- Registered owner
- Tgf Aviation LLC
- Location
- Lafayette, LA
- Owner type
- LLC
- Serial number
- TT450
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Certificate issued
- March 28, 2023
- Expires
- March 31, 2030
- Mode S code
- ADD127
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 44
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1982 | 1 |
|---|---|
| 1983 | 1 |
| 1984 | 1 |
| 1986 | 2 |
| 1987 | 1 |
| 1990 | 3 |
| 1991 | 1 |
| 1992 | 3 |
| 1993 | 3 |
| 1994 | 1 |
| 1996 | 8 |
| 1997 | 5 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 5 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 1 |
| 2005 | 3 |
| 2007 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 2 |
Airframe · Swearingen SA227-TT
AD 2017-07-01Propellers/PropulsorsAD 2016-25-12Horizontal Stabilizer StructureAD 2016-15-02Flight ControlsInformation bulletins that may apply · 14
Advisory, not mandatory.
Airframe · Swearingen SA227-TT
SAIB 2026-15Forward Pressure BulkheadSAIB 2026-14Rudder Control System, BrakeSAIB CE-20-09Nacelle/Pylon, Frame/Spar/RibSAIB CE-18-11Flight Controls, Elevator Control SystemSAIB CE-17-04Landing Gear, Main Landing GearSAIB CE-16-06Flight Controls, Rudder Control SystemSAIB CE-16-04Engine Controls, Power LeverSAIB CE-15-09Windows; Flight Compartment WindowsSAIB CE-15-05R1Flight Controls, Aileron Control SystemSAIB CE-13-42Wings, AileronsSAIB CE-13-41Landing Gear, Landing Gear ActuatorSAIB CE-13-10Windshield/Door Rain/Ice RemovalSAIB CE-12-08Flight Controls, Elevator Control SystemSAIB CE-11-26Wings: Wing SkinHistorical bulletins · 1
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 97ZZZX2372Master Cylinder · leakingDURING A ROUTINE AND B LETTER CHECK, FOUND BOTH PILOTS' LEFT AND RIGHT MASTER CYLINDERS LEAKING. BOTH CYLINDERS WERE REPLACED.SDR 97ZZZX2371Fairing · chafedBOTH LEFT AND RIGHT ENGINE EXHAUST PIPE FAIRINGS WERE FOUND CHAFED COMPLETELY THROUGH THE LOWER PORTION OF THE SEAL AND INNER FLANGE OF THE FAIRINGS. THIS WAS DISCOVERED DURING THE NORMAL A AND B LETTER CHECK INSPECTION.SDR 97ZZZX2370Fairing · chafedBOTH LEFT AND RIGHT ENGINE EXHAUST PIPE FAIRINGS WERE FOUND CHAFED COMPLETELY THROUGH THE LOWER PORTION OF THE SEAL AND INNER FLANGE OF THE FAIRINGS. THIS WAS DISCOVERED DURING THE NORMAL A AND B LETTER CHECK INSPECTION.SDR 97ZZZX2369Switch · miswiredDURING THE PROCESS OF TROUBLESHOOTING A YAW DAMPENER PROBLEM, DISCOVERED THE POSITION OF THE SWITCH (RIGHT OR LEFT),INDICATING FROM WHICH BUS IT RECEIVED POWER, WAS REVERSED. CORRECTED THIS CONDITION AND ASSUMED THE AIRCAFT HAS BEEN WIRED THIS WAY SINCE IT WASDR 97ZZZX2364Skin · chafedDURING AN ENGINE EXHAUST PIPE FAIRING CHANGE, DISCOVERED A STEEL BRAIDED FUEL VENT LINE HAD CHAFED INTO THE TOP SKIN OF THE LEFT WING NEAR THE EXHAUST PIPE. THE CHAFED AREA WAS 1.25 INCHES LONG, .4375 INCH WIDE BY .017 INCH DEEP. FAIRCHILD ENGINEERING DETERMSDR 97ZZZX533Battery · leakingDURING AN INSPECTION, THE ELT BATTERY WAS DUE FOR REPLACEMENT. FOUND BATTERY LEAKING WHEN REMOVED. NO DAMAGE WAS FOUND TO ELT UNIT. OPS CHECKS SATISFACTORY WITH NEW BATTERY INSTALLED. APPEARED TO LEAK AROUND CORNER OF CASE THAT WAS SEALED AT MANUFACTURER.
STCs that may be installed · 94
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Swearingen SA227-TT
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller