Gulfstream Aerospace G-1159A

Service difficulty reports · 145

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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"

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SDR ESPA2019F00224Wing · corrodedRIGHT WING HAS CORROSION ON AFT SPAR AT RBS343.May 17, 2019 · N163PA · Gulstm G1159A · Wing SparSDR ESPA2019F00223Spar · corrodedFOUND CORROSION ON WING AFT SPAR AT RBS 406.May 17, 2019 · N163PA · Gulstm G1159A · Wing SparSDR 2016F00212Flap System · inoperativeFLAPS WOULD NOT EXTEND DURING DESCENT. DIVERTED AND DECLARED AND EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT.Oct 17, 2016 · N50BH · Gulstm G1159A · Trailing Edge Flap Control SystemSDR 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 TROUBLESHOOTSep 2, 2016 · N163PA · Gulstm G1159A · Cabin Pressure Control SystemSDR 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 RETURApr 8, 2015 · N360MB · Gulstm G1159A · Landing Gear Door Retract SectionSDR 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 ADDITIONJan 20, 2015 · N992NA · Gulstm G1159A · Rudder Tab Control SystemSDR BQVA20150109001Converter · faultyLEFT AC & LEFT DC POWER FAIL INDICATORS ILLUMINATED.Jan 9, 2015 · N58AJ · Gulstm G1159A · AC Generation SystemSDR 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 FURTHERJul 10, 2014 · Gulstm G1159A · Passenger Compartment WindowsSDR 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.Apr 21, 2014 · N58AJ · Gulstm G1159A · Wing SparSDR 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.Mar 25, 2014 · N492A · Gulstm G1159A · Drag Control SystemSDR BKEA2014012000040Windscreen · failedLEFT WINDSCREEN FAILED,Jan 18, 2014 · N175BG · Gulstm G1159A · Flight Compartment WindowsSDR BKEA2014012000039Windscreen · failedLEFT WINDSCREEN FAILED.Jan 18, 2014 · N175BG · Gulstm G1159A · Flight Compartment WindowsSDR 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 TJan 4, 2014 · N55ME · Gulstm G1159A · Engine (Turbine/Turboprop)SDR 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.Dec 11, 2013 · N58AJ · Gulstm G1159A · Auxiliary Power Unit (APU) DoorsSDR 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 FUEMay 8, 2013 · N50BH · Gulstm G1159A · Fuel StorageSDR 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.May 6, 2013 · N221WR · Gulstm G1159A · Cabin Cooling SystemSDR 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 SIGNJan 30, 2013 · N901EH · Gulstm G1159A · Flight Compartment WindowsSDR 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 CJul 8, 2012 · N221CM · Gulstm G1159A · Turbine SectionSDR 2012F00114Probe · groundedDURING CLIMB OUT, 1/3 RT ROLL WAS REQUIRED TO MAINTAIN LEVEL FLIGHT. THE ACFT RETURNED TO DEPARTURE.Jun 11, 2012 · N62MW · Gulstm G1159A · Fuel System WiringSDR 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.Apr 17, 2012 · N477WG · Gulstm G1159A · Leading Edge DevicesSDR 2012F00077Skin · dentedDURING POST FLIGHT WALK-AROUND BY FLIGHT CREW NOTICED A POSSIBLE BIRD STRIKE AND DENT ON LT OTBD L/E.Apr 17, 2012 · N477WG · Gulstm G1159A · Wing, Plate/SkinSDR 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.Nov 7, 2011 · N109DD · Gulstm G1159A · Wing, Attach FittingsSDR 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.Apr 15, 2011 · N58AJ · Gulstm G1159A · Wing, Plate/SkinSDR 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 DESTINAJan 16, 2011 · N918BG · Gulstm G1159A · Engine (Turbine/Turboprop)SDR 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 Sep 27, 2010 · N855SA · Gulstm G1159A · Passenger/Crew DoorsSDR 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 WAug 18, 2010 · N50BH · Gulstm G1159A · Fuselage Main, BulkheadSDR 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 DEVELOPAug 9, 2010 · N456AL · Gulstm G1159A · APU Bleed Air SystemSDR 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 Apr 7, 2010 · N58AJ · Gulstm G1159A · Wing, Plate/SkinSDR 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.Apr 7, 2010 · N58AJ · Gulstm G1159A · Fuselage Main, Attach FittingsSDR 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 Feb 23, 2010 · N58AJ · Gulstm G1159A · Landing Gear Position and WarningSDR BQVA2010010400004Windshield · crackedRIGHT SIDE WINDSHIELD OUTER PANE FAILURE DURING FLIGHT. REMOVED AND REPLACED WINDSHIELD.Jan 2, 2010 · N50BH · Gulstm G1159A · Flight Compartment WindowsSDR 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. Sep 23, 2009 · N366JA · Gulstm G1159A · Drag Control ActuatorSDR 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.Aug 31, 2009 · N62MW · Gulstm G1159A · Life RaftSDR 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 CAug 31, 2009 · N62MW · Gulstm G1159A · Life RaftSDR 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)Jul 18, 2009 · N399AP · Gulstm G1159A · TireSDR 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 PERCENApr 19, 2009 · N366JA · Gulstm G1159A · Engine (Turbine/Turboprop)SDR 2010F00114Windshield · crackedLEFT WINDSHIELD OUTER PANE CRACKED AT FL410, DESCENT TO 10,000 FT AND RETURNED TO AIRPORT. NO LOSS OF PRESSURIZATIONJan 3, 2009 · N213BA · Gulstm G1159A · Flight Compartment WindowsSDR 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, SEVEREJul 7, 2008 · N797BD · Gulstm G1159A · TireSDR 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)Mar 29, 2008 · N800TD · Gulstm G1159A · Turbine Engine Combustion SectionSDR 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 Sep 13, 2007 · N776MA · Gulstm G1159A · Engine Fuel DistributionSDR 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 STAug 31, 2007 · N818S · Gulstm G1159A · Smoke DetectionSDR 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 ANJul 26, 2007 · N457JC · Gulstm G1159A · Flight Compartment WindowsSDR 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. Jun 25, 2007 · N2NA · Gulstm G1159A · Engine Bleed Air SystemSDR 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 SERVIJun 13, 2007 · N473KT · Gulstm G1159A · Wing, Attach FittingsSDR 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 May 18, 2007 · N50BH · Gulstm G1159A · Wing, Attach FittingsSDR 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.May 16, 2007 · N50BH · Gulstm G1159A · Fuselage Main, Attach FittingsSDR 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 INSMar 30, 2007 · N300WY · Gulstm G1159A · Wing, Plate/SkinSDR 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 ALLOWFeb 12, 2007 · N400WY · Gulstm G1159A · Wing, Plate/SkinSDR 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 TRAFeb 8, 2007 · N416WM · Gulstm G1159A · Engine Exhaust SystemSDR 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.Feb 1, 2007 · N982RK · Gulstm G1159A · Wing, Plate/Skin
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