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 UO22002F00010Line · damagedFOUND NUMEROUS SMALL NICKS AND DENTS IN THE FLARES OF SOME OF THESE TUBES. AFTER PERFORMING CLEANING OF THESE VENDOR SUPPLIED OXYGEN CLEAN TUBES, INDICATIONS WERE THAT SOME OF THE TUBES WERE DIRTY FROM THE VENDOR.SDR UO22002F00007Rivet · misinstalledTHIS IS A DISCREPANCY FROM THE FACTORY. FOUND A RIVET IN THE HOLE BUT NOT BUCKED. THIS WAS LOCATED IN THE FRAME STRUCTURE AND WIRE SUPPORT ATTACHMENT POINT, APPROXIMATELY 10 INCHES LEFT OF THE TOP CENTER OF THE FUSELAGE.SDR UO22002F00009Swivel · misinstalledTHE TOP SWIVEL POINT APPEARS TO BE INCORRECTLY SWAGED ALLOWING GREASE TO EXCAPE PAST THE SWAG AND THE CASTING.SDR 2002FA0000537Seat Belt · failedPASSENGER SEAT BELT BUCKLE FALLS APART. THIS IS THE 4TH INSTANCE OF THIS.SDR UO22002F00005Tube · mismanufacturedTHIS TUBE CAME NEW WITH THE FLARE INSTALLED ON THE WRONG END FOR PROPER INSTALLATION. MFG HAS ISSUED DWG 30-1080269 TO ALTER THIS NEW PART.SDR UO22002F00011Fitting · overtorquedWHILE INSPECTING (SN 046) FOUND THAT THE 2ND O2 BOTTLE INSTALLATION PLUMBING CAN NOT BE INSTALLED ACCORDING TO STC ST09748SC. THIS STC CALLS OUT MAX TORQUES ON THE PLUMBING FITTINGS. THE FITTINGS LEAK AT MAX TORQUES EVEN WITH THE TAPE ALLOWED INSTALLED ON THSDR G1X2002F00003Caliper · leakingSCRAPER SEALS FAILING. 3 AIRCRAFT, S BRAKE ASSEMBLIES SO FAR. SCRAPER SUPPORTS PISTON GUIDE AND IS COMING UNSEATED. THE GUIDE THEN SHIFTS IN THE BORE AND COCKS THE PISTON SIDEWAYS AND THE SEAL BECOMES INEFFECTIVE. WAITING ON ENGINEERING DISPOSITION FROM ABSDR G1X2002F00002Caliper · leakingSCRAPER SEALS FAILING. 3 AIRCRAFT, BRAKE ASSEMBLIES SO FAR. SCRAPER SUPPORTS PISTON GUIDE AND IS COMING UNSEATED. THE GUIDE THEN SHIFTS IN THE BORE AND COCKS THE PISTON SIDEWAYS AND THE SEAL BECOMES INEFFECTIVE. WAITING ON ENGINEERING DISPOSITION FROM ABSSDR G1X2002F00001Bracket · bentFDR POTENTIOMETER BRACKET INTERFERING WITH AILERON ACTUATOR AT FULL TRAVEL, BRACKET IS MOUNTED TOO FAR FORWARD DUE TO .1250 SHIM USED BETWEEN AFT SPAR AND THE BRACKET. SHIM SHOULD BE REMOVED AND POTENTIOMETER ADJUSTED FOR NEW POSITION. SHIELD SHOULD ALSO BE SDR G1X2002F00000Bracket · bentFDR POTENTIOMETER BRACKET INTERFERING WITH AILERON ACTUATOR AT FULL TRAVEL, BRACKET IS MOUNTED TOO FAR FORWARD DUE TO .1250 SHIM USED BETWEEN AFT SPAR AND THE BRACKET. SHIM SHOULD BE REMOVED AND POTENTIOMETER ADJUSTED FOR NEW POSITION. SHIELD SHOULD ALSO BE SDR VO22002F00000Hose · failedTHIS HOSE FAILED WHERE THE HOSE MEETS ITS END FITTING. THE HOSE COMPLETELY SEPARATED FROM THE END FITTING. THE HOSE WAS DATED O1/01. REPLACED THE SUSPECTED HOSES WITH NEW HOSES (DO NOT USE HOSES THAT THE MFG DATE IS 12/00 THE REMOVED HOSES RETURN TO IA)SDR VO22001F00000Screw · improper partIN FLIGHT AFT BAGGAGE FIRE WARNING LIGHT WENT OFF AND THE PRESSURIZATION SYSTEM TO THE AIRCRAFT BAGGAGE AREA WAS ISOLATED. AFTER LANDING THE RIGHT HAND BAGGAGE PANEL WAS REMOVED AND FOUND THAT THE HEATING ELEMENT CANNON PLUG BACKSHELL SCREWS WERE TOO LONG ANDSDR 2002FA0000026Starter Gen · failedSTARTER GEN FAILED.SDR