Gulfstream Aerospace G-1159A
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 = 'G1159A' 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 = 'G1159A' 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 ESPA2019F00224Wing · corrodedRIGHT WING HAS CORROSION ON AFT SPAR AT RBS343.SDR ESPA2019F00223Spar · corrodedFOUND CORROSION ON WING AFT SPAR AT RBS 406.SDR 2016F00212Flap System · inoperativeFLAPS WOULD NOT EXTEND DURING DESCENT. DIVERTED AND DECLARED AND EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT.SDR ESPA2016F00182Unknown · malfunctionedAFTER TAKEOFF, ENROUTE, AT ALTITUDE THE AIRCREW EXPERIENCED SOME TURBULENCE AND THE PIC REPORTED A SUDDEN LOSS OF PRESSURIZATION. THEY DECLARED AN EMERGENCY DESCENT TO THE NEAREST AIRFIELD. WE DISPATCHED A TECH TO TROUBLESHOOT THE PROBLEM. UPON TROUBLESHOOTSDR VM0R2015FA0000158Door · malfunctionedACFT HAD AN AFTER TAKEOFF NOSE GEAR DOOR CLOSING PROBLEM. THE CREW REPORTED A WIND NOISE AND VIBRATION ISSUE AND NOTED THE RED GEAR HANDLE LIGHT WAS ILLUMINATED INDICATING AN INCOMPLETE RETRACTION OF THE LANDING GEAR. THE GEAR WAS EXTENDED AND THE ACFT RETURSDR 2015FA0000018Cable · out of adjustIMPROPER DEFLECTION OF RUDDER TRIM CABLE AT FS 163 CAUSING, SAWING, AT LIGHTNING PASSTHRU HOLE. THE MAINTENANCE AND PARTS MANUALS DO NOT SHOW THE BRACKET AND PULLEY ASSY IN THIS AREA. WHEN THE PULLEYS ARE REMOVED, THE CABLES REMAIN IN A POSITION FOR ADDITIONSDR BQVA20150109001Converter · faultyLEFT AC & LEFT DC POWER FAIL INDICATORS ILLUMINATED.SDR 2014FA0000466Window · failedWHILE CLIMBING THROUGH 390 TO FL430 THE RT AFT-MOST PASSENGER WINDOW CRACKED AND BLEW OUT. THEN THE RT ENGINE FLAMED OUT. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO LAND. AIRPORT FIRE AND RESCUE DISPATCHED AND THE ACFT TAXIED TO THE RAMP WITHOUT FURTHERSDR BQVA20140425001Spar Cap · corrodedDURING COMPLIANCE OF CMP CODE 279010 LT AILERON HINGE INSPECTION, A SMALL AREA OF CORROSION WAS FOUND ON THE WING AFT LOWER SPAR CAP JUST OTBD OF THE CTR AILERON HINGE.SDR Y3PR201403270001Attach Bolt · crackedDURING LT FLIGHT SPOILER BELLCRANK INSPECTION, MAGNETIC PARTICLE INSPECTION INDICATED A POSSIBLE CRACK AROUND THE ENTIRE CIRCUMFERENCE OF THE PINS HEAD. REPLACED PIN WITH NEW PIN.SDR BKEA2014012000040Windscreen · failedLEFT WINDSCREEN FAILED,SDR BKEA2014012000039Windscreen · failedLEFT WINDSCREEN FAILED.SDR AOYA20140104001Engine · power lossENGINE START & TAXI CHECKS WERE NORMAL. A ROLLING TAKEOFF WAS PERFORMED TO COMPUTED EPR'S. ALL ENG PARAMETERS WERE NORMAL DURING TAKEOFF ACCELERATION UNTIL A DROP IN THE LT ENG EPR TO APPROXIMATELY 1.9. THE LT ENG THRUST LEVER DID NOT RESPOND TO AN ATTEMPT TSDR BQVA20131211001Skin · corrodedDURING COMPLIANCE OF FUSELAGE EXTERIOR INSPECTION, CMP CODE 531020, FOUND CORROSION AT APU EXHAUST OPENING. STANDARD REPAIR APU DOOR SKIN FS 617.562 CURRENTLY IN PROGRESS.SDR A8OA2013050800005Fuel Cell · leakingDURING CLIMB NOTICED FUEL LEAKING FROM TOP OF LT WING. LEAK STOPPED AT 21,000 POUNDS INDICATED. AS A PRECAUTION THE CREW RETURNED TO