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 W6JA2019112017038Controller · failedAT FL430 CREW RECEIVED A "CABIN DIFFERENTIAL PRESSURE WARNING" REQUIRING AN EMERGENCY DESCENT. CABIN DID NOT REACH AN UNSAFE ALTITUDE AND EMERGENCY OXYGEN MASKS DID NOT DROP. MAINTENANCE DETERMINED CABIN PRESSURIZATION SELECTOR / CONTROLLER FAILED. AS A PRECAUSDR 2020F00035Engine · failedAT FL450 EXPERIENCED MODERATE TO SEVERE TURBULENCE. WHILE ADJUSTING THRUST LEVERS TO MAINTAIN AIRSPEED, EXPERIENCED A RIGHT POWERPLANT FAILURE. POWERPLAANT WAS RESTARTED AT FL250.SDR W6JA201910105037Downlock Switch · failedDURING APPROACH INTO KMCI GEAR WAS SELECTED DOWN AND THE NOSE LANDING GEAR DOWN LOCK INDICATION FAILED TO ILLUMINATE. FLIGHT CREW DECLARED AN EMERGENCY AND FOLLOWED CHECKLIST PROCEDURES FOR A GEAR NOT LOCKED CONDITION AND COMPLETED A SAFE LANDING. PINNED ALL LSDR 2019FA0000228Rivet · looseTHE AIRCRAFT CAME IN FOR AN INSPECTION AND WE NOTICED THE BOTTOM ROW OF RIVETS NEXT TO THE FUSELAGE ON BOTH SIDES OF THE VERTICAL STABILIZER HAVE BEEN WORKING. WE CONTACTED GULFSTREAM AND ARE WORKING TO GET A FIX FOR THE ISSUE.SDR W6JA201906197034Acm · failedAFTER DEPARTURE, SMOKE WAS OBSERVED IN THE CABIN, ALONG WITH A CAUTIONARY EICAS MESSAGE LT COOL TURB HOT. CREW SELECTED THE L PACK TO OFF, SMOKE SLOWLY DISSIPATED AND FLIGHT DIVERTED BACK TO DEPARTURE. REMOVED FAILED LT COOLING TURBINE AND INSTALLED OVERHAULEDSDR W6JA20190529032Unknown · odorDURING CRUISE FLIGHT AT ALTITUDE, THE FLIGHT CREW RECEIVED A “LT COOL TURB HOT” EICAS WARNING AND AN ODOR ASSOCIATED WITH THE HIGH TEMP. FLIGHT CREW USED CHECKLIST AND SHUTOFF LT ACM SYSTEM AND CONTINUED FLIGHT. DURING THE TIME THE WARNING OCCURRED THE CABIN ASDR BKEA2019040500004Warning Light · illuminatedRETURNED TO DEPARTURE IMMEDIATELY AFTER DEPARTURE WITH A RIGHT THRUST REVERSER UNLOCK LIGHT THAT ILLUMINATED DURING TAKEOFF. OPENSDR 2019FA0000106Valve · lockedWHEEL ANTI-ROTATION VALVE (P/N 1159SCH224-1) LOCKED UP CAUSING NR 3 AND NR 4 TIRE TO FLAT SPOT UPON LANDING.SDR W6JA20190214030Blade · damagedDURING TAKEOFF ROLL OUT, JUST PAST V1, CREW HEARD A SERIES OF POPPING NOISES FROM THE NR 2 ENGINE. DUE TO CURRENT AIRSPEED, CREW OPTED TO CONTINUE ROTATION & LIFTOFF. NR 2 ENGINE INDICATIONS BEGAN TO FLUCTUATE & PIC REDUCED POWER TO IDLE, WHILE SIC DECLARED ANSDR U5OA2019021100001Warning System · activatedUPON GEAR RETRACTION THE FLIGHT CREW OBSERVED A GEAR UP AND LOCKED INDICATION ISSUE WITH THE GEAR HANDLE ILLUMINATED RED. THE FLIGHT CREW ALERTED ATC AND FOLLOWED THE CHECKLIST ACCORDINGLY. THEY WENT GEAR DOWN AND OBSERVED NO DOWN AND LOCKED INDICATION FOR THESDR O2GA2019012447401Windshield · crackedDURING CRUISE FLIGHT LEFT WINDSHIELD OUTER PANE SHATTERED. MAINTENANCE REMOVED AND REPLACED LEFT WINDSHIELD. AIRCRAFT WAS RETURNED TO SERVICE.SDR U5OA201812281157Outflow