Gulfstream Aerospace G-V
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 = 'GV' 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 = 'GV' 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 2016FA0000331Engine · shutdownDURING CRUISE FLIGHT, THE NR 2 ENGINE SHUTDOWN. DID NOT ATTEMPT RESTART. FOLLOWED POH AND LANDED.SDR CA151214004Case · corroded(CAN) DURING PRELIMINARY INSPECTION OF THE FAN CASE (LEVEL 3 OVERHAUL) MINOR BULGING OF THE FAN TRACK LINING WAS NOTICED AT BOTTOM DEAD CENTER POSITION. IN ORDER TO DETERMINE THE ROOT CAUSE OF THIS BULGING, THE INSPECTOR HAS REQUESTED FOR REMOVAL OF THE AFFECTSDR 2015F00114Steering Unit · failedSTEAR BY WIRE FAIL ON LANDING, ANNUNCIATED WHEN GEAR EXTENDED ON 2 LANDINGS.SDR BTVR2015081402Strut · corrodedLEFT ENGINE ALIGNMENT STRUT HAS EVIDENCE OF CORROSION INSIDE TUBES.SDR BTVR20150814001Strut · corrodedRIGHT ENGINE ALIGNMENT STRUT HAS EVIDENCE OF CORROSION INSIDE TUBES.SDR DXTA2015030205989Trim System · malfunctionedCLIMBING OUT OF FL220 USING ELEC NOSE DOWN TRIM, RECEIVED AN FGC 1 FAIL MSG. PITCH TRIM DISENGAGED. FGC 2 FAILED WHEN TRYING TO TRIM AFTER REENGAGING ELEC TRIM. FGC 1 REMAINED FAILED. MANUAL TRIM WAS VERY STIFF & ALMOST FELT LIKE A BINDING MOVEMENT. TRISDR 9PVA2015030500001Pump · failedCREW REPORTED LT MAIN FUEL BOOST PUMP FAILED IN FLIGHT.SDR 2014FA0000623Windshield · failedACFT WAS ON A REPOSITIONING FLIGHT. APPROXIMATELY 22 MINUTES INTO THE FLIGHT, AND AFTER LEVELING OFF AT FL400, CREW NOTED DISCOLORATION IN THE UPPER RT CORNER OF THE PILOTS WINDSHIELD. THE DISCOLORATION GREW, UNTIL THE THE WINDSHIELD ULTIMATELY FAILED, CRACSDR Y3PR20140120002Line · chafedLEFT ELEVATOR UPPER FORWARD OTBD PRIMARY CABLE IS CHAFING ON BAGGAGE DOOR SEAL PNEUMATIC LINE BELOW APU ENCLOSURE AT BS 782. OPENSDR CA130905004Bulb · shorted(CAN) HAD A FAILURE OF COPILOTS MASTER WARNING ANNUNCIATOR. TROUBLESHOOTING REVEALED THAT 1 OF 4 LED LIGHT BULBS HAD FAILED SHORTED. THIS RESULTED IN ALL 4 BULBS FAILING TO ILLUMINATE. WITH THE FAILURE OF ONLY 1 BULB IN THE ANNUNCIATOR, NONE OF THE OTHER BUSDR 2013FA0000337Seat Belt · mismanufacturedNYLON WEBBING AND THREAD WAS USED WHEN THE OEM DATA STATES POLYESTER WEBBING AND THREAD SHOULD HAVE BEEN USED. THE LENGTHS OF THE BELTS ARE NOT WITHIN THE OEM TOLERANCE, IMPROPER IDENTIFICATION, THE OEM DATA WAS NOT TRANSFERRED ONTO THE TAGS, COULD COMPROMISE SDR 9PMA2013042400002Downlock Switch · failedLOWERED LANDING GEAR AND RECEIVED A NOSE WHEEL STEERING FAIL MESSAGE. PERFORMED A GO AROUND AND WENT OVER CHECKLIST. LANDED, ENGAGED NOSE WHEEL STEERING, CAUTION LIGHT WENT OUT AND HAD NOSE WHEEL STEERING. TAXIED AIRCRAFT TO FBO WITHOUT INCIDENT. FOUND DOWNSDR DXTA2013032505332Uplock Switch · out of adjustON TAKEOFF WITH GEAR HANDLE UP, GREEN GEAR INDICATIONS LIGHTS WENT OUT, BUT RED LIGHT IN THE GEAR HANDLE REMAINED ILLUMINATED, FOLLOWED SHORTLY