Grumman G-1159

Service difficulty reports · 159

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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 = 'G1159'
  ORDER BY difficulty_date DESC"

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SDR FAUA20190325101Aileron · icedAT CRUISE ALTITUDE AILERONS WOULD NOT RESPOND, PILOT HAD TO PULL AILERON ROLL DISCONNECT FOUND THAT THE LT WOULD RESPOND AND RT STILL HAD NO RESPONSE PILOT DECLARED EMERGENCY AND ASK FOR A NEW DESTINATION TO KGJT UPON SHORT FINAL INTO KGJT PILOT REPORTED REGAIMar 25, 2019 · N143C · Gulstm G1159 · Aileron Control SystemSDR FAUA20190220100Tire · failedTAKEOFF RUN WITH V1 WAS 124 KNOTS AND ROTATION VR 136,2 KNOTS PRIOR TO ROTATION EXPERIENCED A STRONG VIBRATION AND CONTINUED WITH TAKEOFF TO ACHIEVE A SPEED OF V2 PLUS 10. ONCE AIRBORNE THE VIBRATION STOPPED. CHECKED HYDRAULICS AND FUEL QUANTITY FOR ANY, ALL Feb 19, 2019 · N403SL · Gulstm G1159 · TireSDR 2017FA0000616Clamp · corrodedWHILE WORKING IN THE TAIL COMPARTMENT, THE MECHANIC NOTICED CORROSION ON A CLAMP ON BLEED AIR LINE 1159AC-20023-1 WHERE IT CONNECTS TO BLEED AIR LINE 1159AC-20044-7. CLOSE VISUAL INSPECTION REVEALED THE CLAMP TO BE SEVERELY CORRODED AND READY TO FAIL.Dec 4, 2017 · Gulstm G1159 · Pneumatic Distribution SystemSDR ESPA2016F00081Seal · leakingENROUTE AT FL410 . HEARD A LOUD NOISE COMING FROM THE FRONT ENTRANCE DOOR AND SUSPECTED A DOOR SEAL LEAK. THE CABIN BEGAN TO CLIMB AT A RAPID RATE. ELECTED TO REQUEST A LOWER ALTITUDE WITH ATC WHILE WORKING ON THE ISSUE. BEGAN A DESCENT TO THE ASSIGNED ALTMar 2, 2016 · N183PA · Gulstm G1159 · Passenger/Crew DoorsSDR QY5R201404090001Fuel Line · brokenWHILE ON GROUND WITH APU RUNNING, A MAJOR FUEL LEAK WAS SEEN COMING OUT THE REAR FUSELAGE. APU WAS SHUTDOWN AND AN INVESTIGATION REVEALED A BROKEN FUEL LINE AT ONE OF THE FUEL NOZZLES. THE FUEL WAS SPRAYING INSIDE THE APU ENCLOSURE AND LEAKING OUT FUSELAGE ACApr 3, 2014 · N105TB · Gulstm G1159 · APU Engine Fuel and ControlSDR 2013FA0000250Flapper Valve · failedOVER A 4 YEAR PERIOD, THIS ACFT HAS EXPERIENCED 2 INSTANCES OF IN-FLIGHT ROLL BACK AND SHUTDOWN OF THE RT ENGINE. IN BOTH CASES ENGINE COULD BE RESTARTED AND SUBSEQUENT EXTENSIVE EVALUATION AND INSPECTION REVEALED NO DEFECTS. ACFT OPERATED WITHOUT INCIDENT Apr 18, 2013 · N10123 · Gulstm G1159 · Aircraft Fuel Distribution SystemSDR BQVA201103210009Stringer · corrodedSURFACE CORROSION WAS DETECTED ON THE HORIZONTAL FLANGES OF STRINGER 8 ON BOTH THE LEFT AND RIGHT CONNECTING ANGLES.Mar 15, 2011 · N540EA · Gulstm G1159 · Wing, Longeron/StringerSDR BQVA2011031400008Shim · corrodedSURFACE CORROSION FOUND ON STRINGER 24L AND