- Registered owner
- Tkn Holdings LLC
- Location
- Pima, AZ
- Owner type
- LLC
- Serial number
- 340A0368
- Year built
- 1977
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- June 11, 1996
- Certificate issued
- August 11, 2022
- Expires
- August 31, 2029
- Mode S code
- A218B2
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental TSIO-520 model are included below.
On this page
Airworthiness directives that may apply · 89
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1969 | 1 |
|---|---|
| 1970 | 1 |
| 1971 | 1 |
| 1972 | 2 |
| 1975 | 1 |
| 1976 | 1 |
| 1977 | 2 |
| 1978 | 3 |
| 1979 | 2 |
| 1980 | 6 |
| 1981 | 3 |
| 1982 | 2 |
| 1985 | 1 |
| 1987 | 2 |
| 1988 | 5 |
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 1 |
| 1993 | 4 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 2 |
| 1997 | 1 |
| 1998 | 5 |
| 1999 | 1 |
| 2000 | 2 |
| 2001 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2007 | 2 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 2 |
| 2014 | 2 |
| 2016 | 3 |
| 2020 | 1 |
| 2022 | 3 |
| 2023 | 6 |
| 2026 | 1 |
See all 100 ADs
Information bulletins that may apply · 19
Advisory, not mandatory.
See all 20 bulletins
NTSB investigations
No NTSB investigations matched to N234PSMatched 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 Cessna 340A 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 · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2005FA0000642Pan · crackedDURING ANNUAL INSPECTION, TECH WAS INSPECTING TAIL SECTION. PAN IS ATTACHED TO A BULKHEAD WHICH ARE THE PRIMARY STRUCTURE (AFT) FOR THE HORIZONTAL AND VERTICAL STABILIZERS. TAIL FLEX IS TRANSFERRING TO THIS ASSY AND IS CAUSING CRACKS ON THE RADIUS. (K)SDR FJC4285Bolt · bentDURING INSPECTION OF THE ELEVATOR SYSTEM THE TECHNICIAN DISCOVERED THE ELEVATOR BELLCRANK BOLT BENT. WE HAVE FOUND SEVERAL BENT IN OUR FLEET, AND WOULD SUGGEST THAT ALL OPERATORS HAVE THE BOLT AND BEARING INSPECTED AS SOON AS POSSIBLE.SDR 2002FA0000452Cylinder · failedIN FLIGHT, PILOT NOTICED REDUCTION IN MANIFOLD PRESSURE. PILOT DESCENDED WHEN COMPLETE FAILURE AND SEPARATION OF THE NR 4 CYLINDER ON THE LEFT ENGINE OCCURRED. CYLINDER HEAD SEPARATED FROM BARREL. ENGINE WAS SECURED AND SHUT DOWN. PROP WAS FEATHERED. THE
STCs that may be installed · 357
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 340A
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