DEPARTURE AND LANDED SAFELY. FOUND SCREWS LOOSE ON PANELS 21-FT UPR-25 AND 21-FT UPR-26 TIGHTENED SCREWS AND CHECKED FOR FUESDR 2013F00110Cooling Turbine · failedDURING CRUISE AT FL320, ACFT EXPERIENCE SMOKE IN THE CABIN. ACFT RETURNED TO DEPARTURE. INITIAL INVESTIGATION REVEALED TO A FAULTED COOLING TURBINE UNIT. FURTHER THE CONDENSER DRAIN LINE FROM THE TURBINE UNIT IS CRACKED FROM A PREVIOUS REPAIR MADE.SDR A8OA201301300003Windshield · crackedAFTER CRUISING FOR APPROX 1.5 HOURS THE CREW WITNESSED A LOUD CRACKING NOISE AND NOTICED THE PILOT SIDE, LT WINDSHIELD HAD CRACKED. THE WINDOW WAS SPIDERED VEINED WITH CRACKS COVERING THE ENTIRE SURFACE. THE CREW DONNED OXYGEN MASKS TURNED ON SEAT BELT SIGNSDR DVYA20120711001Turbine · damagedDURING APPROACH WHEN THROTTLES WERE RETARDED THE RIGHT ENGINE FLAMED OUT, ENGINE WAS SECURED AND UNEVENTFUL LANDING ACCOMPLISHED. UPON INVESTIGATION FOUND THE RIGHT ENGINE LOW PRESSURE COMPRESSOR/LOW PRESSURE TURBINE SECTION WOULD NOT ROTATE. HIGH PRESSURE CSDR 2012F00114Probe · groundedDURING CLIMB OUT, 1/3 RT ROLL WAS REQUIRED TO MAINTAIN LEVEL FLIGHT. THE ACFT RETURNED TO DEPARTURE.SDR GZXA20120417001Skin · damagedDURING POST FLIGHT WALK AROUND OF AIRCRAFT FLIGHT CREW NOTICE A SMALL DENT IN LEFT OUTBOARD LEADING EDGE. APPARENTLY CAUSED BY A BIRD STRIKE DURING UNKNOWN PHASE OF FLIGHT INTO AIRPORT.SDR 2012F00077Skin · dentedDURING POST FLIGHT WALK-AROUND BY FLIGHT CREW NOTICED A POSSIBLE BIRD STRIKE AND DENT ON LT OTBD L/E.SDR BQVR2011110700010Attach Fitting · corrodedDURING COMPLIANCE OF CMP CODES 576511 & 576516, WINGLET ATTACH HARDWARE INSPECTION (LT & RT), CORROSION FOUND IN THE WINGLET ATTACH BORES ONCE THE BUSHINGS WERE REMOVED.SDR BQVA2011041900009Winglet · corrodedDURING COMPLIANCE OF CMP CODES 576511 & 576516 WINGLET ATTACH HARDWARE (LEFT & RIGHT) - INSPECTION (144 MONTH), SOME CORROSION WAS FOUND IN THE WINGLET ATTACH BORES ONCE THE BUSHINGS WERE REMOVED.SDR 2011F00019Engine · flamed outAT FL 430, ENCOUNTERED MODERATED MOUNTAIN WAVE WITH AIRSPEED FLUXUATION OF MACH .80 TO .72. AT THIS TIME WE HAD THE NR 2 ENGINE FLAMEOUT. PERFORMED NORMAL DESCENT TO AIRSTART ENVELOPE, COMPLIED WITH AIRSTART CHECKLIST, NO DEFECTS NOTED, CONTINUED TO DESTINASDR 2010FA0001095Attach Bracket · cracked(S6NR) FLIGHT CREW REPORTED MAIN ENTRY DOOR WOULD HANG AT CLOSURE, INVESTIGATED ANOMALY AND DISCOVERED UPPER MAIN ENTRY DOOR ATTACH FITTING CRACKED. CONTACTED MFG STRUCTURAL DEPT AND DIVULGED FINDINGS. AFTER CONVERSATION WITH TECH SUPPORT, WAS INFORMED OF A SDR BQVA2010082300007Bulkhead · corrodedSUSPECTED CORROSION FOUND DURING INSPECTION OF THE FS 580 BULKHEAD SKIN SPLICE, AREA LONGERONS AND STRINGERS 24 L/R IN ACCORDANCE WITH CMP 539540. AFTER FURTHER NDT THE AREA WAS FOUND TO HAVE MINOR SURFACE CORROSION WHICH WAS REMOVED AND TREATED. FINDINGS WSDR 2010FA0000834Duct · damagedDURING POST FLIGHT INSP WITH THE APU RUNNING AND BLEED AIR SELECTED ON, IT WAS NOTED THAT THERE WAS A HOLE IN THE INSULATION OF THE APU AND GROUND START DUCT, AND BLEED AIR FELT TO BE