N984J

Destroyed
Minor

Johnson ZODIAC CH 601 HDS S/N: 63848

Accident Details

Date
Friday, March 24, 2000
NTSB Number
DEN00LA064
Location
WEST JORDAN, UT
Event ID
20001212X20619
Coordinates
40.620399, -111.980369
Aircraft Damage
Destroyed
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

Total failure of an oil line fitting, resulting in oil exhaustion and subsequent engine seizure. Factors were the poor fitting installation by the pilot, and unsuitable terrain on which to make a forced landing.

Aircraft Information

Registration
N984J
Make
JOHNSON
Serial Number
63848
Engine Type
Reciprocating
Model / ICAO
ZODIAC CH 601 HDS R185
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
JOHNSON REX S
Address
7226 S 2980 E
Status
Deregistered
City
SALT LAKE CITY
State / Zip Code
UT 84121-4267
Country
United States

Analysis

On March 24, 2000, at 1132 mountain standard time, a Johnson Zodiac CH 601 HDS, N984J, registered to and operated by the pilot, was destroyed when it collided with objects and terrain 100 yards south of the southwest boundary of Salt Lake City Municipal 2 Airport, Salt Lake City, Utah. The private pilot, the only occupant, received minor injuries. Visual meteorological conditions prevailed for the personal flight, and no flight plan had been filed for the personal flight being conducted under Title 14 CFR Part 91. The flight originated from Salt Lake City Municipal 2 Airport just before the accident.

According to the pilot's accident report, this was the airplane's second flight. He took off on runway 34 and remained in the traffic pattern. While on the downwind leg and approaching the base leg turn, the engine began "misfiring and/or running very rough." Smoke filled the cabin, the engine began to lose power, then seized. The pilot said the "high sink rate and the headwind caused [him] to fall short of the runway by 200 yards." The airplane clipped a high stack of PVC pipes and impacted the ground inverted.

According to the FAA inspector who examined the airplane, the pilot had "removed the engine oil pressure sending unit from the engine oil pressure port, located on the right side of the engine-driven oil pump housing. He then installed a common automotive brass T-fitting, to which he attached both the oil pressure sending unit and a Hobbs hour meter fluid pressure-activated switch. The T-fitting failed in the pipe thread, flush with the pump housing exterior surface. The arm of the 'sending unit assembly' was about 4.5 inches, with an estimated weight of about 7 ounces. The path of the engine cooling air directed the leaking oil to the cabin air heat muff, where it was burned by the muffler prior to entering the cabin, accounting for the smoke in the cabin."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN00LA064