- Registered owner
- Crouse John A
- Location
- Sterling, AK
- Owner type
- Individual
- Serial number
- 50811
- Year built
- 1960
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard
- Airworthiness date
- June 4, 1960
- Certificate issued
- February 15, 2017
- Expires
- February 28, 2030
- Mode S code
- ACEBED
From the FAA registry file of October 27, 2026. The registry lists only the engine series, so ADs for every Continental O-470 model are included below.
On this page
NTSB investigations · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB ANC01LA063Accident · No injuriesLimited investigationFinal reportFairbanks, AKThe pilot's failure to refuel the airplane, his inadequate preflight planning/decision making, and subsequent fuel exhaustion during cruise flight.NTSB DEN84LA182Accident · No injuriesLimited investigationFinal reportLustre, MTDue to strong crosswind conditions at the prepared landing strip, the pilot elected to land in an open field. On touchdown, the right main landing gear encountered a hole, breaking the mounting structure and collapsing the gear. A ground loop ensued. The…NTSB UNK65X1413Accident · No injuriesClosedLeeville, LA
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 20010601010999AFaribanks, AK(-23)On a personal flight from iksgiza lake to fai, pilot reported that his engine lost power. Pilto landed safely with substantail damage to the aircraft in the tundra 20.4 miles west of fairbanks, Alaska. It was noted by FAA inspectors at the scene of the…Accident 19840616025129ARoll-Out (Fixed Wing) · Lustre, MTCollided with a chuck hole while landing in a farm field.
Airworthiness directives that may apply · 57
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 | 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 |
| 2006 | 1 |
| 2007 | 1 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 1 |
| 2020 | 1 |
| 2022 | 3 |
| 2023 | 5 |
See all 68 ADs
Information bulletins that may apply · 14
Advisory, not mandatory.
Airframe · Cessna 180C
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
Service difficulty reports
No reports matched to N9311TGeneral 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 180C aircraft
STCs that may be installed · 609
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 180C
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.