Gulfstream AM Corp Comm Div 690D

Service difficulty reports · 31

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 = '690D'
  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.

SDR CA160222010Fuel Line · worn(CAN) WHILE REMOVING LT STARTER/GEN FOR INSPECTION PURPOSES IT WAS FOUND THE FUEL LINE (P/N 3102762-1) WAS RUBBED ALMOST ALL OF THE WAY THROUGH BY THE PROPELLER GOVERNOR. AFTER REMOVAL OF THE FUEL LINE IT WAS THEN FOUND THAT THE FUEL LINE WAS RUBBING ON THE OIFeb 22, 2016 · Gulstm 690D · Engine Fuel DistributionSDR CA120901002Eyebolt · cracked(CAN) DURING THE 5 YEAR LANDING GEAR INSPECTION, A CRACK WAS DISCOVERED IN THE EYEBOLT BY THE NDT TECH. THE NDT OF MANY ITEMS ON THE LANDING GEAR ARE NOT REQUIRED BY THE MFG BUT WE DO IT PROACTIVELY AND HAVE HAD SOME FINDINGS. THE TYPE CERTIFICATE HOLDER WANTSep 1, 2012 · Gulstm 690D · Main Landing Gear Attach SectionSDR CA120901001Bracket · cracked(CAN) DURING 5 YEAR INSPECTION OF LANDING GEAR, A CRACK WAS DISCOVERED IN THE UPLOCK BRACKET BY THE NDT TECHNICIAN. MANY OF THE PARTS IN THE 5 YEAR INSPECTION ARE NOT CALLED TO BE NDT INSP BUT PROACTIVELY WE DO NDT MANY OF THESE COMPONENTS. THE TYPE CERTIFICSep 1, 2012 · Gulstm 690D · Main Landing GearSDR CA080924005Windshield · cracked(CAN) ACFT WAS ON A MEDEVAC FLIGHT AT NIGHT AT CRUISE ALTITUDE OF 16000 FT WHEN THE FLIGHT CREW HEARD A NOISE LIKE A SLAP. THEY COULD SEE THEN THAT THE RT WINDSHIELD WAS CRACKED. ACFT RETURNED WITHOUT FURTHER INCIDENT. INSP FOUND THE WINDSHIELD OUTER PANEL HSep 18, 2008 · Gulstm 690D · Flight Compartment WindowsSDR CA080708001O-Ring · worn(CAN) AFTER LANDING AND DURING WALK AROUND FLIGHT CREW FOUND FUEL LEAKING FROM RT WING OTBD OF NACELLE. FURTHER INSP BY MAINT FOUND FUEL LEAKING FROM FUEL INTERCONNECT PIPE COUPLING ASSY. NEW O-RINGS INSTALLED, LEAK CHECKS CARRIED OUT AND ACFT RETURNED TO SERVJun 22, 2008 · Gulstm 690D · Aircraft Fuel Distribution SystemSDR CA070402006Windshield · cracked(CAN) DURING A ROUTINE MEDIVAC FLIGHT AT AN ALTITUDE OF 12,000 FEET, THE FLIGHT CREW VISUALLY NOTED THAT THE RT WINDSHIELD WAS CRACKED ACROSS THE UPPER OB CORNER. AIRCRAFT RETURNED TO BASE. INSPECTION OF THE WINDSHIELD FOUND THE OUTER WINDOW PANE CRACKED APPRMar 15, 2007 · Gulstm 690D · Flight Compartment WindowsSDR CA070115013Fillet · cracked(CAN) DURING INSPECTION OF THE AIRCRAFT A CRACK WAS SUSPECTED IN THE RT UPPER FILLET WING TO FUSELAGE. NON DESTRUCTIVE TESTING CONFIRMED (2) CRACKS, 25 MM AND 18 MM LENGTH. LT UPPER FILLET INSPECTED BY NDT AND NO CRACKS FOUND. AN APPROVED REPAIR CARRIED OUT.Dec 19, 2006 · Gulstm 690D · Wing Miscellaneous StructureSDR CA070115012Angle · cracked(CAN) FLIGHT CREW REPORTED LOWER THAN NORMAL CABIN DIFFERENTIAL PRESSURE. A GROUND