Gulfstream Aerospace LP GALAXY
Service difficulty reports · 90
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 = 'GALAXY' 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 = 'GALAXY' 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 2026FA0000741Windshield · smokeSMOKE WAS OBSERVED EMITTING FROM THE LOWER SECTION OF THE R/H WINDSHIELD IN THE AREA OF THE HEATING ELEMENT. THE CREW TURNED OFF THE WINDSHIELD HEAT, AT WHICH TIME THE SMOKE CEASED.SDR 2026FA0000402Carbon Seal · leakingDURING DEPARTURE THE CREW NOTICED SMOKE IN THE CABIN. NOTIFIED TOWER AND RETURNED TO ICT. STANDARDAERO BORESCOPED THE ENGINE AND FOUND THE #5 CARBON SEAL LEAKING. REMOVED ENGINE FOR REPAIR AND INSTALLED A RENTAL ENGINE. TEST FLIGHT WAS SUCCESSFUL WITH NO SMOKESDR 2026FA0000284Carbon Seal · leakingDURING TAKE OFF FOR A SCHEDULED TEST FLIGHT REQUIRED FOR THE REINSTALLATION OF THE #1 ENGINE. IT WAS NOTICED THERE WAS SMOKE COMING IN THE CABIN AND COCKPIT GASPERS. AN EMERGENCY WAS DECLARED AND RETURNED TO AIRPORT WITH NO OTHER INCIDENT. THE FOLLOWING DAY MASDR 2025F00275Windshield · crackedKVNY TO MMSD. ONE HOUR INTO FLIGHT, RIGHT WINDSHIELD EXTERNAL LAYER CRACKED AT 39,000 FT. CREWS DECLARED PAN PAN PAN AND FOLLOWED QRH. FLIGHT RETURNED TO KVNY AND LANDED UNEVENTFUL.SDR 2025FA0000753Window · crackedPILOT REPORTED THEY DEPARTED KSNA AT 1501Z ON 10/23/2025. DESTINATION WAS KADS. WEATHER WAS NOT A FACTOR. FLIGHT WAS UNEVENTFUL UNTIL INITIAL CLIMB. APPROXIMATELY 15 MIN AFTER TAKEOFF, DURING AN INTERMEDIATE LEVEL OFF AT FL270 AND MACH 0.78, THEY HEARD A VERY SDR 2021FA0000195Anti-Skid Sys · failedON LANDING IN KASE THE ANTI-SKID SYSTEM FAILED AFTER 3-4 SECOUNDS. ANTI-SKID WAS RESET AND UPON RESET ALL TIRES BLEW AT THE SAME TIME AND LOSS BREAKING.SDR 2022FA0000019None · corrodedSKIN CORROSION FOUND UNDER ANTENNAS ON AIRCRAFT BELLYSDR CWQA201906040001Smoke Detector · false activationDURING CRUISE, CREW RECEIVED BAGGAGE SMOKE EICAS MESSAGE. CHECK LIST FOLLOWED, DESCENDED QUICKLY, EMERGENCY DECLARED, AND UNSCHEDULED LANDING PERFORMED WITHOUT INCIDENT.