Valve · inoperativeUNABLE TO MAINTAIN CABIN PRESSURIZATION ON CLIMB OUT ABOVE 12,000 FEET IN AUTO OR MANUAL MODE.SDR 2019FA0000012Safety Valve · failedCREW RECIEVED WARNING ON EICAS "CABIN LOW".SDR W6JA20181112028Uplock Hook · out of positionAFTER LIFTOFF FROM KVNY NOTED LEFT MAIN GEAR DID NOT RETRACT. CYCLED GEAR BACK DOWN AND SECOND RETRACTION ATTEMPT FAILED AGAIN. EXTENDED MAIN LANDING GEAR AND HAD NORMAL OPERATION WITH ALL THREE GREENS INDICATED, FLYING BY TOWER TO CONFIRM ALL LANDING GEAR EXTSDR W6JA20181014027Controller · malfunctionedAIRCRAFT PRESSURIZATION SYSTEM WENT INTO MANUAL MODE AND INTERMITTENT CASS MESSAGES APPEARED AND CLEARED WHILE IN CRUISE AND FINAL DESCENT. OBTAINED A SPECIAL FLIGHT PERMIT AND RELOCATED THE AIRCRAFT TO KPCD FOR MAINTENANCE. COMPLIED WITH ACSB BUS SWEEP AND TSDR W6JA20180919026Control Valve · crackedCOMBINED HYDRAULIC SYSTEM FAILURE ON SHORT FINAL TO BIKF. UPON LANDING NOTED HYDRAULIC LEAK COMING FROM RT LANDING GEAR WHEEL WELL AREA. FOUND "FLIGHT POWER SHUTOFF VALVE" LEAKING IN RT MAIN GEAR WELL. INSTALLED NEW VALVE P/N 1159SCH246-5 S/N 888. INSTALLATIONSDR 2018FA0000480Actuator · failedDISCREPANCY:HORIZONTAL STAB ACTUATOR P/N OFF 1159SCC200-43 S/N 97-909 FAILED DURING FLIGHT.
RESOLUTION: GULFSTREAM INSTALLED REPAIRED UNIT P/N 1159SCC200-45 S/N 1271 OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE SEPTEMBER 8, 2018SDR W6JA2018083027025Transducer · malfunctionedDURING CLIMB OUT AT FLT LEVEL 120, THE CABIN EXPERIENCED UNCONTROLLED PRESSURIZATION RESULTING IN THE CREW PERFORMING AN EMERGENCY DECENT. UPON SLOWING AIRCRAFT AND GEAR EXTENSION NORMAL PRESSURIZATION CONTROL WAS REGAINED. INSTALLED CABIN DIFFERENTIAL PRESSURSDR W6JA20180805023Unknown · smokeDURING CRUISE FLIGHT, AT 45,000FT AGL, THE FLIGHT CREW ACTIVATED THE ENGINE COWL ANTI-ICE AND SAW SLIGHT SMOKE IN COCKPIT AND CABIN. IMMEDIATELY TURNED OFF THE SYSTEM AND SMOKE CLEARED FROM CABIN. CONTINUED FLIGHT WITH NO FURTHER ISSUES. PERFORMED AN OPS CHESDR BQVA2018061400201Bearing · corrodedDURING INSPECTION, SIGNS OF RUST WERE DETECTED ON THE HORIZONTAL STABILIZER AFT PIVOT BUSHINGS, ON THE LEFT AND RIGHT SIDES. PIVOT BOLTS AND BEARING WAS REPLACEED.SDR BQVA2018060500001Skin · corrodedDURING COMPLIANCE OF CMP CODE 532085, THE LEFT AND RIGHT OVERWING AREAS BETWEEN THE DRAG BEAM AND WING TO BODY FAIRING, BS 257.5 - 512, FUSELAGE SKIN CORROSION WAS FOUND WHERE AFT WING ROOT MEETS THE FUSELAGE, STRINGERS 23 LT AND RT, BS 498-526.SDR W6JA20180503020Valve · failedLT NR 1 AND 2 MAIN TIRES BLOWN OUT DURING NORMAL LANDING. AIRCRAFT SUSTAINED ADDITIONAL DAMAGE DUE TO DEBRIS FROM TIRE. TECHNICIANS EVALUATED AND PREPARED AIRCRAFT FOR ONE-TIME FERRY FLIGHT FROM KBOS TO KBAF FOR PERMANENT REPAIRS. REMOVED FAILED ANTI ROTATION SDR E0X2018F00000Switch · out of adjustAIRCRAFT WAS IN MAINTENANCE TO REPLACE