- Registered owner
- Uas Transervices Inc
- Location
- Boca Raton, FL
- Owner type
- Corporation
- Serial number
- AT-625B
- Year built
- 1985
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- October 9, 1985
- Certificate issued
- April 12, 2007
- Expires
- January 31, 2030
- Mode S code
- A2469C
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 N246DHMatched 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
No FAA accident or incident reports matched to N246DHMatched 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 Fairchild SA227-AT aircraft
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JIKA2025061201Bellcrank · brokenTHE FLIGHT CREW SELECTED THE LANDING GEAR TO THE DOWN AND LOCKED POSITION; THE RH MAIN LANDING GEAR DID NOT INDICATE THAT IT WAS SAFELY DOWN AND LOCKED ONCE IN POSITION. THE CAPTAIN PERFORMED AN EMERGENCY LANDING GEAR MANUAL EXTENSION TO ENSURE THAT THE POSITISDR JIKA2016072601Actuator · bindingON APPROACH, LANDING GEAR WAS SELECTED TO THE DOWN POSITION, THE NOSE LANDING GEAR DID NOT EXTEND. THE PILOT PERFORMED A FLY BY OF THE CONTROL TOWER TO CONFIRM THE INDICATION. THE PILOT MANUALLY EXTENDED THE LANDING GEAR USING THE EMERGENCY PROCEDURES, THE NSDR JIKA2016071901Electrical Sys · power lossENROUTE, THE PILOT REPORTED A LIGHTNING STRIKE AND LOSS OF ELECTRICAL POWER. THE PILOT CONTACTED ATC, DECLARED AN EMERGENCY AND LANDED AT THE NEAREST AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT, ENGINES AND PROPELLERS NO EVIDENCE OF LIGHTNING STSDR JIKA2015021801Bulb · faultyDURING CRUISE FLIGHT, THE PILOT NOTICED THE LT ENG OIL TEMP INDICATED ABOVE REDLINE, APPROX 110 DEGREES. THE PILOT ELECTED TO DIVERT BACK, DURING DESCENT THE OIL PRESS INDICATED IN THE YELLOW ARC, APPROX 65 PSI, AT THAT POINT PILOT DECIDED TO PERFORM A PRECAUSDR JIKA2014093002Wire · brokenEN ROUTE PILOT NOTICED THE RT OVERHEAT CB POPPED & WOULD NOT RESET. PILOT PERFORMED PRECAUTIONARY PROCEDURES & PERFORM IN FLIGHT SHUTDOWN OF RT ENG & ENG SECURING CHECKLIST ITEMS. PILOT DECLARED AN EMER & LANDED AT WITHOUT FURTHER INCIDENT. TROUBLESHOOTING SDR JIKA2013073001Switch · lack of lubeRIGHT LANDING GEAR DID NOT EXTEND ON APPROACH. EMERGENCY GEAR EXTENSION PERFORMED, THREE GREEN INDICATIONS. LANDED WITHOUT FURTHER INCIDENT. ACFT WAS FERRY FLOWN BACK, INSPECTED GEAR, NO DISCREPANCIES NOTED. CLEANED AND LUBRICATED GEAR AND SWITCHES. PERFORMESDR JIKA2013042901Bulb · faultyPILOT REPORTED THAT ON CLIMB-OUT THROUGH 6000 FT, THE LEFT ENGINE OIL TEMP ROSE INTO THE CAUTION RANGE. IT RETURNED TO NORMAL AFTER REDUCING POWER, BUT RETURNED TO THE CAUTION RANGE WHEN THE POWER WAS INCREASED TO CLIMB POWER SETTINGS AGAIN. THE PILOT DECLARSDR JIKA200400001Packing · cutAFTER TAKE-OFF AT APPROXIMATELY 6000 FT AGL, PILOT NOTED LT ENGINE R.P.M. DROPPED FROM 100 PERCENT TO 97 PERCENT WITH SPEED LEVER FULL FORWARD. SHORTLY AFTER, COCKPIT FILLED UP WITH BLUE SMOKE AND LT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. PILOT SHUT
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