MAINTENANCE EVALUATION DID NOT FIND ANY HARD FAILURES, EVIDENCE OF OVERHEATED/BURNT COMPSDR CA190329022Regulator Valve · failed(CAN) CREW REPORTED ENGINE ROLLED BACK DURING FLIGHT AT ABOUT 33000FT. DURING TROUBLESHOOTING THE PRESSURE REGULATING SHUT-OFF VALVE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR K5SR2016T27895Starter Gen · malfunctionedDURING NR 2 ENGINE START, THE STARTER GENERATOR AUTOMATIC CUTOUT FEATURE WHICH IS TO OCCUR AT 60 PERCENT N2 DID WORK. PILOT HAD TO MANUALLY DE-SELECT STARTER GENERATOR FROM OPERATING. REMOVED AND REPLACED THE STARTER GENERATOR. OPS CHECKED SATISFACTORY.SDR W6JA20160914009Fuel Door · departedAIRCRAFT RECEIVED FUEL, CREW THEN TAXIED AIRCRAFT TO ACTIVE RUNWAY TO WAIT APPROXIMATELY 15 MINUTES. AT NO POINT DURING THEIR WAIT DID THE REFUEL DOOR ILLUMINATE ON EICAS. AFTER DEPARTING RUNWAY AT 400-500 FEET ABOVE GROUND, THE REFUEL DOOR INDICATION ILLUMINASDR W6JA20160802008Control Unit · faultedTHE CREW NOTED A RED LEFT "BLEED AIR LEAK" EICAS MESSAGE FOR AN ENGINE BLEED AIR LEAK. MESSAGE ILLUMINATED AT FLIGHT 350. CREW FOLLOWED THE QRH PROCEDURES TO SHUT THE ENGINE DOWN DUE TO THE "BLEED AIR LEAK" MESSAGE WOULD NOT EXTINGUISH. CREW DID DECLARE AN EMSDR CWQA20160318001Roller · brokenDURING FLIGHT, CREW HEARD A THUMP & RECEIVED BAGGAGE DOOR OPEN MSG, NO NOTICEABLE PRESSURIZATION ISSUE NOTED. CHECKLIST FOLLOWED & UNSCHEDULED LANDING PERFORMED WITHOUT INCIDENT. EVALUATION FOUND THE BAGGAGE DOOR FWD LATCH PIN ROLLER BROKEN, ALLOWING DOOR TOSDR CA150525001Oil System · leaking(CAN) DURING CLIMB, CREW REPORTED HAZE AND SLIGHT ODOR IN THE CABIN. THERE WERE NO OTHER ISSUES REPORTED. CREW ELECTED TO RETURN TO AIRPORT OF DEPARTURE AND PERFORMED AN UNEVENTFUL LANDING. A SIMILAR EVENT WAS REPORTED IN 25 APRIL.SDR CA150518008Unknown · smoke(CAN) A PAX REPORTED SMOKE IN CABIN. THE EVENT WAS NOTED DURING CLIMB FROM AT APPROX 12K FEET. SUSPECTED THE ISSUE TO BE OIL MIST. DECLARED AN EMER & RETURNED TO DEPARTURE AIRPORT. THE ACFT LANDED & TAXIED WITHOUT ANY ISSUES. TROUBLESHOOTING REVEALED THATSDR CWQA20150223001Actuator · leakingDURING CRUISE AT FL410, CREW RECEIVED HYD LEVEL LOW RT LIGHT FOLLOWED BY AUX HYD PUMP ON LIGHT. CHECKLIST FOLLOWED, EMER DECLARED & UNSCHEDULED LANDING PERFORMED WITHOUT INCIDENT. EVALUATION FOUND EVIDENCE OF LT MAIN GEAR ACTUATOR LEAKING FROM HOUSING TO PISSDR DXTR2014082001Bracket · crackedANGLE AT BS 487 ON TOP OF FUEL BLADDER STRUCTURE IS CRACKED IN HALF. R & R BRACKET IAW G-200-53-144 AND ENGINEERING REPAIR ORDER ERO-605951.SDR DXTR2014072101Unknown · vibrationAT FL210, HAD AN AIRFRAME VIBRATION NOTICED AT 300 KIAS AND INCREASED AS AIRSPEED INCREASED. INTENSITY INCREASED IN LT TURNS, CLIMBS, DESCENTS, AUTO-PILOT ON & OFF, YAW DAMPER ON & OFF, RUDDER BIAS ON & OFF. HAD NO EFFECT. THERE WAS NO ABNORMAL VIBRATION IN