- Registered owner
- Veldhuizen Stuart L
- Location
- Dublin, TX
- Owner type
- Individual
- Serial number
- CD-1089
- Year built
- 1967
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- April 6, 1967
- Certificate issued
- July 23, 2019
- Expires
- July 31, 2029
- Mode S code
- AD0C70
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental I0-470 model are included below.
On this page
Airworthiness directives that may apply · 59
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1963 | 1 |
|---|---|
| 1967 | 1 |
| 1972 | 3 |
| 1973 | 1 |
| 1974 | 2 |
| 1975 | 2 |
| 1976 | 1 |
| 1977 | 1 |
| 1978 | 1 |
| 1979 | 2 |
| 1980 | 1 |
| 1981 | 3 |
| 1985 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1991 | 2 |
| 1993 | 2 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 2 |
| 2001 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 2 |
| 2009 | 1 |
| 2010 | 2 |
| 2012 | 1 |
| 2019 | 2 |
| 2022 | 3 |
| 2023 | 6 |
| 2024 | 1 |
See all 69 ADs
Information bulletins that may apply · 11
Advisory, not mandatory.
Airframe · Beech 35-C33
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-15-22Wing Leading Edge Hinge-Pin CorrosionSAIB CE-12-36Flight Controls: AileronSAIB CE-12-18Flight Controls: Elevator Control Cable ConditionSAIB CE-11-21Flight Controls: Trailing Edge Flaps; Flap Nose Rib CrackingEngine · Continental I0-470 series
SAIB NE-20-05POWERPLANT - Engine Camshaft Gear Tooth FractureSAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-15Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control LeversSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-09-08Reciprocating Engine Cylinder SectionNTSB investigations
No NTSB investigations matched to N94SSMatched 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 35-C33 aircraft
FAA incident reports
No FAA accident or incident reports matched to N94SSMatched 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 35-C33 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 SW15200110535Bushing · improper partTHE INCORRECT BUSHING WAS IDENTIFIED DURING DEMINSIONAL INSPECTION OF THE COUNTER- WEIGHT PRIOR TO INSTALLATION.SDR SW15200110531Doubler · crackedDURING 100 HOUR INSPECTION FOUND CRACKS IN THE DOUBLER TALL PN 002440000143. THE DOUBLER IS CRACKED JUST FORWARD OF THE AFT BULKHEAD APPROX 1 INCH JUST BEFORE THE RADIUSED AREA EXTENDING OUTBOARD .2500.
STCs that may be installed · 534
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 35-C33
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