# Service difficulty reports: Gulfstream Aerospace ASTRA SPX

A list on [Gulfstream Aerospace ASTRA SPX](https://openairdocs.org/model/gulfstream-aerospace-astra-spx.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 136 reports

- [SDR CA190617027](https://openairdocs.org/sdr/CA190617027.md): Duct · damaged · Jun 13, 2019 · Israel ASTRASPX · Turbine Engine Bypass Section
  > (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 FR
- [SDR CA190330001](https://openairdocs.org/sdr/CA190330001.md): Ground Wire · overheated · Mar 26, 2019 · Israel ASTRASPX · Electrical Power System Wiring
  > (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 AND
- [SDR 7SJA201808150001](https://openairdocs.org/sdr/7SJA201808150001.md): Autopilot Sys · malfunctioned · Jun 23, 2018 · N818WB · Israel ASTRASPX · Autopilot System
  > AFTER TAKEOFF, DURING CLIMB OUT, CREW ENGAGED THE AUTOPILOT AND EXPERIENCED AN UNCOMMAND AUTOPILOT PITCH AND YAW. DISCONNECTED THE AUTOPILOT AND RETURNED TO DEPARTURE.
- [SDR 2018F00147](https://openairdocs.org/sdr/2018F00147.md): Seal · pinched · Mar 30, 2018 · N818WB · Israel ASTRASPX · Door Warning System
  > DURING 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 7SJA20180108001](https://openairdocs.org/sdr/7SJA20180108001.md): Cabin Pressure · malfunctioned · Jan 7, 2018 · N818WB · Israel ASTRASPX · Cabin Pressure Control System
  > DURING 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 2018F00003](https://openairdocs.org/sdr/2018F00003.md): Line · cracked · Aug 25, 2017 · N314AD · Israel ASTRASPX · Fuel Controlling System
  > NR 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 DBCA201611190006](https://openairdocs.org/sdr/DBCA201611190006.md): Fire Loop · failed · Nov 19, 2016 · N363NH · Israel ASTRASPX · Fire Detection
  > 10 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 DBCA2016060200003](https://openairdocs.org/sdr/DBCA2016060200003.md): Line · failed · Jun 2, 2016 · N363NH · Israel ASTRASPX · Hydraulic System, Main
  > ON 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 LEAK
- [SDR DBCA2014080800003](https://openairdocs.org/sdr/DBCA2014080800003.md): Actuator · faulty · Aug 8, 2014 · N919CH · Israel ASTRASPX · Trailing Edge Flap Actuator
  > ON 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 GOO
- [SDR Y9PA20140116002](https://openairdocs.org/sdr/Y9PA20140116002.md): Tube · damaged · Jan 7, 2014 · N818WF · Israel ASTRASPX · Passenger/Crew Doors
  > INPUT TUBE TO INFLATABLE DOOR SEAL HAS A BLOWN HOLE WHERE IT ATTACHES TO THE DOOR SEAL.
- [SDR CA130920018](https://openairdocs.org/sdr/CA130920018.md): Warning Message · false activation · Sep 17, 2013 · Israel ASTRASPX · Pneumatic Indicating System
  > (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 CA130823010](https://openairdocs.org/sdr/CA130823010.md): Shroud · misinstalled · Aug 21, 2013 · Israel ASTRASPX · APU Exhaust System
  > (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 STABILIZERS
- [SDR Y9PA20140605001](https://openairdocs.org/sdr/Y9PA20140605001.md): Lens · damaged · Jul 12, 2013 · N818W · Israel ASTRASPX · Exterior Lighting
  > INSTALLED LAMPS 4553 BULB & IT BURNED A HOLE IN THE LANDING LIGHT LENS.
- [SDR Y9PA201306180001](https://openairdocs.org/sdr/Y9PA201306180001.md): Thermister · out of tolerance · Jun 18, 2013 · N610SM · Israel ASTRASPX · Battery/Charger System
  > AFTER 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 DBCA201305230007](https://openairdocs.org/sdr/DBCA201305230007.md): Cable · disengaged · May 23, 2013 · N919CH · Israel ASTRASPX · Leading Edge Slat Control System
  > ENROUTE, "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 CA130110002](https://openairdocs.org/sdr/CA130110002.md): Frame · burned · Dec 31, 2012 · Israel ASTRASPX · Fuselage Main, Structure
  > (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 RDI
- [SDR CA121121003](https://openairdocs.org/sdr/CA121121003.md): Bottle · failed · Nov 21, 2012 · Israel ASTRASPX · Landing Gear Retraction/Extension System
