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 N93A20060325Shutoff Valve · stuckUNABLE TO OPEN INTERIOR BAGGAGE DOOR IN FLIGHT, DUE TO BAGGAGE COMPARTMENT SHUTOFF VALVE BEING STUCK. (ACTIVATES ABOVE SPECIFIC ALTITUDE AND RELEASES BELOW SPECIFIC ALTITUDE.Mar 25, 2006 · N507QS · Gulstm GV · Pressure Regulator/Outflow ValveSDR 2006FA0000382Lamp · inoperativeDURING ROUTINE LAMP REPLACEMENT, IT WAS DISCOVERED THAT ONE END OF THE REMOVED UNIT WAS DISCOLORED. THE DISCOLORATION WAS THOUGHT TO BE DUE TO OVERHEATING. THE LOCATION OF THE FAILED LAMP WAS IN THE GALLEY OVERHEAD. INSTALLED NEW UNIT OF SAME MFG AND PN. OMar 23, 2006 · N1KE · Gulstm GV · Passenger Compartment LightingSDR 2006FA0000174Computer · failedDURING A RECENT FLIGHT DISPLAY UNITS 1,2, AND 3 BLINKED ON AND OFF. DISPLAY UNITS 1, 2 CYCLED ON AND OFF DISPLAY UNIT 3 WAS RED X`D. DURING THAT TIME AN AMBER (MAU 3A FAIL) MESSAGE DISPLAYED AND A BLUE (DATABASE CONFIG) MESSAGE ALSO DISPLAYED. AFTER 5-8 SECFeb 16, 2006 · N5PG · Gulstm GV · Indicating/Recording SystemSDR UG8AGM06001Actuator · bypassingON APPROACH, NOSE LANDING GEAR DID NOT EXTEND NORMALLY. EXTENDED GEAR USING EMERGENCY PROCEDURE. ANALYSIS REVEALED NOSE LANDING GEAR UPLOCK ACTUATOR BYPASSING HYDRAULIC FLUID. REMOVED AND REPLACED NOSE GEAR UPLOCK ACTUATOR. PERFORMED OPERATIONAL TEST PER GJan 27, 2006 · N5101 · Gulstm GV · Landing Gear ActuatorSDR 5075121805Windshield · failedLT WINDSHIELD SMOKED THEN CRACKED.Dec 18, 2005 · N518QS · Gulstm GV · Flight Compartment WindowsSDR 507512092005Insulation · odorACRID ODOR FROM LEFT PILLAR BETWEEN LT WINDSHIELD AND SIDE WINDOW.Dec 9, 2005 · N518QS · Gulstm GV · Standard Practices/StructuresSDR 12082005Odor · detectedBURNING SMELL IN COCKPIT. MAINTENANCE FOUND SPIRAL WRAP TOUCHING PILOTS MAP LIGHT ASSEMBLY AND OVERHEATING.Dec 8, 2005 · N518QS · Gulstm GV · Flight Compartment LightingSDR 64712072005Idg · failedLEFT ENGINE IDG FAILED IN FLIGHT, ATTEMPTED APU START WAS UNSUCESSFUL.Dec 7, 2005 · N511QS · Gulstm GV · AC Generator-AlternatorSDR 5075120605Wire · burnedCREW SMELLED A SULFER BURNING ODOR AND A PUFF OF SMOKE AT WINDSHIELD. MAINTENANCE FOUND LOOSE CONNECTION AT WINDSHIELD HEAT TERMINAL BLOCK.Dec 6, 2005 · N518QS · Gulstm GV · Ice/Rain Protection System WiringSDR 62309302005Rib · damagedON POST FLIGHT DAMAGE NOTED TO FAIRING ON OUTSIDE PORTION OF RT STABILIZER LOWER SURFACE.Sep 3, 2005 · N506QS · Gulstm GV · Horizontal Stabilizer, Spar/RibSDR 2004FA0000884Trunnion Pin · corrodedAIRCRAFT IN MAINTENANCE FOR THE SCHEDULED 5 YEAR LANDING GEAR CORROSION INSPECTION, FOUND AFT TRUNNION PINS AND THRU BOLT NAS1962C56 SEVERELY CORRODED. PARTS REPLACED WITH NEW.Nov 22, 2004 · N23M · Gulstm GV · Landing Gear Retraction/Extension SystemSDR 2004FA0000922Trunnion Pin · corrodedAIRCRAFT IN MAINTENANCE FOR THE SCHEDULED 5 YEAR LANDING GEAR CORROSION INSPECTION. FOUND AFT TRUNNION PINS AND THRU BOLT PN: NAS1962C56 SEVERELY CORRODED. PART REPLACED WITH NEW.Nov 22, 2004 · N300K · Gulstm GV · Main Landing Gear Attach SectionSDR 2004FA0000608Line · looseAT FL 410 RECEIVED A CABIN PRESSURE LOW (RED) MESSAGE ON YTHE CAS. AIRCRAFT INITIATED EDM APPROX. FL 380 CAS MESSAGE EXTINGUISHED LEVELED OFF AT FL 200. UNDECLARED AN EMERGENCY. APPROX. 