FAULTY RIGHT HAND THRUST REVERSER ACTUATOR. AIRCRAFT WAS RETURNED TO SERVICE ON 03/28/2018. UPON ATTEMPTING TAKEOFF BOUND FOR KAPC, THE CREW REJECTED THE TAKEOFF DUE TO A RIGHT HAND THRUST REVERSER UNLOCK INDICATION. TSDR W6JA20181230019Controller · failedDURING CLIMB OUT, AUTOMATIC PRESSURE CONTROL FAILED IN FLIGHT, CAUSING AN OVER-PRESSURIZATION OF CABIN. FLT CREW RETURNED TO DEPARTURE. TROUBLESHOT SYSTEM TO A FAILED CABIN PRESSURIZATION CONTROLLER. INSTALLED A REPAIRED UNIT. PERFORMED IN ACCORDANCE WITH SDR FOMA2018050100002Rod · crackedFINDING NOTED ON OTHER FLEET AIRCRAFT TRIGGERED SPECIAL EMPHASIS VISUAL INSPECTION. NOTED LONGITUDINAL CRACKS THROUGH RIVET POINT DUE TO EXPANSION FROM METAL CORROSION ON LEFT HAND AS WELL AS RIGHT HAND MAIN LANDING GEAR ROD ASSEMBLY, MAIN LANDING GEAR FAIRINGSDR W9FA20180212008Hinge Fitting · wornRIGHT ELEVATOR NR 3 LOWER HINGE FITTING WORN. REPAIRED IAW DRAWING SE05000102, REV E.SDR W9FA20180212007Hinge Fitting · wornRIGHT ELEVATOR NR 3 UPPER HINGE FITTING WORN. REPAIRED IAW DRAWING SE05000102, REV E.SDR W9FA201802120006Hinge Fitting · wornLEFT ELEVATOR NR 4 LWR HINGE FITTING WORN. REPAIRED IAW DRAWING SE05000102, REV E.SDR W9FA201802120004Hinge Fitting · wornLEFT ELEVATOR NR 4 UPPER HINGE FITTING WORN. REPAIRED IAW DRAWING SE05000102 REV E.SDR W9FA201802120003Hinge Fitting · wornLEFT ELEVATOR NR 3 UPPER HINGE FITTING, WORN. REPAIRED IAW DRAWING SE05000102 REV E.SDR W9FA201802120002Hinge Fitting · wornLEFT ELEVATOR NR 1 UPPER HINGE FITTING, DIAMETER IS ABOVE GO - NO GO LIMITS OF 0.3132. REPAIRED IAW DRAWING SE05000102 REV E.SDR W9FA201802120001Bushing · looseLEFT GROUND SPOILER ACTUATOR OUTBOARD UPPER BELLCRANK, WING MOUNT HOLE SLIP BUSHING LOOSE IN HOLE.SDR FOMA2018050100001Rod · crackedROUTINE POST-FLIGHT VISUAL INSPECTION NOTED LONGITUDINAL CRACKS THROUGH RIVET POINT DUE TO EXPANSION FROM METAL CORROSION ON LEFT AND RIGHT MAIN LANDING GEAR ROD ASSEMBLES, MAIN LANDING GEAR FAIRING, REMOVED THE AFFECTED PARTS AND REPLACED WITH NEW.SDR W9FA201802071Hinge Fitting · out of toleranceDURING AILERON TRIM TAB INSPECTION, HINGE FITTING OUT OF TOLERANCE. REPAIRED IAW 1159CSH20600. MAJOR REPAIR.SDR O2GA2018013031301Roller · defectiveFLAP ASYMMETRY FAULT AFTER TAKEOFF. AIRCRAFT YAWED TO RIGHT WITH AUTOPILOT ON. DISCONNECTED THE AUTOPILOT AND DIVERTED WITH 10 DEGREE FLAPS. MAINTENANCE REPLACED THE DEFECTIVE LEFT FLAP ROLLERS, FULL FLAP SYSTEM LUBE AND OPERATIONAL CHECK. A SUCCESSFUL OPERSDR W6JA20180102018Actuator · leakingFLIGHT CREW RECEIVED "LOW HYD QTY" WARNING IN FLIGHT, DECLARED AN EMERGENCY AND RETURNED TO KVNY FOR MAINTENANCE. MAINTENANCE EVALUATION DETERMINED RT MLG SIDE BRACE ACTUATOR LEAKING, P/N 1159SCL202-145, S/N A961, INSTALLATION 05/22/2014 IN "SERVICEABLE" CONDISDR UVVR2017122200047Valve · failedAFTER TAKEOFF, LANDING GEAR HANDLE WAS RAISED. RED