# Service difficulty reports: Gulfstream Aerospace GVI

A list on [Gulfstream Aerospace GVI](https://openairdocs.org/model/gulfstream-aerospace-gvi.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 52 reports

- [SDR 2026FA0000647](https://openairdocs.org/sdr/2026FA0000647.md): Line · leaking · Aug 17, 2026 · N706GA · Gulstm GVI · Passenger Oxygen System
  > WHILE 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.D
- [SDR 2026FA0000530](https://openairdocs.org/sdr/2026FA0000530.md): Mount · out of position · Jun 19, 2026 · N71Z · Gulstm GVI · Engine Mount Section
  > DURING 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 WHICH
- [SDR 2026FA0000243](https://openairdocs.org/sdr/2026FA0000243.md): Wire Harness · exposed · Mar 30, 2026 · N331AB · Gulstm GVI · Light System Wiring
  > AIRCRAFT 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 GROUND
- [SDR 2025FA0000788](https://openairdocs.org/sdr/2025FA0000788.md): Actuator · warning message · Nov 24, 2025 · N540LF · Gulstm GVI · Elevator Control System
  > EICAS MESSAGE NOTING RIGHT HAND ELEVATOR HYDRAULIC ACTUATOR FAILURE.
- [SDR Y9PA2025111010000](https://openairdocs.org/sdr/Y9PA2025111010000.md): Flap · not reported · Nov 7, 2025 · N650FJ · Gulstm GVI · Trailing Edge Flaps
  > RIGHT 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 THE
- [SDR 2025F00252](https://openairdocs.org/sdr/2025F00252.md): Attach Bracket · misinstalled · Oct 29, 2025 · N201CE · Gulstm GVI · Nacelle/Pylon, Main Frame
  > LH ENGINE FIXED COWL FORWARD LOWER ATTACHMENT BRACKET INSTALLED INCORRECTLY (180 DEGREES/WRONG WAY AROUND).
- [SDR 2025FA0000690](https://openairdocs.org/sdr/2025FA0000690.md): Mec · smoke · Oct 8, 2025 · N100AL · Gulstm GVI · Aileron Control System
  > CREW 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 T
- [SDR 2025FA0000696](https://openairdocs.org/sdr/2025FA0000696.md): Warning Message · intermittent · Oct 7, 2025 · N66ZG · Gulstm GVI · Landing Gear Position and Warning
  > INTERMITTENT "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 S
- [SDR 2025FA0000369](https://openairdocs.org/sdr/2025FA0000369.md): Warning Message · illuminated · May 20, 2025 · N228ZD · Gulstm GVI · Landing Gear Position and Warning
  > DURING 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 J7SA2025020700431](https://openairdocs.org/sdr/J7SA2025020700431.md): Microwave Oven · faulted · Jan 17, 2025 · N667FX · Gulstm GVI · Buffet/Galleys
  > BURNING 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 2024F00252](https://openairdocs.org/sdr/2024F00252.md): Electrical Sys · faulted · Oct 13, 2024 · N999YY · Gulstm GVI · DC Power Distribution System
  > RIGHT 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 FAULT
- [SDR 2024FA0000490](https://openairdocs.org/sdr/2024FA0000490.md): Bellcrank · cracked · Jul 10, 2024 · N812RB · Gulstm GVI · Drag Control System
  > CHECK 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 FOR
- [SDR J7SA2024051600399](https://openairdocs.org/sdr/J7SA2024051600399.md): Windshield · arced · May 10, 2024 · N136ZC · Gulstm GVI · Flight Compartment Windows
  > AIR 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 CHEC
- [SDR 2024FA0000278](https://openairdocs.org/sdr/2024FA0000278.md): Windshield · cracked · Apr 3, 2024 · N113CS · Gulstm GVI · Flight Compartment Windows
  > EN-ROUTE FROM KHOU TO KTEB THE CREW EXPERIENCED PILOT SIDE WINDSHIELD CRACKED. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO KTUL.