ESCAPING. FURTHER INVESTIGATION FOUND THAT A TWO (2) INCH CRACK HAD DEVELOPSDR BQVA2010041200006Skin · corrodedDURING A WING NDT INSPECTION OF THE LT WING PLANK AT FS 452 BL 33, CORROSION WAS FOUND. ENGINEERING HAS DETERMINED THIS CORROSION IS EXCESSIVE ENOUGH TO REQUIRE ACCOMPLISHMENT OF ASC 229, WHICH WILL REMOVE THE CORROSION ON THE PLANK AND INSTALL A THREE PIECE SDR BQVA2010040900005Attach Fitting · crackedDURING THE REQUIRED EDDY CURRENT INSPECTION OF THE FS 793 BULKHEAD CAP ANGLE, CRACKS WERE FOUND AROUND LEFT AND RIGHT BOLT HOLES IN THE CAP ANGLE FOR THE VERTICAL FIN ATTACHMENT.SDR BQVA2010030100005Downlock Switch · defectiveAIRCRAFT DEPARTED FROM KHPN EN ROUTE TO KFPR. CREW SELECTED GEAR HANDLE DOWN AND RECEIVED A RED HANDLE WARNING INDICATION. AIRCRAFT FLEW PAST CONTROL TOWER TO VERIFY THE LANDING GEAR WAS DOWN. RETRACTED LANDING GEAR AND DIVERTED TO KPBI AND LANDED WITH OUT SDR BQVA2010010400004Windshield · crackedRIGHT SIDE WINDSHIELD OUTER PANE FAILURE DURING FLIGHT. REMOVED AND REPLACED WINDSHIELD.SDR WWQ2009F00002Valve · leakingAFTER TAKEOFF, WHEN THE CREW SELECTED GEAR UP THEY NOTICE UNUSUAL SOUNDS. ALL INDICATIONS SEEMED TO BE NORMAL AND FLAPS WERE SELECTED UP. THE COMBINE HYDRAULIC SYS BEGAN TO FALL. THE CREW GOT INDICATIONS THAT THE PRESSURE WAS LOW, THEN OK, THEN LOW AGAIN. SDR AI5R2009RS002Bottle · emptyTHE LIFE RAFT ARRIVED AT OUR FACILITY FOR ANNUAL INSPECTION. UPON INSPECTING AND WEIGHING THE CO2 CYLINDER, IT WAS DISCOVERED THAT THE CYLINDER WAS EMPTY.SDR AI5R2009RS001Cylinder · emptyUPON INSPECTING THE HYDROSTATIC TEST DATE ON THE CO2 CYLINDER, IT WAS DETERMINED THAT THE CYLINDER WAS DUE FOR HYDROSTATIC TESTING, AND WE THEN PULLED THE CYLINDER CABLE TO RELEASE THE CO2 FROM INSIDE THE CYLINDER. UPON DOING THIS, WE DISCOVERED THAT IT THE CSDR 2009FA0000760Tire · failedON TAKEOFF AT 1622Z, ACFT BLEW NR 4 RT OTBD TIRE. UPON RETURN LANDING BACK AT DEPATURE, THE FOLLOWING DAMAGE WAS FOUND: RT INBD FLAP, RT LWR COWL, RT ENG T/R, AND RT GEAR DOOR OTBD. THIS TIRE SN FALLS WITHIN GY SB 2008-32-001. (K)SDR WWQ2009F00000Engine · failedDURING CLIMB OUT, AFTER TAKEOFF, APPROXIMATELY 5K FEET THE CREW HEARD A LOUD BANG FROM THE LT ENGINE. THE CREW CHECKED THE ENGINE PARAMETERS AND FOUND 0 EPR AND NOTICED THAT THE POWER LEVER WAS UNRESPONSIVE ON THE LT ENGINE. LP HP WAS APPROXIMATELY 30 PERCENSDR 2010F00114Windshield · crackedLEFT WINDSHIELD OUTER PANE CRACKED AT FL410, DESCENT TO 10,000 FT AND RETURNED TO AIRPORT. NO LOSS OF PRESSURIZATIONSDR YJU2008F00000Tire · unserviceablePILOTS REPORTED THAT ON TAKEOFF, THEY FELT A BUMP FOLLOWING THE VR CALLOUT. AFTER LANDING, IT WAS DISCOVERED THAT THE NR 3 MAIN TIRE TREAD HAD COMPLETELY SEPARATED FROM THE TIRE DOWN TO THE CORD AREA. THE TREAD COMING OFF DAMAGED THE FLAP TORQUE TUBE, SEVERESDR O2G2008F00000Blade · failedHIGH T,V,I INDICATION AFTER TAKEOFF ON LT ENGINE. AC LANDED, FOUND 2.5 OF 1ST STAGE BLADE MISSING AND DAMAGE TO OTHER BLADES. (K)SDR 2007FA0000958Regulator · failedPILOTS REPORT FELT HEAVY VIBRATION FOR 3 TO 4 SECONDS, THEN