PRESSURIZATION CHECK WAS CARRIED OUT AND FOUND LEAK IN AREA OF AFT PRESSURE BULKHEAD LOWER SECTION. FURTHER INSPECTION REVEALED A CRACK IN THE BEND RADIUS OF ANGLE P/N 320035-50Dec 14, 2006 · Gulstm 690D · Fuselage Main, BulkheadSDR CA060714003Timer · failed(CAN) DURING CLIMB FLIGHT CREW NOTED VISUALLYTHAT WING DE-ICER BOOTS WERE INFLATED AND WOULD NOT DEFLATE. FLIGHT CREW SELECTED BLEED AIR CLOSED RESULTING IN BOOTS DEFLATING AND RETURNED TO DEPARTURE BASE. MAINTENANCE FOUND THE DE-ICE TIMER TO BE CAUSE OF FAULJul 4, 2006 · Gulstm 690D · Airfoil Anti/De-ice SystemSDR CA060714002Blower · burned(CAN) DURING DESCENT FLIGHT CREW NOTED A STRONG ODOR FROM THE HEATER OUTLETS. CREW SELECTED RECIRCULATION BLOWER SWITCH OFF AND LANDED AIRCRAFT. GROUND OPERATION CHECK OF THE ENVIRO SYSTEM FOUND RT RECIRCULATION BLOWER INOPERATIVE. FURTHER INSPECTION OF THE BLJun 5, 2006 · Gulstm 690D · Air Distribution FanSDR CA060501005Window · cracked(CAN) COCKPIT RT OVERHEAD WINDOW REMOVED FOR INSPECTION AFTER FINDING THE LT WINDOW CRACKED. WINDOW FOUND TO HAVE 2 CRACKS ORIGINATING FROM 2 SCREW ATTACHMENT HOLES. WINDOW REPLACED WITH NEW. (TC NR 20060501005)Apr 28, 2006 · Gulstm 690D · Flight Compartment WindowsSDR CA060501004Window · cracked(CAN) COCKPIT LT OVERHEAD WINDOW SHOWED SIGNS OF PRESSURIZATION LEAK. WINDOW REMOVED TO REPLACE GASKET AND FOUND WINDOW CRACKED. CRACKS ORIGINATING FROM 4 SCREW ATTACHMENT HOLES. NEW WINDOW INSTALLED. (TC NR 20060501004)Apr 28, 2006 · Gulstm 690D · Flight Compartment WindowsSDR CA051129005Uplock · failedFAILED TO DISENGAGE. SECOND EXTENSION WORKED FINE.Oct 25, 2005 · Gulstm 690D · Landing Gear Position and WarningSDR CA050427012Bolt · bentLT MLG FAILED TO UNLOCK. AIRCRAFT RECEIVED DAMAGETO LT PROP AND UNDERSIDE OF FUSELAGE.Apr 10, 2005 · Gulstm 690D · Landing Gear Retraction/Extension SystemSDR 2005FA0000376Shaft · brokenSHAFT SECURING TORQUE LINK TO RT MLG STRUT FOUND BROKEN DURING INSPECTION. THIS TORQUE LINK IS AT TOP OF STRUT AND ROTATES LOWER STRUT 90 DEGREES DURING RETRACT/ EXTEND CYCLE. INSTALLED NEW SHAFT. (K)Jan 21, 2005 · N909HH · Gulstm 690D · Main Landing GearSDR CA060117004Spar · crackedINSPECTION OF THE AIRCRAFT FOUND THE HORIZONTAL STABILIZER UPPER HORIZONTAL SPAR CRACKED. CRACKED SPAR REMOVED AND NEW PART INSTALLED.Nov 5, 2004 · Gulstm 690D · Horizontal Stabilizer, Spar/RibSDR 62691Tire · groovedTHIS AIRCRAFT HAS CLEVELAND BRAKES INSTALLED. THE CLEARANCE BETWEEN THE TIRE SIDEWALL AND BRAKE IN MINIMAL. WHEN THE SIDEWALL FLEXES DURING LANDING IT CONTACTS THE BRAKE CAUSING A 360 DEGREE GROVE IN THE TIRE SIDEWALL. THIS DOES NOT SEEM TO OCCUR WITH OTHERJan 16, 2003 · N909HH · Gulstm 690D · TireSDR CA030108005Gyro · failed(CAN) RT GYRO HORIZON INDICATOR