N5191X

Substantial
Serious

CHAMPION 7ECAS/N: 692

Accident Details

Date
Saturday, July 23, 2011
NTSB Number
ERA11LA416
Location
Hinesville, GA
Event ID
20110723X10313
Coordinates
31.871389, -81.561668
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The total loss of engine power due to the improper installation of the carburetor air filter by maintenance personnel, which resulted in the filter becoming dislodged and obstructing the carburetor. Contributing to the accident was the pilot did not maintain adequate airspeed during the forced landing, which resulted in an aerodynamic stall.

Aircraft Information

Registration
N5191X
Make
CHAMPION
Serial Number
692
Year Built
1969
Model / ICAO
7ECA

Registered Owner (Historical)

Name
SALE REPORTED
Address
3011 W BUCKEYE RD
Status
Deregistered
City
PHOENIX
State / Zip Code
AZ 85009-5734
Country
United States

Analysis

On July 23, 2011, about 0752 eastern daylight time, a Champion 7ECA, N5191X, experienced a total loss of engine power after takeoff from the Midcoast Regional Airport (LHW), Hinesville, Georgia. The certificate private pilot sustained serious injuries and the passenger reported minor injuries. The airplane sustained substantial damage to the fuselage and wings. The airplane was registered to and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed and no flight plan was filed. The flight was originating at the time of the accident.

The pilot reported the airplane had climbed to about 900 feet after takeoff when the engine experienced a total loss of engine power. He initiated a turn back towards the airport. During the approach to land, the airplane stalled and collided with an airport fence.

Examination of the wreckage by a Federal Aviation Administration inspector revealed no anomalies with the airframe or flight controls. Examination of the carburetor revealed a large piece of foam from the air filter element was lodged in the carburetor venturi inlet. The FAA Inspector stated the air filter element had been installed improperly resulting in the foam element separating and being drawn into the carburetor inlet.

Review of the airplane logbooks revealed an engine overhaul was completed 31 hours before the accident. According to the pilot, a Brackett Aero Filter air filter element was installed during the engine overhaul.

Review of performance data for the Champion 7ECA revealed the airplane will stall at 44 knots.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA11LA416