SDR 9JLA2014072106430Actuator · defectiveTHE CREW REPORTED THAT THEY RECEIVED RT THRUST REVERSER FAIL CAS MSG ILLUMINATED DURING LANDING. THE THRUST REVERSER WOULD NOT FULLY DEPLOY. TROUBLESHOOTING FOUND THE RT SECONDARY LATCH ACTUATOR PN 288D0487-511 DEFECTIVE. THE LATCH ACTUATOR WAS REPLACED WITSDR DXTR2014061001Attach Angle · crackedANGLE AT FS 487 ON TOP OF FUEL BLADDER STRUCTURE IS CRACKED THROUGH.SDR 9JLA2014042106437Duct · crackedDURING POST FLIGHT CHECKS, BLUE WATER WAS NOTED DRIPPING FROM ACFT BELLY PANEL. INVESTIGATION FOUND THE LAVATORY WASTE DRAIN DUCT CRACKED INBD OF THE LAVATORY SERVICE PANEL. THE LAVATORY DRAIN DUCT WAS REMOVED & IT WAS NOTED THAT THERE WERE SEVERAL ATTEMPTS SDR DXTA2013112005574Engine · damagedCLIMBING THROUGH 38000' IN MAX CLIMB DETENT 290KTS TWO DISTINCT BANGS, SIMILAR TO COMPRESSOR STALLS, WERE FELT THROUGH FLOOR, RUDDERS & CONTROLS. ALL INSTRUMENT READINGS WERE NORMAL EXCEPT 1/4 SCALE ON RT VIB METER. DISCONNECTED A/P DES TO 24000 SLOWED 250KTSSDR 9BPA2012FA0000714Flex Line · failedPAX OXYGEN SYSTEM FAILED TO DEPLOY DURING FUNCTIONAL CHECK. UPON INVESTIGATION, MX FOUND MULTIPLE O2 FLEX LINES HAD FAILED AT MULTIPLE LOCATIONS ON EACH LINE. BASE PN ON ALL FLEX LINES IS O2C20T1. A TOTAL OF 6 LINES BLEW OUT. ALL WERE DIFFERENT LOT NUMBERS ANSDR CA120813008Engine · vibration(CAN) ON A REVENUE FLIGHT, THE FLIGHT CREW REPORTED THAT THE NR 2 ENGINE VIBRATION GAUGE WAS NOTED TO BE BETWEEN THE GREEN AND YELLOW BAND BUT THE VIBRATION COULD NOT BE FELT. THE PILOT THROTTLE BACK THE POWER TO IDLE WITH NO CHANGE ON THE VIBRATION INDICATIOSDR DXTA2012051104974Warning Light · illuminatedON APPROACH, AT 170KIAS THE LANDING GEAR WAS LOWERED. THE NOSE AND LT MAIN GEAR INDICATIONS WERE NORMAL. THE RT MAIN GEAR SHOWED AMBER FOR ABOUT 10 SECONDS FOLLOWED BY A RED INDICATION. THE ANTI-SKID FOR THE RT BRAKE INDICATED OFF. AFTER ABOUT 45 SECONDS THSDR DXTA2012030704907Selector Valve · leakingON GEAR EXTENSION, RECEIVED GREEN LIGHTS FOR LT MAIN AND NOSE GEAR BUT THE RT MAIN INDICATED YELLOW FOR APPROX 20 SECONDS FOLLOWED BY A RED "UNSAFE" INDICATION FOR ABOUT 30 SECONDS. ALSO SHOWED THE RT ANTISKID SYS INOPERATIVE. THE RT MAIN GEAR LIGHT THEN TSDR DXTA2011080204680Actuator · inoperativeUPON GEAR EXTENSION, THE RT MAIN GEAR INDICATION TURNED AMBER FOR A SHORT PERIOD OF TIME, THEN TURNED RED. THE RT ANTI-SKID OFF ILLUMINATED AS WELL. RECYCLED THE GEAR. EVENTUALLY GOT 3 GREEN INDICATIONS AND LANDED UNEVENTFULLY. DID NOT USE MANUAL GEAR EXTENSDR 2011F00095Sensor · damagedEICAS MESSAGE CARGO COMPARTMENT SMOKE MESSAGE. DISCOVERED CARGO COMPARTMENT HEAT BLANKET TEMPERATURE SENSOR DAMAGED CAUSING HEAT BLANKET TO OVERHEAT. PRIASDR 2011FA0000108Inlet Screen · wornON RECEPTION FOR MX THE LT ENGINE INLET ACOUSTIC MESH WAS FOUND DEPARTED FROM INLET AREA AT 3PM POSITION