Gulfstream Aerospace G-IV
Service difficulty reports · 842
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 = 'GIV' 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 = 'GIV' 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 2022F00435Cabin Pressure · malfunctionedAIRCRAFT DEPARTED FROM KAPF ON A REPOSITION LEG AT 1300 ENROUTE TO KTMB. LANDED AND PICKED UP 3 PASSENGERS. DEPARTED KTMB FOR KVNY AT 1430. AFTER TAKEOFF DURING CLIMB OUT, OUTFLOW VALVE FULLY CLOSED AND CABIN PRESSURIZED TO -3500 FT. DIFFERENCE OF PRESSURE EXCSDR 2022F00464Mount · corrodedFWD SIDE OF LOWER WING PLANKS HAVE EXFOLIATION CORROSION AT BREAST PANEL MOUNTING FLANGES. FWD MID CABIN FS 261 - 348.SDR 2022FA0000492Outflow Valve · abnormalDURING A DESCENT TO FL380 FROM FL 450
AS THE AIRCRAFT ALTITUDE CAPTURED AT FL 380 THE CABIN BEGAN TO CLIMB SUDDENLY
I SELECTED MANUAL ON THE PRESSURIZATION AND ATTEMPTED TO CLOSE THE OUTFLOW VALVES BUT WAS UNABLE TO
CLOSE THEM. THE CABIN CONTINUED TO CLIMB SDR 9JLA2022072822982Actuator · leakingTHE BASE MAINTENANCE TEAM FOUND DURING POST-FLIGHT CHECKS THE STEERING UNIT LEAKING. THE MAINTENANCE PROVIDER REMOVED THE LEAKING NOSE WHEEL STEERING ACTUATOR AND REPLACED WITH AN OVERHAULED ACTUATOR. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFTSDR U5OA_N960DPNone · corrodedLH WING TO FUSELAGE AFT BL 33.187 CLOTHESPIN FITTING WAS FOUND TO HAVE CORROSION DURING INSPECTION REQUIRING EXTENSIVE SHEET METAL REPAIRS.SDR VQMA202205060001Window · separatedDURING CRUISE FLIGHT BETWEEN PANC AND KSYA, THE LH AFT EMERGENCY EXIT WINDOW OUTER PANE CRACKED AND SEPARATED FROM THE AIRCRAFT. THE SEPARATED WINDOW SECTIONS WERE INGESTED INTO THE LH ENGINE. THE AIRCRAFT RETURNED SAFELY TO PANC. NO LOSS OF PRESSURIZATION SDR 9JLA2022042522973Pitot Head · failedTHE FLIGHT CREW REPORTED OF A LEFT PITOT HEAT FAIL ANNUNCIATOR ILLUMINATED. THE MAINTENANCE VENDOR TROUBLESHOT THE LEFT PITOT SYSTEM AND FOUND PITOT HEAD FAILED. REMOVED THE DEFECTIVE PITOT HEAD AND INSTALLED A NEW PITOT HEAD. OPERATIONAL CHECKS WERE SATISFACTSDR DXTA2022022157080Tiller · defectiveNOSE WHL STR INOP CAS: LOWERED L/G FOR LANDING AND GOT "STEER BY WIRE FAIL" CAS. COMPLETED QRH PROCEDURES AND MSG STILL ILLUMINATED. RAISED L/G AND DIVERTED TO AIRPORT WITH BIGGER RWY. LOWERED L/G AGAIN AND CAS DID NOT REAPPEAR. CONDUCTED NORMAL LANDING ANSDR 2022FA0000096None · noneCREW REPORTED HYDRULIC FLUCTUATON AND QUANTITY DROP ON COMBINED SYSTEM DURING CRUISE, AIRCRAFT RETURNED
FROM FLIGHT (FLT. #60616 KBAF-LFML), REFER TO TECH. LOG SEQ. #502658. ON GROUND CHECKED FOR HYDRAULIC LEAK. NIL FOUND.