  > (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 2011FA0000802](https://openairdocs.org/sdr/2011FA0000802.md): Shaft · separated · Dec 7, 2011 · N801RS · Israel ASTRASPX · Turbine Engine Compressor Section
  > ENGINE 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 PJEA2011F00001](https://openairdocs.org/sdr/PJEA2011F00001.md): Pump · inoperative · Nov 7, 2011 · N108CG · Israel ASTRASPX · Hydraulic Pump (Electric/Engine), Main
  > UPON 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 PJEA2011F00000](https://openairdocs.org/sdr/PJEA2011F00000.md): Windshield · cracked · Nov 7, 2011 · N108CG · Israel ASTRASPX · Flight Compartment Windows
  > UPON 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 TH
- [SDR CWQA11032011](https://openairdocs.org/sdr/CWQA11032011.md): Hydraulic Line · chafed · Nov 1, 2011 · N796HR · Israel ASTRASPX · Hydraulic System, Main
  > DURING 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 USE
- [SDR 26N2011F00002](https://openairdocs.org/sdr/26N2011F00002.md): Starter Gen · damaged · Sep 11, 2011 · N411MM · Israel ASTRASPX · Starter-Generator
  > CREW 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 PREVIOUSLY
- [SDR DBCA2010083000028](https://openairdocs.org/sdr/DBCA2010083000028.md): Actuator · failed · Aug 30, 2010 · N919CH · Israel ASTRASPX · Stabilizer Control System
  > ON 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 Y9PAN818WF709](https://openairdocs.org/sdr/Y9PAN818WF709.md): Relay · failed · Jul 23, 2009 · N818WF · Israel ASTRASPX · Autopilot System
  > DURING 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 FOUN
- [SDR Y9PAN610SM609](https://openairdocs.org/sdr/Y9PAN610SM609.md): Aileron · delaminated · Jun 15, 2009 · N610SM · Israel ASTRASPX · Ailerons
  > DURING PRE-FLIGHT OF AIRCRAFT BEFORE DEPARTURE, FOUND RT AILERON WITH SEVERE DELAMINATION, APPROX 6 X 24 INCHES.
- [SDR U5QA06015](https://openairdocs.org/sdr/U5QA06015.md): Ecu · failed · Jan 9, 2009 · N115BR · Israel ASTRASPX · Trailing Edge Flap Control System
  > "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 E
- [SDR CA080818003](https://openairdocs.org/sdr/CA080818003.md): O-Ring · failed · Aug 6, 2008 · Israel ASTRASPX · Engine Bleed Air System
  > (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 T
- [SDR U5QA06010](https://openairdocs.org/sdr/U5QA06010.md): Slat System · malfunctioned · Feb 20, 2008 · N115BR · Israel ASTRASPX · Leading Edge Slat Control System
  > AIRCRAFT 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 MAINT
- [SDR 2008FA0000110](https://openairdocs.org/sdr/2008FA0000110.md): Antenna · gouged · Feb 15, 2008 · N411MM · Israel ASTRASPX · VHF Communications System
  > FOLLOWING 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 APP
- [SDR 2007FA0000976](https://openairdocs.org/sdr/2007FA0000976.md): Rotor · separated · Oct 29, 2007 · N400CP · Israel ASTRASPX · Turbine Section
  > IAW SERVICE BULLETIN TFE731-72-5175. BLADE SEPARATION ON ONE LPT3 BLADE AS LISTED IN TABLE 1 OF S/B 72-5175.
- [SDR 2007FA0000468](https://openairdocs.org/sdr/2007FA0000468.md): Windshield · cracked · May 1, 2007 · N411MM · Israel ASTRASPX · Flight Compartment Windows
  > THE 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 2007FA0000062](https://openairdocs.org/sdr/2007FA0000062.md): Retainer · separated · Oct 4, 2006 · N1125S · Israel ASTRASPX · Turbine Section
  > ON 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 FINDINGS
- [SDR YNTA200687701](https://openairdocs.org/sdr/YNTA200687701.md): Skin · delaminated · Aug 31, 2006 · N877D · Israel ASTRASPX · Ailerons
  > RIGHT 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 2006FA0000125](https://openairdocs.org/sdr/2006FA0000125.md): Aileron · delaminated · Jan 11, 2006 · N918MJ · Israel ASTRASPX · Ailerons
  > RT AILERON UPPER SKIN FOUND DELAMINATED FROM HONEYCOMB CORE. DELAMINATION COVERS MORE THAN 50 PERCENT OF UPPER SURFACE. AILERON REPLACED WITH SERVICEABLE UNIT. (K)