TO 6PM POSITION. ENGINE DIGESTED THE MESH CAUSING DAMAGE TO THE INLET CASE & STATOR GUIDE VANES.SDR DXTA200803089Wire · out of positionUPON FULL POWER APPLICATION AT APPROX 40KTS, RED BLEED PRESS / TEMP HI WARNING LIGHTCAME ON. ABORTED TAKEOFF. FOUND OVERPRESSURE SWITCH WIRES VERY CLOSE TO AN AIR SERVICE LINE. MOVED WIRES AWAY FROM SERVICE LINE. COMPLETED A SECOND ENG RUN. OPS CHECK GOOSDR DXTA200802759Float Valve · failedIN CRUISE FLIGHT AT FL380 WE NOTICED FUEL LEAKING OUT OVER THE LT AILERON. REMOVED DEFECTIVE LEFT WING VENT FLOAT VALVE AND INSTALLED NEW VALVE PER G200 CMP 28501.SDR DXTA200702431Sight Glass · crackedLT ENG OIL PRESS LOW EICAS MSG ON CLIMB OUT. (OIL PRESS 5 PSI INDICATED ON LT ENG) COMPLIED WITH QRH AND SECURED/SHUTDOWN ENG. REMOVED LT ENGINE UPPER AND LOWER COWLS. FOUND OIL FILLER NECK SIGHT GLASS LEAKING. REMOVED OIL FILLER NECK SIGHT P/N 30B6275-01 NSN SDR 2007FA0000014Life Raft · misriggedTHIS RAFT WAS INSTALLED ON AC BUT MAY BE INSTALLED ON OTHER SIMILAR AC. MOORING LINE (FIRING LINE) WAS FOUND RIGGED WRONG. LINE WAS TIED TO LIFE RAFT FIRST AND THEN TO THE PULL CABLE. THE LINE SHOULD BE TIED TO THE PULL CABLE FIRST AND THEN TO THE LIFE RAFTSDR 2007FA0000013Life Raft · misriggedTHIS RAFT WAS INSTALLED ON AC BUT MAY BE INSTALLED ON OTHER SIMILAR AC. MOOORING LINE (FIRING LINE) WAS FOUND RIGGED WRONG. LINE WAS TIED TO THE RAFT FIRST AND THEN TO PULL CABLE. THE LINE SHOULD BE TIED TO THE PULL CABLE FIRST AND THEN TO THE LIFE RAFT. RSDR 2007FA0000012Life Raft · misriggedTHIS RAFT WAS INSTALLED ON AC BUT MAY BE INSTALLED ON OTHER SIMILAR AC. MOORING THE LINE (FIRING LINE) WAS FOUND RIGGED WRONG. LINE WAS TIED TO LIFE RAFT FIRST AND THEN TO THE PULL CABLE. THE LINE SHOULD BE TIED TO THE PULL CABLE FIRST AND THEN TO THE LIFE SDR DXTA200601483Odor · unknownDURING FLIGHT FROM AFW TO EGE, STRONG EXHAUST ODOR IN THE COCKPIT AND DID NOT GO AWAY UNTIL AFTER SHUTDOWN. BORESCOPED LT, RT, APU BLEED AIR DUCTS LEADING TO ACM AND TRIM VALVES. FOUND NO TRACES OF ANY FUEL OR OIL. PERFORMED 30 MINUTE RUN ON BOTH ENGINES ANSDR DXTA200601317Engine · warning messageUPON APPLICATION OF TAKEOFF POWER, HAD A MASTER WARNING INDICATION. IT APPEARED TO BE THE BLEED PRESS/TEMP HI MESSAGE. MESSAGE WENT OUT IMMEDIATELY WHEN RETARDING THE THROTTLES. RAN APE FOR 30 MINS. RAN BOTH ENGINES FOR 20 MINS. ADVANCED BOTH ENGINES INDISDR O2G2006F00001Controller · failedAT FL370 AUTO PRESSURIZATION FAILED IN AUTO MODE. CAPTAIN DEPLOYED MASK AND SWITCHED TO MANUAL MODE AND RECOVERED CABIN ALTITUDE. REMOVED AND REPLACED PRESSURE CONTROLLER. (K)SDR O2G2006F00000Controller · failedAT FL370 AUTO PRESSURIZATION FAILED IN AUTO MODE. CAPTAIN DEPLOYED MASK AND SWITCHED TO MANUAL MODE AND RECOVERED CABIN ALTITUDE. COULD NOT CONTROL CABIN ALT PRESSURE IN MANUAL. CHANGED PRESSURE CONTROLLER AND FOUND