HEARD A LOUD BANG FOLLOWED BY LT ENGINE SPOOLING DOWN. AIRCRAFT SAFELY LANDED AT AIRPORT. CONTACTED MFG, WHO DISPATCHED A RESPONSE CREW TO AIRPORT. FOUND THAT THE FUEL FLOW REGULATOR HAD FAILED IN SDR Y9PAN818S83107Smoke Detector · malfunctionedAFTER TAKEOFF, LAV SMOKE ALARM ANNUNCATOR ILLUMINATED, CREW REPORTED THAT THEY INSPECTED THE LAV AREA FOR SIGNS OF SMOKE AND FIRE, NONE OBSERVED. THE ANNUNCATOR WENT OUT AND THEN CAME BACK ON. THE CREW THEN ELECTED TO DIVERT. UPON LANDING, THE APU WOULD NOT STSDR S8A2007F00000Window · crackedAC DEPARTED AT APPROX 1930 ON 7/26/2007 AT APPROX 150 MILES OUT AND FL 350 A LOUD POP WAS HEARD IN THE CABIN. FLIGHT CREW INVESTIGATED AND NOTED THE NR 3 RT CABIN WINDOW OUTER PANE CRACKED. AT THAT TIME FLIGHT CREW DECLARED AN EMERGENCY, RETURNED AND MADE ANSDR 2007FA0000540Ring · missingTHE COMPONENT OEM (REPORT 4-193), THE MM (CHAPTER 36-02-00), IPC (CHAPTER 36-10-00) AND THE CMP WORK CARDS (364040, 364045) ARE MISSING THE REQUIREMENT TO INSPECT AND INSTALL GAMMA RING (PN) M1213-400 DURING THE INSTALLATION OF THE PNEUMATIC SYSTEM PRECOOLER. SDR UG8A2007PA03SAttach Fitting · corrodedLT AFT IB WING ATTACH FITTING HAS CORROSION AT OB EDGE AT FS 452, BL 33.COMPLIED WITH AIRCRAFT SERVICE CHANGE 229, WING TO FUSELAGE IB ATTACH CONNECTION FUSELAGE STATION 452 LT SIDE, REPLACEMENT/MODIFICATION. GENERATED FAA FORM 337. AIRCRAFT RETURNED TO SERVISDR BQVA200752271Attach Fitting · corrodedWING TO FUSELAGE ATTACH FITTING AT FS 452 BL 33 (LEFT SIDE), CORROSION DETECTED DURING THE SCHEDULED ULTRASONIC INSPECTION. THE CORROSION ON THE OUTBOARD SURFACE IS .158 INCH IN DEPTH, .125 INCH IN LENGTH; AND .125 INCH IN DIAMETER. [07-03-07] ENGINEERING SDR BQVA200751871Attach Fitting · crackedDURING THE REQUIRED EDDY CURRENT INSPECTION OF THE FS 793 BULKHEAD CAP ANGLE, CRACK INDICATIONS WERE NOTED ON BOTH SIDES. THE CRACKS ARE ABOVE THE .5 INCH BOLT HOLES IN THE CAP ANGLE FOR VERTICAL FIN ATTACHMENT.SDR 2007FA0000322Skin · corrodedDURING A WING NDT INSPECTION OF THE UPPER RT WING PLANK AT FS 452 AND BL 33, CORROSION WAS NOTED IN THIS AREA. ENGINEERING HAS DETERMINED THIS CORROSION IS EXCESSIVE ENOUGH TO REQUIRE ACCOMPLISHMENT OF ASC 229, WHICH REMOVES THE CORROSION ON THE PLANK AND INSSDR C4S2007F00000Skin · corrodedDURING A WING INSPECTION ACCOMPLISHED APRIL 9, 2006, CORROSION WAS NOTED IN THE UPPER RT WING PLANK AT FS 452 AND BL33. THE CORROSION DID NOT REQUIRE REPLACEMENT OF THE PART AND DID NOT REQUIRE BLENDING THAT EXCEEDED THE MFG ALLOWANCES. MFG ENGINEERING ALLOWSDR BUE2007F00002Bolt · sheared( REF NR: 287N416WM) DURING INSPECTION FOUND THE RT EJECTOR OB BEARING FITTING UPPER BOLT SHEARED, LOWER BOLT BENT/BEGINNING TO SHEAR, IB BEARING FITTING UPPER AND LOWER BOLTS BENT/BEGINNING TO SHEAR, AND THE IB AND OB TRANSLATOR LINKS BENT. REPLACED BOTH TRASDR BQVA200721071Wedge · damagedDURING THE SCHEDULED 72 MONTH LT WING WEDGE INSPECTION CMP 575030, ONE WING WEDGE HOLD DOWN RIVNUT WAS FOUND TO BE IN AN OVERSIZED HOLE.
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