEMBLY WAS REQUIRED TO BE REPLACED DUE TO A R ENG THRUST REVERSER DEFECT. DURING REPLACEMENT OF THE TQA IAW G650ER AMM 76-10-01 REV 15, STEP C.7 - "REMOVE GUST LOCK INHIBIT BSDR J7SA2023030600001None · noneRUDDER FAIL CAS ON SHORT FINAL. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RUDDER REMOTE ELECTRONICS UNIT 16. PERFORMED SUCCESSFUL RUDDER ACTUATING SYSTEM IBIT SUITE A TEST. PERFORMED SUCCESSFUL RUDDER FUNCTIONAL TEST. CLOSED LEFT AND RIGHT VERTICAL STABILSDR J7SA2023021600350None · noneDISCOVERED LEFT AND RIGHT-HAND HYDRAULIC PUMP CONNECTORS LOOSE FITTING AND BENT IN THE ENGINE DRIVEN HYDRAULIC PUMP. UPON REMOVAL, DISCOVERED CORROSION/DEBRIS IN THE ENGINE PUMP SIDE OF THE PLUGS AS WELL AS THE LOCKING FEATURE TOTALLY NONEXISTENT, AND PINS CORSDR 2022FA0000238None · noneWHILE WE TRIED TO PURGE THE WATER SYSTEM B ON N650ER SMOKE APPEAR ON THE CABIN, RIGHT AFTER THE AIRCRAFT WAS POWER DOWN. INITIAL INVESTIGATION CARRIED OUT FOUND R/H MAIN TRU EXTREMELY HOT AND COOLING FAN NOT WORKING.
SQUAWK 8.52 ON W/O SC21602 RAISED.SDR 2022FA0000002None · jammedTHE FORWARD LAVATORY LATCH LOCK JAMMED IN THE LOCKED POSITION. OCCUPIED MECH ASSY (RH) P/N GSI SA65034-2SDR 2021FA0000234Wire · severedDURING ROUTINE POSTFLIGHT INSPECTION, FOUND WIRED GOING TO THE LH ENGINE FIRE BOTTLE SQUIBS TO BE SEVERED. SUSPECT POOR WIRING QUALITY FROM GULFSTREAM/AND OR POOR WIRING DESIGN FOR AREA AND INTENDED USE.SDR 7ORR2021081314785Blade · fracturedENGINE HEALTH MONITORING NOTED A CHANGE IN TGT MARGIN. POST-FLIGHT BSI INSPECTION OF THE ENGINE REVEALED A SINGLE HPT STAGE 1 BLADE THAT HAS RELEASED AT APPROXIMATELY 25% HEIGHT AND CAUSED SECONDARY DOWNSTREAM DAMAGE TO THE ENGINE. THE RELEASED HPT BLADE AIRFSDR J7SA2021072600287Manifold · failedCREW RECEIVED A RIGHT ELEVATOR DISCONNECT FAIL CAS MESSAGE THREE TIMES WHILE IN ROUTE TO NTAA. OCCURRED ABOUT 2 HOURS OUT FROM THEIR DESTINATION. CREW FOLLOWED QRH PROCEDURE AND MAINTAINED CONTROL OF AIRCRAFT THROUGHOUT THE WHOLE PROCESS. AIRCRAFT LANDED WITHOSDR 2021FA0000172Quick Disconnect · damagedTHRUST REVERSER RETURN HYDRAULIC QUICK DISCONNECT (QD) FITTINGS AND NIPPLES IN THE ENGINE PYLON AREA KEEP FAILING AND RESULTING IN FLUID LEAKING. THE INITIAL FAILURE WAS NOTED DURING A FEB 2021 GULFSTREAM SERVICE CENTER VISIT, THAT WHEN THE QD WAS DISCONNECTEDSDR J7SA2021040200281Microwave Oven · odorDURING DESCENT, WHILE MICROWAVE WAS IN USE, CREW DISCOVERED ELECTRICAL SMELL AND SMALL MIST OF SMOKE. AIRCRAFT LANDED WITHOUT INCIDENT AT KAUS. MICROWAVE DEACTIVATED VIA VCB 2430. ACCOMPLISH LATEST