N1937E

Substantial
Serious

AERONCA 7AC S/N: 7AC-5504

Accident Details

Date
Friday, March 31, 1995
NTSB Number
LAX95LA150
Location
EL CAJON, CA
Event ID
20001207X03155
Coordinates
32.839263, -116.880393
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

a loss of engine power due to an in-flight separation of the fuel system gascolator glass bowl resulting in a premature fuel exhaustion. The rough/uneven terrain is a factor in this accident.

Aircraft Information

Registration
Make
AERONCA
Serial Number
7AC-5504
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
7AC CH7A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
7AC

Registered Owner (Current)

Name
HIGGINSON ROBERT C
Address
9569 BROOKSIDE AVE
City
BEN LOMOND
State / Zip Code
CA 95005-9502
Country
United States

Analysis

On March 31, 1995, at 1030 hours Pacific standard time, an Aeronca 7AC, N1937E, collided with the terrain while executing an emergency landing at El Cajon, California. The emergency landing resulted from a total loss of engine power. The pilot was conducting a local visual flight rules personal flight. The airplane, registered to and operated by the pilot and passenger, sustained substantial damage. The certificated airline transport pilot sustained minor injuries; the passenger sustained serious injuries. Visual meteorological conditions prevailed. The flight originated at Gillespie Field, San Diego, California, at 1015 hours.

A Federal Aviation Administration (FAA), San Diego Flight Standards District Office, airworthiness inspector conducted the on-scene investigation. The inspector reported the airplane came to rest, right-side-up, in a rough surface, high-vegetation field about 300 yards north of Interstate 8. The right wing was canted downward. The airplane sustained extensive structural damage, including a buckled firewall, but the propeller was in the horizontal position and undamaged.

San Diego Fire Department personnel told the inspector they did not detect a strong fuel odor when they arrived at the accident site. The inspector noted that the fuel tank contained " . . . only a small unmeasurable amount of fuel . . . ."

The fuel tank was not compromised during the accident; however, the glass gascolator bowl was missing. The inspector found pieces of the gascolator bowl imbedded in the seal area. Recovery personnel told the inspector that there were no glass remnants of the gascolator under or within the surrounding area of the wreckage.

The FAA inspector established continuity of the engine gear and valve train assembly. The inspector reported the presence of thumb compression when the crankshaft was rotated.

The spark plugs exhibited normal operating signatures. Both magnetos produced spark when their respective drive shafts were rotated.

Champion Aircraft Corporation Service Helps and Hints #15, Replacing of Glass Gascolator Bowl with Metal Gascolator Bowls, was originally issued on August 23, 1946, and reissued on July 1, 1964. The service letter states, in part:

It has been reported that a few glass gascolator bowls have broken. Reports indicate the glass bowl broke near the bottom and was caused by a combination of vibration and too much pressure applied on the adjustment clamp.

In order to eliminate any such possibility, we are changing to metal gascolator bowls as standard equipment on both our Champion Serial #4641 and up and Chief Serial #582 and up.

Compliance with this service letter is not mandatory. This issue is not addressed in an airworthiness directive.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX95LA150