- [SDR J7SA2024032100386](https://openairdocs.org/sdr/J7SA2024032100386.md): Actuator · unserviceable · Mar 16, 2024 · N653FX · Gulstm GVI · Rudder Control System
  > BEGINNING 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 SECT
- [SDR J7SA2024032200387](https://openairdocs.org/sdr/J7SA2024032200387.md): Bushing · missing · Mar 13, 2024 · N658FX · Gulstm GVI · Elevator Control System
  > DURING 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 G65
- [SDR 7P9A2024040100001](https://openairdocs.org/sdr/7P9A2024040100001.md): Software · corrupted · Feb 28, 2024 · N650GU · Gulstm GVI · Ground Proximity System
  > ON 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 T
- [SDR 2023FA0000788](https://openairdocs.org/sdr/2023FA0000788.md): Unknown · unknown · Nov 27, 2023 · N822MK · Gulstm GVI · Aileron Control System
  > AIRCRAFT 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 3
- [SDR 2023FA0000542](https://openairdocs.org/sdr/2023FA0000542.md): Connector · unknown · Sep 15, 2023 · N500ES · Gulstm GVI · Hydraulic Power System Wiring
  > BACK 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 7ORR202309150036](https://openairdocs.org/sdr/7ORR202309150036.md): Blade · fractured · Sep 13, 2023 · N270LE · Gulstm GVI · Turbine Section
  > HPT 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 ESC
- [SDR CWQA20230712001](https://openairdocs.org/sdr/CWQA20230712001.md): Unknown · unknown · Jul 10, 2023 · N900KS · Gulstm GVI · Flight Control System
  > DURING 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 AIRCRA
- [SDR 2023FA0000212](https://openairdocs.org/sdr/2023FA0000212.md): Fire Bottle · clogged · Apr 12, 2023 · N650HC · Gulstm GVI · Fire Bottle, Portable
  > AFTER 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 DISCHARG
- [SDR J7SA2023040300355](https://openairdocs.org/sdr/J7SA2023040300355.md): Unknown · unknown · Mar 20, 2023 · N653FX · Gulstm GVI · Cabin Equipment/Furnishings
  > MICROWAVE 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 2023FA0000144](https://openairdocs.org/sdr/2023FA0000144.md): Autothrottle Sys · missing · Mar 17, 2023 · N919PE · Gulstm GVI · Auto Throttle System
  > DURING 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 B
- [SDR J7SA2023030600001](https://openairdocs.org/sdr/J7SA2023030600001.md): None · none · Feb 23, 2023 · N380ER · Gulstm GVI · Flight Control System
  > RUDDER 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 STABIL
- [SDR J7SA2023021600350](https://openairdocs.org/sdr/J7SA2023021600350.md): None · none · Feb 8, 2023 · N650FX · Gulstm GVI · Hydraulic Filter, Main
  > DISCOVERED 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 COR
- [SDR 2022FA0000238](https://openairdocs.org/sdr/2022FA0000238.md): None · none · Apr 26, 2022 · N650ER · Gulstm GVI · Electrical Power System
  > WHILE 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 2022FA0000002](https://openairdocs.org/sdr/2022FA0000002.md): None · jammed · Jan 4, 2022 · N200ES · Gulstm GVI · Lavatories
  > THE FORWARD LAVATORY LATCH LOCK JAMMED IN THE LOCKED POSITION. OCCUPIED MECH ASSY (RH) P/N GSI SA65034-2
- [SDR 2021FA0000234](https://openairdocs.org/sdr/2021FA0000234.md): Wire · severed · Aug 15, 2021 · N500ES · Gulstm GVI · Fire Protection System Wiring
  > DURING 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 7ORR2021081314785](https://openairdocs.org/sdr/7ORR2021081314785.md): Blade · fractured · Aug 9, 2021 · N22T · Gulstm GVI · Turbine Section
  > ENGINE 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 AIRF
- [SDR J7SA2021072600287](https://openairdocs.org/sdr/J7SA2021072600287.md): Manifold · failed · Jul 9, 2021 · N651FX · Gulstm GVI · Elevator Control System
  > CREW 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 WITHO
- [SDR 2021FA0000172](https://openairdocs.org/sdr/2021FA0000172.md): Quick Disconnect · damaged · Jun 14, 2021 · N1901G · Gulstm GVI · Engine Thrust Reverser
  > THRUST 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 DISCONNECTED
- [SDR J7SA2021040200281](https://openairdocs.org/sdr/J7SA2021040200281.md): Microwave Oven · odor · Mar 30, 2021 · N651FX · Gulstm GVI · Buffet/Galleys
