- Registered owner
- Uas Transervices Inc
- Location
- Boca Raton, FL
- Owner type
- Corporation
- Serial number
- U-210
- Year built
- 1983
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- September 22, 1983
- Certificate issued
- April 30, 2007
- Expires
- January 31, 2030
- Mode S code
- A6881A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 28
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1971 | 5 |
|---|---|
| 1972 | 2 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1989 | 1 |
| 1990 | 1 |
| 1992 | 3 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 1 |
| 2001 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 1 |
| 2021 | 1 |
| 2023 | 1 |
See all 30 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N52RPMatched 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 Beech C-99 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JIKA20191118301Wire · shortedTHE PILOT REPORTED THAT ON APPROACH INTO KABQ THE LANDING GEAR FAILED TO EXTEND, THE CONTROL CIRCUIT BREAKER POPPED IMMEDIATELY AFTER LOWERING HE LANDING GEAR SELECTOR HANDLE TO THE GEAR DOWN POSITION. THE PILOT PERFORMED A GO AROUND TO INVESTIGATE THE DISCRESDR JIKA2016102901Bearing · failedON THE ROLL-OUT AFTER AN UNEVENTFUL LANDING AT KMQY, THE PILOT REPORTED NO BRAKE AUTHORITY ON THE RT SIDE. DURING HIS POST FLT INSP IT WAS DISCOVERED THE NR 3 WHEEL TIRE ASSEMBLY WAS NOT PRESENT ON THE AC AND THE NR 3 BRAKE ASSEMBLY APPEARED TO BE LEAKING. MSDR JIKA2014060501Stud · strippedEN-ROUTE FROM KBUF TO KROC AT 7000’ MSL THE PILOT OBSERVED THE MASTER CAUTION LIGHT ILLUMINATE & THE RT ENG SUFFERED A COMPLETE LOSS OF POWER RESULTING IN THE AUTO FEATHER SYS ENGAGING. THE PILOT FOLLOWED THE ENG FAILURE CHECKLIST & SECURED THE RT ENG. THE P
STCs that may be installed · 139
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech C-99
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