Gulfstream Aerospace G-V

Service difficulty reports · 145

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 = 'GV'
  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 2025F00233Clamp · looseWHILE DESCENDING THROUGH FL180, AFTER SELECTING WING ANTI-ICE TO ON, A CAUTION MESSAGE "BAG EER HOT" MESSAGE ILLUMINATED, FOLLOWED BY SMOKE IN THE CABIN, THEN COCKPIT. NO OTHER INDICATIONS. THE PILOT DECLARED AN EMERGENCY AND WAS GRANTED A STRAIGHT IN TO BIKF.Oct 5, 2025 · N176S · Gulstm GV · Airfoil Anti/De-ice SystemSDR 2025FA0000423Psu · leakingDURING OXYGEN PASSENGER OXYGEN SYSTEM (MANUAL / AUTO MODE) - FUNCTIONAL CHECK IAW GVII-G600 AMM 35-20-01, AFTER MANUALLY DEPLOYING MASKS A SOUND OF ESCAPING OXYGEN WAS HEARD. UPON PSU LOWERING IN THE AFT LH CABIN, THE OXYGEN WAS FOUND TO BE LEAKING FROM THE PSJun 25, 2025 · N221RW · Gulstm GV · Passenger Oxygen SystemSDR 2025FA0000375Circuit Breaker · arcedAPPLIED A/C POWER AND CHECKED APU CB'S. CONFIRMED FAULT REPORTED BY CREW. CB "FIRE DETECTION APU 2601" TRIPPED AND UNABLE TO RESET IT. CYAN CAS " APU FIRE DETECTOR FAIL" WAS ALSO POSTED. UPON INVESTIGATION FOUND WIRE W197D20-4 (28VDC - SINGLE WIRE) DAMAGED. May 27, 2025 · N720LF · Gulstm GV · Fire Protection System WiringSDR 2025FA0000132Duct · disconnectedAIRCRAFT REPORTED RH BLEED AIR LOW AND AFT EQUIPMENT HOT MESSAGES. ON INSPECTION INTO THE TAIL COMPARTMENT, THE BLEED AIR DUCTING HAS BEEN FOUND DISCONNECTED.Feb 25, 2025 · N920BM · Gulstm GV · Pneumatic Distribution SystemSDR 2025FA0000086Coupler · miswiredPERFORMED TROUBLESHOOTING IAW GVII-G600 IWDM REV.3 42-11-00. MEASURED ASCB #2 BACKUP BUS END RESISTOR REF DES "103R8" IN SYSTEM MONITOR TEST PANEL SUCCESSFULLY. GAINED ACCESS TO ASCB BUS COUPLER #1 AND FOUND WIRING STRIPPED FROM TOO LONG DISTANCE EXPOSING CEFeb 6, 2025 · N318AG · Gulstm GV · Electrical Power System WiringSDR PAZR202408010001Pump · shearedAFTER APPROXIMATELY 45 MIN OF FLIGHT, RED CAS MESSAGE “R ENG LOW OIL PRES” WAS DISPLAYED IN COCKPIT. OBSERVED A STEADY BUT SLOW INCREASE ON THE RIGHT ENGINE OIL TEMPERATURE. RETURNED TO MAINTENANCE FACILITY. INVESTIGATION REVEALED OIL PUMP SPLINED DRIVE COUPLIJul 13, 2024 · N194MF · Gulstm GV · Turbine Engine Oil SystemSDR 2023FA0000773Wire · arcedDURING MAINTENANCE OF 73028. WIRING CHECKS WERE CARRIED OUT FOR HYDRAULIC SHUT OFF VALVE CYAN MESSAGE WITH SSPC TRIPPED. DURING CHECKS CABLE FOUND CHAFFED WITH SIGNS OF BURNING. TROUBLESHOOTING AND REPAIR ONGOING AT TIME OF SUBMISSIONNov 22, 2023 · N600EB · Gulstm GV · Hydraulic Power System WiringSDR 2023FA0000019None · noneGULFSTREAM GVII-G600 INCLUDES GULFSTREAM STC