- Registered owner
- Uas Transervices Inc
- Location
- Boca Raton, FL
- Owner type
- Corporation
- Serial number
- U-146
- Year built
- 1971
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- March 30, 1972
- Certificate issued
- April 30, 2007
- Expires
- January 31, 2030
- Mode S code
- A520A2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 43
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 | 3 |
| 1974 | 1 |
| 1975 | 1 |
| 1976 | 1 |
| 1977 | 1 |
| 1978 | 2 |
| 1979 | 1 |
| 1980 | 1 |
| 1982 | 3 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1990 | 2 |
| 1992 | 3 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 1 |
| 1998 | 1 |
| 2001 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 2 |
| 2021 | 1 |
| 2023 | 1 |
See all 45 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N4299AMatched 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 B-99 aircraft
FAA incident reports · 6
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20151123020809ICruise/Level Flight · Eugene, ORDuring an IFR flight (night, IMC conditions) the #1 inverter failed. The pilot switched to the #2 inverter, but it failed to power the aircraft systems. The result was loss of many of the engine instruments, some primary flight indicators and navigational…Incident 20030228003119IRoll-Out (Fixed Wing) · Oakland, CA(-23) Received notification of inbound BE-99 to oak with an unsafe NLG indication. Visual observation from another aircraft in flight was that the NLG was swinging backward and forward. I witnessed the aircraft execute a normal touchdown; the pilot holding…Incident 19940712033399IFcd/Prec Ldg From Cruise · Oakland, CAUnable gear up light,returned. Unable get down light on nose gear. Nose gear collapsed landing. Actuator lost fluid.Incident 19910109002679IFinal Approach-IFR · Bakersfield, CASmoke in cockpit on approach. Landed safely. Electrical short in circuit breaker backlight panel assembly.Incident 19850220009069ILevel Off Touchdown · Manassas, VAGear would not lock down and low hydraulic fluid light came on. Crack in left main gear actuator end cap.Incident 19800122016519INormal Cruise · New Orleans, LAFire detector test switch shorted out. Copilot pulled engine fire detector circuit breaker. Continued flight.
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JIKA2016033101O-Ring · leakingON TAXI OUT, THE PILOT REPORTED THAT THE RT BRAKE WAS INEFFECTIVE. THE PILOT USED DIFFERENTIAL ENG CONTROLS & TAXIED BACK TO THE LOADING RAMP WITHOUT INCIDENT. REPLACED THE O RING PACKING’S, PN MS28775-220, IN THE RT BRAKE ASSEMBLY, SERVICED & BLED THE BRAKESDR JIKA2015112301Inverter · faultyEN-ROUTE THE PILOT REPORTED A DUEL INVERTER FAILURE, DUE TO THE IFR WEATHER CONDITIONS. THE PILOT DECLARED AN EMER & DIVERTED WHERE THE WEATHER CONDITIONS WERE VFR. THE PILOT LANDED WITHOUT INCIDENT. TROUBLESHOOTING REVEALED A FAULTY NR 1 INVERTER. REPLACESDR JIKA2015021001Indicator · shortedIN CRUISE, VISUALLY OBSERVED A SMALL AMOUNT OF SMOKE IN THE COCKPIT & THEN THE LT OIL PRESS CB POPPED. AFTER THE CB POPPED THE SMOKE DISSIPATED. RETURNED & LANDED WITHOUT INCIDENT. TROUBLE SHOT THE LT OIL PRESS SYS & FOUND THE INDICATOR HAD SHORTED INTERNALSDR JIKA2014112001Connector · brokenDURING CRUISE ATTITUDE PILOT HEARD AN ELEC CLICK AT THE SAME TIME NOTICED AN OZONE & HOT ELECTRONICS SMELL. THE PILOT NOTICED THE RT OIL PRESS GAUGE CB & THE RT OIL PRESS WARNING CB HAD POPPED. RETURNED & LANDED WITHOUT FURTHER INCIDENT. TROUBLESHOOTING REV
STCs that may be installed · 140
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech B-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