# Service difficulty reports: Gulfstream Aerospace G-1159A

A list on [Gulfstream Aerospace G-1159A](https://openairdocs.org/model/gulfstream-aerospace-g-1159a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 145 reports

- [SDR ESPA2019F00224](https://openairdocs.org/sdr/ESPA2019F00224.md): Wing · corroded · May 17, 2019 · N163PA · Gulstm G1159A · Wing Spar
  > RIGHT WING HAS CORROSION ON AFT SPAR AT RBS343.
- [SDR ESPA2019F00223](https://openairdocs.org/sdr/ESPA2019F00223.md): Spar · corroded · May 17, 2019 · N163PA · Gulstm G1159A · Wing Spar
  > FOUND CORROSION ON WING AFT SPAR AT RBS 406.
- [SDR 2016F00212](https://openairdocs.org/sdr/2016F00212.md): Flap System · inoperative · Oct 17, 2016 · N50BH · Gulstm G1159A · Trailing Edge Flap Control System
  > FLAPS WOULD NOT EXTEND DURING DESCENT. DIVERTED AND DECLARED AND EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT.
- [SDR ESPA2016F00182](https://openairdocs.org/sdr/ESPA2016F00182.md): Unknown · malfunctioned · Sep 2, 2016 · N163PA · Gulstm G1159A · Cabin Pressure Control System
  > AFTER TAKEOFF, ENROUTE, AT ALTITUDE THE AIRCREW EXPERIENCED SOME TURBULENCE AND THE PIC REPORTED A SUDDEN LOSS OF PRESSURIZATION. THEY DECLARED AN EMERGENCY DESCENT TO THE NEAREST AIRFIELD. WE DISPATCHED A TECH TO TROUBLESHOOT THE PROBLEM. UPON TROUBLESHOOT
- [SDR VM0R2015FA0000158](https://openairdocs.org/sdr/VM0R2015FA0000158.md): Door · malfunctioned · Apr 8, 2015 · N360MB · Gulstm G1159A · Landing Gear Door Retract Section
  > ACFT HAD AN AFTER TAKEOFF NOSE GEAR DOOR CLOSING PROBLEM. THE CREW REPORTED A WIND NOISE AND VIBRATION ISSUE AND NOTED THE RED GEAR HANDLE LIGHT WAS ILLUMINATED INDICATING AN INCOMPLETE RETRACTION OF THE LANDING GEAR. THE GEAR WAS EXTENDED AND THE ACFT RETUR
- [SDR 2015FA0000018](https://openairdocs.org/sdr/2015FA0000018.md): Cable · out of adjust · Jan 20, 2015 · N992NA · Gulstm G1159A · Rudder Tab Control System
  > IMPROPER DEFLECTION OF RUDDER TRIM CABLE AT FS 163 CAUSING, SAWING, AT LIGHTNING PASSTHRU HOLE. THE MAINTENANCE AND PARTS MANUALS DO NOT SHOW THE BRACKET AND PULLEY ASSY IN THIS AREA. WHEN THE PULLEYS ARE REMOVED, THE CABLES REMAIN IN A POSITION FOR ADDITION
- [SDR BQVA20150109001](https://openairdocs.org/sdr/BQVA20150109001.md): Converter · faulty · Jan 9, 2015 · N58AJ · Gulstm G1159A · AC Generation System
  > LEFT AC & LEFT DC POWER FAIL INDICATORS ILLUMINATED.
- [SDR 2014FA0000466](https://openairdocs.org/sdr/2014FA0000466.md): Window · failed · Jul 10, 2014 · Gulstm G1159A · Passenger Compartment Windows
  > WHILE CLIMBING THROUGH 390 TO FL430 THE RT AFT-MOST PASSENGER WINDOW CRACKED AND BLEW OUT. THEN THE RT ENGINE FLAMED OUT. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO LAND. AIRPORT FIRE AND RESCUE DISPATCHED AND THE ACFT TAXIED TO THE RAMP WITHOUT FURTHER
- [SDR BQVA20140425001](https://openairdocs.org/sdr/BQVA20140425001.md): Spar Cap · corroded · Apr 21, 2014 · N58AJ · Gulstm G1159A · Wing Spar
  > DURING COMPLIANCE OF CMP CODE 279010 LT AILERON HINGE INSPECTION, A SMALL AREA OF CORROSION WAS FOUND ON THE WING AFT LOWER SPAR CAP JUST OTBD OF THE CTR AILERON HINGE.