- [SDR CA050929002](https://openairdocs.org/sdr/CA050929002.md): Cap · loose · Sep 23, 2005 · Israel ASTRASPX · Turbine Engine Oil System
  > (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 A
- [SDR 2005FA0001266](https://openairdocs.org/sdr/2005FA0001266.md): Seat · broken · Aug 25, 2005 · N882GA · Israel ASTRASPX · Flight Compartment Equipment
  > DURING REUPHOLSTERY OF PILOT SEAT, FOUND BACKREST FRAME BROKEN. CONTACTED MFG AND WAS GIVEN REPAIR TO ADD WELDED DOUBLERS. (CE09200505050) (K)
- [SDR AJC2005F00011](https://openairdocs.org/sdr/AJC2005F00011.md): Bearing · failed · Jul 22, 2005 · N387PA · Israel ASTRASPX · Fuel Control/Turbine Engines
  > CREW 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 2005FA0001203](https://openairdocs.org/sdr/2005FA0001203.md): Attach Bracket · leaking · Jul 5, 2005 · N610SM · Israel ASTRASPX · Fuel Storage
  > FUEL 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 COV
- [SDR AJC2005F00007](https://openairdocs.org/sdr/AJC2005F00007.md): Pump · failed · Jun 30, 2005 · N387PA · Israel ASTRASPX · Fuel Boost Pump
  > THE 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 SER
- [SDR 2005FA0000806](https://openairdocs.org/sdr/2005FA0000806.md): Control Unit · out of tolerance · May 3, 2005 · Israel ASTRASPX · Leading Edge Slat Control System
  > THE 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 38
- [SDR 2005FA0000805](https://openairdocs.org/sdr/2005FA0000805.md): Control Unit · out of tolerance · May 3, 2005 · Israel ASTRASPX · Leading Edge Slat Control System
  > THE 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 38
- [SDR 2005FA0000726](https://openairdocs.org/sdr/2005FA0000726.md): Fcu · out of tolerance · May 3, 2005 · Israel ASTRASPX · Leading Edge Slat Control System
  > THE 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 VO
- [SDR 2005FA0000624](https://openairdocs.org/sdr/2005FA0000624.md): Fcu · out of tolerance · May 3, 2005 · Israel ASTRASPX · Leading Edge Slat Control System
  > THE 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 VOLT
- [SDR AJC2005F00002](https://openairdocs.org/sdr/AJC2005F00002.md): Ahrs · intermittent · Mar 27, 2005 · N387PA · Israel ASTRASPX · Integrated Flight System
  > ON 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 LANDE
- [SDR CA050321007](https://openairdocs.org/sdr/CA050321007.md): Engine · making metal · Mar 14, 2005 · Israel ASTRASPX · Engine (Turbine/Turboprop)
  > (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 FI
- [SDR AJC2005F00001](https://openairdocs.org/sdr/AJC2005F00001.md): Engine · vibration · Mar 7, 2005 · N387PA · Israel ASTRASPX · Engine (Turbine/Turboprop)
  > AC 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 PER
- [SDR LEGR200500001](https://openairdocs.org/sdr/LEGR200500001.md): Door · cracked · Feb 18, 2005 · N108C · Israel ASTRASPX · Landing Gear Doors
  > DURING 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 AJC2005F00000](https://openairdocs.org/sdr/AJC2005F00000.md): Uplock Switch · out of adjust · Dec 29, 2004 · N387PA · Israel ASTRASPX · Landing Gear Position and Warning
  > AC 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 WITH
- [SDR CA040430002](https://openairdocs.org/sdr/CA040430002.md): Pump · failed · Apr 25, 2004 · Israel ASTRASPX · Engine Fuel Pump
  > (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 F
- [SDR CA040402003](https://openairdocs.org/sdr/CA040402003.md): Door · misrigged · Mar 25, 2004 · Israel ASTRASPX · Landing Gear Doors
  > (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.

Next page: https://openairdocs.org/model/gulfstream-aerospace-astra-spx/reports.md?page=2

## 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 = 'ASTRASPX'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/gulfstream-aerospace-astra-spx/reports

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