N6165B

Substantial
None

Cessna 182A S/N: 34165

Accident Details

Date
Thursday, July 1, 1999
NTSB Number
DEN99LA110
Location
SALT LAKE CITY, UT
Event ID
20001212X19239
Coordinates
40.810054, -111.940460
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A total loss of engine power (nonmechanical) for reasons undetermined. Factors were the existence of conditions conducive to carburetor icing, and unsuitable terrain on which to make a forced landing.

Aircraft Information

Registration
N6165B
Make
CESSNA
Serial Number
34165
Engine Type
Reciprocating
Model / ICAO
182A C182
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MCCULLOUGH ENGINEERING
Address
1567 E STRATFORD AVENUE
Status
Deregistered
City
SALT LAKE CITY
State / Zip Code
UT 84106
Country
United States

Analysis

On July 1, 1999, at 1606 mountain daylight time, a Cessna 182A, N6165B, owned and operated by McCullough Engineering, was substantially damaged during a forced landing in Salt Lake City, Utah. The private pilot, the only occupant aboard, was not injured. Visual meteorological conditions prevailed, and no flight plan had been filed for the personal flight being conducted under Title 14 CFR Part 91. The flight originated in Loa, Utah, approximately 1430.

According to the pilot's accident report, he had been receiving vectors for spacing around traffic. When he was finally cleared to land, he was higher than traffic pattern altitude. He decided to slip the airplane to dissipate some of the excess altitude. At a point where he felt he was in the proper position to complete a normal landing, he ended the slip and advanced the throttle. The engine lost power and steps to restore power were unsuccessful. The pilot made an off-airport forced landing. The airplane struck the street curb which knocked off the nose landing gear, then collided with a stop sign, bus stop sign, and a fence, incurring extensive damage to the wings. The airplane then skidded to a halt.

On July 20, 1999, the engine was functionally tested under the direction of an FAA aviation safety inspector-maintenance. No discrepancies were noted. The inspector opined that the power loss may have been due to the engine "loading up" when power was applied after a prolonged period of idle power.

Shortly after the accident, at 1620, the temperature and dew point at Salt Lake City International Airport were 33 degrees C. (91.4 degrees F.) and 9 degrees C. (48.2 degrees F.), respectively.

According to the Carburetor Icing Curve, light icing at glide and cruise power settings are possible.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN99LA110