SOME CORROSION FOUND ON THE SHIM DURING THE FS 580 BULKHEAD COMSCAN INSPECTION (CMP CODE 539435). (ORIGINAL SUBMISSION 3/14/11)Mar 9, 2011 · N540EA · Gulstm G1159 · Fuselage Main, Longeron/StringerSDR 2010FA0000498Control Cable · wornDURING A PREFLIGHT INSPECTION WITH THE AILERON UP, EXCESSIVE WEAR OF THE FORWARD OUTBOARD AILERON CABLE WAS NOTED AT THE RBS 189 FAIRLEAD. THE PHENOLIC PROTECTOR WAS IN GOOD CONDITION EVEN THOUGH THE CABLE HAD BEEN RUBBING ON IT. MANY STRANDS WERE WORN THROUGHMay 20, 2010 · N105TB · Gulstm G1159 · Aileron Control SystemSDR EYDAN128KGC1FODCompressor · distortedON 09/10/09 THE AIRCRAFT DEPARTED EWR ENROUTE TO OPF, DURING CLIMB IN ICING CONDITIONS; AT 33,400 FT, THE NR 1 ENGINE HAD A COMPRESSOR STALL AND STARTED TO ROLL BACK. THE CREW INITIATED A RELIGHT AND THE ENGINE RETURNED TO NORMAL OPERATION. MAINTENANCE INSPECSep 10, 2009 · N128KG · Gulstm G1159 · Turbine Engine Compressor SectionSDR 2009FA0000285Wire · shortedDURING A SCHEDULED MX VISIT & TROUBLESHOOTING OF LT WING LOGO LIGHT DEFECT, A WIRING SHORT WAS FOUND BETWEEN THE WING/TIP TANK DISCONNECT AND THE BULKHEAD CONNECTOR IN THE TIP TANK DRY BAY. THE WIRING WAS REMOVED FROM THE CONDUIT (RUNNING THROUGH THE WET AREAApr 7, 2009 · Gulstm G1159 · Fuel System WiringSDR 2009FA0000882Acm · bindingUNIT WAS INSTALLED WITH 8.6.1 HOURS. THE TURBINE WAS BINDING AND CAUSING OVERHEAT AND SMOKE IN THE CABIN. UNIT WAS REPLACED WITH AN AS REMOVED UNIT AND AN OPS CHECK WAS COMPLIED WITH. OIL LEVEL CHECK NO DEFECTS NOTED. THIS UNIT HAS LASTED OVER 150 HOURS ANMar 4, 2009 · N400M · Gulstm G1159 · Cabin Cooling SystemSDR 2009FA0000881Acm · bindingUNIT WAS INSTALLED AS AN OVERHAULED UNIT. WITH 21.1 HOURS ON THE UNIT. THE TURBINE WAS BINDING AND CAUSING OVERHEAT AND SMOKE IN THE CABIN. UNIT WAS REPLACED WITH AN O/H UNIT AND AN OPS CHECK WAS COMPLIED WITH. OIL LEVEL CHECK, NO DEFECTS NOTED. THIS WAS Mar 4, 2009 · N400M · Gulstm G1159 · Cabin Cooling SystemSDR 2009FA0000880Acm · bindingACM WAS INSTALLED AS AN OVERHAULED UNIT. OIL SERVICE AND NEW WATER SEPARATOR SOCK INSTALLED. GROUD RAN SYSTEM, DID COMPLETE OPS CHECK NO LEAKAGE. 50.6 HOURS AFTER THE ACM WAS BINDING INSIDE, MAKING A LOUD SCRAPING NOISE. UNIT WAS REMOVED AND REPLACED WITH Mar 1, 2009 · N400M · Gulstm G1159 · Cabin Cooling SystemSDR Y9PAN930LS82208Transponder · intermittentMODE C TRANSPONDERS READ 500 FT HIGH 99 PERCENT OF THE TIME (IN CRUISE). TROUBLESHOOTING IN PROCESS, WILL AMEND FORM WHEN DETERMINATION OF CAUSE 8/22/08. RAN PITOT/STATIC SYS TO 45,000 FT AND CHECKED OUT PUT OF TRANSPONDER SYS WITH ATC601 TEST SET AND INDICAug 22, 2008 · N930LS · Gulstm G1159 · ATC Transponder