- Registered owner
- Sierra American Corporation
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- LW-76
- Year built
- 1974
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- April 11, 1997
- Certificate issued
- February 12, 1997
- Expires
- July 31, 2029
- Mode S code
- A13135
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 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1990 | 2 |
| 1992 | 2 |
| 1997 | 3 |
| 1998 | 4 |
| 1999 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2021 | 1 |
| 2023 | 1 |
See all 50 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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 2025F00171Oil System · low pressureDEPARTED GYH-ADS, AT FL180 PILOT NOTED SPARKS BY THE RT ENGINE AND THEN THE OIL PRESSURE WARNING LIGHT ACTIVATED AND PRESSURE GAUGE SHOWED 0. ENGINE WAS SHUTDOWN, ATC CONTACTED AND PERFORMED AN UNSCHEDULED LANDING AT THE NEAREST AIRPORT.SDR HAEA20190614001Axle · missingON DEPARTURE FROM KGVT THE CREW HEARD A NOISE FROM THE RH WING AREA, NOT SURE WHAT IT WAS THEY LEFT THE GEAR DOWN AND LOCKED AND PERFORMED A FLY BY THE TOWER AND DETERMINUED THE RH M/L/G PISTON/AXLE ASSEMBLY WAS MISSING. THE AIRCRAFT WAS FLOWN TO KAFW WHERE THSDR HAEA2015040500231Rudder Mast · damagedDURING PHASE 1 ACFT INSPECTION, DISCOVERED THE RUDDER TO BELL CRANK RT ATTACH BOLT MISSING. FURTHER INVESTIGATION REVEALED THE BOLT HAD FAILED. AN INSPECTION OF THE RUDDER TORQUE TUBE WAS CONDUCT & IT WAS NOTED THAT THE ATTACH HOLES OF THE BELL CRANK & RUDDE
STCs that may be installed · 305
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech E-90
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.