  > DURING 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 2021FA0000009](https://openairdocs.org/sdr/2021FA0000009.md): Cable · shorted · Dec 17, 2020 · N888XM · Gulstm GVI · Battery/Charger System
  > THE 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 2020FA0000527](https://openairdocs.org/sdr/2020FA0000527.md): Wire Harness · sparks · Dec 6, 2020 · N100JS · Gulstm GVI · Electrical Power System Wiring
  > AFTER 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 MGTY2020062900004](https://openairdocs.org/sdr/MGTY2020062900004.md): Bearing · cracked · Jun 29, 2020 · N650XA · Gulstm GVI · Main Landing Gear Strut/Axle/Truck
  > DURING 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 MGTY2020062900003](https://openairdocs.org/sdr/MGTY2020062900003.md): Wire · chafed · Jun 29, 2020 · N650XA · Gulstm GVI · Fire Protection System Wiring
  > WHILST 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 OUT
- [SDR MGTY2020062900002](https://openairdocs.org/sdr/MGTY2020062900002.md): Wire · chafed · Jun 29, 2020 · N650XA · Gulstm GVI · Fire Protection System Wiring
  > 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 INSULAT
- [SDR MGTY2020062900001](https://openairdocs.org/sdr/MGTY2020062900001.md): Wire · chafed · Jun 29, 2020 · N650XA · Gulstm GVI · Fire Protection System Wiring
  > WHILST 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 2020F00088](https://openairdocs.org/sdr/2020F00088.md): Control Unit · defective · Feb 26, 2020 · N311CG · Gulstm GVI · AC Power Distribution System
  > APPROX 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 IN
- [SDR 2019FA0000380](https://openairdocs.org/sdr/2019FA0000380.md): Valve · constricted · Nov 16, 2019 · N828SN · Gulstm GVI · Engine (Turbine/Turboprop)
  > "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 36
- [SDR 2019FA0000359](https://openairdocs.org/sdr/2019FA0000359.md): Manifold · contaminated · Oct 1, 2019 · Gulstm GVI · Rudder Control System
  > IN 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 LO
- [SDR KKVA20190701003](https://openairdocs.org/sdr/KKVA20190701003.md): Reu · failed · Jun 25, 2019 · N700MK · Gulstm GVI · Aileron Control System
  > CRUISING 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 LD2R2019032700001](https://openairdocs.org/sdr/LD2R2019032700001.md): Battery · overheated · Mar 25, 2019 · N93M · Gulstm GVI · Battery/Charger System
  > WHILE 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 GR422017101800511](https://openairdocs.org/sdr/GR422017101800511.md): Aileron · malfunctioned · Oct 5, 2017 · N672GA · Gulstm GVI · Aileron Control System
  > DURING 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 2017FA0000511](https://openairdocs.org/sdr/2017FA0000511.md): Aileron Sys · malfunctioned · Oct 5, 2017 · N672GA · Gulstm GVI · Aileron Control System
  > DURING 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 BEI
- [SDR MGTY20160708075](https://openairdocs.org/sdr/MGTY20160708075.md): Battery Cable · mismanufactured · Jul 8, 2016 · N900KS · Gulstm GVI · Electrical Power System Wiring
  > LEFT 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 BR
- [SDR 2016FA0000240](https://openairdocs.org/sdr/2016FA0000240.md): Door Seal · contaminated · May 17, 2016 · N6D · Gulstm GVI · Doors
  > DURING 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 P
- [SDR 2016FA0000243](https://openairdocs.org/sdr/2016FA0000243.md): Power Supply · shorted · May 9, 2016 · N6D · Gulstm GVI · Flight Control System
  > ON 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 B
- [SDR 2016FA0000241](https://openairdocs.org/sdr/2016FA0000241.md): Seal · contaminated · May 9, 2016 · N6D · Gulstm GVI · Doors
  > DURING 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

Next page: https://openairdocs.org/model/gulfstream-aerospace-gvi/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 = 'GVI'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/gulfstream-aerospace-gvi/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.