- Registered owner
- Uas Transervices Inc
- Location
- Boca Raton, FL
- Owner type
- Corporation
- Serial number
- AT-624B
- Year built
- 1985
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- October 8, 1985
- Certificate issued
- April 12, 2007
- Expires
- January 31, 2030
- Mode S code
- A242E5
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 · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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.
Accident 20000128017959ADescent · Fayetteville, AR(.4)On departure for the night air taxi cargo flight, the flight crew experienced a problem with the crew intercom system. The crew initiated their descent at a 'later than normal distance' from the airport, and as a result, a power reduction below 25 percent…Incident 19910803035949IFcd/Prec Ldg From Cruise · Des Moines, IARear cargo door unsafe light came on en route. Landed safely. Unable to duplicate problem.
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JIKA20180905101Wire Harness · defectiveTHE PILOT REPORTED WHILE PERFORMING AN OPERATIONAL CHECK FLIGHT FOR THE CORRECTIVE ACTION OF THE LEFT ENGINE FUEL BYPASS AND TORQUE DROP DISCREPANCY. AFTER TAKE-OFF FROM KCVG, THE CREW EXPERIENCED A HARD LEFT ENGINE BYPASS ISSUE AND ERRATIC EXHAUST GAS TEMPERASDR JIKA2016042101Striker · missingON FINAL APPROACH, WHEN THE PILOT SELECTED THE LG TO THE DOWN POSITION, THE LT MLG DOWN & LOCKED INDICATION DID NOT ILLUMINATE. THE PILOT FOLLOWED THE EMER PROCEDURES TO MANUALLY EXTEND THE LG & THE LT MLG DOWN & LOCKED LIGHT ILLUMINATED & THE PILOT LANDED WISDR JIKA2015031001Wire · faultyDURING CRUISE FLIGHT, THE PILOT NOTICED THAT THE RT ENG OIL TEMP GAUGE WAS FLUCTUATING & READING ABOVE THE RED LINE. THE PILOT FOLLOWED THE PROCEDURES IN THE QRH & REDUCED POWER, OIL TEMP REMAINED ABOVE THE RED LINE. THE PILOT PERFORMED AN INFLIGHT SHUTDOWN SDR JIKA2013101800001Line · leakingON REACHING CRUISE ALTITUDE OF 21,000 FT, WITHIN FIVE MINUTES, RIGHT HYDRAULIC FAIL ANNUNCIATOR ILLUMINATED. OPENED QUICK REF HANDBOOK TO FIND APPLICABLE ITEMS THAT MIGHT HELP ISOLATE AND DETERMINE PROBLEM. DIVERTED. IN 2 MINUTES, HYD PRESSURE WENT TO ZERSDR JIKA2013071100001Hydraulic Line · leakingAFTER DEPARTURE, AND CLIMBING THROUGH 12,000, HYD PRESSURE DROPPED TO ZERO, AND BOTH HYD PRESSURE ANNUNCIATORS ILLUMINATED. AN EMERGENCY DECLARED, AND EXTENDED GEAR MANUALLY AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX DISCOVERED THAT THE FLARE ON SDR JIKA2013050801Hydraulic Line · crackedTHE PILOT REPORTED THAT ON CLIMBOUT FROM KMIA BOTH HYDRAULIC FAIL ANNUNCIATOR’S ILLUMINATED. THE PILOT IMMEDIATELY TRIED TO LOWER THE LANDING GEAR WITHOUT SUCCESS. THE PILOT DIVERTED BACK TO KMIA, DECLARED AN EMERGENCY, PUMPED THE LANDING GEAR DOWN AND LAND
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