REPLACED COMBINED HYD. SYSTEM RESERSDR 2022FA0000071Windshield · crackedDURING FLIGHT PILOT SIDE OUTER PANE CRACKEDSDR DXTA2022013156000Switch · defectiveEMERG LIGHT SWITCH: ON THE OVERHEAD PANEL, THE EMERGENCY LIGHTS ON SWITCH CAPSULE HAS NO INDICATION OF "LIGHTS" DURING THE SYSTEM TEST OR WHEN THE CAPSULE IS PRESSED. THERE IS NO OTHER INDICATION OF THIS SYSTEM IN THE COCKPIT PER MEL 33-22.// SIGNOFF// REMOVEDSDR DXTA2022012455610Engine · damagedRIGHT ENGINE ENGINE HARDWARE: ON DESCENT THE RIGHT ENGINE MOMENTARILY LOST POWER, SHUTTERED, AND THE IGNITER CAME ON. THE PROBLEM MAY HAVE OCCURRED EARLIER DURING CLIMB OUT BUT WAS MISSED DIAGNOSED AS TURBULENCE. BUT THE IGNITER DID COME ON TWICE DURING THE SDR DXTA2022011955140Bulb · burned outEMERG EXIT SIGN/LIGHT: EMERGENCY EXIT LIGHTS RIGHT SIDE CABIN ABOVE CREDENZA, ONE BULB MISSING IN EACH EXIT SIGN. //SIGHOFF// REPLACED BURNED OUT LAMPS WITH TWO LAMPS P/N OL6839BPE FROM JET EAST STOCK IAW G-450 MM 33-50-00SDR DXTA2022011455140None · noneEMERG EXIT SIGN/LIGHT: EMERGENCY EXIT LIGHTS RIGHT SIDE CABIN ABOVE CREDENZA, ONE BULB MISSING IN EACH EXIT SIGN.SDR 2022F00073Controller · shortedWINDSHIELD HEAT CONTROLLER FAILURE CAUSING OVER HEATING OF LEFT FORWARD SIDE WINDSCREEN. PILOTS REPORTED SMOKE IN THE COCKPIT FROM BUS BAR CONNECTION ON WINDOW. MAINTENANCE PERSONNEL DETERMINED SMOKING BUS BAR WAS CAUSED BY OVER VOLTAGE / AMPERAGE CONDITION OFSDR 1JCA202112221001Warning Message · illuminatedENROUTE FROM LSGG-RJAA WITH 4 CREW ON BOARD AND 0 PAX. FL 430 OVER RUSSIA AT TIME 2000Z WE HAD 2 AMBER CAS MESSAGES, L ELEVATOR FAIL AND FCS MAINTENANCE REQUIRED. WE DECLARED A PAN AND AFTER RUNNING CHECKLIST CONCLUDED TO DIVERT FOR LANDING. OUR ALTERNATE UESDR 9JLA2021120722965Hydraulic Line · leakingTHE MAINTENANCE TEAM REPORTED THAT DURING POSTFLIGHT CHECKS FINDING THE LEFT AILERON ACTUATOR HOSE LEAKING FLUID. THE MAINTENANCE TEAM REMOVED AND REPLACED THE HOSE ASSY. WITH NEW. LEAK CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 9JLA2021120722964Control Valve · defectiveFLIGHT CREW REPORTED THAT THE APU LOAD CONTROL VALVE BEING INTERMITTENT IN OPERATION. THE MAINTENANCE VENDOR DETERMINED THE APU CONTROL VALVE WAS DEFECTIVE. THE VALVE WAS REMOVED AND REPLACED WITH AN OVERHAULED VALVE. OPERATIONAL AND LEAK CHECKS WERE SATISFACTSDR 9JLA2021110822962Unknown · smokeTHE FLIGHT CREW REPORTED THAT SMOKE ENTERED THE CABIN AND COCKPIT DURING CRUISE FLIGHT FROM MYNN TO KATL. THE FLIGHT CREW DONNED OXYGEN MASKS. AN EMERGENCY WAS DECLARED AND THE FLIGHT WAS DIVERTED TO KPBI FOR LANDING AND INVESTIGATION INTO THE SMOKE. THE APPROSDR W6JA20211024049Transmitter · failedAIRCRAFT DEPARTED PHOG @2221Z FOR KLAX. DURING CRUISE AT