REVISION, ELECTRICAL WIRING INSTALLATIONS (ATA 97) INSPECTION,SDR 2021FA0000009Cable · shortedTHE ARCING WAS CAUSED BY TWO PROBLEMS: A) EBHA BATTERY POSITIVE CABLE P368A00-2 SHORTED TO GROUND ADJACENT TO THE BATTERY CONNECTOR BECAUSE THE CABLE INSULATION TERMINATED VERY CLOSE TO THE END OF THE CABLE PROTECTIVE BRAIDING. THE BRAIDING CAME INTO CONTACT SDR 2020FA0000527Wire Harness · sparksAFTER GAINING ACCESS TO THE DOOR DAMPER TO PERFORM REPLACEMENT WHILE REACHING UNDER THE FLOOR TO REMOVE THE DOOR DAMPER, IAW G500 AMM52-14-01, CONTACT WAS MADE WITH THE 72043-R112 LOOM ASSEMBLY. THE ENGINEER FELT A SHOCK IN HIS HAND AND SAW SPARKING/ARCING. SDR MGTY2020062900004Bearing · crackedDURING SCHEDULED REMOVAL OF LT MLG SHOCK ABSORBER IT WAS NOTED THAT THE UPPER BEARING WAS CRACKED AND SPLIT COMPLETELY IN HALF. PARTIAL PENETRATION ON THE RT UPPER SHOCK ABSORBER BEARING WAS ALSO NOTED. ITEM TO BE REPLACED.SDR MGTY2020062900003Wire · chafedWHILST CARRYING OUT CMP APU FIRE EXTINGUISHING FIRING CIRCUITRY INTEGRITY OPERATIONAL CHECK, SYSTEM FAILED EXTINGUISHING FIRING INTEGRITY CHECK DUE TO BROKEN WIRE ON LT FIRE BOTTLE CONNECTOR 053E1P1. WIRE 2W105H20-4 WAS FOUND TO BE SEVERELY CHAFED THROUGH OUTSDR MGTY2020062900002Wire · chafedCARRYING OUT FIRE BOTTLE CIRCUIT INTEGRITY OPERATIONAL CHECKS, RT FIRE EXTINGUISHER BOTTLE BLUE NR 1 SHOT. CONNECTOR 053E2P1 WIRE 2W106A20N-4 FOUND TO BE CHAFED, AND WIRE 2W102H20-4 FOUND TO BE SEVERELY CHAFED THROUGH OUTER INSULATION, BRAID AND INNER INSULATSDR MGTY2020062900001Wire · chafedWHILST CARRYING OUT FIRE BOTTLE CIRCUIT INTEGRITY OPERATIONAL CHECKS, RT FIRE EXTINGUISHER BOTTLE BLUE NR 1 SHOT. CONNECTOR 053E2P1 WIRE 2W106A20N-4 FOUND TO BE CHAFED, AND WIRE 2W102H20-4 FOUND TO BE SEVERELY CHAFED THROUGH OUTER INSULATION, BRAID AND INNER SDR 2020F00088Control Unit · defectiveAPPROX FOUR HOURS AND THIRTY MINUTES INTO THE FLIGHT AT FL430, WE FELT A SUDDEN JOLT IN THE FLIGHT CONTROL, FOLLOWED BY NUMEROUS AMBER AND BLUE CAS MESSAGES AND AUDIBLE ALERTS SOUNDING. THE AUTOPILOT AND AUTO THROTTLES IMMEDIATELY DISENGAGED AND MOST OF THE INSDR 2019FA0000380Valve · constricted"LEFT ENGINE FAIL" CAS MESSAGE FOLLOWED BY AUTO RELIGHT. CREW FOLLOWED QRH PROCEDURES AND AIRCRAFT LANDED SAFELY. TROUBLESHOOTING REVEALED HP#5 VALVE TO BE CONSTRICTED DUE TO COMPRESSION RING OUT OF PLACE. COMPRESSION RING WAS CORRECTLY INSTALLED PER AMM 36SDR 2019FA0000359Manifold · contaminatedIN CRUISE AT FL341, AC 6235 (REG# B-88322) INDICATED RUDDER FAILURE CONDITION, POSTED AMBER "RUDDER FAIL" CAS MSG AND