ST04324AT-D THAT INCLUDES AN ELECTRICALLY OPERATED 'FORWARD CABIN POCKET DOOR'. THE GULFSTREAM PASSENGER BRIEFING CARD DOES NOT ADDRESS THE LOCATION OR INSTRUCTIONS FOR PASSENGER OPENING/EXISTING THROUGH THIS DOOR Jan 9, 2023 · N699GA · Gulstm GV · Standard Practices/StructuresSDR 2021FA0000411None · bindsDISCRPANCY:PILOT NOTIFIED MAINTENANCE AND OPERATIONS IN FLIGHT THE #1 & # 2 FLIGHT GUIDANCE COMPUTER IS INTERMITTENT, AND THE PITCH TRIM DISENGAGED. CORRECTIVE ACTION:GULFSTREAM MAINTENANCE FOUND A PITCH TRIM SERVO DRUM AT FAULT. THE PITCH TRIM SERVO DRUM AND Nov 20, 2021 · N588AT · Gulstm GV · Elevator Tab Control SystemSDR J7SA2021112200302Mount · crackedUNCOMMANDED PITCH TRIM DOWN DURING FLIGHT. FOUND ELEVATOR TRIM SERVO MOUNTING BRACKET CRACKED. REMOVED CRACKED BRACKET; LOCATED, DRILLED, AND INSTALLED NEW ELEVATOR TRIM SERVO MOUNTING BRACKET IAW GULFSTREAM GV SRM 51-42-00. P/N 1159C50423-129.Nov 20, 2021 · N727PR · Gulstm GV · Elevator Tab Control SystemSDR CWQA20210524001Bellcrank · brokenDURING APPROACH JUST AFTER CREW SELECTED FLAPS 39, ONCE FLAPS FULLY DEPLOYED, CREW NOTICED A SLIGHT UN-COMMANDED ROLL/BANK TO THE LEFT. CREW WAS ABLE TO CORRECT WITH RIGHT AILERON INPUT. CHECKLIST FOLLOWED, UNEVENTFUL LANDING PERFORMED. MAINTENANCE EVALUATIMay 19, 2021 · N703RK · Gulstm GV · Aileron Control SystemSDR Y9PA2021081803175Flange · corrodedEXFOLIATION CORROSION ON THE RIGHT FORWARD-CENTER WING BOX REBATE FLANGE, JUST OUTBOARD OF SINGLE POINT.Mar 17, 2021 · N125GH · Gulstm GV · Fuselage Main, StructureSDR Y9PA2021081800317Torque Tube · corrodedPOST CORROSION REMOVAL AND EVALUATION, ENGINEERING DETERMINED THAT THE REMAINING MATERIAL THICKNESS ON THE RUDDER TORQL'E TUBE ATI ACH EARS DOES NOT MEET AIRWORTHINESS REQUIREMENTS.Mar 17, 2021 · N125GH · Gulstm GV · Rudder StructureSDR Y9PA202108180507Flange · corrodedCORROSION WAS IDENTIFIED ON BOTH SIDES OF VERTICAL STABILIZER REBATE FLANGES. REMOVED 64 NUTPLATE, CLEANED CORROSION FROM BELOW THE 64 REMOVED NUTPLATES, INSTALLED NUT PLATES ON THE VERTICAL STABILIZER REBATE FLANGES IN ACCORDANCE WITH GV SRM CH 51-42-00.Mar 17, 2021 · N125GH · Gulstm GV · Vertical StabilizerSDR Y9PA202108180317Skin · corrodedLH AND RH WING PLANK AT TRAILING EDGE OF AILERON AREAS. HAVE CORROSION ON THE PLANKS AROUND NUTPLATES FOR CLOSEOUT PANELS, TO INCLUDE OUTBOARD TRAILING EDGE OF BOX AREA BETWEEN AILERONS AND WINGLETS.Mar 17, 2021 · N125GH · Gulstm GV · Wing, Plate/SkinSDR Y9PA03172021.1Access Door · corrodedCORROSION FOUND ON STRUCTURE WHERE EXTERNAL APU ACCESS DOOR MATES TO THE FUSELAGE.Mar 17, 2021 · N125GH · Gulstm GV · Auxiliary Power Unit (APU) DoorsSDR Y9PA92920Steering Unit · bindsON LANDING AIRCRAFT WOULD NOT STEER TO THE LEFT. AIRCRAFT CAME TO A STOP. HOWEVER, AIRCRAFT ENDED UP WITH NOSE WHEEL IN GRASS OFF OF RUNWAY. RUNWAY EXCURSION.Sep 4, 2020 · N9102 · Gulstm GV · Steering UnitSDR W6JA20200711039Eec · malfunctionedPILOT REPORTED LT ENGINE PARAMETERS DIFFERENT THAN RT ENGINE, PARTICULARLY DESCRIBED AS LT FUEL FLOW DOWN TO 1250 LBS, HP DROP, LP DROP, AND HP VIBRATION WENT UP WITH THROTTLE MOVEMENT NOTED BETWEEN 0.48 AS HIGH AS 0.51 (THIS VIBE STILL WITHIN TOLERANCE/LIMIT)Jul 11, 2020 · N776RB · Gulstm GV · Fuel Controlling SystemSDR 2020FA0000136Manifold · crackedWHILE WAITING FOR PASSENGERS WITH THE APU RUNNING FUEL BEGAN RUNNING OUT OF THE BACK OF THE AIRCRAFT NEAR THE PANEL WHERE THE MARKER BEACON ANTENNA IS MOUNTED. APU WAS IMMEDIATELY SHUT DOWN AND THE FIRE DEPARTMENT CONTACTED. UPON INSPECTION OF THE APU IT WAS NFeb 11, 2020 · N278PH · Gulstm GV · APU Engine Fuel and ControlSDR 2020FA0000107Circuit Breaker · trippedLANDING GEAR CONTROL CIRCUIT BREAKER ON COCKPIT OVERHEAD PANEL POPPED. ATTEMPTED 1 RESET AND BREAKER POPPED AGAIN. LANDING GEAR HAD TO BE EXTENDED USING THE EMERGENCY EXTENSION SYSTEM.Dec 10, 2019 · N280PH · Gulstm GV · Landing Gear Retraction/Extension SystemSDR BKEA201912030001Warning Light · illuminatedON TAKE OFF AND CLIMB, LEFT GEAR AMBER LIGHT REMAINED ON AFTER GEAR HANDLE PLACE IN UP POSITION. RETURNED TO DEPARTURE.Dec 2, 2019 · N888XY · Gulstm GV · Landing Gear Position and WarningSDR Y9PA20191004189Lock · failedWHEN LINE-SERVICE OPENED THE MAIN ENTRY CABIN DOOR HE HEARD A LOUD POP. UPON INSPECTION, FOUND THAT THE MAIN ENTRY DOOR SECONDARY LOCKING MECHANISM FAILED.Oct 2, 2019 · N9102 · Gulstm GV · Passenger/Crew DoorsSDR CWQA2019090300000Windshield · faultyDURING DESCENT CREW NOTICED A SMALL AMOUNT OF SMOKE COMING OUT OF LEFT WINDSHIELD HEAT CONNECTOR, CREW TURNED OFF LEFT WINDSHIELD HEAT AND SMOKE STOPPED IMMEDIATELY. CHECK LIST FOLLOWED, AND SCHEDULED LANDING PERFORMED WITHOUT INCIDENT. MAINTENANCE EVALUATIONAug 27, 2019 · N585JC · Gulstm GV · Flight Compartment WindowsSDR AOQA201908061001Line · brokenDISCOVERED DURING GROUND OPERATION. NO AIR WAS FELT AT THE BACK OF THE TAT PROBES. INSPECTION OF THE BLEED AIR FEED LINE STARTING AT THE TAT SOLENOID IN THE AFT EQUIPMENT BAY AREA FOUND A LINE HAD SEPARATED JUST AFTER AN ADEL SUPPORT CLAMP. NO ADDITIONAL SURROJul 31, 2019 · N820HB · Gulstm GV · Navigation SystemSDR 2020FA0000101Compressor Blade · galledDURING ROUTINE 1000 HOUR REAPPLICATION OF THE DRY FILM LUBRICANT ON THE FAN BLADE ROOT AREA IT WAS NOTICED THAT GAULLING