- Registered owner
- Smith Timothy E
- Location
- Anchorage, AK
- Owner type
- Individual
- Serial number
- 32885
- Year built
- 1957
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard
- Airworthiness date
- April 22, 1957
- Certificate issued
- June 26, 1991
- Expires
- July 31, 2027
- Mode S code
- AD55D1
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 · 56
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 | 2 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 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 |
| 2007 | 1 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 1 |
| 2020 | 1 |
| 2022 | 3 |
| 2023 | 5 |
See all 67 ADs
Information bulletins that may apply · 14
Advisory, not mandatory.
Airframe · Cessna 180A
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 ANC15CA065Accident · No injuriesData collectionFinal reportHomer, AKThe pilot's loss of directional control during landing, resulting in a collision with terrain.NTSB ANC06CA097Accident · No injuriesData collectionFinal reportAnchor Point, AKThe pilot's inadequate compensation for wind conditions, which resulted in a collision with high brush during the landing flare. A factor contributing to the accident was wind gusts.
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 20150822024029ALanding: Rollout · Homer, AKAircraft landed on the beach at silver salmon creek. After landing and at the end of rollout the right tire hit a sand drift and the aircraft spun around like a ground loop striking the left wing and left elevator. Three passengers on board- no injuries.Accident 20060724016119ALevel Off Touchdown · Homer, AK(-23) On 7/24/06, at approximately 12:30 local time, N9588B, a Cessna 180A, sustained substantial damage while landing on an unimproved dirt airstrip on the west side of cook inlet, approximately 27 nautical miles west of ninilchik, Alaska. The flight was…
Service difficulty reports
No reports matched to N9588BGeneral 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 180A aircraft
STCs that may be installed · 600
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 180A
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.