BY AMBER CAS MESSAGE "N GEAR NOT UP". KEPT AIRSPEED BELOW 200 KCAS, FOLLOWED CHECKLIST, AND GEAR CAME BACK DOWN NORSDR 2012F00260Spigot · corrodedRT HORIZONTAL STAB SPIGOT FITTING CORRODED.SDR GR4D2012FA601Spigot · corrodedLEFT HORIZONTAL STAB SPIGOT FITTING CORRODED.SDR 2012FA0000713Bonding Strap · shortedDURING CRUISE, CREW REPORTED AN INTERMITTENT FIRE WARNING INDICATION ON NR 1 ENGINE, WHICH SUBSEQUENTLY TURNED INTO A STEADY INDICATION. FOLLOWED PROCEDURES IN THE AFM IN ORDER TO CONFIRM OR EXCLUDE VALIDITY OF INDICATION. DETERMINED INDICATION WAS FALSE. SDR DXTA2012101805151Windshield · failedLEFT, FORWARD WINDSHIELD FAILED IN FLIGHT AT FL450. OUTER HEATING PANE ONLY. R & R WINDSHIELD. OPS & LEAK CHECKED GOOD. REF. CMP 561005, B04027 & STANDARD PRACTICES FAS W/O NR 12-2319.SDR 2012FA0000670Skin · delaminatedRT GROUND SPOILER ASSY IS DELAMINATED BEYOUND LIMITS. SEE W/O SC2193.19.1 AND 18.6.3.SDR BKEA20120720001Warning System · activatedDURING FLIGHT LEFT AFT FLOOR CAS MESSAGE ILLUMINATED. PROCEDED TO GO THREW EMERGENCY CHECK LIST AND LANDED AIRCRAFT AT KFAR.SDR DXTA2012060404985Ground Wire · arcedWHILE WORKING AUX FUEL PUMP PROBLEM, FOUND WHERE GROUND WIRE HALF ARC THROUGH FUSELAGE. FOUND AN EXCESSIVE AMOUNT OF CORROSION AND SIGNS OF ARCHING ON GROUND STUD TO AUX PUMP. REPAIRED IAW CS289825.SDR DXTA2012052904980Rod · disconnectedON DEPARTURE, "RT MAIN GEAR NOT UP" MESSAGE WITH RED LIGHT IN THE HANDLE. MESSAGE APPEARED AFTER TAKEOFF. ON LANDING, FOUND RT MLG FOLLOW-UP DOOR DISCONNECTED. PERFORMED LANDING GEAR CYCLING OPS TEST GV CMP 32. OPS TESTED GOOD. PERFORMED VISUAL INSPECTION SDR LD2R20120403001Adapter · backed outWHILE PERFORMING A SERVICE BULLITIN TO REPLACE THE FUEL PUMP SPLINE ADAPTER, WE FOUND THE ENGINE DRIVEN FUEL PUMP DRIVE SHAFT TO BE MIGRATING OUT OF THE FUEL PUMP AND INTO THE ACCESSORY GEAR CASE. UPON INSPECTION OF THE GEAR CASE WE FOUND A RETAINING PLUG IN SDR DXTA2012031504921Warning Message · false activationLEFT ENGINE DATA MISCOMPARE. HIGH OIL TEMP CAS MESSAGES. PRECAUTIONARY SHUTDOWN. COULD NOT DUPLICATE DISCREPANCY.SDR DXTA2012030204894Warning Message · false activationFINAL APPROACH, 170 KTS, FLAPS 20, GEAR SELECTED DOWN & RECEIVED NORMAL DOWN THREE GREEN. DURING DECELERATION TO APPROX 150 KTS, RECEIVED AMBER RT MLG UNSAFE CAS MESSAGE FOLLOWED BY AUDIBLE ALERT FOR "TOO LOW/GEAR NOT DOWN." ON GO AROUND, KEPT GEAR DOWN. AT 2SDR DXTA2012021404876Brake Sys · malfunctionedBRAKES ARE EXTREMELY GRABBY. APPLYING STEADY PRESSURE RESULTS IN NO INITIAL PRESSURE UNTIL INDICATION READS 300 PSI, THEN BREAKS START TO GRAB.SDR 2011FA0000730Display · failedAFTER 2.5 HOURS OF GROUND AND FLIGHT OPERATION ON 10-21-2011, AN ACRID/SMOKEY ODOR WAS NOTICED IN THE COCKPIT. ALL SYS WERE FOUND TO BE OPERATING NORMALLY. APPROX 40 MINUTES LATER, SMOKE WAS OBSERVED EMANATING FROM THE PILOT'S CMC1100 EDU. THE UNIT