FL410 @ 2233Z A YELLOW " COMB HYD FAIL ", CAS MESSAGE ILLUMINATED. CREW RE-SET THE ANNUNCIATOR MULTIPLE TIMES AS MESSAGE RETURNED MULTIPLE TIMES, AFTER 5 MINUTES THE MESSAGE EXTINGUISHED. CREW REVIEWED TSDR WWQA826102221Hose · leakingIN FLIGHT, RECEIVED A HYD QUANTITY AMBER MESSAGE, NOTICED THE HYDRAULIC QUANTITY COMING UP ON LOW. HYD QUANTITY WENT RED ON THE ON THE COMBINED QUANTITY WHILE THE INFLIGHT QUANTITY REMAINED NORMAL. AIRCRAFT DID NOT HAVE ANY HYDRAULIC FAILURES ON LANDING AND TASDR 7GYA20211005003None · noneLEFT THRUST REVERSOR UNLOCK LIGHT ON AFTER TAKE OFF
SDR 7GYA20210930002Flap System · failedFLAPS FAILED TO MOVE WHILE AIRCRAFT WAS CONFIGURED FOR LANDING, SEVERAL ATTEMPTS TO MOVE FLAPS FROM 0 DEGREE TO 10 DEGREE WERE MADE IN FLIGHT AND AGAIN ON THE GROUND.SDR U5OA202108310001O-Ring · failedCREW NOTICED THE COMBINED SIDE HYDRAULIC QUANTITY INDICATION TO BE LOW, INITIALLY PRESSURE WAS HOLDING NORMAL (3000PSI), THE DECISION WAS MADE TO LAND THE AIRCRAFT AS SOON AS POSSIBLE, REQUEST WAS MADE AND GRANTED TO LAND AT KFSD. GULFSTREAM'S FAST WAS DISPATSDR 7GYA20210827001Flap System · faultedFLAPS FAILED TO MOVE WHEN AIRCRAFT WAS BEING CONFIGURED TO LAND. LANDED WITH NO FLAPS.SDR 2022FA0000400Trunnion Pin · damagedDURING TAKEOFF ROLL, PILOT NOTICED A PROGRESSIVE VIBRATION COMING FROM THE NOSE WHEEL AND REJECTED THE TAKEOFF. DURING DECELERATION THE NOSE GEAR DEPARTED THE AIRCRAFT AT THE TRUNNION TO AIRFRAME ATTACHMENT POINTS RENDERING AIRCRAFT UNCONTROLLABLE. THE AIRCRSDR 2021FA0000207Seat Track · corrodedCABIN LEFT HAND INBOARD AFT SEAT TRACK WAS CORRODED BEYOND THE MANUFACTURES LIMITS. RECEIVED GULFSTREAM ENGINEERING TO BLEND SURFACE CORROSION AND REMOVE SEAT TRACK TANGS IN THE AFFECTED AREA.SDR 2021FA0000206Acm · failedOIL SMOKE ENTERING THE CABIN AT FLOOR LEVEL. TROUBLESHOT THE CAUSE OF PROBLEM TO A FAILED LEFT AIR CYCLE MACHINE, THE PART WAS REPLACED WITH AN OVERHAULED ASSEMBLY. ALSO THEY FOUND FOD IN THE RIGHT HEAT EXCHANGER WITH SIGNS OF OVERHEATING, IT WAS REPLACED WITSDR 2021F00274Unknown · smokeAIRCRAFT WAS ENROUTE TO NEXT DESTINATION WHEN CREW EXPERIENCED OIL SMOKE ENTERING THE CABIN AT FLOOR LEVEL. THEY DECLARED AN EMERGENCY AND LANDED AT NEAREST AIRPORT KSAV. WHERE THE AIRCRAFT IS CURRENTLY AWAITING JET EDGE APPROVED MAINTENANCE VENDOR TO PERFORM SDR 9JLA2021061834254Converter · failedTHE FLIGHT CREW REPORTED THAT THE RIGHT CONVERTED FAILED IN FLIGHT. THE CREW ATTEMPTED TO RESET PER THE QRH BUT UNIT FAILED TO RESET. THE MAINTENANCE VENDOR TROUBLE SHOT AND DETERMINED THAT THE RIGHT ENGINE CONVERTER HAD FAILED. THE UNIT WAS REMOVED AND REPLACSDR U5OA202107020001Tire · failedLH MLG TIRES BLOWN ON LANDING AT KPDK. GULFSTREAM FAST