- Registered owner
- Brown Christopher C
- Location
- Sheridan, WY
- Owner type
- Individual
- Serial number
- 30309
- Year built
- 1970
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- September 26, 1970
- Certificate issued
- January 8, 2015
- Expires
- January 31, 2028
- Mode S code
- A8C630
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 · 52
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 2 |
|---|---|
| 1973 | 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 |
Airframe · Bellanca 17-30A
AD 2022-03-15Fuel Quantity IndicatorAD 2014-20-12FuselageAD 2008-05-11Muffler and tailpipe assembliesInformation bulletins that may apply · 13
Advisory, not mandatory.
Airframe · Bellanca 17-30A
SAIB 2025-07Reciprocating Engine SuperchargerSAIB 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 · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 19980501014959AFcd/Prec Ldg From Cruise · Brewton, ALLost power unable prop speed control. Hit fence landing. Left wing sheared. Crankshaft broke. Improper toh torque. (.4) on may 1, 1998, at 1230 CST a Bellanca BL-17-30A, N6645V, lost engine power and was forced to make an emergency landing in a field near…Incident 19950223005319IFinal Approach · Chickasha, OKNarrative: pilot stated that it was dusk and he could tell there was barely enough light to see runway. R/h gear hit a fence post at south end of runway may have turned wheel sideways. Landed on runway, a/c veered right, r/h gear folded r/h wing struck…
Service difficulty reports
No reports matched to N6645VGeneral 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 17-30A aircraft
STCs that may be installed · 244
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Bellanca 17-30A
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