G1X2001F00002Windshield · crackedAIRCRAFT DESCENDED FROM FL410 TO FL250 AND HEARD A LOUD POP SOUND. THE COPILOTS WINDSHIELD WAS SHATTERED IN THE INNER LAYERS. NO ICING CONDITIONS OR INDICATION OF STRIKE HAD OCCURRED.SDR G1X2001F00001Windshield · crackedAFTER APPROXIMATELY 5 HOURS OF FLIGHT AT FL430, THE PILOTS WINDSHIELD SHATTERED IN THE INNER LAYERS. WINDSHIELD HEAT WAS ON LOW. NO ICING CONDITIONS OR INDICATION OF STRIKE HAD OCCURRED.SDR G1X2001F00000Windshield · crackedWINDSHIELD ON COPILOTS SIDE SHATTERED IN FLIGHT.SDR VO22002F00001Rivet · wrong partFOUND NUMEROUS RIVETS THAT ATTACH THE STRAKES TO THE AFT FUSELAGE TO BE MS20450 TUBULAR RIVETS, NOT THE MS20470AD (BJ5) RIVETS CALLED FOR ON DRAWING. THE MS20450 TUBULAR RIVETS WERE OBSOLETED IN THE UNITED STATES IN 1968. GALAXY ENGINEERING WAS CONTACTED ANDSDR UO22001F00009Clip · brokenFOUND THE WINDOW CLIP, PN 4AS3421001009 LOCATED AT THE 7 O'CLOCK POSITION ON THE LEFT HAND NR 4 WINDOW COMPLETELY BROKEN OFF, APPROXIMATELY 1.40 INCHES FROM THE SCREW HOLD DOWN END. THE BREAK RAN NEARLY STRAIGHT, AND NEARLY PARALLEL WITH THE EDGE OF THE WINDOSDR UO22001F00008Coupling · splitFOUND THIS CABIN PRESSURIZATION, LOW PRESSURE, BLED AIR COUPLING(HOSE) SPLIT. THE SPLIT WAS APPROX 1 INCH FROM THE END OF THE HOSE AND 50 PERCENT AROUND IT, RUNNING PARALLEL TO ITS END. UNABLE TO DETERMINE IF IT SPLIT WAS CAUSED BY DAMAGE AT INSTALLATION OR SDR UO22001F00007Seat Belt · mismanufacturedON THREE NEW SEAT BELTS, THE METAL CLASP PART ON THE MALE SIDE, WAS .032 INCHES TO .040 INCHES TOO WIDE TO INSERT IN THE 1.125 INCH RECEPTACLE.SDR UO22001F00006Wire · misinstalledPOWER AND GROUND WIRE ROUTED TO APU STARTER THROUGH FIRE WALL WER ROUTED 180 DEGREES OUT OF SEQUENCE AND CONNECTED TO WRONG SIDE OF APU STARTER. THIS CONDITION EXISTED FROM THE MANUFACTURER. ADDITIONAL WIRE MARKINGS DESIGNATING GROUND AND POWER CABLES SHOULDSDR UO22001F00005Wire · misinstalledPOWER AND GROUND WIRES ROUTED TO APU STARTER THROUGH FIRE WALL WERE ROUTED 180 DEGREES OUT OF SEQUENCE AND SUBSEQUENTLY CONNECTED TO WRONG SIDE OF APU STARTER. THIS CONDITION EXISTED FROM THE MANUFACTURER. ADDITIONAL WIRE MARKINGS DESIGNATING GROUND AND POWESDR UO22001F00001Shock Mount · chafedA REPAIR WAS GENERATED TO CORRECT FOR A POSSIBLE METAL TO METAL CHAFING PROBLEM. AN INSPECTION REVEALED THAT THE UPPER AFT EDGE OF THE FORWARD FUEL TANK INTERFERES WITH THE FORWARD LOWER CORNERS OF THE FLAP DRIVE MOTOR SHOCK MOUNT SUPPORTS. PROBABLE CAUSE: SDR UO22001F00000Flapper Valve · leakingTHE AIRCRAFT CREW REPORTED THAT WHEN THE PLANE SAT OVERNIGHT, THE CENTER TANK WOULD HAVE MORE FUEL IN THE MORNING. WHEN THE NEW WING ROOT FLAPPER VALVES WERE INSTALLED THE FUEL MIGRATION CEASED. THE OLD (REMOVED) FLAPPER VALVES WERE MISSING THEIR RETENTION SSDR UO22001F00003Channel · misdrilledAN ELONGATED FASTENER HOLE WAS MIS DRILLED FROM THE MANUFACTURER. A REPAIR WAS GENERATED FOR THE RIGHT HAND RADIO RACK SUPPORT CHANNEL. PROBABLE CAUSE: MANUFACTURINGSDR UO22001F00002Shock Mount · chafedA REPAIR WAS GENERATED TO CORRECT FOR A POSSIBLE METAL TO METAL CHAFING