LOOSE DUCT IN CABIN UNDER FLOOR AREA THATSDR DXTA200500980Fuel Filter · cloggedLEFT FUEL PRESS, LOW CAS MESSAGE ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AT 75 KNOTS. REPLACED FUEL FILTERS (BOTH ENGINES) AND LEAK CHECKED, NO LEAKS NOTED. OP'S CHECKED FUEL SYS FOR PRESS LOW CAS MESSAGE. SYS OP'S CHECKS GOOD, REF PW MAINT MAN 73-00-SDR DXTA200500975Trim System · malfunctionedIMMEDIATELY AFTER TAKEOFF THE NORMAL PITCH TRIM FROZE AT 2.6 DEG SETTING. AFTER SEVERAL MINUTES AND SEVERAL ATTEMPTS AT NOSE DOWN TRIM, SYSTEM WORKED NORMAL, HOWEVER SPEED WAS < 180 KIAS. ITEM IS UNDER INVESTIGATION.SDR 62GX20281Static Port · corrodedAIRCRAFT ADC (AIR DATA COMPUTER) - 200 FT SPLIT ON APPROACH TO LAND IN HEAVY RAIN. FOUND MOISTURE IN STATIC PORTS (4 EA) DURING POST FLIGHT INSPECTION. CLOSER INSPECTION REVEALED CORROSION ON THE INTERIOR OF THE STATIC PORTS. EXISTING STATIC PORTS (ST600R) SDR DXTA200400269Amplifier · overheatedDURING FLIGHT CREW DETECTED SMOKE IN THE COCKPIT, NOTICED SMOKE COMING OUT FROM BEHIND THE BOTTOM FORWARD 2 DRAWS. TURNED THE GALLEY POWER OFF AND AFTER A FEW MINUTES THE SMOKE STOPPED. CONTINUED FLIGHT TO DESTINATION WITHOUT INCIDENTS. - INSPECTED GALLEY ARESDR DXTA200400258Odor · detectedAFTER 1.5 HOURS INTO FLIGHT, CREW NOTICED EXHAUST ODOR IN COCKPIT, SELECTED DIFFERENT AIR SUPPLY AND PROBLEM REMAINED. PRECAUTIONARY DIVERTED TO ABQ. ITEM IS UNDER INVESTIGATION.SDR DXTA200300164Actuator · malfunctionedAFTER TAKEOFF DURING FLAP RETRACTION THE LEFT AND NOSE GEAR UNLOCK LIGHTS ILLUMINATED AND THE RIGHT GEAR WENT TO RED, ACCOMPLISHED AIR TURNBACK TO LAS. ADJUSTED RIGHT HAND MLG ACTUATOR LOCK PRESSURE TO THE GULFSTREAM -200 MM CHAPTER 32-10-10, PERFORMED FUNCTISDR V9B2003F00003Actuator · inoperativeRUDDER TRIM WOULD NOT MOVE. FOUND LOWER TRIM ACTUATOR RECEIVING POWER BUT IT WOULD NOT MOVE. INSTALLED NEW LOWER ACT PN 4AS5830510-013 BUT COULD NOT TIME ACTUATORS TOGETHER, SO REPLACED THE UPPER ACTUATOR AND WAS ABLE TO RIG ACTUATOR TOGETHER.SDR V9B2003F00002Actuator · inoperativeRUDDER TRIM INOPERATIVE. FOUND LOWER RUDDER TRIM ACTUATOR RECEIVING ELECTRICAL POWER BUT THE TRIM ACTUATOR WOULD NOT MOVE.SDR DXTA200300028Oil Cap · looseON CLIMBOUT RIGHT ENGINE LOW OIL PRESSURE MESSAGE CAME ON. RETARDED THROTTLE TO IDLE AND ENGINE PRESS DROPPED TO ZERO. SHUTDOWN THE RIGHT ENGINE PER CHECKLIST AND LANDED SAFELY AT CMH.SDR 2002FA0001223Servo · failedSERVO CAUSED AUTOPILOT MISTRIM CONDITION AND EVENTUALLY DID NOT PERMIT AUTOPILOT TO ENGAGE.SDR UO22002F00012Fastener · misinstalledTWO FASTENERS IN THE FUSELAGE TANK APPEAR TO BE MISINSTALLED WITH NO EDGE DISTANCE. THEY ALSO DUE NO SIT FLUSH. THESE FASTENERS ARE ACCESSED THRU THE UPPPER FUSELAGE PANELS 252 AR AND 250AT, AND ARE ONE ON EACH SIDE OF THE FAR UPPER CORNERS OF THE TANK.
Back to Gulfstream Aerospace LP GALAXY