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 TI92004F00000Starter Gen · failedSTARTER GENERATOR FAILED (OVERHEATED AND DROPPED OFF LINE).SDR AUS20040029Planetary Gear · vibrates(AUS) RT ENGINE VIBRATION. INVESTIGATION FOUND THE VIBRATION CAME FROM THE PLANETARY GEARSET.SDR CA031125003Bracket · misinstalled(CAN) PROBLEM WAS FOUND ON LT SIDE GEAR DOOR STOP. BRACKET WAS INSTALLED BY AIRCRAFT MFG IN THE WRONG POSITION AND WRONG PN IAW MFG IPC BRACKET WAS CHANGED AND DOOR RIGGED IAW MM AND WORKED OK.SDR CA031028005Door · detached(CAN) AT 30,000 FT. ON DESCENT AT 300KIAS A SHUDDER WAS FELT ON AIRCRAFT. ALL GEAR INDICATION WAS NORMAL. LANDING GEAR LOWERED FOR LANDING ALL GREEN LIGHTS NO RED LIGHT IN HANDLE. LANDED NORMALLY, AT CHALKSIT WAS OBSERVED LT OUTBOARD GEAR DOOR WAS SEPERATED FSDR CA031024007Pump · leaking(CAN) ASTRA SPX SN 079 EXPERIENCED A STRIPPED FUEL LINE FITTING ON THE RT ENGINE MOTIVE FLOW PUMP INLET PORT. FOUND DURING THE ENGINEER'S MORNING POST-FLIGHT INSPECTION, 21 OCT 2003. THE AIRCRAFT EXPERIENCED HEAVY TURBULENCE THE PREVIOUS NIGHT,THOUGH THIS IS NSDR CA030929004Steering Sys · malfunctioned(CAN) AFTER TOUCH DOWN APROX 80 KNOTS THE NOSE GEAR STEERING WHEEL AUTOMATILLY WHEN TO A FULL LEFT TURN COMMAND. THE AIRCRAFT DEPARTED THE RUNWAY TO THE LT AND CAME TO A REST AT APROX 90 DEGREES TO THE RUNWAY IN THE SOIL AREA NEXT TO RUNWAY. THE RT WING TIP STSDR JGV2003F00002Fuel Tank · leakingFUEL LEAKING INTO CABIN FROM CENTRAL TANK LOWER. INSUFFICIENT AMOUNT OF SEALANT APPLIED TO INTERIOR TANK AND EXTERIOR PORTION OF FUEL TANK. FUEL FLOWING OUT OF CABIN DRAIN. INSULATION IN LEAKING AREA SOAKED WITH FUEL. (CE09200304095)SDR 2003FA0000908Fuel Tank · leakingFUEL LEAKING INTO THE AIRCRAFT CABIN FROM THE AIRCRAFT CENTER TANK DUE TO IMPROPER INTERNAL AND EXTERNAL SEALING AT MANUFACTURE. THE FUEL TANK FASTENERS APPEAR TO HAVE BEEN INSTALLED WITHOUT ADEQUATE SEALING. RECOMMEND ACO NOTIFICATION AS THIS HAS BEEN AN HISDR CA030704002Sleeve · damaged(CAN) DURING ROUTINE A-CHECK A DAMAGED SLEEVE WAS FOUND ON THE AIR CONDITIONING DUCT FROM THE COOLING TURBINE TO THE WATER SEPERATOR UNIT. THE DUCT HAD A 1 CM DIAMETER HOLE IN THE SIDE WALL ALLOWING THE AIR TO DUMP UNDER THE BAGGAGE FLOOR. NO ADDITIONAL DAMAGESDR 2003FA0000653Door · out of rigRED INTRANSIT LIGHT STAYED ON AFTER SELECTING GEAR UP. RIGGED RT MLG INBOARD DOOR AND RIGGED RT AND LT OUTBOARD. MLG DOORS IAW MM 32-10-07. FUNCTIONAL CHECKED GOOD.SDR CA030424004Duct · cracked(CAN) DURING A 1000 HR INSPECT, AFT BAGGAGE COMPARTMENT INTERIOR WAS REMOVED, ALLOWING INSPECTION ACCESS TO THE RAM AIR DUCT. THIS PLASTIC DUCT IS LOCATED ON THE RIGHT HAND SIDE TUCKED TIGHTLY AGAI NST THE FUSELAGE SKIN AT STA 350. DURING INSPECTION, A 10 INCHSDR O9I2003F00000Housing · leakingPILOT REPORTED OIL ON LEFT ENGINE COWLING AFTER FLIGHT. PERFORMED GROUND RUN OF ENGINE AND FOUND PIN HOLE IN ENGINE DRIVEN OIL SUPPLY PUMP HOUSING.SDR 27527601Windshield · failedAIRCRAFT STATIC ON RAMP WITH APU RUNNING. WINDSHIELD OUTER PLY SHATTERED. WINDSHIELD REPLACED.SDR CA021108004Cap · leaking(CAN) DEPARTED ENROUTE 30 MIN AFT. DEPARTURE CLIMBING THROUGH FL310 POP/BANG HEARD FOLLOWED BY HYD LIGHT THEN LT HYD PUMP LIGHT THEN DECREASE IN HYD PRESSURE TO 1500 PSI. RT