LAX92LA097

NTSB accident investigation · Cessna 120 · Sonoma, CA · January 21, 1992

Accident · No injuriesLimited investigationFinal report
Date
January 20, 1992, 16:02 local (Jan 21, 1992, 00:02 UTC)
Place
Sonoma, CA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N3010NCessna 120
Weather
Visual (VMC) · Day
Status
Completed · report August 13, 1993
Report
Approved by Office Director
FAA report
19920120000739A
Case key
27540

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

Engine failure due to a binding mixture control shaft. The binding mixture control shaft was the result of inadequate maintenance which allowed the accumulation of moisture and water in the carburetor to remain for an extended period of time causing rust and corrosion. A factor in the accident was the unsuitable nature of the terrain for the forced landing attempt.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - nonmechanicalTakeoff - initial climb
Fuel system,carburetor - contaminationCause
Mixture control - jammedCause
Fuel system - not maintainedOther maintenance personnelCause
Powerplant controls - not maintainedOther maintenance personnelCause
Forced landingDescent - emergency
Terrain condition - none suitableFactor
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - rough/uneven
Terrain condition - ditch

Analysis

The pilot and passenger departed for a local flight to practice landings. At about 200 to 300 feet AGL on the crosswind leg, the engine quit. An attempt to restart the engine failed and the pilot landed the aircraft in a pasture which was sloped, rough and had a dry creek bed in it. Upon reaching the creek bed, the airplane nosed over. Examination of the aircraft revealed that the carburetor mixture control linkage was frozen and would not respond to movement of the cockpit control. Disassembly of the carburetor revealed evidence of moisture and water contamination, accumulated over an extended period of time, which caused rust, corrosion and binding of the mixture control shaft in the lean to near idle cutoff position. Examination of the engine records revealed that the last time the carburetor was overhauled was about June 2, 1983, while installed in an experimental aircraft. The engine was installed in the accident aircraft on may 17, 1991, after accumulating about 132 hours in about 8 years and 6 months. The manufacturer recommends that the carburetor be overhauled every 5 calender years.

Aircraft

Registration
N3010N
Reported as
Cessna 120
Category
Airplane
Serial number
13268
Airframe hours
7,777
Engine
Continental C-90-12F, 90 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Andrew J. Bowe, Jr
Registered owner
Andrew J. Bowe, Sr
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 17, 1991 · 71 hours before

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
18
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
442 total · 18 in this make and model · 363 as pilot in command · 72 in the last 90 days · 14 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
120° at 4 knots
Visibility
7 statute miles
Lowest ceiling
5,000 ft overcast
Temperature
50 °F
Altimeter
30.00 inHg

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.