- Registered owner
- Uas Transervices Inc
- Location
- Boca Raton, FL
- Owner type
- Corporation
- Serial number
- AT-560
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Certificate issued
- May 1, 2007
- Expires
- September 30, 2027
- Mode S code
- A728BA
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 · Swearingen 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 · Swearingen 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 N560UPMatched 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 Swearingen SA227-AT aircraft
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20160113000469ITaxi · Burbank, CADuring taxi for takeoff, the main landing gear, shaft (pin) connecting the lower torque link to the right hand main landing gear strut, sheared and eventually came out of the torque link. This caused the wheel and tire assembly to swivel, forcing the aircraft…Incident 20140325004589ITaxi · Huntsville, ALWhile taxiing to 36L on taxi way w pilot was cleared for takeoff. Upon reaching taxi way W8 he attempted a turn towards 36L and the nose wheel stearing was unresponsive. While attempting to stop the aircraft by breaking the right break pedal master cyl rod…Incident 19880623046099IRoll-Out (Fixed Wing) · Sioux Falls, SDPIC lost directional control on rollout. Applied unequal pressure on brakes. Struck a runway light. Had crosswinds.
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JIKA2019020901Connector · contaminatedTHE PILOT REPORTED WHILE ON FINAL APPROACH INTO KSMX THAT THE AIRCRAFT MADE AN UNCOMMANDED NOSE PITCH DOWN ATTITUDE AT APPROXIMATELY 200’ AGL. THE PILOT DECLARED AN EMERGENCY THEN LANDED WITHOUT INCIDENT IN KSMX. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THSDR JIKA2017011602Line · leakingTHE PILOT WAS ENROUTE, WHEN BOTH LEFT AND RIGHT HYDRAULIC PRESSURE LOW ANNUNCIATORS ILLUMINATED. THE PILOT NOTED HYDRAULIC PRESSURE DROPPING BELOW NORMAL LIMITS. THE PILOT NOTIFIED COMPANY DISPATCH AND ARRANGED TO RETURN TO DEPARTURE. THE PILOT FOLLOWING EMERGSDR JIKA2015030101Indicator · faultyDURING APPROACH, THE PILOT SELECTED THE LG TO THE EXTEND POSITION, THE PILOT RECEIVED A THREE GREEN DOWN & LOCKED LG INDICATOR LIGHTS INITIALLY, SHORTLY AFTER THE RT LG LIGHT EXTINGUISHED. PERFORMED A PRECAUTIONARY MANUAL EXTENSION OF LG TO VERIFY LG WAS DOWNSDR JIKA2014032501Rod · brokenDURING PRE-TAKEOFF CHECKS OF ACFT SYS WHILE TAXIING, PILOT NOTICE THE NOSE WHEEL STEERING WAS SLOW TO RESPOND. ACFT WAS APPROACHING A TURN & PILOT ATTEMPTED TO APPLY BRAKES, RT BRAKE PEDAL BROKE & PILOT FOOT SLIPPED WHICH RESULTED IN PILOT VEERING OFF TAXIWAYSDR JIKA2013101201Power Supply · failedON INITIAL DESCENT, PILOT SMELLED SMOKE IN THE COCKPIT, CHECKED ANNUNCIATOR PANEL AND FOUND EVIDENCE OF SMOKE. PROCEEDED WITH QUICK REFERENCE HANDBOOK PROCEDURE AND DECLARED AN EMERGENCY. TURNED RADAR OFF, SMOKE APPEARED TO STOP. LANDED WITHOUT FURTHER INCISDR MEJA1201Uplock Bearing · failedMFE-SAT - FLT 1851 - AFTER TAKEOFF, THE RIGHT MAIN GEAR SHOWED INTRANSIT LIGHT REMAINED ON. FLIGHT CREW CYCLED GEAR WITH NO CHANGE IN INDICATION. AIRCRAFT RETURNED TO MFE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND UPLOCK ROLLER BEARING FROZEN. SDR MEJA9508002Limit Switch · failedMAF - LEFT MAIN GEAR WOULD NOT FULLY RETRACT ON TAKEOFF, ATTEMPTED 4 GEAR CYCLES WITH NO LUCK. A NORMAL LANDING WAS MADE AT THE DEPARTURE POINT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACED THE LEFT MAIN GEAR LANDING GEAR UP LIMIT SWITCH. INSTALLED SDR MEJA9501002Connector · wetON FLIGHT 1851 IN CRUISE THE RIGHT WING OVERHEAT LIGHT CAME ON. AIRCRAFT TURNED BACK AND RETURNED TO MFE WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND MOISTURE IN THE WING ROOT CONNECTOR FOR THE WING OVERHEAT LIGHT SYSTEM. CLEANED AND D
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 · Swearingen 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