- [SDR Y3PR201403270001](https://openairdocs.org/sdr/Y3PR201403270001.md): Attach Bolt · cracked · Mar 25, 2014 · N492A · Gulstm G1159A · Drag Control System
  > DURING LT FLIGHT SPOILER BELLCRANK INSPECTION, MAGNETIC PARTICLE INSPECTION INDICATED A POSSIBLE CRACK AROUND THE ENTIRE CIRCUMFERENCE OF THE PINS HEAD. REPLACED PIN WITH NEW PIN.
- [SDR BKEA2014012000040](https://openairdocs.org/sdr/BKEA2014012000040.md): Windscreen · failed · Jan 18, 2014 · N175BG · Gulstm G1159A · Flight Compartment Windows
  > LEFT WINDSCREEN FAILED,
- [SDR BKEA2014012000039](https://openairdocs.org/sdr/BKEA2014012000039.md): Windscreen · failed · Jan 18, 2014 · N175BG · Gulstm G1159A · Flight Compartment Windows
  > LEFT WINDSCREEN FAILED.
- [SDR AOYA20140104001](https://openairdocs.org/sdr/AOYA20140104001.md): Engine · power loss · Jan 4, 2014 · N55ME · Gulstm G1159A · Engine (Turbine/Turboprop)
  > ENGINE START & TAXI CHECKS WERE NORMAL. A ROLLING TAKEOFF WAS PERFORMED TO COMPUTED EPR'S. ALL ENG PARAMETERS WERE NORMAL DURING TAKEOFF ACCELERATION UNTIL A DROP IN THE LT ENG EPR TO APPROXIMATELY 1.9. THE LT ENG THRUST LEVER DID NOT RESPOND TO AN ATTEMPT T
- [SDR BQVA20131211001](https://openairdocs.org/sdr/BQVA20131211001.md): Skin · corroded · Dec 11, 2013 · N58AJ · Gulstm G1159A · Auxiliary Power Unit (APU) Doors
  > DURING COMPLIANCE OF FUSELAGE EXTERIOR INSPECTION, CMP CODE 531020, FOUND CORROSION AT APU EXHAUST OPENING. STANDARD REPAIR APU DOOR SKIN FS 617.562 CURRENTLY IN PROGRESS.
- [SDR A8OA2013050800005](https://openairdocs.org/sdr/A8OA2013050800005.md): Fuel Cell · leaking · May 8, 2013 · N50BH · Gulstm G1159A · Fuel Storage
  > DURING CLIMB NOTICED FUEL LEAKING FROM TOP OF LT WING. LEAK STOPPED AT 21,000 POUNDS INDICATED. AS A PRECAUTION THE CREW RETURNED TO DEPARTURE AND LANDED SAFELY. FOUND SCREWS LOOSE ON PANELS 21-FT UPR-25 AND 21-FT UPR-26 TIGHTENED SCREWS AND CHECKED FOR FUE
- [SDR 2013F00110](https://openairdocs.org/sdr/2013F00110.md): Cooling Turbine · failed · May 6, 2013 · N221WR · Gulstm G1159A · Cabin Cooling System
  > DURING CRUISE AT FL320, ACFT EXPERIENCE SMOKE IN THE CABIN. ACFT RETURNED TO DEPARTURE. INITIAL INVESTIGATION REVEALED TO A FAULTED COOLING TURBINE UNIT. FURTHER THE CONDENSER DRAIN LINE FROM THE TURBINE UNIT IS CRACKED FROM A PREVIOUS REPAIR MADE.
- [SDR A8OA201301300003](https://openairdocs.org/sdr/A8OA201301300003.md): Windshield · cracked · Jan 30, 2013 · N901EH · Gulstm G1159A · Flight Compartment Windows
  > AFTER CRUISING FOR APPROX 1.5 HOURS THE CREW WITNESSED A LOUD CRACKING NOISE AND NOTICED THE PILOT SIDE, LT WINDSHIELD HAD CRACKED. THE WINDOW WAS SPIDERED VEINED WITH CRACKS COVERING THE ENTIRE SURFACE. THE CREW DONNED OXYGEN MASKS TURNED ON SEAT BELT SIGN
- [SDR DVYA20120711001](https://openairdocs.org/sdr/DVYA20120711001.md): Turbine · damaged · Jul 8, 2012 · N221CM · Gulstm G1159A · Turbine Section
  > DURING APPROACH WHEN THROTTLES WERE RETARDED THE RIGHT ENGINE FLAMED OUT, ENGINE WAS SECURED AND UNEVENTFUL LANDING ACCOMPLISHED. UPON INVESTIGATION FOUND THE RIGHT ENGINE LOW PRESSURE COMPRESSOR/LOW PRESSURE TURBINE SECTION WOULD NOT ROTATE. HIGH PRESSURE C
- [SDR 2012F00114](https://openairdocs.org/sdr/2012F00114.md): Probe · grounded · Jun 11, 2012 · N62MW · Gulstm G1159A · Fuel System Wiring
  > DURING CLIMB OUT, 1/3 RT ROLL WAS REQUIRED TO MAINTAIN LEVEL FLIGHT. THE ACFT RETURNED TO DEPARTURE.
- [SDR GZXA20120417001](https://openairdocs.org/sdr/GZXA20120417001.md): Skin · damaged · Apr 17, 2012 · N477WG · Gulstm G1159A · Leading Edge Devices
  > DURING POST FLIGHT WALK AROUND OF AIRCRAFT FLIGHT CREW NOTICE A SMALL DENT IN LEFT OUTBOARD LEADING EDGE. APPARENTLY CAUSED BY A BIRD STRIKE DURING UNKNOWN PHASE OF FLIGHT INTO AIRPORT.
- [SDR 2012F00077](https://openairdocs.org/sdr/2012F00077.md): Skin · dented · Apr 17, 2012 · N477WG · Gulstm G1159A · Wing, Plate/Skin
  > DURING POST FLIGHT WALK-AROUND BY FLIGHT CREW NOTICED A POSSIBLE BIRD STRIKE AND DENT ON LT OTBD L/E.
- [SDR BQVR2011110700010](https://openairdocs.org/sdr/BQVR2011110700010.md): Attach Fitting · corroded · Nov 7, 2011 · N109DD · Gulstm G1159A · Wing, Attach Fittings
  > DURING COMPLIANCE OF CMP CODES 576511 & 576516, WINGLET ATTACH HARDWARE INSPECTION (LT & RT), CORROSION FOUND IN THE WINGLET ATTACH BORES ONCE THE BUSHINGS WERE REMOVED.
- [SDR BQVA2011041900009](https://openairdocs.org/sdr/BQVA2011041900009.md): Winglet · corroded · Apr 15, 2011 · N58AJ · Gulstm G1159A · Wing, Plate/Skin
  > DURING COMPLIANCE OF CMP CODES 576511 & 576516 WINGLET ATTACH HARDWARE (LEFT & RIGHT) - INSPECTION (144 MONTH), SOME CORROSION WAS FOUND IN THE WINGLET ATTACH BORES ONCE THE BUSHINGS WERE REMOVED.