WAS THENSDR DXTA2011100604746Smoke Detector · false activationAFT LAV SMOKE RED CAS MSG ILLUMINATED IN FLIGHT. TROUBLESHOOTING FOUND DEFECTIVE SMOKE DETECTOR. REMOVED DEFECTIVE DETECTOR. INSTALLED REPAIRED UNIT. OPS CHECKED GOOD. WORK DONE IAW CMP 261502.SDR 2011FA0000636Panel · damagedAPPROX 4" DIAMETER HOLE IN INNER BYPASS DUCT PANEL OVER NR1 IGNITOR OF RT ENGINE.SDR 2011FA0000443Hose · leakingLEFT HYD SYS OIL LEAKAGE WAS DETECTED ON THE SYNOPTIC DISPLAY. AT FL410 AND 1.5 HOURS OUT THE PIC ELECTED TO TURN BACK TO DEPARTURE. WITH 0.5 GALLONS OF HYD FLUID REMAINING, THE ACFT LANDED WITHOUT INCIDENT. MX DETECTED FLUID LEAKAGE FROM THE LT PYLON. UPOSDR 2011F00114Warning System · shortedDURING CRUISE, FLIGHT CREW REPORTED INTERMITTENT FIRE WARNING ON NR 2 ENGINE. FLIGHT CREW FOLLOWED PROCEDURES IN AFM IN ORDER TO CONFIRM OR EXCLUDE VALIDITY OF INDICATION. FLIGHT CREW DETERMINED INDICATION WAS FALSE. MX TROUBLESHOT SYS AND DETERMINED THAT WISDR EW7A2011F00112Fire Warning · false activationDURING CRUISE, FLIGHT CREW REPORTED INTERMITTENT FIRE WARNING INDICATION ON NR 2 ENGINE. FLIGHT CREW FOLLOWED PROCEDURES IN AFM IN ORDER TO CONFIRM OR EXCLUDE VALIDITY OF INDICATION. FLIGHT CREW DETERMINED INDICATION WAS FALSE. MX VERIFIED THAT THE INDICATIOSDR 2011FA0000300Line · chafedTHE LT SYS HYD FLUID LEAKAGE WAS DETECTED AT MIDPOINT OF A 2 HR FLIGHT AT FL 410. DURING DESCENT, THE INDICATION WENT CLOSE TO ZERO. THE PIC ELECTED TO DIVERT FOR THE LARGER 12,000 FT RUNWAY IN CASE THE BRAKES AND NOSE WHEEL STEERING WERE DEGRADED. THE LANDSDR DXTA2011042204553Resolver · inoperativeON TAKEOFF, WHEN FLAPS WERE RETRACTED, STAB DID NOT COME FULLY UP. RECEIVED AN AMBER CAS MESSAGE, UNCOMMANDED STAB AND BLUE CAS MESSAGES FLAP/STAB. MX-RQD A-B AND FLAP/STB SYS FLAP A MESSGE. STAB PART OF FLAP POSITION INDICATOR SHOWED AMBER AND NOT FULLY UPSDR AMCR201103Module · inoperativeVIDEO FAILED IN CABIN ENTERTAINMENT SYS. UPON REMOVING THE AUDIO/VIDEO MODULE, THE MODULE HAD A DISTINCT BURNED ODOR TO IT. A REPLACEMENT MODULE WAS INSTALLED AND WAS INOPERATIVE. REPLACEMENT UNIT DISPLAYED CODE "NO" WHICH MEANS "NEVER ONLINE". A SECOND UNITSDR AMCR201102Module · shortedORIGINALLY, THE ACFT HAD A CABIN MANAGEMENT MODULE DEGRADATION IN WHICH THE GALLEY POWER WAS INTERMITTENT. THIS MODULE ALSO CONTROLS THE LAVATORY LIGHTING. THE REPLACEMENT COMPONENT, REPAIRED BY REPAIR FACILITY, IMMEDIATELY POPPED THE CIRCUIT BREAKER, WHICH RESDR DXTA2011030704494Pressure Switch · failedLEFT MAIN FUEL PUMP FAILED IN FLIGHT. R & R LT MAIN FUEL PUMP PRESSURE SWITCH WORK ACCOMPLISHED IAW GV CMP 284305.SDR 2011FA0000124Life Raft · mismanufacturedAFTER INFLATION DURING A ROUTINE INSPECTION OF LIFE RAFT, OBSERVED THE LOWER BOUYANCY TUBE IS CONSIDERABLY SMALLER IN DIAMETER & CIRCUMFERENCE WHEN COMPARED TO UPPER BOUYANCY TUBE. AS A RESULT, THE LOWER TUBE SEAMS (INTERIOR