10 MIN LATER RECEIVED ANOTHER CABIN PRESSURE LOW MESSAGE, DECLARED AN EMEJun 25, 2004 · N300K · Gulstm GV · Hoses and TubesSDR QRX2004F00002Switch · failedSWITCH FAILED. FOUND THE SWITCH HOUSING FULL OF WATER. THIS SWITCH IS LOCATED ON THE TOP SIDE OF THE ENGINE NACELLE. IT APPEARS TO HAVE WATER MIGRATING THROUGH THE SWITCH PLUNGER INTO THE HOUSING. THIS COULD COME FROM BEING PARKED IN THE RAIN OR AIRCRAFT BOct 29, 2003 · N130GV · Gulstm GV · Engine Thrust ReverserSDR EC3R200300001Controller · corrodedDURING A ROUTINE SCHEDULED INSPECTION, PASSENGER CABIN ENTERTAINMENT SYSTEM CONTROLLER P/N 1451-1-1 AND 1-1-2 COMPONENTS WERE BEING REPLACED DUE TO CUSTOMER REQUEST, PRIOR TO INSTALLATION A BENCH CHECK WAS PERFORMED ON UNITS AND THE UNITS FAILED TEST. UPON OPEApr 24, 2003 · Gulstm GV · Entertainment SystemSDR UG82001F00007Pump · damagedENGINE DRIVEN HYDRAULIC PUMP, DAMAGED.Sep 11, 2001 · N910DC · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR UG82001F00006Pump · damagedENGINE DRIVEN HYDRAULIC PUMP, DAMAGED.Sep 11, 2001 · N910DC · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 2001FA0000484Thermoswitch · wrong partFOUND THERMAL SWITCH PN 512T130B150001 INSTALLED. REMOVED SWITCH AND INSTALLED PN GAS850DF512-250 REV B. THIS SWITCH CORRECTED PROBLEM. THE REMOVED SWITCH CAUSED (FIRE WARNING LIGHT FOR THE LEFT AFT DUCT) TO COME ON. NO LEAKS NOTED. THE SWITCH REMOVED WASSep 6, 2001 · N15UC · Gulstm GV · Fire DetectionSDR 20010613CW016Pump · deterioratedFLUID SAMPLE TAKEN AT 100 HR INTERVAL SHOW THAT THE PUMP NEEDS TO BE REPLACED. REPLACE PUMP AND BLED SYSTEM WITH SIGHT GAUGE INSTALLED IN RETURN LINE OF HYDRAULIC RIG, TO HELP EVALUATE AIR REMOVAL FROM SYSTEM.May 29, 2001 · N83M · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 20010601CW013Clip · shearedNR 1 BRAKE, OUTBOARD ROTOR, DRIVE CLIPS FAILED AND SHEARED OFF THE ROTOR. EIGHT(8) SHEARED OFF OUT OF SIXTEEN (16) TOTAL PER ROTOR. CAUSE: THE CARBON FIBER ROTOR MATERIAL, FAILED. BRAKE WAS REPLACED WITH OVERHAULED UNIT. NO OTHER DAMAGE WAS NOTED. AIRCRMay 9, 2001 · N920DC · Gulstm GV · BrakeSDR 20010427CW005Computer · incorrectAFTER DEPLOYING AND STOWING THE THRUST REVERSERS THE THRUST REVERSER MISCOMPARE ANNUNCIATOR ILLUMINATED MOMENTARILY. APPARENT CAUSE WAS DCU DATA LATCH UP. CONFIRMED BOTH T/RS TO BE STOWED PROPERLY AND RESET DCU, NR 1 AND NR 2 WITH NO FURTHER OCCURRENCE.Apr 10, 2001 · N5102 · Gulstm GV · Engine Thrust ReverserSDR 20010503CW002Pump · defectiveFLUID CONTAMINATION IN RIGHT ENGINE PUMP WAS THE LATEST MODEL AND WAS NEW AT INSTALLATION AND HAS ONLY BEEN OPERATED FOR 48.4 HOURS. WE ARE GETTING BETTER TIME OUT OF THE OLD STYLE PUMPS.Mar 29, 2001 · N73M · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 20010312CW002Tire · failedNOSEWHEEL TIRE HAS SEPARATION OF TREAD FROM CARCUS. BONDING BETWEEN TREAD AND CARCUS DEBONDED.Feb 13, 2001 · Gulstm GV · TireSDR 20001229SH013Terminal Block · damagedKPTK - DURING