- [SDR 2011F00019](https://openairdocs.org/sdr/2011F00019.md): Engine · flamed out · Jan 16, 2011 · N918BG · Gulstm G1159A · Engine (Turbine/Turboprop)
  > AT FL 430, ENCOUNTERED MODERATED MOUNTAIN WAVE WITH AIRSPEED FLUXUATION OF MACH.80 TO.72. AT THIS TIME WE HAD THE NR 2 ENGINE FLAMEOUT. PERFORMED NORMAL DESCENT TO AIRSTART ENVELOPE, COMPLIED WITH AIRSTART CHECKLIST, NO DEFECTS NOTED, CONTINUED TO DESTINA
- [SDR 2010FA0001095](https://openairdocs.org/sdr/2010FA0001095.md): Attach Bracket · cracked · Sep 27, 2010 · N855SA · Gulstm G1159A · Passenger/Crew Doors
  > (S6NR) FLIGHT CREW REPORTED MAIN ENTRY DOOR WOULD HANG AT CLOSURE, INVESTIGATED ANOMALY AND DISCOVERED UPPER MAIN ENTRY DOOR ATTACH FITTING CRACKED. CONTACTED MFG STRUCTURAL DEPT AND DIVULGED FINDINGS. AFTER CONVERSATION WITH TECH SUPPORT, WAS INFORMED OF A
- [SDR BQVA2010082300007](https://openairdocs.org/sdr/BQVA2010082300007.md): Bulkhead · corroded · Aug 18, 2010 · N50BH · Gulstm G1159A · Fuselage Main, Bulkhead
  > SUSPECTED CORROSION FOUND DURING INSPECTION OF THE FS 580 BULKHEAD SKIN SPLICE, AREA LONGERONS AND STRINGERS 24 L/R IN ACCORDANCE WITH CMP 539540. AFTER FURTHER NDT THE AREA WAS FOUND TO HAVE MINOR SURFACE CORROSION WHICH WAS REMOVED AND TREATED. FINDINGS W
- [SDR 2010FA0000834](https://openairdocs.org/sdr/2010FA0000834.md): Duct · damaged · Aug 9, 2010 · N456AL · Gulstm G1159A · APU Bleed Air System
  > DURING POST FLIGHT INSP WITH THE APU RUNNING AND BLEED AIR SELECTED ON, IT WAS NOTED THAT THERE WAS A HOLE IN THE INSULATION OF THE APU AND GROUND START DUCT, AND BLEED AIR FELT TO BE ESCAPING. FURTHER INVESTIGATION FOUND THAT A TWO (2) INCH CRACK HAD DEVELOP
- [SDR BQVA2010041200006](https://openairdocs.org/sdr/BQVA2010041200006.md): Skin · corroded · Apr 7, 2010 · N58AJ · Gulstm G1159A · Wing, Plate/Skin
  > DURING A WING NDT INSPECTION OF THE LT WING PLANK AT FS 452 BL 33, CORROSION WAS FOUND. ENGINEERING HAS DETERMINED THIS CORROSION IS EXCESSIVE ENOUGH TO REQUIRE ACCOMPLISHMENT OF ASC 229, WHICH WILL REMOVE THE CORROSION ON THE PLANK AND INSTALL A THREE PIECE
- [SDR BQVA2010040900005](https://openairdocs.org/sdr/BQVA2010040900005.md): Attach Fitting · cracked · Apr 7, 2010 · N58AJ · Gulstm G1159A · Fuselage Main, Attach Fittings
  > DURING THE REQUIRED EDDY CURRENT INSPECTION OF THE FS 793 BULKHEAD CAP ANGLE, CRACKS WERE FOUND AROUND LEFT AND RIGHT BOLT HOLES IN THE CAP ANGLE FOR THE VERTICAL FIN ATTACHMENT.
- [SDR BQVA2010030100005](https://openairdocs.org/sdr/BQVA2010030100005.md): Downlock Switch · defective · Feb 23, 2010 · N58AJ · Gulstm G1159A · Landing Gear Position and Warning
  > AIRCRAFT DEPARTED FROM KHPN EN ROUTE TO KFPR. CREW SELECTED GEAR HANDLE DOWN AND RECEIVED A RED HANDLE WARNING INDICATION. AIRCRAFT FLEW PAST CONTROL TOWER TO VERIFY THE LANDING GEAR WAS DOWN. RETRACTED LANDING GEAR AND DIVERTED TO KPBI AND LANDED WITH OUT
- [SDR BQVA2010010400004](https://openairdocs.org/sdr/BQVA2010010400004.md): Windshield · cracked · Jan 2, 2010 · N50BH · Gulstm G1159A · Flight Compartment Windows
  > RIGHT SIDE WINDSHIELD OUTER PANE FAILURE DURING FLIGHT. REMOVED AND REPLACED WINDSHIELD.