SystemSDR WWQ2008F00003Transceiver · shortedAC WAS DISPATCHED, THE CREW CAPTAIN AND F/O DEPARTED AT 13:40 ENROUTE. AT APPROX 13:50, WHILE CLIMBING OUT OF 8000 FEET, PILOTS NOTICED THE RADAR SCREEN START TO FLICKER. CAPT IMMEDIATELY SHUT THE RADAR OFF. A SHORT WHILE LATER PILOTS SMELLED WHAT APPEARED Aug 2, 2008 · N712AS · Gulstm G1159 · Weather Radar SystemSDR WWQ2008F00000Display · shortedFLIGHT WW171. DEPARTED MIV TO IAD. CLIMBING OUT OF 8000 FT, CREW NOTICED THE RADAR SCREEN START TO FLICKER. IMMEDIATELY SHUT THE RADAR OFF. CREW DETECTED WHAT APPEARED TO BE SMOKE RELATED TO ELECTRICAL FIRE. CREW SAW HEAVY SMOKE COMING OUT OF THE DASHBOARAug 2, 2008 · N712AS · Gulstm G1159 · Weather Radar SystemSDR N382008F00000Bearing · failedAT START UP OF THE RT ENGINE, THE PILOT NOTICED A VIBRATION AND THE ENGINE WAS SHUT DOWN, TROUBLESHOT PROBLEM. IT WAS DETERMINED THAT A HIGH PRESSURE TURBINE BEARING HAD FAILED. (K)Mar 17, 2008 · N192FG · Gulstm G1159 · Turbine SectionSDR 120107Engine · vibrationAFTER LANDING, TEMP.AROUND -12C, FREEZING FOG, CREW ELECTED TO TURN OFF ANTI-ICE AFTER LND. AIRCRAFT SAT FOR 1 HR,ENG'S STARTED. LT ENG HAD VIBRATION HUMMING, RT ENG WAS STABLE.TAXIED OUT W/ANTI-ICE ON THRUOUT. A/C TOOKOFF, IT SEEMED TO BE SMOOTH ON THE ROLLDec 17, 2007 · N183PA · Gulstm G1159 · Engine (Turbine/Turboprop)SDR ESPA100107Windshield · crackedDURING DECENT AT 20,000 FEET THE CO-PILOTS WINDSHIELD DEVELOPED CRACK STARTING FROM THE RT SIDE BOLT PATTERN AND EXTENDING DOWN AND ACROSS. CREW DECIDED TO DIVERT, AS THE CRACK HAD SPLIT INTO (2) CRACKS. ALSO, DECLARED AN EMERGENCY TO ATC PROCEEDING VISUALLYOct 17, 2007 · N183PA · Gulstm G1159 · Flight Compartment WindowsSDR 2007FA0000209Audio Control · shortedUNIT WAS MANUFACTURED IN AUGUST 06 AND WAS INSTALLED IN DECEMBER 06. THE UNIT POPPED THE CIRCUIT BREAKER ON THE FIRST TRIP. THE UNIT WAS SENT IN FOR REPAIR AND REINSTALLED IN FEBRUARY 07 AND FAILED AGAIN ON THE FIRST FLIGHT.Mar 6, 2007 · N685SF · Gulstm G1159 · Audio Integrating SystemSDR JBGA200700001Windshield · sparksGOING INTO AIRPORT, PILOT NOTICED SPARKS DANCING AROUND PILOTS WINDSHIELD. ON THE GROUND MAINTENANCE FOUND WINDSHIELD DELAMINATING, REMOVED AND REPLACED WINDSHIELD.Jan 1, 2007 · Gulstm G1159 · Windshield/Door Rain/Ice RemovalSDR 2006FA0001015Tee Fitting · crackedUPON POST FLIGHT INSPECTION THE PILOT NOTICED SMALL AMOUNT OF HYDRAULIC FLUID SEEPING FROM THE BOTTOM OF THE RADOME. MAINTENANCE DETERMINED THAT THE LEAK WAS COMING FROM A BULKHEAD TEE IN THE NOSE LANDING GEAR DUMP VALVE LINE. THE LEAK WAS INITIALLY THOUGHT Oct 19, 2006 · N750RA · Gulstm G1159 · Fuselage Miscellaneous StructureSDR N382006F00003Attach