ACCOMPLISHMENT OF GAC CB41 FOR IDG SWEDGED TERMINAL INTEGRITY, ONE OF THE TERMINAL LUGS PULLED OFF THE FEEDER WIRE BY HAND. IMPROPERLY SWEDGED TERMINAL END. GULFSTREAM DISPATCHED TECH TO REPLACE ALL TERMINAL LUGS ON INTEGRATED DRIVE GENERATOR''Dec 20, 2000 · N910DC · Gulstm GV · Alternator-Generator DriveSDR 20001219SH002Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDED TO BE REPLACED. REPLACED PUMP, WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 640.8 HOURS. TOTAL CYCLES 347. (X)Nov 16, 2000 · N93M · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 20001219SH001Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDED TO BE REPLACED. REPLACED PUMP, WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 640.8 HOURS. TOTAL CYCLES 347.Nov 16, 2000 · N93M · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 20001218SH037Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP, WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 640.8 HOURS. TOTAL CYCLES 347. (X)Nov 16, 2000 · N93M · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 20001218SH028Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 812.0 HOURS. TOTAL CYCLES 546. (X)Nov 16, 2000 · N83M · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 20001218SH027Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP, WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 812.0 HOURS. TOTAL CYCLES 546. (X)Nov 16, 2000 · N83M · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 20001218SH025Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THAT THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP. WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 850.3 HOURS. TOTAL CYCLES 567. (X)Nov 16, 2000 · N73M · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 20001218SH024Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 850.3 HOURS. TOTAL CYCLES 567. (X)Nov 16, 2000 · N73M · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 20000829SH018Brake · crackedROTOR OF THE NR 2 BRAKE ASSEMBLY HAD SMALL CRACKS. THESE CRACKS CAN BE SEEN BY LOOKING THROUGH THE VENTILATION HOLES IN THE WHEEL. REPLACED THE BRAKE ASSEMBLY, THE WHEEL WAS NOT DAMAGED BECAUSE NONE OF THE CLIPS HAD COME LOOSE. (X)Aug 15, 2000 · N93M · Gulstm GV · BrakeSDR 20000817SH007Rotor · crackedWHILE DOING A PRE-FLIGHT INSPECTION, NOTICED THE NR 2 BRAKE OUTBOARD ROTOR DRIVE CLIPS APPEARED TO BE SPLINTERING AND CRACKING. REMOVED THE WHEEL AND FOUND THE NR 1 ROTOR CLIP WAS CRACKED AND THE NR 2 ROTOR FORWARD DRIVE CLIPS WERE BROKEN LOOSE. REPLACED BOTAug 11, 2000 · N73M · Gulstm GV · BrakeSDR 20000817SH006Rotor · crackedWHILE DOING A PRE-FLIGHT INSPECTION, NOTICED NR 2 BRAKE OUTBOARD ROTOR DRIVE CLIPS APPEARED TO BE SPLINTERING AND CRACKING. REMOVED THE WHEEL AND FOUND THE NR 1 ROTOR CLIP WERE CRACKED AND THE NR 2 ROTOR FORWARD DRIVE CLIPS WERE BROKEN LOOSE. REPLACED BOTH BAug 11, 2000 · N73M · Gulstm GV · BrakeSDR 20000613SH015Brake · damagedREMOVED NR 1 WHEEL FOR TIRE CHANGE. WHILE INSPECTING BRAKE ASSY, NOTICED ALL THE KEYWAY SLOTS ON THE OUTBOARD ROTOR WERE COMPLETELY MISSING. SOME DAMAGE