LIGHT REMAINED ILLUMINATED IN LANDING GEAR HANDLE. LANDING GEAR HANDLE WAS LOWERED BUT GREEN LIGHT WOULD NOT ILLUMINATE FOR RIGHT MAIN LANDING GEAR. LEFT GEAR AND NOSE GEARING INDICATED DOWN AND LOCKED. LANDINSDR 2018F00047Iru · unknown. WE ROLLED OUT ON THE HEADING AND DEPARTURE CONTROL NOTIFIED US SHORTLY AFTER THAT WE WERE NOT ON ASSIGNED HEADING AND IN FACT 90 DEGREES OFF. WE DECIDED TO RETURN TO TEB AS WE WERE ALREADY BELOW MAX LANDING WEIGHT AND JETSMARTER WOULD BE ABLE TO ASSIST THE PSDR U5OA2011114000037Sensor · malfunctionedAFTER DEPARTURE, AUTO PRESSURIZATION FORCED OUTFLOW VALVE CLOSED, OVER PRESSURIZING CABIN. CAS MESSAGE INDICATED. FOLLOWED QRH, PERFORMED MANUAL SELECTION AND REGULATED CABIN PRESSURE. LEVELED OFF AND ASKED FOR DIVERSION. . PRESSURIZATION WAS CONTROLLABLE IN SDR DVYA201711200001Trunnion · corrodedDURING A 5000 LANDING GEAR INSPECTION, CORROSION WAS NOTED IN THE LEFT AND RIGHT MAIN LANDING GEAR TRUNNION BORES. REPAIRED IAW CS27764.SDR UG8A201710120001Attach Fitting · corrodedRUST COMING FROM THE LEFT HORIZONTAL-VERTICAL PIVOT LUG FITTING HALVES AND BEARING BORE. OVERSIZED TO FIRST OVERSIZE. CADMIUM PLATED IAW QQ-P-416 TYPE 2 CLASS 3. INSTALLED OVERSIZE BEARING IAW GAMPS 7120. ALL REWORK WAS ACCOMPLISHED IAW DRAWING SE05455106 RESDR 2017FA0000476Heating Element · shortedAFT GALLEY FLOOR HEATER PAD SHORTED OUT AND CREATED SMOKE IN THE CABIN DURING CLIMBOUT. GALLEY FLOOR HEAT SYSTEM WAS SUBSEQUENTLY DEACTIVATED.SDR 2017FA0000308Computer · inoperativeINTERMITTENT FAILURE OF THE TCAS COMPUTER. A REPLACEMENT UNIT WAS WAS INSTALLED AND TESTED SATISFACTORILY. THE ACFT SUBSEQUENTLY DEPARTED. THE OPERATOR HAS SINCE REPORTED THAT THE TCAS SYSTEM IS INOPERATIVE.SDR DXTAT2PL6D0059ZEUValve · failedFUEL COCK WOULD NOT GO OFF ON RIGHT ENGINE. SEVERAL ATTEMPTS FAILED. AFTER TROUBLESHOOTING FUEL COCK HANDLE NOT SHUTTING OFF ON RIGHT ENGING. FOUND OPERATING LEVER ON HIGH PRESSURE FUEL SHUT OFF VALVE LOCKING UP. REMOVED RT ENGINE GIGHT PRESSURE FUEL SHUTOFFSDR XPTA2017062100004Drive Shaft · disconnectedACFT DEPARTED. NO ISSUES DURING CLIMB. WHILE PASSING THRU FL 240, IT WAS OBSERVED THE ACFT HAD EXCESSIVE NOSE UP TRIM. AUTOPILOT ENGAGED AT THE TIME. THE ACFT, ASIDE FROM TRIM, FLEW NORMALLY. LEVELED OFF AT FL 410. AT CRUISE, AUTOPILOT HELD ACFT LEVEL, BUT TRSDR G02R20170802004Floorboard · puncturedFLOORBOARD PUNCTURED IN THE TOP SKIN OF FLOOR.SDR G02R20170724011Fitting · corrodedLEFT AND RIGHT HORIZ STAB PIVOT BUSHINGS AND LUGS CORRODED.SDR G02R20170724010Hinge Fitting · corrodedVERTICAL FIN, RUDDER HINGE, UPPER FITTING IS CORRODED.SDR G02R20170724009Hinge Fitting · corrodedVERTICAL FIN, RUDDER HINGE, CENTER FITTING IS PITTEDSDR G02R20170724008Hinge Fitting · corrodedVERTICAL FIN, RUDDER HINGE, LOWER FITTING IS PITTED.
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