TOPPLED AND WOULD NOT ERECT. SENT TO REPAIR, CALIBRATION AND TESTED.Dec 6, 2002 · Gulstm 690D · Directional Gyro and Indicating SystemSDR 2001FA0000324Stringer · corrodedWHILE REPLACING FUEL BAG, STRINGER 6A, LEFT WING INBOARD WAS FOUND TO BE AFFECTED BY GENERAL SURFACE AND PITTING CORROSION. THE CORROSION ON THE STRINGER WAS LOCATED BETWEEN WING STATION 24 AND 39, AND AFFECTED THE STRINGER UP TO AN APPROXIMATE DEPTH OF .08 IAug 27, 2001 · N120EK · Gulstm 690D · Fuselage Main, Longeron/StringerSDR CA010321014Gcu · shorted(CAN) RT GENERATOR WOULD NOT COME ON LINE. SWITCHED R/H GENERATOR TO LT GENERATOR CONTROL UNIT (GCU) WORKED FINE. REPLACED RT GCU AND IT SHORTED OUT AND SMOKED. UNIT HAD OTSO.Feb 28, 2001 · Gulstm 690D · DC RegulatorSDR CA010226020Exciter · shorted(CAN) LT ENGINE WOULD NOT START. NO IGNITION. IGNITION SYSTEM CHECKED AND THE EXCITER WAS FOUND TO BE AT FAULT.Feb 1, 2001 · Gulstm 690D · ExciterSDR CA991231066Fuel Control · leaking(CAN) FUEL CONTROL LEAKING BEYOND ALLOWABLE LIMITS FROM DRAIN MAST.Dec 12, 1999 · Gulstm 690D · Fuel Control/Turbine EnginesSDR CA981027023Windshield · cracked(CAN) WINDSHIELD OUTER GLASS FOUND CRACKED CLOSE TO HEATING ELEMENT.Oct 20, 1998 · Gulstm 690D · Flight Compartment WindowsSDR CA980908046Windshield · cracked(CAN) WINDSHIELD OUTER GLASS CRACKED IN THE TOP RIGHT HAND CORNER.Aug 22, 1998 · Gulstm 690D · Flight Compartment WindowsSDR CA980512024Windshield · cracked(CAN) WINDSHIELD OUTER GLASS FOUND CRACKED CLOSE TO HEATING ELEMENT.May 1, 1998 · Gulstm 690D · Flight Compartment WindowsSDR CA980512023Engine · noisy(CAN) DURING DAILY INSPECTION, MAINTENANCE FOUND A SCRAPPING SOUND IN THE ENGINE WHEN TURNING THE PROPELLER BY HAND. SUBMITTER SUSPECTS HOT SECTION PROBLEM.Apr 16, 1998 · Gulstm 690D · Engine (Turbine/Turboprop)SDR CA980311029Windshield · cracked(CAN) THE WINDSHIELD OUTER GLASS CRACKED WHILE ON DESCENT. ACFT TT: 9,794 HOURS.Feb 10, 1998 · Gulstm 690D · Flight Compartment WindowsSDR CA971117012Rib · cracked(CAN) LEFT WING INBOARD FLAP TRAILING EDGE RIB CRACKED. AIRCRAFT TT: 9,794 HOURS.Nov 5, 1997 · Gulstm 690D · Trailing Edge FlapsSDR CA970807054Windshield · cracked(CAN) THE WINDSHIELD OUTER GLASS CRACKED WHEN ON DESCENT INTO AIRPORT.Jul 17, 1997 · Gulstm 690D · Flight Compartment WindowsSDR CA960527011Torque Linkshaft · broken(CAN)ON ROLL OUT ON LANDING, THE AIRCRAFT'S R/H TIRE BLEW. FURTHER INSPECTION REVEALED THAT THE TORQUE LINK SHAFT WAS ALSO BROKEN.May 14, 1996 · Gulstm 690D · Main Landing Gear Strut/Axle/TruckSDR CA951211018Windshield · cracked(CAN)THE WINDSHIELD OUTER GLASS CRACKED WHEN ON DESCENT TO AIRPORT.Oct 21, 1995 · Gulstm 690D · Flight Compartment Windows
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