Gulfstream Aerospace ASTRA SPX
Service difficulty reports · 136
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 = 'ASTRASPX' 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 = 'ASTRASPX' 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 CA190617027Duct · damaged(CAN) DURING ROUTINE INSPECTION, NOTICED THAT THERE WAS SOME DAMAGE ON LH ENGINE ON THE OUTER BYPASS DUCT JUST AFT OF THE IGNITION BOX. BORESCOPED THE ENGINE AND ENGINE RUNS CARRIED OUT FOR VIBE CHECK WHICH INDICATED A SERVICEABLE ENGINE. REMOVED THE ENGINE FRSDR CA190330001Ground Wire · overheated(CAN) DURING GROUND OPERATION IT WAS NOTED THAT THE AIRCRAFT WOULD NOT ACCEPT EXTERNAL GOUND POWER, TROUBLESHOOTING OF THE EXTERNAL POWER ELECTRICAL SYSTEM FOUND THE EXTERNAL POWER GROUND LEAD TO AIRCRAFT RIB TO BE AT FAULT. CARRIED OUT GROUND (G45) REPAIR ANDSDR 7SJA201808150001Autopilot Sys · malfunctionedAFTER TAKEOFF, DURING CLIMB OUT, CREW ENGAGED THE AUTOPILOT AND EXPERIENCED AN UNCOMMAND AUTOPILOT PITCH AND YAW. DISCONNECTED THE AUTOPILOT AND RETURNED TO DEPARTURE.SDR 2018F00147Seal · pinchedDURING CLIMB OUT. THE CREW EXPERIENCED A MAIN PAX DOOR WARNING LIGHT. IAW QRH RETURNED TO DEPARTURE. INSPECTED THE DOOR SEAL, AND FOUND IT TO BE PINCHED AND PROTRUDING, PUSHED BACK INTO PLACE, OPS GOOD.SDR 7SJA20180108001Cabin Pressure · malfunctionedDURING CRUISE AT FL410, THE CABIN PRESSURE BEGAN CLIMBING OVER 2000 FPM. RAPIDLY RISING TO FL270. EXECUTED AN EMERGENCY DESCENT AND LEVELED OFF AT 17,000 FT AND RETURNED TO DEPARTURE.SDR 2018F00003Line · crackedNR 2 ENGINE RIGID FUEL LINE FROM THE FUEL CONTROL TO THE FUEL MANIFOLD, FOUND CRACKED. RESULTING IN AN ENGINE SHUTDOWN AND FAILURE TO RESTART IN FLIGHT. REMOVED THE FAILED RIGID LINE AND INSTALLED NEW FLEXIBLE FUEL HOSE IAW LMM.SDR DBCA201611190006Fire Loop · failed10 MINUTES INTO FLIGHT, THE LEFT ENGINE LOWER SQUIB LIGHT ILLUMINATED. CREW RETURNED TO DEPARTURE. LANDING WAS UNEVENTFUL. MAINTENANCE FOUND LEFT AFT FIRE LOOP HAD FAILED AND REPLACED THE FIRE LOOP. OPS CHECKED GOOD.SDR DBCA2016060200003Line · failedON APPROACH, CREW EXPERIENCED HYDRAULIC QTY LOW LIGHT FOLLOWED BY HYDRAULIC PRESSURE AND BOTH HYDRAULIC PUMP LIGHTS INTERMITTENTLY ON LANDING. CREW ALSO NOTED INTERMITTENT BRAKING AND NOSE STEERING DIFFICULTIES. MAINTENANCE SUSPECTS SPEED BRAKE LINE IS LEAKSDR DBCA2014080800003Actuator · faultyON DEPARTURE THE FLAPS & SLATS WOULD NOT RETRACT. CREW DIVERTED & LANDING WAS UNEVENTFUL. COMPLETED FUNCTIONAL CHECKS OF THE FLAPS & SLATS. FOUND LT NR 3 FLAP ACTUATOR INTERNAL POSITION POTENTIOMETER ERRATIC. REPLACED FLAP ACTUATOR. OPERATIONS CHECKED GOOSDR Y9PA20140116002Tube · damagedINPUT TUBE TO INFLATABLE DOOR