Fitting · corrodedIAW MM, TO COMPLY WITH THE 24 MONTH NDT REQUIREMENTS UNDER THE ULTRASONIC, CORROSION WAS FOUND UNDER THE LT FWD WING ATTACHMENT FITTING AT FUSELAGE STA 345, BUTT LINE 40. (K)Jul 3, 2006 · N192FG · Gulstm G1159 · Fuselage, Wing Attach FittingsSDR CA051014002Blades · damagedGII SERIAL 236 IN NR 1 POSITION HAS EXPERIENCED FOD DAMAGE. THE DAMAGE HAS BEEN FOUND TO THE LPC5 BLADES AND HPC1 BLADES. THE REST OF THE HP COMPRESSOR HAS YET TO BE INSPECTED. THE DAMAGE HAS BEEN CAUSED BY THE RELEASE OF ONE LP OGV INNER BOLT WASHER AND NUOct 12, 2005 · Gulstm G1159 · Turbine Engine Compressor SectionSDR N382005F00005Uplock Switch · disconnectedON TAKEOFF WITH GEAR UP, THE GEAR HANDLE LIGHT WAS ON. PRELIMINARY TROUBLESHOOTING DETERMINED THAT THE LT MAIN GEAR DOOR UP SWITCH WAS AT FAULT. WHEN REPLACING SWITCH, FOUND A LOOSE WIRE AT A BUTT SPLICE. (K)Oct 12, 2005 · N510SR · Gulstm G1159 · Landing Gear Door Retract SectionSDR YNT2005F00000Stringer · corrodedCORROSION ON STRINGER L17, FS 336, CORROSION REMOVED AND A REPAIR STRAP INSTALLED OVER REPAIRED AREA. (SW05200510589) (K)Jul 19, 2005 · N188JS · Gulstm G1159 · Fuselage Main, Longeron/StringerSDR 2005FA0001034Proximity Switch · looseAC DEPARTED FOR 3 DAY TRIP. AC MADE A STOP TO PICK UP 1 PASSENGER, THEN TOOK OFF AND HEADED TO PICK UP ANOTHER PASSENGER. ON EXTENDING THE GEAR, LT GEAR DOWN AND LOCKED LIGHT FAILED TO LITE. CREW TRIED 6 TIMES BY RETRACTING AND EXTENDING GEAR TO NO AVIAL. Jun 11, 2005 · N900DH · Gulstm G1159 · Landing Gear Position and WarningSDR 2005FA0000887Skin · crackedREPAIRED SKIN ON RUDDER LEADING EDGE AT THE NR 2 RUDDER HINGE POINT. (K)Jun 7, 2005 · N117MS · Gulstm G1159 · Rudder, Plate/SkinSDR 2005FA0000390Duct · damagedWITH APU RUNNING AND AIR SELECTED ON APU BLEED AIR OPENED HOLE IN INSULATION BY CUTTING BACK INSULATION. FOUND HOLE IN WELDED SEAM BETWEEN TO DUCTS (Y) DUCT NOMINCLATURE IS; DUCT ASSY, APU AND GROUND START.Mar 22, 2005 · N400M · Gulstm G1159 · APU Bleed Air SystemSDR 2005FA0000269Cowling · corrodedDURING RT ENGINE MID-LIFE UPDATES, RT FIXED COWL WAS INSPECTED AND CORROSION WAS NOTED. FIXED COWL WAS REPAIRED.Sep 2, 2004 · N826GW · Gulstm G1159 · Nacelle/Pylon, Plate/SkinSDR 2005FA0000268Panel · corrodedDURING WIG (LT) NDT INSPECTION EXFOLIATION CORROSION NOTED ON WING UPPER PLANK AND FRONT BEAM BETWEEN RBS 284 THRU 375. REMOVED EXFOLIATION CORROSION IAW SRM. REPAIRS COMPLETED.Sep 2, 2004 · N826GW · Gulstm G1159 · Wing, Plate/SkinSDR 2005FA0000267Bulkhead · crackedDURING COMPLIANCE OF NDT EDDY CURRENT INSP OF FS-793.75 BULKHEAD, CAP ANGLE WAS FOUND CRACKED. NEW CAP ANGLE WAS INSTALLED IAW DWG NR SE20000210, REV. D.Sep 