# Service difficulty reports: Gulfstream AM Corp Comm Div 690D A list on [Gulfstream AM Corp Comm Div 690D](https://openairdocs.org/model/gulfstream-am-corp-comm-div-690d.md). Newest first. General aviation reporting is voluntary. - [SDR CA160222010](https://openairdocs.org/sdr/CA160222010.md): Fuel Line · worn · Feb 22, 2016 · Gulstm 690D · Engine Fuel Distribution > (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 OI - [SDR CA120901002](https://openairdocs.org/sdr/CA120901002.md): Eyebolt · cracked · Sep 1, 2012 · Gulstm 690D · Main Landing Gear Attach Section > (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 WANT - [SDR CA120901001](https://openairdocs.org/sdr/CA120901001.md): Bracket · cracked · Sep 1, 2012 · Gulstm 690D · Main Landing Gear > (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 CERTIFIC - [SDR CA080924005](https://openairdocs.org/sdr/CA080924005.md): Windshield · cracked · Sep 18, 2008 · Gulstm 690D · Flight Compartment Windows > (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 H - [SDR CA080708001](https://openairdocs.org/sdr/CA080708001.md): O-Ring · worn · Jun 22, 2008 · Gulstm 690D · Aircraft Fuel Distribution System > (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 SERV - [SDR CA070402006](https://openairdocs.org/sdr/CA070402006.md): Windshield · cracked · Mar 15, 2007 · Gulstm 690D · Flight Compartment Windows > (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 APPR - [SDR CA070115013](https://openairdocs.org/sdr/CA070115013.md): Fillet · cracked · Dec 19, 2006 · Gulstm 690D · Wing Miscellaneous Structure > (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. - [SDR CA070115012](https://openairdocs.org/sdr/CA070115012.md): Angle · cracked · Dec 14, 2006 · Gulstm 690D · Fuselage Main, Bulkhead > (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 320035-50 - [SDR CA060714003](https://openairdocs.org/sdr/CA060714003.md): Timer · failed · Jul 4, 2006 · Gulstm 690D · Airfoil Anti/De-ice System > (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 FAUL - [SDR CA060714002](https://openairdocs.org/sdr/CA060714002.md): Blower · burned · Jun 5, 2006 · Gulstm 690D · Air Distribution Fan > (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 BL - [SDR CA060501005](https://openairdocs.org/sdr/CA060501005.md): Window · cracked · Apr 28, 2006 · Gulstm 690D · Flight Compartment Windows > (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) - [SDR CA060501004](https://openairdocs.org/sdr/CA060501004.md): Window · cracked · Apr 28, 2006 · Gulstm 690D · Flight Compartment Windows > (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) - [SDR CA051129005](https://openairdocs.org/sdr/CA051129005.md): Uplock · failed · Oct 25, 2005 · Gulstm 690D · Landing Gear Position and Warning > FAILED TO DISENGAGE. SECOND EXTENSION WORKED FINE. - [SDR CA050427012](https://openairdocs.org/sdr/CA050427012.md): Bolt · bent · Apr 10, 2005 · Gulstm 690D · Landing Gear Retraction/Extension System > LT MLG FAILED TO UNLOCK. AIRCRAFT RECEIVED DAMAGETO LT PROP AND UNDERSIDE OF FUSELAGE. - [SDR 2005FA0000376](https://openairdocs.org/sdr/2005FA0000376.md): Shaft · broken · Jan 21, 2005 · N909HH · Gulstm 690D · Main Landing Gear > SHAFT 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) - [SDR CA060117004](https://openairdocs.org/sdr/CA060117004.md): Spar · cracked · Nov 5, 2004 · Gulstm 690D · Horizontal Stabilizer, Spar/Rib > INSPECTION OF THE AIRCRAFT FOUND THE HORIZONTAL STABILIZER UPPER HORIZONTAL SPAR CRACKED. CRACKED SPAR REMOVED AND NEW PART