- Registered owner
- Perrin James F
- Location
- Bancroft, WI
- Owner type
- Individual
- Serial number
- 18051355
- Year built
- 1964
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- March 6, 1996
- Certificate issued
- October 22, 2018
- Expires
- October 31, 2028
- Mode S code
- A1EE22
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental O-470 model are included below.
On this page
Airworthiness directives that may apply · 58
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1962 | 1 |
|---|---|
| 1963 | 1 |
| 1967 | 1 |
| 1968 | 1 |
| 1969 | 2 |
| 1973 | 3 |
| 1975 | 1 |
| 1977 | 1 |
| 1979 | 3 |
| 1980 | 2 |
| 1981 | 3 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 2 |
| 1988 | 3 |
| 1989 | 1 |
| 1990 | 2 |
| 1991 | 1 |
| 1993 | 2 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 2 |
| 1998 | 3 |
| 1999 | 1 |
| 2000 | 2 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 1 |
| 2020 | 1 |
| 2022 | 3 |
| 2023 | 5 |
See all 69 ADs
Information bulletins that may apply · 14
Advisory, not mandatory.
Airframe · Cessna 180G
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-18-23Passenger Compartment Equipment - Installation of F. Atlee Dodge Aircraft Services LLC. Folding Jump SeatsSAIB CE-17-25ELEVATOR TORQUE TUBE Inspections for cracks and corrosion in elevator torque tubesSAIB CE-12-14Three Alternative Methods of Compliance for AD 2011-10-09SAIB CE-10-40R1Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanesSAIB CE-09-42Lights - Landing Light, Beacon Light and Taxi Light Switch ApplicationsSAIB CE-09-10Availability of Secondary Seat Stops for Pilot and Copilot SeatsSAIB CE-08-02Flight ControlsSAIB CE-01-41R2Flight ControlsEngine · Continental O-470 series
SAIB NE-20-05POWERPLANT - Engine Camshaft Gear Tooth FractureSAIB NE-16-13Powerplant - Prohibited use of sealantSAIB 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 SectionHistorical bulletins · 1
NTSB investigations · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB CEN23LA236Accident · No injuriesClass 4 · LimitedFinal reportStevens Point, WIThe pilot’s failure to maintain directional control during landing that resulted in a ground loop and impact with the runway.NTSB CHI04CA094Accident · No injuriesData collectionFinal reportLong Lake, WIThe pilot flared improperly and failed to maintain directional control during landing.
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 20230608012829ALanding: Rollout · Stevens Point, WIFollowing a normal landing on runway 30, on rollout the aircraft picked up a sudden crosswind from the right. The pilot attempted to counteract the crosswind, but the aircraft veered right and the left wing struck the runway. The aircraft incurred substantial…Accident 20040331006109ALevel Off Touchdown · Eagle River, WI(-23) The pilot of CE-180, N223WH on 3/31/04, departed the Eagle River airport (egv) in order to fly local, to meet the 90 day proficiency requirements. He entered the egv traffic pattern to make his take off and landings. His first landing did not feel right…
Service difficulty reports
No reports matched to N223WHGeneral 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 Cessna 180G aircraft
STCs that may be installed · 587
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 180G
STC SA00709CHInstallation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2, no rev, both dtd 8/30/96, or later FAA app rev.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.