2, 2004 · N826GW · Gulstm G1159 · Fuselage Main, BulkheadSDR 2005FA0000104Cowling · corrodedDURING LT ENGINE MID-LIFE UPDATES, LT FIXED COWL WAS INSPECTED AND CORROSION WAS NOTED. FIXED COWL WAS REPAIRED.Sep 2, 2004 · N826GW · Gulstm G1159 · Nacelle/Pylon, Plate/SkinSDR 2005FA0000103Skin · corrodedDURING WING (RIGHT) NOT INSPECTION, EXFOLIATION CORROSION NOTED ON WING UPPER PLANK AND FRONT BEAM BETWEEN RBS 284 THRU 375. EXFOLIATION CORROSION REMOVED IAW SRM. REPAIRS COMPLETED.Sep 2, 2004 · N826GW · Gulstm G1159 · Wing, Plate/SkinSDR IV42004F00000Bearing · failedDURING CLIMBOUT, 2 HIGH TVI INDICATION ON NR 1 END AFT WAS OBSERVED (APPROX 2.5). AFTER POWER WAS REDUCED, TVI INDICATION REDUCED TO APPROX (.7), SOME FLUCTUATION ON TVI INDICATOR. GEN VOLTAGE WAS NORMAL BUT HAD SPLIT IN GEN AMPERAGE WITH NR 1 GEN SHOWING APAug 31, 2004 · N949NA · Gulstm G1159 · DC Generating SystemSDR ET72004F00000Heat Shield · delaminatedNOTED HEAT SHIELD HAS DISBONDED FROM RT FIX COWL OUTER SKIN AT APPROX FS 596.0 TO NACELLE STATION 179.0 (OIL CAN). INSPECTION OF FIX COWL INTERIOR (INNER SKIN CORE) AT FS 596.0 TO NACELLE STATION 179.0. NO DEFECTS NOTED. FOUND DELAMINATION ON INNER SKIN CORMar 31, 2004 · N668JT · Gulstm G1159 · Engine Cowling SystemSDR DEBAGA11591Relay · failedWITH AIRCRAFT ON GROUND WITH APU RUNNING, THE ESSENTIAL AND MAIN BUSS VOLTAGES DROPPED TO 19VDC. TROUBLESHOT SYSTEM AND FOUND THAT THE REVERSE CURRENT RELAY A700AH SN L13232 DID NOT PROPERLY SERVE AS A REVERSE CURRENT RELAY AND IT FED POWER TO THE DC GENERATORMar 5, 2004 · N900BF · Gulstm G1159 · DC Generating SystemSDR R6U2004F00000Stringer · crackedSTRINGER 24R WAS FOUND TO HAVE A 1.5 INCH CRACK IN THE FLANGE RADIUS AT FS596.00. PROBABLE CAUSE: FATIGUE.Jan 29, 2004 · N251JS · Gulstm G1159 · Fuselage Main, Longeron/StringerSDR 2004F00255Actuator · failedFLAP FAILED TO EXTEND. REPLACED FLAP ACTUATOR DUE TO ASSYEMETRY GEAR FAILURE. (M)Jan 27, 2004 · N524MM · Gulstm G1159 · Trailing Edge Flap ActuatorSDR A8O2004F00000Line · leakingFUEL SYSTEM/FUEL DUMP SYSTEM AFFECTS FUEL FLOW OR LEAKAGE DURING FLIGHT. EMERGENCY ACTION TAKEN DURING FLIGHT DUE TO A COMPONENT OR SYSTEM MALFUNCTION. UPON ROTATION, THE LEFT FUEL FILTER LIGHT CAME ON. THE CREW ACTED FOLLOWING THE EMERGENCY PROCEDURE, DECLDec 14, 2003 · N41AV · Gulstm G1159 · Aircraft Fuel Distribution SystemSDR ZLW2004F00000Pitot Line · cloggedAC WAS ON TAKEOFF ROLL WHEN THE FLIGHT CREW NOTED A SUBSTANTIAL SPLIT BETWEEN AIRSPEED INDICATORS. AC WAS TAXIED BACK FOR TROUBLESHOOTING. PITOT/STATIC CHECKS WERE ACCOMPLISHED AND DISCREPANCY DUPLICATED. ALL PITOT AND STATIC LINES WERE DISCONNECTED AND NITSep 23, 2003 · N36MW · Gulstm G1159 · Pitot/Static SystemSDR QY52003F00000Starter Gen · failedNR 1 ENGINE FAILED TO START. ON INVESTIGATION OF PROBLEM, FOUND STARTER CENTRIFUGAL SWITCH HAD MALFUNCTIONED. ORDERED NEW STARTER. WHEN OLD STARTER WAS REMOVED, IT WAS DISCOVERED THAT THE STARTER SHAFT BEARINGS HAD FAILED, THIS IS MOST LIKELY WHAT TOOK OUT Aug 1, 2003 · N105TB · Gulstm G1159 · Starter-GeneratorSDR IMJ2003F00000Actuator · restrictedCREW REPORTS ROLL CONTROL STIFF OR BINDING ON APPROACH. FOUND RIGHT AILERON ACTUATOR CAUSING PROBLEM. SYSTEM CHECKED FREE UNTIL HYDRAULIC PRESSURE APPLIED, THEN RESTRICTION NOTICED UPON QUICK APPLICATION OF INPUT. UNIT CURE DATE OF 4Q77, TNS/TSO UNK 15150.4Jul 3, 2003 · N33PJ · Gulstm G1159 · Aileron Control SystemSDR CA030611004Ring · cracked(CAN) TIME SHOWN ABOVE IS ENGINE TIME. PART IS OVERHAULED AT ENGINE INSTALLATION. THE TRUNNION ASSEMBLY ATTACHED TO THE FORWARD ENGINE MOUNTING BEAM LINK, ATTACHING ENGINE TO AIRCRAFT, WAS RECEIVED AT RRC WITH ENGINE 8841 FOR REVISION. THE RING NUT LOCKING TRJun 11, 2003 · Gulstm G1159 · Engine Mount SectionSDR CA030324010Bolt · failed(CAN) LP OGV S BOLT FAILED DURING GROUND RUN. THE DAMAGED WAS CONTAINED WITHIN THE ENG. ENG SUFFERED FROM HIGH VIBRATION AND THEN A BOROSCOPE WAS PERFORMED AND THE LP COMPRESSOR ROTOR WAS FOUND DAMAGED. ENG STRIP CONFIRMED THAT ONE OFF OGV BOLT WAS MISSING. MIMar 24, 2003 · Gulstm G1159 · Turbine Engine Compressor SectionSDR NASA51181Nut · missingIN JUNE 2000 DURING A ROUTINE POSTFLIGHT INSPECTION FOD WAS DISCOVERED ON THE LP COMPRESSOR 5TH STAGE BLADES. DURING A SUBSQUENT TEARDOWN IT WAS DISCOVERED THAT A LP COMPRESSOR OGV BOLT AND NUT AND CAME LOOSE AND CAUSED THE DAMAGE TO THE ENGINE. THE BOLT WAS FMar 7, 2003 · N848NA · Gulstm G1159 · Engine (Turbine/Turboprop)SDR ZLW2003F00000Floorbeam · crackedDURING A ROUTINE CABIN BELOW FLOOR INSPECTION, IT WAS FOUND THAT THE AFT FLOORBEAM SECONDARY SUPPORT WAS CRACKED. A NEW PART IS AVAILABLE FROM MFG AND WILL BE INSTALLED PRIOR TO FURTHER FLIGHT.Mar 4, 2003 · N622RR · Gulstm G1159 · Fuselage Main, Floor BeamSDR O2G2003F00004Doubler · corrodedCORROSION PRESENT ON DOUBLERS FORWARD OF BATTERY BOX AND AFT OF BAGGAGE DOOR. REPAIR REQUIRED PULLING BACK SKIN FROM STRINGER 19 TO STRINGER 11 AND FORWARD TO THE FAIRINGS BELOW THE BAGGAGE DOOR AND SPLICING NEW DOUBLER INTO PLACE.Feb 13, 2003 · N524MM · Gulstm G1159 · Fuselage Main, StructureSDR 030002161Window · crackedOUTER PANE OF CABIN WINDOW WAS FOUND CRACKED .5000 INCHES DURING VISUAL INSPECTION. WINDOW WAS REPLACED.Jan 16, 2003 · N96JA · Gulstm G1159 · Passenger Compartment Windows
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