- Registered owner
- Uas Transervices Inc
- Location
- Boca Raton, FL
- Owner type
- Corporation
- Serial number
- AT-602
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Certificate issued
- April 12, 2007
- Expires
- January 31, 2030
- Mode S code
- A23052
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 51
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 | 2 |
| 1992 | 3 |
| 1993 | 4 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 8 |
| 1997 | 5 |
| 1998 | 3 |
| 1999 | 1 |
| 2000 | 5 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 1 |
| 2005 | 3 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2014 | 3 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 2 |
Airframe · Fairchild SA227-AT
AD 2017-07-01Propellers/PropulsorsAD 2016-25-12Horizontal Stabilizer StructureAD 2016-15-02Flight ControlsInformation bulletins that may apply · 14
Advisory, not mandatory.
Airframe · Fairchild SA227-AT
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
No NTSB investigations matched to N240DHMatched 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 Fairchild SA227-AT aircraft
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 19911113056819IFinal Approach-IFR · Syracuse, NYUnsafe landing gear indication on approach. Landed safely. Cleaned landing gear safety switch.Incident 19900103002819INormal Cruise · Cedar Rapids, IARight engine oil pressure warning. Secured and landed. Found cracked fitting on governor reset line.
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JIKA20200227501Wire · damagedDURING TAKEOFF ROLL FROM DFW PITCH TRIM WAS ADJUSTED UP FOR CLIMB. THE TRIM CONTROLS STOPPED WORKING WHILE THE WHEELS LIFTING OFF FROM THE RUNWAY. IT WAS DIFFICULT TO MAINTAIN ALTITUDE ASSIGNED SINCE THE AIRCRAFT KEPT CLIMBING. THE PILOT HAD IMMEDIATELY ADVISESDR JIKA20200129301Mixing Valve · defectiveDURING INITIAL CLIMB FROM DFW, AFTER TURNING ON BLEED AIR VALVES, THE COCKPIT BECAME VERY HOT, EVEN THOUGH THE SYSTEM WAS SET AT THE LOWEST SETTING. TEMP SELECTOR SWITCH WAS RECYCLED THROUGH ALL POSITIONS AND CONTROL KNOB WAS KEPT AT LOWEST SETTING, BUT COCKPSDR JIKA2015010801Hydraulic Line · leakingDURING DECENT, BOTH HYD PRESS WARNING ANNUNCIATORS ILLUMINATED & THE NLG UNSAFE LIGHT ILLUMINATED FOLLOWED BY A DOWN & LOCKED INDICATION. PERFORMED AN EMER EXTENSION OF THE LG & RECEIVED THREE GREEN DOWN & LOCKED INDICATOR LIGHTS. LANDED WITHOUT INCIDENT. ISDR JIKA2013062701Actuator · brokenPILOT REPORTED THAT AFTER EXTENDING THE LANDING GEAR DURING APPROACH, A RT MLG UNSAFE INDICATION WAS OBSERVED. BROKE OFF APPROACH TO TROUBLESHOOT THE UNSAFE INDICATION. PERFORMED THE LANDING GEAR UNSAFE INDICATION CHECKLIST IAW THE QRH AND STILL HAD AN UNSA
STCs that may be installed · 108
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Fairchild SA227-AT
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