- Registered owner
- Travel Link LLC
- Location
- Vienna, VA
- Owner type
- LLC
- Serial number
- 359
- Year built
- 1982
- Type
- Fixed wing multi engine
- Engine
- Turbo-jet
- Airworthiness
- Standard, transport
- Airworthiness date
- July 23, 1982
- Certificate issued
- March 1, 2018
- Expires
- March 31, 2028
- Mode S code
- A637B8
Gulfstream American G-1159ATCDS A12EAAirframe · Gulfstream American G-1159AEngine modelRolls-Royce SPEY MK 511SR
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 31
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 1 |
|---|---|
| 1980 | 1 |
| 1981 | 1 |
| 1990 | 1 |
| 1991 | 2 |
| 1993 | 3 |
| 1994 | 3 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 4 |
| 2004 | 1 |
| 2006 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2012 | 1 |
| 2016 | 2 |
| 2018 | 1 |
| 2023 | 2 |
| 2026 | 1 |
Airframe · Gulfstream American G-1159A
AD 2026-13-02NavigationAD 2023-08-03Flight ControlsAD 2023-10-02Indicating/Recording System, NavigationInformation bulletins that may apply · 3
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N50BHMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Gulfstream American G-1159A aircraft
FAA incident reports
No FAA accident or incident reports matched to N50BHMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Gulfstream American G-1159A aircraft
Reports on N50BH not matched to an aircraft · 1
They name N50BH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2016F00212Flap System · inoperativeFLAPS WOULD NOT EXTEND DURING DESCENT. DIVERTED AND DECLARED AND EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT.SDR A8OA2013050800005Fuel Cell · leakingDURING 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 FUESDR BQVA2010082300007Bulkhead · corrodedSUSPECTED 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 WSDR BQVA2010010400004Windshield · crackedRIGHT SIDE WINDSHIELD OUTER PANE FAILURE DURING FLIGHT. REMOVED AND REPLACED WINDSHIELD.SDR BQVA200752271Attach Fitting · corrodedWING 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 BQVA200751871Attach Fitting · crackedDURING 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 BQVA200677061Smoke · detectedON APPROACH THE FLIGHT CREW NOTICED AN ACRID SMELL, THE AIRCRAFT LANDED AND EXITED THE RUNWAY WITHOUT INCIDENT AT WHICH TIME SMOKE WAS SEEN IN THE AFT GALLEY AND THE OVER COUNTER LIGHT LENS HAD OBSERVABLE FLAMES. THE PILOT REMOVED ELECTRICAL POWER FROM THE GASDR 7706Light · malfunctionedON APPROACH FLIGHT CREW NOTICED AN ACRID SMELL, THE AIRCRAFT LANDED AND EXITED THE RUNWAY WITHOUT INCIDENT AT WHICH TIME SMOKE WAS SEEN IN THE AFT GALLEY AND THE OVER COUNTER LIGHT LENS HAD OBSERVABLE FLAMES. THE PILOT REMOVED ELECTRICAL POWER FROM THE GALLEYSDR 23JAN2006Spar · corrodedDURING MAINTENANCE, WHILE ACCOMPLISHING A SCHEDULED 72 MONTH INSPECTION, 5 PATCHES OF CORROSION WERE FOUND ON THE ON THE AFT SIDE OF THE RT WING REAR SPAR (BEAM WEB) BEHIND THE RAIN CURTAINS AT FASTENER LOCATIONS EXTENDING FROM RBS 359 TO 422. THE MEASURED COSDR EA01BQVA0106ASpar · corrodedDURING MAINTENANCE WHILE ACCOMPLISHING A SCHEDULED 72 MONTH INSPECTION, 8 PATCHES OF CORROSION WERE FOUND ON THE ON THE AFT SIDE OF THE LT WING REAR SPAR (BEAM WEB) BEHIND THE RAIN CURTAINS AT FASTENER LOCATIONS EXTENDING FROM RBS 340 TO 406. THE LARGEST PATCSDR EA0123JAN2006Spar · corrodedDURING MAINTENANCE WHILE ACCOMPLISHING A SCHEDULED 72 MONTH INSPECTION, 8 PATCHES OF CORROSION WERE FOUND ON THE ON THE AFT SIDE OF THE LT WING REAR SPAR (BEAM WEB) BEHIND THE RAIN CURTAINS AT FASTENER LOCATIONS EXTENDING FROM RBS 340 TO 406. THE LARGEST PATC
STCs that may be installed · 678
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Gulfstream American G-1159A
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST00197IBInstallation of the Universal Quick Access Recorder (uQAR)
Earlier aircraft with this N-number · 1
This aircraft carried N50BH before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.