SEAL HAS A BLOWN HOLE WHERE IT ATTACHES TO THE DOOR SEAL.SDR CA130920018Warning Message · false activation(CAN) CLIMBING THROUGH FL280 THE RT "BLEED AIR LEAK" LIGHT ILLUMINATED, RAN THE CHECKLIST WHICH DIRECTED TO SWITCH TO EMERGENCY BLEED SOURCE. AFTER 5 SECONDS, THE BLEED AIR LEAK LIGHT EXTINGUISHED. ALL ENGINE INDICATIONS AND BATTERY TEMPERATURES REMAINED AT SDR CA130823010Shroud · misinstalled(CAN) DURING MAINTENANCE PERFORMING AN APU REMOVAL, THE APU EXHAUST STUB WAS FOUND INCORRECTLY INSTALLED. THIS LEAD TO HOT EXHAUST ON THE FRAME AT BS 492.75 ON THE RT SIDE OF THE ACFT AND CARBON DEPOSITS EVIDENT THROUGHOUT THE TAILCONE, HORIZ/VERT STABILIZERSSDR Y9PA20140605001Lens · damagedINSTALLED LAMPS 4553 BULB & IT BURNED A HOLE IN THE LANDING LIGHT LENS.SDR Y9PA201306180001Thermister · out of toleranceAFTER TAKEOFF, FLIGHT CREW RECEIVED A BATTERY OVERTEMP WARNING AND BATTERY TEMP INDICATION ROSE ABOVE 188 DEGREES C, UPON RETURN, BATTERIES WHERE COLD TO THE TOUCH, PERFORMED RESISTANCE CHECK OF THE THERMISTOR IN THE NR 2 BATTERY AND THE RESISTANCE WAS OUT OF SDR DBCA201305230007Cable · disengagedENROUTE, "SLAT INBALANCE" MESSAGE ILLUMINATED. DIVERTED. LANDED UNEVENTFULLY. FOUND RIGHT SLAT CABLE HAD DISENGAGED FROM SLAT POWER DRIVE. REPLACED SLAT CABLE WITH NEW AND RIGGED. OPS CHECKED GOOD.SDR CA130110002Frame · burned(CAN) GROUND CABLE FOR GPU PLUG ARCED OUT AT ANCHOR NUT BURNING FRAME UNDER ANCHOR NUT AND CAUSED RIVETS TO COME LOOSE. GPU PLUG FAILED INTERMITTENTLY CAUSING FURTHER INVESTIGATION TO FIND CAUSE. REPAIRED 2013/01/10 ADDITIONAL INFORMATION CAN BE FOUND IN RDISDR CA121121003Bottle · failed(CAN) DURING ROUTINE DI, NOTICED EMERGENCY BLOW DOWN BOTTLE WAS INDICATING ZERO. INVESTIGATION REVEALED BOTTLE HAD FAILED AT CONNECTION MANIFOLD ASSY. BOTTLE CONTAINS 3000 PSI NITROGEN.SDR 2011FA0000802Shaft · separatedENGINE REMOVED FOR SCHEDULED 2500 HR, MAJOR PERIODIC INSPECTION AND 5000 HR COMPRESSOR ZONE INSPECTION. DISASSEMBLY FINDINGS REVEALED SEPARATION OF THE SHAFT ADJACENT TO THE HIGH PRESSURE COMPRESSOR AFT CURVIC TEETH.SDR PJEA2011F00001Pump · inoperativeUPON LANDING, AFTER AN UNEVENTFUL 1 HR FLIGHT, PILOTS REPORTED THAT THE AUX HYD PUMP FAILED. AN O/H PUMP WAS SENT, WHERE A QUALIFIED MECH CHANGED THE PUMP ASSY AND THE FLIGHT CONTINUED UNINTERRUPTED.SDR PJEA2011F00000Windshield · crackedUPON LANDING, AFTER AN UNEVENTFUL .8 HR NIGHT FLIGHT. PILOTS REPORTED THAT THE RT WINDSHIELD WAS CRACKED HALF WAY AROUND. AFTER FURTHER INVESTIGATION IT WAS DETERMINED THAT THE CRACK WAS LIMITED TO THE OUTER PAIN. A SPECIAL FLIGHT PERMIT WAS OBTAINED AND THSDR CWQA11032011Hydraulic Line · chafedDURING CRUISE MAIN HYD LIGHT ANNUNCIATOR