- Registered owner
- Uas Transervices Inc
- Location
- Boca Raton, FL
- Owner type
- Corporation
- Serial number
- AT-607B
- Year built
- 1985
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- April 16, 1985
- Certificate issued
- April 12, 2007
- Expires
- January 31, 2030
- Mode S code
- A23409
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every AiResearch TPE331 model are included below.
On this page
Airworthiness directives that may apply · 92
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 1 |
|---|---|
| 1974 | 2 |
| 1975 | 2 |
| 1976 | 1 |
| 1979 | 2 |
| 1980 | 2 |
| 1982 | 1 |
| 1983 | 1 |
| 1984 | 3 |
| 1986 | 2 |
| 1987 | 2 |
| 1988 | 1 |
| 1989 | 1 |
| 1990 | 3 |
| 1991 | 2 |
| 1992 | 3 |
| 1993 | 8 |
| 1994 | 2 |
| 1995 | 3 |
| 1996 | 8 |
| 1997 | 6 |
| 1998 | 5 |
| 1999 | 1 |
| 2000 | 5 |
| 2001 | 2 |
| 2002 | 5 |
| 2003 | 2 |
| 2004 | 1 |
| 2005 | 3 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2011 | 2 |
| 2012 | 2 |
| 2014 | 3 |
| 2015 | 3 |
| 2016 | 4 |
| 2017 | 2 |
| 2018 | 4 |
Airframe · Fairchild SA227-AT
AD 2017-07-01Propellers/PropulsorsAD 2016-25-12Horizontal Stabilizer StructureAD 2016-15-02Flight ControlsInformation bulletins that may apply · 18
Advisory, not mandatory.
See all 19 bulletins
NTSB investigations
No NTSB investigations matched to N241DHMatched 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 N241DHMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JIKA2026012601Hydraulic Line · damagedWHILE PREPARING TO EXTEND THE LANDING GEAR, THE FLIGHT CREW NOTED THAT BOTH HYDRAULIC LOW-PRESSURE LIGHTS WERE ILLUMINATED. QRH PROCEDURES WERE FOLLOWED AND THE LANDING GEAR WAS MANUALLY ACTUATED TO THE DOWN AND LOCKED POSITION. THE LANDING WAS UNEVENTFUL AND SDR JIKA2023040601Unknown · unknownAFTER TAKEOFF FROM KDFW, A VERY STRONG ELECTRICAL BURNING SMELL WAS REPORTED BY THE FLIGHT CREW. PILOTS SWITCHED OFF BLEEDS, HEATING AND COOLING AND SMELL REMAINED. SMELL CAUSED NAUSEA AND HEADACHES FOR BOTH AIRCREW. THE AIRCRAFT RETURNED TO KDFW AND LANDED SDR JIKA202006231601Case · leakingON CLIMB OUT, RIGHT ENGINE OIL TEMP GAUGE WENT TO THE RED LINE AND HELD. AFTER A FEW MINUTES THE OIL TEMPERATURE WENT PAST THE RED LINE AND PRESSURE BEGAN TO DROP. PILOT SHUT DOWN THE ENGINE PER AMF PROCEDURES AND INFORMED CANCUN APPROACH, RIGHT ENGINE WAS SHSDR JIKA2019120200501Overheat Sensor · defectiveSHORTLY AFTER TAKEOFF FROM DFW, RIGHT ENGINE OIL TEMP EXCEEDED TOLERANCES OVER HIGH RED LINE. PILOT PERFORMED PRECAUTIONARY ENGINE SHUT DOWN, ATC DECLARED AN EMERGENCY. AIRCRAFT LANDED BACK AT DFW WITH NO INCIDENT. MAINTENANCE REMOVED AND REPLACED OIL TEMPERASDR JIKA2019062501Hydraulic Line · crackedMAINTENANCE DISCREPANCY: THE PILOT REPORTED DURING CLIMB OUT FROM KCVG THAT BOTH LEFT AND RIGHT HYDRAULIC LOW PRESSURE ANNUNCIATORS ILLUMINATED. THE PILOT INFORMED ATC AND FOLLOWED PROCEDURE AND THEN CONTINUED TO KSUS. THEN PERFORMED A MANUAL LANDING GEAR EXTESDR JIKA20190628301Line · chafedMECHANICAL DISCREPANCY: THE PILOT REPORTED WHILE ON DESCENT INTO KCVG THAT BOTH LEFT AND RIGHT “HYDRAULIC PRESSURE” WARNING LIGHT ANNUNCIATORS ILLUMINATED. THE PILOT FOLLOWING PROCEDURES IN THE QRH PERFORMED MANUAL LANDING GEAR EXTENSION UNTIL A “THREE GREEN” SDR JIKA2016112001Pump · intermittentTHE PILOT WAS EN-ROUTE WHEN THE RT FUEL TRANSFER LIGHT ILLUM. FOLLOWED THE QRH AND SWITCHED TO THE RT AUX FUEL BOOST PUMP FROM THE MAIN AND THE LIGHT EXTINGUISHED. MINUTES LATER THE LT FUEL TRANSFER LIGHT ILLUM AND FOLLOWING THE SAME PROCEDURES AND SWITCHED BOSDR JIKA2015033101Hydraulic Line · leakingDURING CRUISE FLIGHT, AT 21,000’ THE PILOT NOTICED THE RED LT & RT HYD PRESS WARNING LIGHTS ILLUMINATED. THE PILOT CHECKED HIS HYD PRESS GAUGE & IT WAS FLUCTUATING BETWEEN 500 & 1500 PSI FOR 5 SECONDS & THEN WENT TO 0. THE PILOT NOTIFIED THE TOWER OF THE SITSDR JIKA2013012301Actuator · weakAFTER TAKEOFF, PILOT REPORTS THAT THE ELEVATOR TRIM FAILED IN THE PILOT, CO-PILOT AND AUX MODES. REDUCED POWER TO INCREASE CONTROLLABILITY OF THE AIRCRAFT AND RETURNED TO OPF. AFTER LANDING, THE TRIM BEGAN TO WORK AGAIN. MAINTENANCE FOUND THAT THE PITCH TRI
STCs that may be installed · 128
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