PUMP LIGHT ON PRESSURE DROP TO 1500 PSI. A/C TURNED AROUND FOR YYZ, FUEL DUMPED, ASDR AUS20021111Gasket · faulty(AUS) RT BLEED AIR LINE THERMOSTAT GASKET FAILED. FURTHER INVESTIGATION FOUND THAT THE RT BLEED SWITCHING VALVE OUTLET TEMPERATURE WAS HIGH.SDR JGV2002F00008Fastener · interferenceRIVET BUCK TAIL INTERFEARENCE WITH CABIN WINDOW FLANGES ON THE PERIMETER OF WINDOW FRAME. WINDOW SEALS CUT AT FACTORY. REPAIRED PER EO DDA0825W342121 REVD. INSTALLED NEW SEALS, ALL CABIN WINDOWS.SDR CA020430012Fire Loop · intermittent(CAN) WHILE ON DESCENT CREW HAD FIRE INDICATION RT ENGINE. EMERGENCY PROCEDURES INITIATED WHERE BOTH FIRE BOTTLES WERE BLOWN TO EXTINGUISH POSSIBLE FIRE AND ENGINE SHUT DOWN. LIGHT WENT OUT. LANDED WITH CRASH TRUCKS STANDING BY UNEVENTFULL. DURING TAXI IN, LIGSDR CA020501003Switch · malfunctioned(CAN) ON SHUTDOWN, LT ENGINE LOW OIL PRESSURE ANNUNCIATOR LIGHT DID NOT COME ON. INDICATOR LIGHT TEST FOUND SERVICEABLE. PRESSURE CHECKING OF SWITCH WITH NITROGEN FOUND ANNUNCIATOR COMING ON AT 60 PSI AND OFF AT 51 PSI AS MARKED ON SWITCH. SWITCH ASSY REINSTASDR CA011127016Wire · shorted(CAN) LT STARTER GEN WIRE RUBBED THROUGH AND CAUSED DIRECT SHORT TO GROUND IN LT PYLON SUPPORT. WIRE SHORTED AND TOOK GENERATOR OFF LINE. LANDED UNEVENTFULL AT SCOTTSDALE AZ. REPLACED ALL 4 WIRES AND SUPPORT UNDER IAI ENGINEERING ORDER.SDR CA020129004Bolt · failed(CAN) UPON DEPLANING OF A/C AT DESTINATION, PASSENGER NOTIFIED CAPTAIN THAT OUTBOARD PORTION (LATCH SIDE) OF HIS SEAT BELT HAD BECOME DETACHED FROM HIS SEAT WHEN HE ATTEMPTED TO SECURE IT FOR DESCENT INTO AIRPORT. HE HAD THEN MOVED TO ONE OF UNOCCUPIED SEATS ISDR AUS20010945Pipe · worn(AUS) LT ENGINE FUEL LINE CHAFED. FOUND DURING INSPECTION IAW ALERT SBTFE731-A73-5126.SDR JGV2001F00010Window · chippedNR 2 RIGHT CABIN WINDOW WITH LOOSE CHIP ON EDGE. EDGE OF WINDOW WAS CHAFING ON A FUSELAGE RIVET. WINDOW IS CHIPPED BEYOND LIMITS.SDR JGV2001F00007Window · damagedLEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR 1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS ARE OF THE WINDOW. THE WINDOW SEALS ARE CUT AS WELL. IT APPEARS THE WINDOWS WERE TRIMMED OF SDR JGV2001F00006Window · damagedLEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR 1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS AREA OF THE WINDOW. THE WINDOW SEALS ARE CUT AS WELL. THE WINDOWS WERE TRIMMED OF SEALANT (SSDR JGV2001F00005Window · damagedLEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR 1,2,3,4,5, AND 6 WINDOWS HAVE THE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS AREA OF THE WINDOW. THE ASSOCIATED WINDOW SEALS ARE CUT AS WELL. WINDOWS WERE TRIMMED OFSDR JGV2001F00004Window · damagedLEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS AREA OF THE WINDOW. THE ASSOCIATED WINDOW SEALS ARE CUT AS WELL. APPEARS THE WINDOWS WERE TRISDR JGV2001F00003Window · damagedLEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT 1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON VIEWABLE AREA, THIS IS STRESS AREA OF WINDOW. ASSOCIATED WINDOW SEALS ARE CUT AS WELL. IT APPEARS THE WINDOWS WERE TRIMMED OF SSDR 27314102Pump · leakingOIL PUMP LEAKING THRU CASE DUE TO WORMING. REMOVED AND REPLACED OIL PUMP.SDR 27314101Pump · leakingOIL PUMP