ATL96LA115

NTSB accident investigation · Cessna 182 · Smithville, TN · August 3, 1996

Accident · No injuriesLimited investigationFinal report
Date
August 3, 1996, 14:00 local (19:00 UTC)
Place
Smithville, TN
Injuries
5 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N8584TCessna 182
Weather
Visual (VMC) · Day
Status
Completed · report February 18, 1997
Report
Approved by Office Director
FAA report
19960803020829A
Case key
3749

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

Restricted selector valve flow that resulted in fuel starvation. A factor was the automotive fuel that adversely affected an O-ring seal in the fuel selector valve.

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 powerTakeoff - initial climb
Fuel system,selector/valve - blocked(partial)Cause
Fluid,fuel grade - inadequateFactor
Forced landingEmergency landing after takeoff
Hard landingEmergency landing after takeoff

Analysis

During takeoff for the sport parachute operation, the engine sputtered and quit, and the pilot landed the airplane in a residential yard. Examination revealed that fuel flow through the fuel selector valve was restricted. The fuel selector was disassembled, and the O-rings for the left side were found swelled. Placing the O-rings in the same automotive fuel as in the airplane resulted in their swelling so as to restrict flow through the selector valve. The airplane had been STC'd for the use of automotive fuel. No maintenance records were available for the selector valve.

Factual narrative

On August 3, 1996, at 1400 central daylight time, a Cessna 182, N8584T, was substantially damaged during a forced landing in Smithville, Tennessee. The commercial pilot and four passengers were not injured. The airplane was being operated under the provisions of Title 14 CFR Part 91, and visual flight rules, by the Skydive Tennessee. Visual meteorological conditions prevailed at the time, and no flight plan had been filed for the local skydive drop flight. The flight was departing the Smithville airport at the time of the accident.

According to the pilot, the engine surged a few times and then completely lost power on departure. He made a forced landing straight ahead in the yard of a residence. The nose wheel of the airplane hit the ground hard and bent back the nose gear. The engine cowling and propeller struck the ground, and were bent, as the nose gear bent back. The right main landing gear also hit hard and was bent backward six to eight inches. The aircraft had only been in service for one day following maintenance on the fuel system. The pilot did not provide a report of the accident, other than the attached record of telephone interview.

An FAA inspector subsequently discovered two "O" rings in the fuel selector that had swelled, restricting fuel flow to the engine. He noted that the "O" rings were sticky to the touch. The inspector reported that he removed the "O" rings and placed them in a jar with the same automotive fuel and observed that within 15 minutes the "O" rings again enlarged. Maintenance records for the fuel selector valve were not available. The inspector believed that the left side "O" rings were affected more than the right side "O" rings because of their longer exposure time to the automotive fuel.

Aircraft

Registration
N8584T
Reported as
Cessna 182
Category
Airplane
Serial number
18252484
Airframe hours
5,077
Engine
Continental O-470-L, 230 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Registered owner
Skydive Tennessee
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 3, 1996
Departed
0A3
Airport
0A3 · Smithville Municipal

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
32
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Expired
Seat
Left

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 6 knots
Visibility
10 statute miles
Lowest ceiling
5,500 ft broken
Temperature
84 °F, dew point 64 °F
Altimeter
30.00 inHg
Observed at
BNA, 48 nm away

FAA reports on this event · 1

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