ILLUMINATED, THE LT AND RT HYD PUMP LIGHTS STARTED TO ILLUMINATE AND MAIN HYD PRESSURE DROPPED. CHECK LIST FOLLOWED AND UNSCHEDULED LANDING PERFORMED WITHOUT INCIDENT. GEAR EXTENDED NORMALLY, EMERGENCY BRAKES WERE USESDR 26N2011F00002Starter Gen · damagedCREW REPORTED THE LT ENGINE WILL NOT START. NO N1 ROTATION DURING START SEQUENCE. TROUBLESHOT SYSTEM AND FOUND DEFECTIVE START/GEN AND DRIVE SPLINE. R & R START/GEN WITH TSO: 0.0 UNIT AND INSTALLED "NEW" DRIVE SPLINE. REMOVED START/GEN: SN 96011 PREVIOUSLYSDR DBCA2010083000028Actuator · failedON DEPARTURE, HORIZONTAL STABILIZER WOULD NOT TRIM. DIVERTED, LANDING WAS UNEVENTFUL. INSPECTED BY MFG TECHNICIANS DETERMINED FAULT WAS CAUSED BY INTERNAL FAILURE OF HORIZONTAL STABILIZER TRIM ACTUATOR.SDR Y9PAN818WF709Relay · failedDURING CLIMB AFTER ENGAGING THE AUTOPILOT, THE CREW NOTICED THE A/P TRIM FAIL LIGHT ILLUMINATED ON THE MASTER CAUTION PANEL, THEN NOTICED THE AUTOPILOT ADVISORY THAT THE MACH TRIM HAD FAILED. THE CREW RETURNED TO HOME BASE (KHOU). DURING TROUBLESHOOTING FOUNSDR Y9PAN610SM609Aileron · delaminatedDURING PRE-FLIGHT OF AIRCRAFT BEFORE DEPARTURE, FOUND RT AILERON WITH SEVERE DELAMINATION, APPROX 6 X 24 INCHES.SDR U5QA06015Ecu · failed"FLAP UNBAL" LIGHT CAME ON IN FLIGHT CRUISE. PILOT ELECTED TO DIVERT (10,506 FT) AS A PRECAUTION IN CASE FLAPS FAILED TO EXTEND. FLAPS WERE NOT USED AND A UNEVENTFUL LANDING WAS MADE. CREW CYCLED FLAPS AND SYS DID EVENTUALLY FAIL. MX WAS CALLED AND FLAP SLAT ESDR CA080818003O-Ring · failed(CAN) RT BLEED LEAK LIGHT ILLUMINATED IN CLIMB OUT. AC RETURNED TO BASE. CONFIRMED LT BLEED LEAK ON GROUND DURING HIGH POWER ENGINE RUNS. COULD NOT DUPLICATE RT BLEED LEAK ON GROUND. FOUND BOTH BLEED SWITCHING VALVES LEAKING FROM REGULATOR FITTING ASSY. DUE TSDR U5QA06010Slat System · malfunctionedAIRCRAFT FLYING FROM MTN TO RDG IN DESCENT HAD LEADING EDGE SLAT FAULT. SYSTEM SHUT OFF. PILOT OVERRIDE SYSTEM TO DEPLOY FLAPS. CHANGED DESTINATION TO TEB. NO EMERGENCY DECLARED. MADE NORMAL LANDING. ON THE GROUND COULD NOT RESET SYSTEM. LATER HAD MAINTSDR 2008FA0000110Antenna · gougedFOLLOWING REMOVAL OF SATCOM ANTENNA FROM UPPER FUSELAGE FOR INSPECTION, NOTICED FOOTPRINT OF PREVIOUSLY REMOVED NR 1 VHF ANTENNA. UPON INSPECTION OF VHF ANTENNA FOOTPRINT, FOUND NUMEROUS APPARENT MECHANIC INDUCED GOUGES ON FUSELAGE OUTER SKIN. DAMAGE WAS APPSDR 2007FA0000976Rotor · separatedIAW SERVICE BULLETIN TFE731-72-5175. BLADE SEPARATION ON ONE LPT3 BLADE AS LISTED IN TABLE 1 OF S/B 72-5175.SDR 2007FA0000468Windshield · crackedTHE WINDSHIELD ON THE PILOT`S SIDE CRACKED DURING FLIGHT AT F/L 41,000 FT ON 4/24/2007. THE WINDSHIELD HAD 3104.6 TT. (K)SDR 2007FA0000062Retainer · separatedON 10/4/2006, 4TH AIRCRAFT EXPERIENCED A LT ENGINE EXHAUST FIRE AFTER ENGINE START AND PRIOR TO DEPARTURE. ENGINE WAS REMOVED AND RETURNED TO MFG FOR REPAIR. ENGINE WAS DISASSEMBLED IAW LMM 72-03-06, REV 8 FOR ENGINEERING INVESTIGATION. DISASSEMBLY FINDINGSSDR YNTA200687701Skin · delaminatedRIGHT AILERON UPPER SURFACE DELAMINATED SUBSTANTIALLY FROM WING RIB 19 TO 22 AND WIDTH OF APPROXIMATELY 4-5 INCHES. THIS DEFECT OCCURRED WITH NO WARNING. THE AREA IS INSPECTED DURING PREFLIGHT AND POSTFLIGHTS AND THE AIRCRAFT HAD BEEN IN MAINTENANCE FOR DUE SDR 2006FA0000125Aileron · delaminatedRT AILERON UPPER SKIN FOUND DELAMINATED FROM HONEYCOMB CORE. DELAMINATION COVERS MORE THAN 50 PERCENT OF UPPER SURFACE. AILERON REPLACED WITH SERVICEABLE UNIT. (K)SDR CA050929002Cap · loose(CAN) AFTER TAKEOFF,LOSS OF LT ENGINE OIL PRESSURE. SHUT DOWN LT ENGINE, DECLARED EMERGENCY AND RETURNED TO BASE. ENGINE SHOWED SIGNS OF OIL LEAK ON LT COWL. INVESTIGATED OIL LEAK AND FOUND THE OB OIL CAP LOOSE. INSPECTED OIL CAP/DIP STICK O-RING AND LOCKING ASDR 2005FA0001266Seat · brokenDURING REUPHOLSTERY OF PILOT SEAT, FOUND BACKREST FRAME BROKEN. CONTACTED MFG AND WAS GIVEN REPAIR TO ADD WELDED DOUBLERS. (CE09200505050) (K)SDR AJC2005F00011Bearing · failedCREW REPORTED DEPARTURE, ENROUTE, RT ENGINE DEEC COMPUTER TRIPPED TO MANUAL MODE, FOLLOWED BY THE LOSS OF THE N1 GGE INDICATION. FLIGHT CONTINUED NORMALLY, THEN EXPERIENCED A RT ENGINE VIBRATION WHICH CLIMBED TO .8 ON THE VIBRATION INDICATOR. REDUCED PWR ON SDR 2005FA0001203Attach Bracket · leakingFUEL LEAKING INTO CABIN. CUSTOMER SQKD FUEL SMELL INSIDE CABIN. REMOVED INTERIOR AND FLOOR PANELS AND FOUND ATTACHMENT BRACKETS MOUNTED INTO WING TANK (INCLUDING COLLECTOR BOX) FASTENERS LEAKING BADLY. DURING BOOST PUMP OPERATION, FUEL LEAK INCREASED TO COVSDR AJC2005F00007Pump · failedTHE RT TANK STANDBY FUEL PUMP (BOOST PUMP) DID NOT OPERATE WHEN SELECTED (ON) DURING PREFLIGHT INSPECTION. MAINTENANCE DEFUELED AIRCRAFT AND REPLACED THE RT TANK FUEL PUMP AND INSTALLED NEW GASKET. OPERATIONAL CHECK GOOD IAW MM. AIRCRAFT WAS RETURNED TO SERSDR 2005FA0000806Control Unit · out of toleranceTHE FSECU HAS A RELIABILITY PROBLEM. HERE IS THE FAULT HISTORY BELOW; SERVICE TIME ON S/N 131 IS 6.1 HOURS. SERVICE TIME ON S/N 149 IS 0.8 HOURS. SERVICE TIME ON S/N 140 IS 328.2 HOURS. SERVICE TIME ON S/N 107 IS 605.4 HOURS. SERVICE TIME ON S/N 317 IS 38SDR 2005FA0000805Control Unit · out of toleranceTHE FSECU HAS A RELIABILITY PROBLEM. HERE IS THE FAULT HISTORY BELOW; SERVICE TIME ON S/N 131 IS 6.1 HOURS. SERVICE TIME ON S/N 149 IS 0.8 HOURS. SERVICE TIME ON S/N 140 IS 328.2 HOURS. SERVICE TIME ON S/N 107 IS 605.4 