ON THE BLADE ROOT WAS BEYOND THE .004 MANUFACTURE LIMIT. A FLY ON DISPOSITION WAS NOT GRANTED BY ROLLS ROYCE AND ALL 24 BLADES ON THE BOTHJun 7, 2019 · N278PH · Gulstm GV · Turbine Engine Compressor SectionSDR J7SA20190122001Unknown · odorFLIGHT ATTENDANT SMELLED A FAINT ELECTRICAL ODOR. REMOVED EQUIPMENT AND ACCESS PANELS FROM BAGGAGE COMPARTMENT. REMOVED FLOOR BOARDS FROM BAGGAGE AND LAV. INSPECTED AVIONICS BOXES, WIRING AND PNEUMATICS IN BAGGAGE AND UNDER FLOOR. THERE WERE NO SIGNS OF BURNT Jan 22, 2019 · N136FX · Gulstm GV · Air Distribution SystemSDR J7SA20190218001Unknown · odorSTRONG ELECTRICAL ODOR IN BAGGAGE COMPARTMENT AFTER LANDING. REMOVED ACCESS PANELS IN BAGGAGE AREA. I INSPECTED ALL ELECTRICAL COMPONENTS ASN CABLE CONNECTIONS. NO DISCREPANCIES NOTED. NO ODOR WAS EVIDENT AT TIME OF INSPECTION. AIRCRAFT IS RETURNED TO SERVICE.Jan 18, 2019 · N136FX · Gulstm GV · Air Distribution SystemSDR 2CPA2019F00036Cowling · delaminatedDELAMINATION (BLISTER) OF INNER BARREL OF ENGINE INLET COWL AT THE 9 O'CLOCK POSITION.Aug 3, 2018 · N780W · Gulstm GV · Engine Cowling SystemSDR 2017FA0000169Control Valve · wrong partWHEN LANDING GEAR SELECTED DOWN, THE LANDING GEAR CONTROL CIRCUIT BREAKER TRIPPED. DUPLICATED ON JACKS. WHEN GEAR DOWN SELECTED, THE HYD PRESSURE TO THE DOWN SOLENOID RESISTANCE GOES HIGH AND AMPS EXCEEDS THE RATED 5 AMP CIRCUIT BREAKER. REPLACED THE -15 CApr 26, 2017 · N253CM · Gulstm GV · Landing Gear Retraction/Extension SystemSDR GR4R201610290014Stop Fitting · brokenLT ELEVATOR I/B STOP IS BROKEN.Oct 29, 2016 · N502QS · Gulstm GV · Elevator Miscellaneous StructureSDR GR4R201610290013Hinge Fitting · crackedAT NR 3 HINGE O/B FITTING IS CRACKED.Oct 29, 2016 · N502QS · Gulstm GV · Elevator StructureSDR GR4R201610290012Hinge Fitting · crackedAT NR 3 HINGE I/B FITTING IS CRACKED.Oct 29, 2016 · N502QS · Gulstm GV · Elevator StructureSDR GR4R201610290011Hinge Fitting · crackedAT NR 4 HINGE I/B FITTING IS CRACKED.Oct 29, 2016 · N502QS · Gulstm GV · Elevator StructureSDR GR4R201610290010Hinge Fitting · crackedAT NR 4 HINGE I/B FITTING IS CRACKED.Oct 29, 2016 · N502QS · Gulstm GV · Elevator StructureSDR GR4R201610290009Stop Fitting · chafedI/B STOP HAS DEEP RUB MARK AND SIGNS OF ARCHING.Oct 29, 2016 · N502QS · Gulstm GV · Elevator Miscellaneous StructureSDR GR4R201610290008Lug · corrodedLEFT INBOARD PIVOT LUG ON THE HORIZONTAL STABILIZER HAS AN AREA OF PITTING AT THE 12 O'CLOCK POSITION.Oct 29, 2016 · N502QS · Gulstm GV · Horizontal Stabilizer Miscellaneous StructureSDR GR4R201610290007Fitting · crackedRT HORIZONTAL STABILIZER RUB BLOCK FITTING CRACKED.Oct 29, 