- Registered owner
- Lje Air LLC
- Location
- Park Ridge, IL
- Owner type
- LLC
- Serial number
- TH-1480
- Year built
- 1985
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- June 5, 1985
- Certificate issued
- November 13, 2025
- Expires
- November 30, 2032
- Mode S code
- A7742A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 55
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1966 | 1 |
|---|---|
| 1972 | 2 |
| 1973 | 3 |
| 1974 | 3 |
| 1975 | 1 |
| 1976 | 1 |
| 1977 | 2 |
| 1978 | 1 |
| 1979 | 1 |
| 1984 | 1 |
| 1987 | 1 |
| 1988 | 2 |
| 1990 | 1 |
| 1991 | 2 |
| 1992 | 1 |
| 1993 | 2 |
| 1997 | 2 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 3 |
| 2001 | 5 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 1 |
| 2005 | 3 |
| 2007 | 2 |
| 2008 | 2 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2013 | 1 |
| 2022 | 1 |
| 2023 | 2 |
See all 55 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Beech 58
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-15-22Wing Leading Edge Hinge-Pin CorrosionSAIB CE-13-22Electrical Power System Circuit Breaker SwitchSAIB CE-12-36Flight Controls: AileronSAIB CE-11-28Airplane Fuel and Electrical Systems on Hawker Beechcraft Corporation Twin Engine Airplanes.SAIB CE-11-21Flight Controls: Trailing Edge Flaps; Flap Nose Rib CrackingSAIB CE-04-04SAIB CE-02-19NTSB investigations
No NTSB investigations matched to N58GEMatched 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 58 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR N58AN58GENOV2Counterweight · looseENGINE FAILED IN FLIGHT. IT IS SUSPECTED THAT ONE OF THE COUNTERWEIGHTS HAD COME LOOSE DURING OPERATION.SDR 2009F00105Counterweight · failedIN FLIGHT ENG SHUTDOWN, DUE TO SEPARATION OF CRANKSHAFT COUNTERWEIGHT. THIS CAUSED BOTH LWR ENGINE MOUNTS TO FAIL AS WELL AS SUBSTANTIAL DAMAGE TO CRANKSHAFT AS WELL AS CAMSHAFT, CYLINDERS, CASE, LIFTERS, RODS, ETC. THIS OCCURRED IN FLIGHT, PILOT EXPERIENCESDR 2009F00107Crankshaft · brokenLT ENG HAD UNCOMMANDED ENG SHUTDOWN IN CRUISE FLIGHT. ENG PROPELLER WAS THEN FEATHERED AND ENG SECURED IAW MANUAL. CHECKED ENG UPON REMOVAL AND FOUND CRANKSHAFT BUSTED, SPUN BEARINGS AT LEAST. CASE WAS UNABLE TO BE SPLIT DUE TO SOME CYL DAMAGE. LANDING WASSDR N582008F00000Cylinder · crackedCRACK FOUND BETWEEN FUEL INJECTION BOSS AND SPARK PLUG BOSS. (S)SDR 200805210001Cylinder · failedBURN THROUGH HOLE FOUND ON TOP OF NUMBER 4 CYLINDER BETWEEN SPARK PLUG HOLE AND EXHAUST VALVE.
STCs that may be installed · 349
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 58
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