PROBLEM. AN INSPECTION REVEALED THAT THE UPPER AFT EDGE OF THE FORWARD FUEL TANK INTERFERES WITH THE FORWARD LOWER CORNERS OF THE FLAP DRIVE MOTOR SHOCK MOUNT SUPPORTS HAT SECTIONS. PROBSDR 20010612CW016Controller · failedDEFECTIVE UNIT CAUSES AIRCRAFT TO AUTO PRESSURIZE, EICAS MISCOMPARE MESSAGE AND FAULT LIGHT TO ILLUMINATE. NO PROBABLE CAUSE FOR CABIN PRESSURE CONTROLLER FAILURE.SDR 20010612CW009Duct · leakingLEFT HAND CABIN INTERIOR UPPER CONDITIONED AIR DUCT WAS REMOVED FROM AIRCRAFT DUE TO AIR LEAKING FROM OUTBOARD OF DUCT. LEAKS WERE LOCATED DURING BENCH PRESSURE TESTING TO 5 PSI. REPAIRED LEAKS PER SPECIFICATIONS, PROBABLE CAUSE WOULD BE A MANUFACTURE DEFECTSDR 20010604CW011Duct · misalignedTHE FLEX COUPLER COULD NOT BE INSTALLED DUE TO MISALIGNMENT OF APU GENERATOR EXHAUST DUCT AND ADJOINING DUCT ON RIGHT HAND SIDE OF FUSELAGE.SDR 20010604CW010Duct · misalignedTHE FLEX COUPLER COULD NOT BE INSTALLED DUE TO MISALIGNMENT OF GENERATOR DUCT (APU) AND ASSOCIATED DUCT ON RIGHT HAND SIDE OF FUSELAGE.SDR 20010604CW009Actuator · malfunctionedORIGINAL EQUIPMENT RUDDER TRIM ACTUATOR FROZE UP AT ALTITUDE. WHEN DESCENDING TO WARMER AIR, THE ACTUATOR STARTED WORKING BUT NOT ALLOWING FOR FULL RUDDER TRIM TRAVEL. ACTUATOR WAS REPLACED WITH SERVICEABLE ACTUATOR.SDR 20010604CW008Valve · leakingORIGINAL INSTALLATION POWER BRAKE VALVE WAS FOUND TO BE LEAKING INTERNALLY CAUSING SKYDROL FLUID TO BE SPILLED ON THE PRESSURE SIDE OF THE FORWARD PRESSURE BULKHEAD.SDR 20010531CW005Duct · leakingRIGHT HAND UPPER AIR DUCT WAS FOUND TO BE LEAKING AT FACTORY SEALED SEAMS CAUSING LOW AIRFLOW TO RIGHT SIDE OF CABIN CONDITIONED AIR OUTLETS.SDR 20010530CW005Duct · misalignedTHE FLEX COUPLER COULD NOT BE INSTALLED DUE TO THE MISALIGNMENT OF THE DUCT FROM THE APU GENERATOR AND THE EXHAUST DUCT ON THE RIGHT SIDE OF THE FUSELAGE.SDR 20010529CW002Duct · misalignedTHE FLEX COUPLER COULD NOT BE INSTALLED DUE TO THE MISALIGNMENT OF THE DUCT FROM THE GENERATOR AND THE EXHAUST DUCT ON THE RIGHT SIDE OF THE FUSELAGE.SDR 20010507CW018Valve · crackedAT 41,000 FT. AIRCRAFT CABIN PRESSURE TARTED TO DROP. CREW RETURNED FOR MAINTENANCE WITHOUT INCIDENT. FOUND 1 INCH VERTICAL CRACK ON VALVE SEAT OF SAFETY VALVE.SDR G1X2002F00004Caliper · leakingSCRAPER SEALS FAILING. 3 AIRCRAFT S BRAKE ASSEMBLIES SO FAR. SCRAPER SUPPORTS PISTON GUIDE AND IS COMING UNSEATED. THE GUIDE THEN SHIFTS IN THE BORE AND COCKS THE PISTON SIDEWAYS AND THE SEAL BECOMES INEFFECTIVE. WAITING ON ENGINEERING DISPOSITION FROM ABSSDR 2002FA0000031Starter · failedSTARTERS ARE FAILING WITH ONLY 200 TO 300 HOURS.SDR 2002FA0000030Fitting · brokenFITTING HOLDS CABIN ENTRANCE DOOR AIR SPRING. SPRING GIVES DOOR SUPPORT DURING OPENING. DOOR SUPPORT DURING OPENING, FITTING BROKE ALLOWING DOOR WEIGHT TO HAVE TO BE SUPPORTED BY CREW. PART TT 1100 HRSSDR 20000328SH011Windshield · failedTHE PILOT''S WINDSHIELD (INNER PANE) SHATTERED AT FL 430. AT THIS TIME THERE IS NO POSSIBLE CAUSE. THE WINDSHIELD IS BEING SHIPPED TO THE MANUFACTURER TO DETERMINE CAUSE. (X)
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