- Registered owner
- Grady Excavating Inc
- Location
- Mukilteo, WA
- Owner type
- Corporation
- Serial number
- LW-305
- Year built
- 1978
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- October 23, 1978
- Certificate issued
- September 10, 2018
- Expires
- September 30, 2028
- Mode S code
- A03196
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
No NTSB investigations matched to N111TCMatched 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 E-90 aircraft
FAA incident reports
No FAA accident or incident reports matched to N111TCMatched 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 E-90 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 CUX2002F00002Stiffener · crackedRIGHT WING UPPER FORWARD STIFFENER (PN 50-120068-7) WAS DISCOVERED CRACKED DURING A ROUTINE PHASE 1 INSPECTION. THE CRACK BEGAN AT THE INBOARD EDGE, EMANATING OUTWARD THROUGH THE FIRST 2 RIVET HOLES FOR A TOTAL LENGTH OF 1.55 INCHES. THE DAMAGED PART WAS REMSDR CUX2002F00001Skin · crackedRIGHT ELEVATOR TRIM TAB OUTER SKIN WAS DISCOVERED CRACKED AT THE UPPER INBOARD AFT CORNER DURING A ROUTINE PHASE 1 INSPECTION. THE CRACK BEGAN AT A SKIN ATTACH COUNTER SUNK RIVET AND EXTENDED FORWARD AND FAT APPROXIMATELY .350 INCH IN EACH DIRECTION. THE TABSDR CUX2002F00000Fitting · scratchedLEFT WING LOWER FORWARD INBOARD WING BOLT ATTACH FITTING (PN 50-120073-7) WAS DISCOVERED TO HAVE 3 SMALL SCRATCHES DURING A REPETITIVE INSPECTION OF AD. THE SCRATCHES WERE LOCATED ON THE ATTACH BOLT WASHER SEARING FACE RADIUS IN AN AXIAL DIRECTION AND WERE AP
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.
Earlier aircraft with this N-number · 2
These aircraft carried N111TC before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.