- Registered owner
- Jvs86 LLC
- Location
- Scottsdale, AZ
- Owner type
- LLC
- Serial number
- LJ-627
- Year built
- 1974
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- March 12, 1974
- Certificate issued
- July 8, 2022
- Expires
- July 31, 2029
- Mode S code
- A55CDB
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 45
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 2 |
|---|---|
| 1976 | 2 |
| 1977 | 4 |
| 1978 | 4 |
| 1979 | 1 |
| 1980 | 1 |
| 1981 | 1 |
| 1982 | 1 |
| 1985 | 2 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1990 | 2 |
| 1992 | 2 |
| 1993 | 1 |
| 1997 | 2 |
| 1998 | 4 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 1 |
| 2008 | 1 |
| 2021 | 1 |
| 2023 | 1 |
See all 48 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N4447WMatched 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 C90 aircraft
FAA incident reports
No FAA accident or incident reports matched to N4447WMatched 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 Beech C90 aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EBTR20170523015Engine · shutdownON DESCENT FROM UGN TO ARB HEARD POP, AIRCRAFT YAWED, NOTICED RIGHT ENGINE FUEL FLOW AND ITT DIMINISHING TO 0. VISUAL OF ENGINE COWL NO DEFECTS NOTED. FOLLOWED FLIGHT MANUAL PROCEDURES FOR ENGINE RESTART USING ISOLATION SWITCH NO FUEL FLOW OR ITT REGISTERED ANSDR EBTR201610150001Pump · inoperativeENROUTE FROM APN TO MKG, DURING CRUISE AT 8,000 FT APPROXIMATELY 20 MINUTES FROM MKG, FUEL SYSTEM AUTOMATICALLY SWITCHED TO CROSSFEED TO SUPPLY FUEL TO RT ENGINE, INDICATING THAT THE RT ENGINE HAD A FUEL PRESSURE DROP. THIS IS NORMAL SEQUENCE OF EVENTS FOR AI
STCs that may be installed · 347
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech C90
STC SA02054SEInstallation of winglets and related system changes.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.