WAS DISPATCHED TO THE AIRCRAFT TO ASSESS AND REPAIR AS NECESSARY. IT WAS DEEMED NECESSARY TO REPOSITION THE AIRCRAFT TO A GULFSTREAM FACILITY TO PERFORM THE REQUIRED REPAIRS. GULFSTREAM FAST TECHNICIANS SDR 9JLA2021052534253Gasket · leakingTHE FLIGHT CREW REPORTED THAT DURING FLIGHT WHILE PRESSURIZED 7.5 PSI A LOUD UNIDENTIFIED NOISE IS IN THE CABIN. THE MAINTENANCE VENDOR PERFORMED GROUND PRESSURIZATION RUN AND FOUND AIR LEAKING FROM UPPER ADF ANTENNA. A NEW GASKET WAS INSTALLED. LEAK CHECKS SASDR Y9PA20210818507Sleeve · corrodedRUDDER TORQUE TUBE, MID AND UPPER HINGE ATTACHMENT SLEEVES HAVE AREAS OF PITTING CORROSIONSDR 2021FA0000106Engine · flamed outAIRCRAFT DEPARTED SOUDA BAY IN ROUTE TO BANGKOK WHEN THE RIGHT ENGINE UNCOMANDED SHUTDOWN. THE CREW FOLOWED THE AFM PROCEDURES AND ATTEMPTED AN AIR START AND WAS UNSUCCESSFUL.THE AIRCRAFT LANDED AT THE INTENDED AIRPORT WITHOUT INCIDENT. THE ENGINE WAS INSPECTESDR 9JLA2021032422944Actuator · failedTHE FLIGHT CREW REPORTED THAT THE APU FAILED TO START WHEN COMMANDED. THE MAINTENANCE VENDOR DETERMINED THAT THE APU INLET DOOR ACTUATOR WAS FAULTY. THE ACTUATOR WAS REPLACED WITH A REPAIRED ACTUATOR AND ADJUSTED AS NEEDED. OPS CHECKS WERE SATISFACTORY AND THESDR 3GJA0001Controller · malfunctionedWHILE INFLIGHT AT 34,000FT, PILOTS WINDSHIELD CRACKED. AIRCRAFT DESCENDED TO NORMAL LANDING IN SRQ. SUSPECT HEAT CONTROLLER TO BE THE CAUSE OF THE WINDSHIELD CRACKING.SDR W6JA20210224044Iru · failedAIRCRAFT ENROUTE FROM KAPF TO KTEB, CREW WERE ALERTED TO AN AMBER CAS MESSAGE "IRS 1-2 COOL FAIL" CREW DIVERTED TO KRSW AND LANDED WITHOUT FURTHER ISSUE. AIRCRAFT AOG, AND RON. MAINTENANCE TROUBLESHOT THE PROBLEM TO A FAILED IRU. THE FAILED IRU WAS DEFERRED SDR VQMA2021021800000Converter · failedDEPARTED YIP TO EYW. DURING TAKE-OFF AFTER V1 THE CREW EXPERIENCED A FAILURE OF THE LEFT CONVERTER (AC&DC). THE TAKE-OFF WAS CONTINUED, ATC WAS NOTIFIED OF THE STATUS AND VECTORED THE CREW BACK TO YIP. THE PIC FLEW THE PLANE AND HANDLED THE RADIO. THE SIC SDR W6JA20210106041Oven · fireCREW REPORTED EXPERIENCING FIRE IN GALLEY, WITH SMOKE IN CABIN. DECLARED AN EMERGENCY TO LAND NEAREST AIRPORT. CO-PILOT WAS ABLE TO CONTAIN FIRE WITH A HAND HELD FIRE EXTINGUISHER TO GALLEY OVEN. SOURCE OF FIRE WAS FROM A CARDBOARD/FOIL CATERING CONTAINER ISDR W6JA20201014040Charger · failedELECTRICAL FAULT WAS TROUBLESHOT TO A FAILED LEFT BATTERY CHARGER, THE BATTERY CHARGER WAS REMOVED AND REPLACED WITH A REPAIRED UNIT, PER GULFSTREAM MAINTENANCE MANUAL PROCEDURES, WITH SATISFACTORY OPERATIONAL CHECKS COMPLETED AND NO FURTHER DISCREPANCY. ALL SDR VQMA2020060300001Unknown · smokeSMOKE IN CABIN EN-ROUTE SEEMINGLY ASSOCIATED WITH A RECENT CONFIGURATION