- Registered owner
- Jansen Vic C
- Location
- Moses Lake, WA
- Owner type
- Individual
- Serial number
- TG-49
- Year built
- 1967
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- December 19, 1967
- Certificate issued
- August 19, 1989
- Expires
- March 31, 2028
- Mode S code
- A82B82
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming TI0-541 model are included below.
On this page
Airworthiness directives that may apply · 41
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 |
|---|---|
| 1968 | 1 |
| 1969 | 1 |
| 1971 | 1 |
| 1972 | 1 |
| 1973 | 1 |
| 1975 | 1 |
| 1977 | 1 |
| 1978 | 2 |
| 1979 | 2 |
| 1983 | 1 |
| 1984 | 1 |
| 1989 | 1 |
| 1990 | 1 |
| 1991 | 2 |
| 1992 | 1 |
| 1995 | 1 |
| 1997 | 2 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 3 |
| 2001 | 1 |
| 2002 | 1 |
| 2005 | 2 |
| 2007 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2013 | 1 |
| 2022 | 2 |
| 2023 | 2 |
| 2024 | 1 |
| 2026 | 1 |
See all 45 ADs
Information bulletins that may apply · 7
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N6252VMatched 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 56TC aircraft
FAA incident reports
No FAA accident or incident reports matched to N6252VMatched 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 56TC aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 20000714SH012Adapter · brokenPILOT MADE AN ABRUPT CONTROL MOVEMENT AND THE ADAPTER ASSY BROKE AT THE WELD. THE CONTROL YOKE CAME OFF, PILOT LANDED THE AIRCRAFT WITHOUT INCIDENT. AD 71-24-10 RELATES TO THIS SPECIFIC PART. SUBMITTER RECOMMENDED ALL ADAPTERS BE REPLACED WITH P/N 96-524029SDR 99ZZZX3275Column · brokenAIRCRAFT ENCOUNTERED TURBULENCE IN-FLIGHT, CONTROL BROKE, PILOT CONTROLLED AIRCRAFT IN ROLL AXIS WITH AUTOPILOT TO SAFE LANDING. WELD BROKE WHERE SHAFT WELDED TO FLANGE OF CONTROL WHEEL ADAPTER ASSEMBLY. AD 71-24-10 WAS C/W 2-17-72. SUBMITTER RECOMMENDED AD
STCs that may be installed · 256
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 56TC
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