- Registered owner
- Woltjer Richard J
- Location
- Pennock, MN
- Owner type
- Individual
- Serial number
- 30110
- Year built
- 1968
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- April 12, 1968
- Certificate issued
- July 23, 1999
- Expires
- October 31, 2027
- Mode S code
- A601FE
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental IO-520 model are included below.
On this page
Airworthiness directives that may apply · 54
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1971 | 2 |
| 1972 | 2 |
| 1974 | 1 |
| 1975 | 1 |
| 1976 | 1 |
| 1977 | 2 |
| 1979 | 1 |
| 1980 | 2 |
| 1981 | 2 |
| 1986 | 2 |
| 1987 | 3 |
| 1988 | 3 |
| 1990 | 1 |
| 1991 | 1 |
| 1993 | 3 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 2 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 2 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 1 |
| 2012 | 1 |
| 2014 | 2 |
| 2016 | 1 |
| 2022 | 3 |
| 2023 | 5 |
See all 66 ADs
Information bulletins that may apply · 12
Advisory, not mandatory.
Airframe · Bellanca 17-30
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemEngine · Continental IO-520 series
SAIB NE-20-05POWERPLANT - Engine Camshaft Gear Tooth FractureSAIB NE-18-16POWERPLANT Alternator Drive CouplingSAIB NE-17-11POWERPLANT Engine damage as a result of kickbackSAIB 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-10-07Reciprocating Engine Cylinder: Identification Information for Superior Air Parts, PMA Cylinder Heads for Teledyne Continental Motors (TCM) IO-520, TSIO-520,and IO-550 Series Engines.SAIB NE-09-08Reciprocating Engine Cylinder SectionSAIB NE-07-09R1Periodic Inspections of ECi Cylinder Assemblies for Cracks in the Aluminum HeadSAIB NE-02-41NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 19951221044379IFinal Approach-IFR · Rock Springs, WYNarrative: robert s. spalding was pilot-in-command of Bellanca viking N4865V on an IFR flight from mohall, north dakota to Rock Springs, Wyoming. Mr. Spalding reported engine trouble approaching Rock Springs. He switched to all four tanks with the engine…Incident 19880702045069IRoll-Out (Fixed Wing) · Rolla, NDRight main gear collapsed on landing rollout. Found extension spring assy had failed. Did not lock gear down.Accident 19860727035159ARoll-Out (Fixed Wing) · Winneconne, WIThe pilot landed dragging the tailskid and the aircraft veered off the side of the runway where the gear collapsed.
Service difficulty reports
No reports matched to N4865VGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Bellanca 17-30 aircraft
STCs that may be installed · 228
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Bellanca 17-30
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