HAD OCCURRED TO THE WHEEL WHEN THE PIECES WERE EXITING. BRAKE AND WHEEL ASSYS WERE REPLACED. (X)May 31, 2000 · N83M · Gulstm GV · Landing Gear Brake SystemSDR 20000613SH004Brake · damagedWHILE REMOVING NR 2 MAIN WHEEL ASSY FOR A TIRE CHANGE, NOTED ON THE BRAKE INSPECTION THAT THE OUTBOARD ROTOR KEYWAY SLOT CLIPS WERE BREAKING AWAY FROM THE ROTOR. WHEEL ASSY HAD SOME DAMAGE FOR LOOSE CLIPS. BRAKE AND WHEEL ASSYS WERE BOTH REPLACED. (X)May 31, 2000 · N83M · Gulstm GV · Landing Gear Brake SystemSDR 99ZZZX4243Wire · chafedINSPECTION OF RIGHT ENGINE INTEGRATED DRIVE GENERATOR FEEDER WIRES REVEALED A CHAFE CONDITION BETWEEN THE WIRE AND THE FIRE LOOP BRACKET AT THE 6 O'CLOCK POSITION. SPACER WAS ADDED TO WIRE BUNDLE CLAMPS TO GIVE PROPER CLEARANCE BETWEEN WIRE BUNDLE AND FIRE LOOct 26, 1999 · N73M · Gulstm GV · Starter-GeneratorSDR 99ZZZX4233Wire · chafedINSPECTION OF RIGHT INTEGRATED DRIVE GENERATOR FEEDER WIRES REVEALED A CHAFE CONDITION BETWEEN THE WIRES AND THE FIRE LOOP BRACKET AT THE 6 O'CLOCK POSITION. DAMAGE TO THE WIRE INSULATION IS WITHIN LIMITS. SPACERS WERE ADDED TO WIRE BUNDLE CLAMPS TO GIVE PROOct 26, 1999 · N93M · Gulstm GV · Starter-GeneratorSDR 99ZZZX4232Wire · chafedINSPECTION OF RIGHT ENGINE INTEGRATED DRIVE GENERATOR FEEDER WIRE REVEALED A CHAFE CONDITION BETWEEN THE WIRES AND THE FIRE LOOP BRACKET AT THE 6 O'CLOCK POSITION. DAMAGE TO THE WIRE INSULATION IS WITHIN LIMITS. SPACERS WERE ADDED TO WIRE BUNDLE CLAMPS TO GIOct 26, 1999 · N83M · Gulstm GV · Starter-GeneratorSDR 99ZZZX4188Monitor · failedCABIN COMPARTMENT AFT TV SCREEN CAUGHT FIRE DURING TAXI FOR TAKEOFF. FORWARD GALLEY HALON FIRE EXTINGUISHER USED TO PUT OUT FLAME. SUBMITTER STATED AT THIS TIME, THE CAUSE OF THE MONITOR FAILURE IS UNDETERMINED.Sep 21, 1999 · N920DC · Gulstm GV · Cabin Equipment/FurnishingsSDR 99ZZZX21Fastener · crackedDURING COMPLIANCE OF SB-BR700-72-900062, FOUND NUMEROUS FASTENERS CRACKED.Nov 4, 1998 · N158AF · Gulstm GV · Aerodynamic FairingsSDR 99ZZZX20Fastener · crackedDURING COMPLIANCE OF SB-BR700-72-900062, FOUND FASTENER MISSING AND NUMEROUS FASTENERS CRACKED.Nov 4, 1998 · N313RG · Gulstm GV · Aerodynamic FairingsSDR 98ZZZX4030Pump · overheatedTHE AIRCRAFT WAS IN CRUISE AT 45,000 FEET WHEN THE R1 HYDRAULIC PUMP FAILED. TEN MINUTES LATER, R2 PUMP FAILED. THERE WAS NO FLUID LOSS AT THIS POINT. ON FINAL WHEN THE LANDING GEAR WAS SELECTED DOWN, THE RIGHT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO.Sep 17, 1998 · N158AF · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 98ZZZX4029Pump · overheatedTHE AIRCRAFT WAS IN CRUISE AT 45,000 FEET WHEN THE R1 HYDRAULIC PUMP FAILED. TEN MINUTES LATER, R2 PUMP FAILED. THERE WAS NO FLUID LOSS AT THIS POINT. ON FINAL WHEN THE LANDING GEAR WAS SELECTED DOWN, THE RIGHT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO.Sep 17, 1998 · N158AF · Gulstm GV · Hydraulic Pump (Electric/Engine), MainSDR 98ZZZX4031Pump · failedNR 1 ENGINE HYDRAULIC PUMP L2 OVERHEATED AND FAILED IN-FLIGHT.Sep 16, 1998 · N777GV · Gulstm GV · Hydraulic Pump (Electric/Engine), Main
Back to Gulfstream Aerospace G-V