- Registered owners
- Brown AnthonyDavila Pablo
- Location
- Pacoima, CA
- Owner type
- Co-owned
- Serial number
- 30053
- Year built
- 1967
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 11, 1967
- Certificate issued
- September 9, 2020
- Expires
- September 30, 2027
- Mode S code
- A5C3CC
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
No NTSB investigations matched to N4702VMatched 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 Bellanca 17-30 aircraft
FAA incident reports · 4
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20210701012139ICruise/Level Flight · Tusayan, AZOn July 1, 2021, at approximately 14:43 mountain standard time (MST), a Bellanca 17-30 (N4702V), experienced a partial loss of engine power and made a precautionary landing 8.7 miles west-southwest of Grand Canyon National park airport (kgcn). The…Incident 20160113000369ILanding: Rollout · Lakeville, MNAfter landing on runway 12 at lvn, right main gear collapsed on landing rollout just prior to initiating turn off from runway.Incident 19871023063549INormal Cruise · El Dorado, KSLow fuel caused engine failure during turn. Aircraft was stalled in, damaging landing gear. No injuries.Incident 19851231076099IForced/Precautionary Landing · Lawrence, KSEngine lost power after takeoff. Restart accomplished just prior to touchdown gear up. Water from sump on preflight.
Service difficulty reports
No reports matched to N4702VGeneral 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