- [SDR WWQ2009F00002](https://openairdocs.org/sdr/WWQ2009F00002.md): Valve · leaking · Sep 23, 2009 · N366JA · Gulstm G1159A · Drag Control Actuator
  > AFTER TAKEOFF, WHEN THE CREW SELECTED GEAR UP THEY NOTICE UNUSUAL SOUNDS. ALL INDICATIONS SEEMED TO BE NORMAL AND FLAPS WERE SELECTED UP. THE COMBINE HYDRAULIC SYS BEGAN TO FALL. THE CREW GOT INDICATIONS THAT THE PRESSURE WAS LOW, THEN OK, THEN LOW AGAIN.
- [SDR AI5R2009RS002](https://openairdocs.org/sdr/AI5R2009RS002.md): Bottle · empty · Aug 31, 2009 · N62MW · Gulstm G1159A · Life Raft
  > THE LIFE RAFT ARRIVED AT OUR FACILITY FOR ANNUAL INSPECTION. UPON INSPECTING AND WEIGHING THE CO2 CYLINDER, IT WAS DISCOVERED THAT THE CYLINDER WAS EMPTY.
- [SDR AI5R2009RS001](https://openairdocs.org/sdr/AI5R2009RS001.md): Cylinder · empty · Aug 31, 2009 · N62MW · Gulstm G1159A · Life Raft
  > UPON INSPECTING THE HYDROSTATIC TEST DATE ON THE CO2 CYLINDER, IT WAS DETERMINED THAT THE CYLINDER WAS DUE FOR HYDROSTATIC TESTING, AND WE THEN PULLED THE CYLINDER CABLE TO RELEASE THE CO2 FROM INSIDE THE CYLINDER. UPON DOING THIS, WE DISCOVERED THAT IT THE C
- [SDR 2009FA0000760](https://openairdocs.org/sdr/2009FA0000760.md): Tire · failed · Jul 18, 2009 · N399AP · Gulstm G1159A · Tire
  > ON TAKEOFF AT 1622Z, ACFT BLEW NR 4 RT OTBD TIRE. UPON RETURN LANDING BACK AT DEPATURE, THE FOLLOWING DAMAGE WAS FOUND: RT INBD FLAP, RT LWR COWL, RT ENG T/R, AND RT GEAR DOOR OTBD. THIS TIRE SN FALLS WITHIN GY SB 2008-32-001. (K)
- [SDR WWQ2009F00000](https://openairdocs.org/sdr/WWQ2009F00000.md): Engine · failed · Apr 19, 2009 · N366JA · Gulstm G1159A · Engine (Turbine/Turboprop)
  > DURING CLIMB OUT, AFTER TAKEOFF, APPROXIMATELY 5K FEET THE CREW HEARD A LOUD BANG FROM THE LT ENGINE. THE CREW CHECKED THE ENGINE PARAMETERS AND FOUND 0 EPR AND NOTICED THAT THE POWER LEVER WAS UNRESPONSIVE ON THE LT ENGINE. LP HP WAS APPROXIMATELY 30 PERCEN
- [SDR 2010F00114](https://openairdocs.org/sdr/2010F00114.md): Windshield · cracked · Jan 3, 2009 · N213BA · Gulstm G1159A · Flight Compartment Windows
  > LEFT WINDSHIELD OUTER PANE CRACKED AT FL410, DESCENT TO 10,000 FT AND RETURNED TO AIRPORT. NO LOSS OF PRESSURIZATION
- [SDR YJU2008F00000](https://openairdocs.org/sdr/YJU2008F00000.md): Tire · unserviceable · Jul 7, 2008 · N797BD · Gulstm G1159A · Tire
  > PILOTS REPORTED THAT ON TAKEOFF, THEY FELT A BUMP FOLLOWING THE VR CALLOUT. AFTER LANDING, IT WAS DISCOVERED THAT THE NR 3 MAIN TIRE TREAD HAD COMPLETELY SEPARATED FROM THE TIRE DOWN TO THE CORD AREA. THE TREAD COMING OFF DAMAGED THE FLAP TORQUE TUBE, SEVERE
- [SDR O2G2008F00000](https://openairdocs.org/sdr/O2G2008F00000.md): Blade · failed · Mar 29, 2008 · N800TD · Gulstm G1159A · Turbine Engine Combustion Section
  > HIGH T,V,I INDICATION AFTER TAKEOFF ON LT ENGINE. AC LANDED, FOUND 2.5 OF 1ST STAGE BLADE MISSING AND DAMAGE TO OTHER BLADES. (K)
- [SDR 2007FA0000958](https://openairdocs.org/sdr/2007FA0000958.md): Regulator · failed · Sep 13, 2007 · N776MA · Gulstm G1159A · Engine Fuel Distribution
  > PILOTS REPORT FELT HEAVY VIBRATION FOR 3 TO 4 SECONDS, THEN HEARD A LOUD BANG FOLLOWED BY LT ENGINE SPOOLING DOWN. AIRCRAFT SAFELY LANDED AT AIRPORT. CONTACTED MFG, WHO DISPATCHED A RESPONSE CREW TO AIRPORT. FOUND THAT THE FUEL FLOW REGULATOR HAD FAILED IN
- [SDR Y9PAN818S83107](https://openairdocs.org/sdr/Y9PAN818S83107.md): Smoke Detector · malfunctioned · Aug 31, 2007 · N818S · Gulstm G1159A · Smoke Detection
  > AFTER TAKEOFF, LAV SMOKE ALARM ANNUNCATOR ILLUMINATED, CREW REPORTED THAT THEY INSPECTED THE LAV AREA FOR SIGNS OF SMOKE AND FIRE, NONE OBSERVED. THE ANNUNCATOR WENT OUT AND THEN CAME BACK ON. THE CREW THEN ELECTED TO DIVERT. UPON LANDING, THE APU WOULD NOT ST
- [SDR S8A2007F00000](https://openairdocs.org/sdr/S8A2007F00000.md): Window · cracked · Jul 26, 2007 · N457JC · Gulstm G1159A · Flight Compartment Windows
  > AC DEPARTED AT APPROX 1930 ON 7/26/2007 AT APPROX 150 MILES OUT AND FL 350 A LOUD POP WAS HEARD IN THE CABIN. FLIGHT CREW INVESTIGATED AND NOTED THE NR 3 RT CABIN WINDOW OUTER PANE CRACKED. AT THAT TIME FLIGHT CREW DECLARED AN EMERGENCY, RETURNED AND MADE AN
- [SDR 2007FA0000540](https://openairdocs.org/sdr/2007FA0000540.md): Ring · missing · Jun 25, 2007 · N2NA · Gulstm G1159A · Engine Bleed Air System
  > THE COMPONENT OEM (REPORT 4-193), THE MM (CHAPTER 36-02-00), IPC (CHAPTER 36-10-00) AND THE CMP WORK CARDS (364040, 364045) ARE MISSING THE REQUIREMENT TO INSPECT AND INSTALL GAMMA RING (PN) M1213-400 DURING THE INSTALLATION OF THE PNEUMATIC SYSTEM PRECOOLER.