HOURS. SERVICE TIME ON S/N 317 IS 38SDR 2005FA0000726Fcu · out of toleranceTHE SLATS FAILED TO EXTEND WHILE PILOTS WERE PERFORMING THE INSPECTIONS BEFORE TAKE-OFF. THE SLATS LOCKED OUT WHILE MECHANIC PLACED THE FLAP/SLAT SELECTOR TO DN POSITION. SLAT UNBALANCE LIGHT CAME ON SIMULTANEOUSLY. TROUBLE SHOOTING FOUND THE FSECU OUTPUT VOSDR 2005FA0000624Fcu · out of toleranceTHE SLATS FAILED TO EXTEND WHILE PILOTS WERE PERFORMING THE INSPECTIONS BEFORE TAKEOFF. THE SLATS LOCKED OUT WHILE MECHANIC PLACED THE FLAP/SLAT SELECTOR TO DN POSITION. SLAT UNBALANCE LIGHT CAME ON SIMULTANEOUSLY. TROUBLESHOOTING FOUND THE FSECU OUTPUT VOLTSDR AJC2005F00002Ahrs · intermittentON APPROACH THE NR 1 AHRS (ATTITUDE HEADING REFERENCE SYS) UNIT OPERATED INTERMITTENTLY, THE UNIT RED FLAGGED THE HEADING AND WAS UNABLE TO ENGAGE THE FLIGHT DIRECTOR. THE CREW WAS UNABLE TO SWITCH THE NR 2 AHRS TO DRIVE THE NR 1 SIDE. AC PROCEEDED AND LANDESDR CA050321007Engine · making metal(CAN) AFTER TAKEOFF, CREW NOTICED NR2 ENG CHIP DETECTOR WARNING LITE ON, FOLLOWED SHORTLY BY NR 2 ENGINE OIL FILTER LITE (WARNING). PILOT REDUCED THRUST ON NR2 ENGINE AND RETURNED TO AIRPORT. MAINTENANCE INSPECTION DISCOVERED METAL ON CHIP DETECTOR AND IN FISDR AJC2005F00001Engine · vibrationAC DEPARTED, ENROUTE, AT FL360 THE RT ENG DEEC COMPUTER TRIPPED TO MANUAL MODE, FOLLOWED BY LOSS OF N1 GGE INDICATION. FLIGHT CONTINUED NORMALLY, EXPERIENCED A RT ENG VIBRATION WHICH CLIMBED TO .8 ON THE VIBRATION INDICATOR. REDUCED POWER ON RT ENG TO 75 PERSDR LEGR200500001Door · crackedDURING ACCOMPLISHMENT OF AD 2004-13-18 FOUND RT MLG DOOR TO BE CRACKED AFTER REMOVAL OF DOOR HINGE. DOOR HINGE IS NOT REQUIRED TO BE REMOVED UNLESS THE AFT DOOR GAP IS LESS THAN 0.25 INCH PER AD AND REFERENCED SERVICE BULLETIN.SDR AJC2005F00000Uplock Switch · out of adjustAC DEPARTED, ENROUTE. AFTER RETRACTING THE GEAR ON CLIMB OUT, THE CREW NOTED THE RED UNSAFE LIGHT IN THE LANDING GEAR HANDLE WAS ILLUMINATED. THE CREW EXTENDED THE GEAR AND GOT THREE GREEN DOWN AND LOCKED LIGHTS. THE AIRCRAFT RETURNED AND LANDED SAFELY WITHSDR CA040430002Pump · failed(CAN) RT ENGINE FUEL FILTER BY-PASS LIGHT FLICKERING AT TAKE-OFF CLIMB POWER SETTINGS. AIRCRAFT RETURN TO MAINTENANCE BASE, MAINTENANCE TECHNICIAN FOUND FUEL FILTER CONTAMINATED BY A LOTS OF FINE GREY SEDIMENT. IT WAS DETERMINED THAT THE ENGINE DRIVEN MOTIVE FSDR CA040402003Door · misrigged(CAN) ON VISUAL INSPECTION AND NDT INSPECTION A CRACK OF 1 INCH WAS FOUND IN THE LT MLG OB DOOR SKIN AREA. IT WAS SUSPECTED THAT AT SOME TIME THE DOOR WAS RIGGED IMPROPERLY, DRAG LINK ADJUSTED TOO SHORT AND STRESSES THE AREA.
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