N3619J

Substantial
None

Cessna 188 S/N: T18803655T

Accident Details

Date
Wednesday, September 25, 1996
NTSB Number
IAD96LA153
Location
PATASKALA, OH
Event ID
20001208X06761
Coordinates
40.000118, -82.669769
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

deterioration and fuel leakage from an engine fuel hose (with a service life that had been exceed, due to inadequate maintenance), which resulted in an engine compartment fire and subsequent damage to the airplane.

Aircraft Information

Registration
Make
CESSNA
Serial Number
T18803655T
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
188 C188
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
T188C

Registered Owner (Current)

Name
FISHER AG SERVICE LLC
Address
4579 TOWNSHIP ROAD 126
City
CARDINGTON
State / Zip Code
OH 43315
Country
United States

Analysis

On September 25, 1996, at 1545 eastern daylight time, a Cessna 188, N3619J, sustained substantial damage during an in-flight fuel fire near Pataskala, Ohio. The certificated commercial pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed and no flight plan was filed for the flight conducted under 14 CFR Part 137. The airplane departed Morrow County Airport in Mount Gilead, Ohio on an aerial application flight.

In the NTSB Form 6120.1/2, the pilot stated that he departed for an application flight and climbed the airplane to 500 feet above ground level. While en route he observed a slight loss of power, and the fuel flow was about "10 gallons an hour below normal." He further stated:

"...Normal emergency procedures, fuel valve okay, mixture rich, emergency fuel pump boost on high with no increase of fuel flow. Started to make turn and 10 seconds later engine failure. Started to discharge wheat seed to extend glide, engine cowling paint blistered and started smoking."

The pilot completed an emergency landing and reported only fire damage to the airplane. An examination of the airplane was performed by a Federal Aviation Administration Aviation Inspector. The Inspector's report stated, "Fuel hose from throttle and control assembly to fuel manifold valve assembly failed a low pressure leak check of 20 PSI air pressure...The band on the hose had P/N 111F417-4S-0430, along with date of 1Q84 (1st quarter 1984), TSO C-53A..."

The owner reported that the hose was installed on February 20, 1990. According to the Cessna Service Manual, Model 188 & T188 Series, "All flexible fluid carrying hoses in the engine compartment should be replaced at engine overhaul or every five years, whichever occurs first."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# IAD96LA153