- [SDR UG8A2007PA03S](https://openairdocs.org/sdr/UG8A2007PA03S.md): Attach Fitting · corroded · Jun 13, 2007 · N473KT · Gulstm G1159A · Wing, Attach Fittings
  > LT AFT IB WING ATTACH FITTING HAS CORROSION AT OB EDGE AT FS 452, BL 33.COMPLIED WITH AIRCRAFT SERVICE CHANGE 229, WING TO FUSELAGE IB ATTACH CONNECTION FUSELAGE STATION 452 LT SIDE, REPLACEMENT/MODIFICATION. GENERATED FAA FORM 337. AIRCRAFT RETURNED TO SERVI
- [SDR BQVA200752271](https://openairdocs.org/sdr/BQVA200752271.md): Attach Fitting · corroded · May 18, 2007 · N50BH · Gulstm G1159A · Wing, Attach Fittings
  > WING TO FUSELAGE ATTACH FITTING AT FS 452 BL 33 (LEFT SIDE), CORROSION DETECTED DURING THE SCHEDULED ULTRASONIC INSPECTION. THE CORROSION ON THE OUTBOARD SURFACE IS.158 INCH IN DEPTH,.125 INCH IN LENGTH; AND.125 INCH IN DIAMETER. [07-03-07] ENGINEERING
- [SDR BQVA200751871](https://openairdocs.org/sdr/BQVA200751871.md): Attach Fitting · cracked · May 16, 2007 · N50BH · Gulstm G1159A · Fuselage Main, Attach Fittings
  > DURING THE REQUIRED EDDY CURRENT INSPECTION OF THE FS 793 BULKHEAD CAP ANGLE, CRACK INDICATIONS WERE NOTED ON BOTH SIDES. THE CRACKS ARE ABOVE THE.5 INCH BOLT HOLES IN THE CAP ANGLE FOR VERTICAL FIN ATTACHMENT.
- [SDR 2007FA0000322](https://openairdocs.org/sdr/2007FA0000322.md): Skin · corroded · Mar 30, 2007 · N300WY · Gulstm G1159A · Wing, Plate/Skin
  > DURING A WING NDT INSPECTION OF THE UPPER RT WING PLANK AT FS 452 AND BL 33, CORROSION WAS NOTED IN THIS AREA. ENGINEERING HAS DETERMINED THIS CORROSION IS EXCESSIVE ENOUGH TO REQUIRE ACCOMPLISHMENT OF ASC 229, WHICH REMOVES THE CORROSION ON THE PLANK AND INS
- [SDR C4S2007F00000](https://openairdocs.org/sdr/C4S2007F00000.md): Skin · corroded · Feb 12, 2007 · N400WY · Gulstm G1159A · Wing, Plate/Skin
  > DURING A WING INSPECTION ACCOMPLISHED APRIL 9, 2006, CORROSION WAS NOTED IN THE UPPER RT WING PLANK AT FS 452 AND BL33. THE CORROSION DID NOT REQUIRE REPLACEMENT OF THE PART AND DID NOT REQUIRE BLENDING THAT EXCEEDED THE MFG ALLOWANCES. MFG ENGINEERING ALLOW
- [SDR BUE2007F00002](https://openairdocs.org/sdr/BUE2007F00002.md): Bolt · sheared · Feb 8, 2007 · N416WM · Gulstm G1159A · Engine Exhaust System
  > ( REF NR: 287N416WM) DURING INSPECTION FOUND THE RT EJECTOR OB BEARING FITTING UPPER BOLT SHEARED, LOWER BOLT BENT/BEGINNING TO SHEAR, IB BEARING FITTING UPPER AND LOWER BOLTS BENT/BEGINNING TO SHEAR, AND THE IB AND OB TRANSLATOR LINKS BENT. REPLACED BOTH TRA
- [SDR BQVA200721071](https://openairdocs.org/sdr/BQVA200721071.md): Wedge · damaged · Feb 1, 2007 · N982RK · Gulstm G1159A · Wing, Plate/Skin
  > DURING THE SCHEDULED 72 MONTH LT WING WEDGE INSPECTION CMP 575030, ONE WING WEDGE HOLD DOWN RIVNUT WAS FOUND TO BE IN AN OVERSIZED HOLE.

Next page: https://openairdocs.org/model/gulfstream-aerospace-g-1159a/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 = 'G1159A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/gulfstream-aerospace-g-1159a/reports

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