OBSERVATION)ARE BOWED INWARD & FLOOSDR AMCR201004Tire · out of round(AMCR) DURING TAKEOFF AND LANDING, CREW REPORTED A NOSE GEAR SHIMMY. MX FOUND THE LT NOSE TIRE TO BE OBLONG-OUT OF ROUND. THERE WAS NO UNUSUAL WEAR OR FLAT SPOTS ON TIRE. MX REPLACED WHEEL ASSY.SDR 2010FA0000197Probe · groovedPILOT WROTE UP ALTIMETER SPLIT, WITH MADC NR 2 SHOWING 240' DIFFERENCE FROM MADC NR 1 & 3. MX PERFORMED PITOT/STATIC LEAK CHECK WHICH SHOWED A STATIC LEAK BEYOND LIMITS FOR MADC NR 2. TROUBLESHOT SYS AND FOUND THE LOWER LT PITOT/STATIC PROBE TO BE LEAKING. SDR N93A021210Dump Valve · brokenAFTER TAKEOFF AND RAISING GEAR HANDLE, GEAR HANDLE RED LIGHT ILLUMINATED. CYCLED GEAR DOWN WITH NORMAL INDICATIONS. ATTEMPTED TO RAISE GEAR AGAIN WITH SAME RESULTS. CYCLED GEAR DOWN WITH ALL 3 GREEN. LANDED NORMAL. MAINTENENCE REMOVED AND REPLACED LANDING GSDR 2009FA0000811Actuator · leakingTESTING PLUG BACKED OUT OF THE RUDDER ACTUATOR CASE, BECAUSE IT WAS NOT SAFTIED, RESULTING IN THE RIGHT HYDRAULIC SYSTEM DRAINING TO ZERO IN FLIGHT.SDR 2009FA0000754Firing Head · damagedDURING ROUTINE INSPECTION OF TWO (2) LIFE RAFTS LAST RETURNED TO SERVICE BY RIVER SERVICES INC. FAA 145 REPAIR STATION NR AI5R727M IN NOVEMBER OF 2008, IT WAS DISCOVERED THAT THE BAYONET PROTECTIVE COVERS REMAINED IN PLACE IN-BETWEEN THE FIRING HEAD AND CYLINDSDR 2009FA0000753Firing Head · damagedDURING ROUTINE INSPECTION OF TWO (2) LIFE RAFTS LAST RETURNED TO SERVICE BY RIVER SERVICES INC. FAA 145 REPAIR STATION NR AI5R727M IN NOVEMBER OF 2008, IT WAS DISCOVERED THAT THE BAYONET PROTECTIVE COVERS REMAINED IN PLACE IN-BETWEEN THE FIRING HEAD AND CYLINDSDR N93A20090423508QSAccumulator · leakingPRIOR TO LANDING, BRAKE PRESSURE GAUGE SHOWED 900 PSI. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT.SDR N93ABeam · crackedCRACK LOCATED ON WING REAM BEAM BEHIND FLIGHT SPOILER ACTUATOR BRACKETS. (LT AND RT) PER CUSTOMER BULLETIN THIS IS A RESULT OF IMPROPER RIGGING OF THE FLIGHT SPOILERS.SDR N93A20081103Beam · crackedCRACK LOCATED ON WING REAR BEAM BEHIND FLIGHT SPOILER ACTUATOR BRACKET. LT AND RT PER CUSTOMER BULLETIN THIS IS A RESULT OF IMPROPER RIGGING OF THE FLIGHT SPOILERS.SDR N93A20061221Contactor · faultyACRID SMELL IN COCKPIT DURING PREFLIGHT. MAINTENANCE DETERMINED ODOR WAS FAULTY AC CONTACTOR.SDR UG8APA06007Pitot Tube · blockedNR 1MADC HAD AN ALTITUDE COMPARATOR AT 15000 FT AND A 400 FT SPLIT FROM MADC AND STDBY AT FL230. IT ALSO HAD A 5 CKAS SPLIT IN AIRSPEED. BLOCKAGE FOUND IN LT UPPER PITOT/STATIC PROBE, OF UNKNOWN ORIGIN. BLEW OUT STATIC LINES USING DRY NITOGEN. INSTALLED NESDR 65810262006Steering Sys · failedNOSE WHEEL STEERING FAIL CASS MESSAGE AS AIRCRAFT LINED UP FOR TAKEOFF.SDR N93A20060328Shutoff Valve · malfunctionedDURING DESCENT AT FL 200 BLUE CAS MESSAGE BAGG COMPT LO PRESS ILLUMINATED. UNABLE TO OPEN INTERIOR BAGGAGE DOOR
Back to Gulfstream Aerospace G-V