CHANGE. RT COWL HEAT TURNED ON, "COOL TURB HOT" CAS MESSAGE, RT COWL HEAT TURNED OFF. RT PACK TEMP TURNED UP IAW COOL TURB HOT CHECKLIST, MESSAGE EXTINGUISHED, SMOKE EVENT FOLLOWED. UPSDR XCGA2020051500001Disk · crackedDURING ENGINE CALENDAR LIFE / OVERHAUL AT ROLLS ROYCE CANADA THE #10 HIGH PRESSURE COMPRESSOR DISK WAS FOUND TO HAVE 3 CRACKS IN THE DOVE TAILS AT THE 2, 4, AND 7 O'CLOCK POSITIONS.SDR 2020FA0000295Wheel · fracturedWHILE TAXIING PRIOR TO TAKEOFF THE NR 3 MAIN GEAR SUB WHEEL FAILED WHERE THE DEMOUNTABLE FLANGE RETAINING RING IS SEATED. THE DEMOUNTABLE FLANGE, RETAINING RING, SEAL AND TIRE DEPARTED THE MAIN GEAR SUB WHEEL WHICH REMAINED ATTACHED TO THE AXLE. AIRCRAFT TAXSDR BKEA202002260001Outflow Valve · malfunctionedAFTER TAKEOFF AND RETRACTING THE GEAR, NOTICED THAT THE AIRCRAFT WAS NOT PRESSURIZING AND THE OUTFLOW VALVE WAS INDICATING WIDE OPEN. SWITCHED TO ADC NR 2, THERE WAS NO CHANGE. LEFT ADC NR 2 ON AND THEN WENT TO MANUAL CONTROL. WAS ABLE TO CONTROL THE OUTFLOSDR BKEA202002180001Flap System · malfunctionedDURING THE APPROACH, THE FLAP STOPPED WORKING AT POSITION 20. EXECUTED A GO AROUND APPROACH TO THE HOLDING FIX. WHILE IN THE HOLD, REFERENCED THE QRH, PARTIAL FLAPS CHECKLIST. ELECTED TO GO TO OUR FILES ALTERNATE. DECLARED AN EMERGENCY AND DIVERTED TO ANOSDR 2020F00265Light · overheatedBAGGAGE OVERHEAD DOME LIGHT CAUSED A MELTING MARK ON PLASTIC BAGGAGE THAT CONTACTED DOME LIGHT LENS. INITIAL CORRECTIVE ACTION WAS TO RELEASE COMPANY WIDE SAFETY NEWSLETTER TO ADVISE OF THIS EVENT AND TO AVOID PLACING ITEMS HIGH ENOUGH TO CONTACT DOME LIGHT LESDR 2020F00264Computer · overheatedAT AN ALTITUDE OF FL410 ABOUT AN HOUR OF FLIGHT, THE CREW DETECTED A SMOLDERING ODOR OF WHAT APPEARED TO BE ELECTRICAL IN NATURE. THE CREW SELECTED GALLEY AND CABIN POWER OFF AND REFERENCED THE QRH FOR SMOKE OR FIRE IN FLIGHT. THE ODOR QUICKLY SUBSIDED AND IT SDR BKEA20200115001Control Panel · malfunctionedCONTROL PANEL WAS NOT SET TO DURING THE MONITORED FLIGHT. WE ALSO NOTED THAT WHEN THE CONTROL PANEL WAS SET, THE SYSTEM REPORTED PROPERLY. SWAPPED IN ANOTHER PANEL FROM N110SN FOR TROUBLESHOOTING WITH THE SAME RESULTS. THE QUESTION THEN BECAME, IS THE CONTROLSDR 2020FA0000004Windshield · crackedPILOTS WINDSHIELD ARCED INTERNALLY CAUSING THE OUTER PANE TO COMPLETELY CRACK DURING CLIMB WHILE PASSING THROUGH FL 39550.SDR W9FA201912050002Thrust Reverser · damagedINSPECT AND REPAIR THRUST REVERSER MOUNT HOLES AS REQUIRED. HOLES 2L,3L,LL, 5L, 8L, 9L, 10L AND 11L. REWORK PER GSL405420001. BUSHINGS REQUIRE INSTALLATION. HOLE 10L IS DEFORMED. HOLE 10L IS DEFORMED WHERE THE TITANIUM FACE OF THE MOUNTING FLANGE MEETS THE AL
Back to Gulfstream Aerospace G-IV