ACCOMPANIED BY LARGE DUTCH ROLL. DIFFICULT TO MAINTAIN ASSIGNED ALTITUDE, PILOT STARTED QRH “RUDDER FAIL” PROCEDURE AND REQUESTED DECENT TO LOSDR KKVA20190701003Reu · failedCRUISING FL400 AND SPEED M.90 WITH AUTOPILOT ON, WE HAD “FCS MAINTENANCE REQUIRED” CAS MESSAGE. APPROXIMATELY 4 HOURS FROM TAKEOFF. QRH PROCEDURES FOLLOWED. THE AUTOPILOT DISCONNECTED AND THE AIRCRAFT SUDDENLY ROLLED TO RIGHT WHEN I PRESSED FLT CNTL RESET SW. SDR LD2R2019032700001Battery · overheatedWHILE IN THE HANGER AND PERFORMING MAINTENANCE ON A DIFFERENT SYSTEM, NOTICED THE RIGHT BATTERY VOLTAGE DROP FROM 28 VOLTS TO 19 VOLTS RAPIDLY. TURNED THE BATTERY SWITCH OFF AND SHUT OFF POWER TO THE AIRCRAFT. VISUAL EXAMINED BATTERY AND THE BATTERY CASE WAS SDR GR422017101800511Aileron · malfunctionedDURING CRUISE AT FL450, AIRCRAFT ROLLED WITH CORRESPONDING AILERON RT FAIL CAS MESSAGE. RT AILERON DISPLACED IN UP POSITION. THREE ATTEMPTED FLIGHT CONTROL RESETS WITH NO EFFECT. CHECKED THE AIRCRAFT AND FOUND NO FAULTS.SDR 2017FA0000511Aileron Sys · malfunctionedDURING CRUISE, THE AIRCRAFT EXPERIENCED A SLIGHT ROLE TO THE COPILOT SIDE OF THE AIRCRAFT. ON BOARD COMPUTERS INDICATED AN AILERON ACTUATOR FAILURE FOR THE RIGHT AILERON. AIRCRAFT RETURNED TO DEPARTURE WITHOUT DECLARING AN EMERGENCY. THE COMPONENTS ARE BEISDR MGTY20160708075Battery Cable · mismanufacturedLEFT MAIN BATTERY LOW VOLTS CAS MESSAGE AS REPORTED BY THE CREW. ON INVESTIGATION IT WAS DISCOVERED THAT THE LT MAIN BATTERY NEGATIVE CABLE TO AIRFRAME TERMINAL HAD BEEN ARCING WHICH HAD CAUSED EXTENSIVE DAMAGE TO THE TERMINAL ITSELF AND ATTACHING AIRFRAME BRSDR 2016FA0000240Door Seal · contaminatedDURING PREFLIGHT OPENED AFTER EQUIPMENT BAY DOOR, BOILER ROOM AND PILOT WAS DOUSED WITH APPROXIMATELY A HALF A CUP OF FUEL WHICH HAD POOLED ON THE INNER SURFACE OF THE DOOR. SUBSEQUENT INVESTIGATION FOUND THAT FUEL LEAKING FROM APU FUEL METERING UNIT DRAIN PSDR 2016FA0000243Power Supply · shortedON PREFLIGHT THE UNINTERRUPTABLE POWER SUPPLY, FOR THE FLY-BY-WIRE SYSTEM WOULD NOT TEST. SUBSEQUENT INVESTIGATION RELEVELED THAT WIGGLING THE CIRCUIT BREAKER ON THE FRONT OF THE UNIT WOULD CAUSE THE UNIT TO INTERMITTENTLY START AND FAIL. UNIT HAD RECENTLY BSDR 2016FA0000241Seal · contaminatedDURING PREFLIGHT OPENED AFTER EQUIPMENT BAY DOOR, BOILER ROOM AND PILOT WAS DOUSED WITH APPROXIMATELY .5 CUP OF FUEL WHICH HAD POOLED ON THE INNER SURFACE OF THE DOOR. SUBSEQUENT INVESTIGATION FOUND THAT FUEL LEAKING FROM APU FUEL METERING UNIT DRAIN PORT IN
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