- Registered owner
- Tld LLC
- Location
- Pasco, WA
- Owner type
- LLC
- Serial number
- LW-20
- Year built
- 1972
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- September 6, 1972
- Certificate issued
- April 17, 2019
- Expires
- April 30, 2029
- Mode S code
- ABF437
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.
| 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 | 2 |
| 1998 | 4 |
| 1999 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2021 | 1 |
| 2023 | 1 |
See all 48 ADs
Information bulletins that may apply · 3
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 · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 19930729034639IRoll-Out (Fixed Wing) · Gillette, WYRight main landing gear wheel bearing failed on rollout. Damaged wheel assembly and right propeller blades.Incident 19881025064779IRoll-Out (Fixed Wing) · Sterling, CONose gear collapsed on rollout. Found no mechanical failure. Pilot stated he had 3 green lights in retract cycle.
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 0016Torque Link · crackedDURING INSPECTION OF UPPER TORQUE KNEE PER THE REQUIREMENTS OF RAYTHEON REOCCURRING SERVICE BULLETIN 32-3134, THE LEFT UPPER TORQUE KNEE ON ONE OF THE MAIN GEARS WAS NOTED TO BE CRACKED IN THE RADIUS OF THE SINGLE LUG. THIS CRACK WAS IN LOCATION NOTED TO BE RSDR CIEA0002Dipstick · looseAPPROXIMATELY 15 MINUTES AFTER TAKEOFF THE PILOT NOTICED A RIGHT ENGINE TORQUE INDICATION FLUCTUATION, FOLLOWED BY A DROPPING OIL PRESSURE INDICATION. THE PILOT REDUCED THE POWER ON THE ENGINE. THE PILOT RETURNED TO THE AIRPORT AND LANDED WITHOUT INCIDENT, WSDR 97ZZZX4479Aileron · crackedWHEN REBONDING STATIC WICKS TO AILERON, MECHANIC NOTICED CRACKS BENEATH BOTH INBOARD AND OUTBOARD STATIC WICK BASES.SDR 96ZZZX5816Torque Knee · crackedAFTER AN INCIDENT CAUSED BY AN UPPER TORQUE KNEE FAILURE, OTHER AIRCRAFT IN THE FLEET ARE BEING INSPECTED. DURING THIS INSPECTION THE UPPER TORQUE KNEE ON THE RIGHT GEAR WAS VISUALLY FOUND TO BE CRACKED. A NEW UNIT WAS INSTALLED. BOTH THE NEW UNIT AND THE O
STCs that may be installed · 299
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.