- Location
- Hanscom Afb, MA
- Owner type
- Government
- Serial number
- 31
- Year built
- 1968
- Type
- Fixed wing multi engine
- Engine
- Turbo-jet
- Airworthiness
- Experimental, research and development, crew training
- Airworthiness date
- July 14, 2022
- Certificate issued
- May 10, 1993
- Expires
- June 30, 2027
- Mode S code
- A018F2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 48
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 1 |
|---|---|
| 1973 | 1 |
| 1974 | 4 |
| 1975 | 3 |
| 1976 | 2 |
| 1978 | 4 |
| 1979 | 1 |
| 1980 | 1 |
| 1981 | 2 |
| 1982 | 1 |
| 1987 | 1 |
| 1990 | 2 |
| 1991 | 1 |
| 1993 | 3 |
| 1994 | 4 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 3 |
| 2004 | 1 |
| 2006 | 1 |
| 2008 | 1 |
| 2012 | 1 |
| 2013 | 1 |
| 2016 | 2 |
| 2023 | 1 |
| 2026 | 1 |
See all 49 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N105TBMatched 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 Grumman G-1159 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QY5R201404090001Fuel Line · brokenWHILE ON GROUND WITH APU RUNNING, A MAJOR FUEL LEAK WAS SEEN COMING OUT THE REAR FUSELAGE. APU WAS SHUTDOWN AND AN INVESTIGATION REVEALED A BROKEN FUEL LINE AT ONE OF THE FUEL NOZZLES. THE FUEL WAS SPRAYING INSIDE THE APU ENCLOSURE AND LEAKING OUT FUSELAGE ACSDR 2010FA0000498Control Cable · wornDURING A PREFLIGHT INSPECTION WITH THE AILERON UP, EXCESSIVE WEAR OF THE FORWARD OUTBOARD AILERON CABLE WAS NOTED AT THE RBS 189 FAIRLEAD. THE PHENOLIC PROTECTOR WAS IN GOOD CONDITION EVEN THOUGH THE CABLE HAD BEEN RUBBING ON IT. MANY STRANDS WERE WORN THROUGHSDR QY52003F00000Starter Gen · failedNR 1 ENGINE FAILED TO START. ON INVESTIGATION OF PROBLEM, FOUND STARTER CENTRIFUGAL SWITCH HAD MALFUNCTIONED. ORDERED NEW STARTER. WHEN OLD STARTER WAS REMOVED, IT WAS DISCOVERED THAT THE STARTER SHAFT BEARINGS HAD FAILED, THIS IS MOST LIKELY WHAT TOOK OUT SDR 20010508CW007Bolt · brokenAN AFTER LANDING, POST FLIGHT INSPECTION, REVEALED 2 BROKEN WHEEL BOLTS ON RIGHT OUTBOARD WHEEL ASSEMBLY. WHEEL AND TIRE ASSEMBLY REMOVED AND ALL WHEEL BOLTS DISCARDED.
STCs that may be installed · 665
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Grumman G-1159
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)