2016 · N502QS · Gulstm GV · Horizontal Stabilizer Miscellaneous StructureSDR GR4R201610290006Fitting · crackedLT HORIZONTAL STABILIZER RUB BLOCK FITTING CRACKED.Oct 29, 2016 · N502QS · Gulstm GV · Horizontal Stabilizer Miscellaneous StructureSDR GR4R201610290005Frame · corrodedFRAMES AT FS 632.00, 684.00 AND 707.00 UNDER WING TO BODY FAIRING 196AB HAS EXTENSIVE CORROSION.Oct 29, 2016 · N502QS · Gulstm GV · Fuselage Main, FrameSDR GR4R201610290004Frame · corrodedFRAME AT FS 674.00 UNDER WING TO BODY FAIRING 196AB HAS CORROSION.Oct 29, 2016 · N502QS · Gulstm GV · Fuselage Main, FrameSDR GR4R201610290003Frame · corrodedFRAME AT FS 660.00 UNDER WING TO BODY FAIRING 196AB HAS CORROSION.Oct 29, 2016 · N502QS · Gulstm GV · Fuselage Main, FrameSDR GR4R201610290002Skin · corrodedRIGHT HORIZONTAL TRAILING EDGE LOWER SKIN UPPER SURFACE HAS CORROSION AT COVE PANEL FLANGES.Oct 29, 2016 · N502QS · Gulstm GV · Horizontal Stabilizer, Plate/SkinSDR GR4R201610290001Skin · corrodedLEFT HORIZONTAL TRAILING EDGE LOWER SKIN UPPER SURFACE HAS CORROSION AT COVE PANEL FLANGES.Oct 29, 2016 · N502QS · Gulstm GV · Horizontal Stabilizer, Plate/SkinSDR GR4R201610280005Beam · chafedLT ENGINE FORWARD CRANE BEAM HAS A CHAFE .1670 LONG X .0860 WIDE X .0420 DEEP, AT LOWER EDGE FROM STEEL BRAIDED DRAIN LINE.Oct 28, 2016 · N502QS · Gulstm GV · Engine Mount SectionSDR GR4R201610280004Angle · crackedFORWARD LOWER INBOARD CORNER OF APU ENCLOSURE HAS CRACKED SUPPORT RIB ON INBOARD WALL.Oct 28, 2016 · N502QS · Gulstm GV · APU Cowling/ContainmentSDR GR4R201610280003Seat Track · corrodedON SEAT TRACK LBL 6, AFT OF FS 515 HAS CORROSION.Oct 28, 2016 · N501QS · Gulstm GV · Fuselage, Seat/Cargo Attach FittingsSDR GR4R201610280002Seat Track · corrodedON SEAT TRACK LBL 6, AFT OF BS 456.5 HAS CORROSIONOct 28, 2016 · N502QS · Gulstm GV · Fuselage, Seat/Cargo Attach FittingsSDR GR4R201610280001Seat Track · corrodedON SEAT TRACK LBL 18.5,K BS 456.5 HAS CORROSION,Oct 28, 2016 · N502Q · Gulstm GV · Fuselage, Seat/Cargo Attach FittingsSDR DBGA201609260001Drive Chain · frozenFROZEN PITCH TRIM ON CLIMB OUT, FOUND CORRODED AND FROZEN PITCH TRIM SERVO DRIVE CHAIN.Sep 21, 2016 · N808JG · Gulstm GV · Elevator Tab Control SystemSDR DXTA20160812KSAV1Lug · damagedAFTER REMOVING BUSHINGS FROM RT SPONSON RIB AFT MOUNT LUG, FOUND NICK ON TOP SIDE OF FITTING. OVERSIZED THE RT AFT SPONSON LUG TO THE FIFTH OVERSIZE WITH A FINAL READING OF 2.5595 " (READINGS WERE TAKEN AT THREE DIFFERENT POSITIONS INSIDE LUG) WORK DONE PEAug 12, 2016 · N509QS · Gulstm GV · Fuselage Structure (General)
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