LEAKING THRU CASE DUE TO WORMING. REMOVED AND REPLACED PUMP.SDR 27515331Pump · leakingOIL PUMP LEAKING THRU CASE DUE TO WORMING. REMOVED AND REPLACED PUMP.SDR CA010307010Actuator · failed(CAN) RUDDER TRIM FREEZING AT ALTITUDE. FOUND UPPER RUDDER TRIM MOTOR TO BE THE PROBLEM.THE TRIM MOTOR WAS REPLACED AND NO FURTHER PROBLEMS HAVE BEEN EXPERIENCED.SDR 20000920SH014Flux Detector · failedTRIP CANCELLED WITH AIRCRAFT ON RAMP DUE TO NO HDG INFO ON PILOT''S PFD AND MFD CAUSED BY FAILURE OF LEFT FLUX VALVE. (X)SDR 20000908SH007Actuator · defectivePILOTS FELT VIBRATION IN RUDDER PEDALS. FOUND EXCESSIVE PLAY (LINEAR) IN UPPER RUDDER TRIM ACTUATOR. REPLACED ACTUATOR. (X)SDR 20000830SH027Seal · blownLOUD ''POP'' HEARD IN-FLIGHT. DOOR SEAL LIGHT ''ON''. DOOR SEAL (PRIMARY) DEFLATED. SECONDARY DOOR SEAL HELD PRESSURE. FOUND PRIMARY DOOR SEAL BLOWN. DOOR SEAL REGULATOR FAILED TO CONTROL PRESSURE. BLEW DOOR SEAL. REPLACED SEAL AND REGULATOR. (X)SDR 99ZZZX4399Relay · failedPART FAILED, CAUSED AUTOPILOT LOSS OF NOSE UP TRIM. NORMAL TRIM WAS NOT EFFECTED.SDR CA991028030Thrust Reverser · cracked(CAN) CRACK FOUND ON LEFT TAIL ROTOR ASSY INSIDE TAILPIPE ON LEFT UPPER EDGE APPROXIMATELY 2 INCHES IN LENGTH.SDR 2000ZZZX39Actuator · frozenBOTH THE TOP AND BOTTOM ROLLER TRIM ACTUATORS BECAME INOPERATIVE AT ALT DUE TO FREEZING. SUBMITTER STATED THIS IS THE SECOND OCCURRENCE OF THIS PROBLEM ON THEIR AIRCRAFT.SDR 99ZZZX3971Vibmeter · stuckNEEDLE STUCK DURING TEST. REPLACED WITH SERVICEABLE UNIT.SDR 99ZZZX3514Float Switch · inoperativeTRANSFER VALVE WOULD NOT WORK IN THE 'AUTO' POSITION. REPLACED SWITCH WITH NEW.SDR 99ZZZX3513Rtv · inoperativeCOPILOT TRV INOPERABLE. REPLACED WITH OVERHAULED UNIT.SDR 99ZZZX3392Triple Indicator · inoperativeAT AN POWER-UP, NEEDLE STAYED AT ZERO IN FUEL TEMPERATURE, CABIN TEMP AND OAT. REPLACED WITH SERVICEABLE UNIT.SDR 99ZZZX3391Ammeter · failedAMPS-METER WILL DROP TO ZERO. WILL RESET BY PUSHING VOLT BUTTON, BUT FALLS BACK TO ZERO IN A FEW SECONDS. REPLACED GAUGE WITH SERVICEABLE UNIT.SDR 99ZZZX3390Radar · inoperativeRADAR IS INOPERATIVE IN ANY MODE. REPLACED.SDR 99ZZZX3389Transponder · failedTRANSPONDER WAS HARD FAILED. REPLACED WITH SERVICEABLE UNIT.SDR 99ZZZX3326Voltmeter · failedRIGHT VOLTMETER/AMMETER AMPS DROP TO ZERO. CAN BE RESET TO NORMAL BY PUSHING VOLTS BUTTON. WILL THEN DROP BACK TO ZERO. REPLACED METER WITH NEW. OPS TESTED NORMAL.SDR 99ZZZX2911Indicator · malfunctionedPILOTS OBSERVED A 'FUEL FILTER BYPASS' INDICATION. FUEL FILTERS WERE CHANGED. INDICATION WAS STILL THERE. CHANGED LEFT ENGINE FUEL DIFFERENTIAL PRESSURE INDICATOR. PROBLEM FIXED.SDR 99ZZZX2593Radar · inoperativeUNIT WILL NOT TEST OR PAINT. INOPERABLE. REPLACED.SDR 99ZZZX2592Tcas · malfunctionedDURING HIGH TEMPERATURES, OUTSIDE UNIT WILL TRIP CIRCUIT BREAKER. REPLACED AND TESTED IN 90 DEGREE FAHRENHEIT (NOT HOT ENOUGH IN MDT). WILL TEST IN SDL, FOR A TRUE TEST.SDR 99ZZZX2591Actuator · leakingLEAKING FROM AROUND PISTON SHAFT. REPLACED WITH NEW UNIT.SDR 99ZZZX2590Actuator · leakingLEAKING FLUID OUT OF EMERGENCY GEAR EXTENSION VALVE. SHUTTLE VALVE ON NLG ACTUATOR WAS FOUND BYPASSING OUT TO THE VENT LINE. PURGED HYDRAULIC LINES AND RPELACED NLG ACTUATOR.
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