- Registered owner
- Investment Opportunities Pursuit LLC
- Location
- Greenville, NC
- Owner type
- LLC
- Serial number
- LJ-1196
- Year built
- 1989
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- April 3, 1989
- Certificate issued
- November 13, 2017
- Expires
- November 30, 2027
- Mode S code
- A04F33
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 34
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1987 | 1 |
|---|---|
| 1989 | 2 |
| 1990 | 1 |
| 1992 | 2 |
| 1993 | 1 |
| 1994 | 1 |
| 1996 | 1 |
| 1997 | 3 |
| 1998 | 4 |
| 1999 | 4 |
| 2001 | 3 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2023 | 1 |
See all 38 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N119SAMatched 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 C90A aircraft
FAA incident reports
No FAA accident or incident reports matched to N119SAMatched 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 C90A aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DDNA2016041400180Bracket · crackedNOTICED CRACK IN RT ELEVATOR TRIM TAB NEAR ACTUATOR BRACKET. DISCONNECTED ACTUATOR FROM TRIM TAB AND FOUND EXCESSIVE MOVEMENT IN BRACKET. UPON FURTHER INSPECTION FOUND FORWARD TWO RIVETS THAT HOLD ACTUATOR ARM TO TRIM TAB HAD SHEARED IN HALF. AND FWD RADIUS OSDR DDNR20160414001Arm · crackedNOTICED CRACK IN RT ELEVATOR TRIM TAB NEAR ACTUATOR ARM. DISCONNECTED ACTUATOR AND FOUND EXCESSIVE PLAY IN TRIM TAB ACTUATOR ARM. UPON FURTHER INSPECTION AND DISASSEMBLY FOUND FWD 2 RIVETS THAT FASTEN ACTUATOR ARM TO RIB HORN HAD SHEARED. ALSO FOUND RIB HORSDR DDNR20151217001Rib · crackedLEFT OTBD FLAP NOSE RIBS CRACKED AT THE ACTUATOR ATTACH POINTS. FOUND UPON PHASE INSPECTION THROUGH INSPECTION HOLES. FLAP ALSO HAD CRACK MIDWAY IN THE SKIN OF THE L/E.
STCs that may be installed · 266
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech C90A
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.
Earlier aircraft with this N-number · 2
These aircraft carried N119SA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.