INSTALLED. - [SDR 62691](https://openairdocs.org/sdr/62691.md): Tire · grooved · Jan 16, 2003 · N909HH · Gulstm 690D · Tire > THIS 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 OTHER - [SDR CA030108005](https://openairdocs.org/sdr/CA030108005.md): Gyro · failed · Dec 6, 2002 · Gulstm 690D · Directional Gyro and Indicating System > (CAN) RT GYRO HORIZON INDICATOR TOPPLED AND WOULD NOT ERECT. SENT TO REPAIR, CALIBRATION AND TESTED. - [SDR 2001FA0000324](https://openairdocs.org/sdr/2001FA0000324.md): Stringer · corroded · Aug 27, 2001 · N120EK · Gulstm 690D · Fuselage Main, Longeron/Stringer > WHILE 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 I - [SDR CA010321014](https://openairdocs.org/sdr/CA010321014.md): Gcu · shorted · Feb 28, 2001 · Gulstm 690D · DC Regulator > (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. - [SDR CA010226020](https://openairdocs.org/sdr/CA010226020.md): Exciter · shorted · Feb 1, 2001 · Gulstm 690D · Exciter > (CAN) LT ENGINE WOULD NOT START. NO IGNITION. IGNITION SYSTEM CHECKED AND THE EXCITER WAS FOUND TO BE AT FAULT. - [SDR CA991231066](https://openairdocs.org/sdr/CA991231066.md): Fuel Control · leaking · Dec 12, 1999 · Gulstm 690D · Fuel Control/Turbine Engines > (CAN) FUEL CONTROL LEAKING BEYOND ALLOWABLE LIMITS FROM DRAIN MAST. - [SDR CA981027023](https://openairdocs.org/sdr/CA981027023.md): Windshield · cracked · Oct 20, 1998 · Gulstm 690D · Flight Compartment Windows > (CAN) WINDSHIELD OUTER GLASS FOUND CRACKED CLOSE TO HEATING ELEMENT. - [SDR CA980908046](https://openairdocs.org/sdr/CA980908046.md): Windshield · cracked · Aug 22, 1998 · Gulstm 690D · Flight Compartment Windows > (CAN) WINDSHIELD OUTER GLASS CRACKED IN THE TOP RIGHT HAND CORNER. - [SDR CA980512024](https://openairdocs.org/sdr/CA980512024.md): Windshield · cracked · May 1, 1998 · Gulstm 690D · Flight Compartment Windows > (CAN) WINDSHIELD OUTER GLASS FOUND CRACKED CLOSE TO HEATING ELEMENT. - [SDR CA980512023](https://openairdocs.org/sdr/CA980512023.md): Engine · noisy · Apr 16, 1998 · Gulstm 690D · Engine (Turbine/Turboprop) > (CAN) DURING DAILY INSPECTION, MAINTENANCE FOUND A SCRAPPING SOUND IN THE ENGINE WHEN TURNING THE PROPELLER BY HAND. SUBMITTER SUSPECTS HOT SECTION PROBLEM. - [SDR CA980311029](https://openairdocs.org/sdr/CA980311029.md): Windshield · cracked · Feb 10, 1998 · Gulstm 690D · Flight Compartment Windows > (CAN) THE WINDSHIELD OUTER GLASS CRACKED WHILE ON DESCENT. ACFT TT: 9,794 HOURS. - [SDR CA971117012](https://openairdocs.org/sdr/CA971117012.md): Rib · cracked · Nov 5, 1997 · Gulstm 690D · Trailing Edge Flaps > (CAN) LEFT WING INBOARD FLAP TRAILING EDGE RIB CRACKED. AIRCRAFT TT: 9,794 HOURS. - [SDR CA970807054](https://openairdocs.org/sdr/CA970807054.md): Windshield · cracked · Jul 17, 1997 · Gulstm 690D · Flight Compartment Windows > (CAN) THE WINDSHIELD OUTER GLASS CRACKED WHEN ON DESCENT INTO AIRPORT. - [SDR CA960527011](https://openairdocs.org/sdr/CA960527011.md): Torque Linkshaft · broken · May 14, 1996 · Gulstm 690D · Main Landing Gear Strut/Axle/Truck > (CAN)ON ROLL OUT ON LANDING, THE AIRCRAFT'S R/H TIRE BLEW. FURTHER INSPECTION REVEALED THAT THE TORQUE LINK SHAFT WAS ALSO BROKEN. - [SDR CA951211018](https://openairdocs.org/sdr/CA951211018.md): Windshield · cracked · Oct 21, 1995 · Gulstm 690D · Flight Compartment Windows > (CAN)THE WINDSHIELD OUTER GLASS CRACKED WHEN ON DESCENT TO AIRPORT. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/model/gulfstream-am-corp-comm-div-690d/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.