N5025C

Substantial
None

Bellanca 7GCBC S/N: 1053-78

Accident Details

Date
Friday, November 27, 1998
NTSB Number
FTW99LA037
Location
STUTTGART, AR
Event ID
20001211X11432
Coordinates
34.490520, -91.550445
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The separation of the left main landing gear bolt.

Aircraft Information

Registration
Make
BELLANCA
Serial Number
1053-78
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
7GCBC B407
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
7GCBC

Registered Owner (Current)

Name
SAMALON WILLIAM S TRUSTEE
Address
PO BOX 33015
City
JUNEAU
State / Zip Code
AK 99803-3015
Country
United States

Analysis

On November 27, 1998, at 1345 central standard time, a Bellanca 7GCBC tailwheel equipped airplane, N5025C, groundlooped during the landing roll at the Stuttgart Municipal Airport, Stuttgart, Arkansas. The airplane, being flow by a private individual under Title 14 CFR Part 91, was owned by Tool Goose Flying Company, Tunica, Mississippi. The private pilot and the pilot rated passenger were not injured and the airplane sustained substantial damage. Visual meteorological conditions prevailed for the personal cross country flight that departed Tunica, Mississippi, at 1310.

During personal telephone interviews, conducted by the investigator-in-charge, the pilot, passenger, and the airport manager reported the following information. The airplane landed in a 3 point attitude on the centerline of runway 18. During the landing roll with approximately 25 knots speed, the airplane veered to the right side of the runway. Application of the left rudder and the left brake by both occupants had no effect. Subsequently, the airplane departed the runway and groundlooped. The pilot and airport manager, who both examined the airplane, found structural damage to the fuselage and the left wing. The left main landing gear and propeller were also damaged. The airport manager reported that the left main wheel "rolled freely."

The FAA inspector reported a separation of a left main landing gear bolt. The reason for the bolt separation was not determined. The pilot estimated that the failed bolt had accumulated 1302.2 flight hours since installation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW99LA037