N6688H

Substantial
None

CESSNA 185 S/N: 185-03335

Accident Details

Date
Thursday, November 3, 1994
NTSB Number
ATL95LA011
Location
ELIZABETHTON, TN
Event ID
20001206X02548
Coordinates
36.329772, -82.229148
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

THE FLEXING OF THE RUDDER PEDAL CONTROL LOCKING ASSEMBLY WHICH RESULTED IN THE COLLAPSE OF THE CO-PILOT'S LEFT PEDAL DURING HEAVY BRAKING.

Aircraft Information

Registration
Make
CESSNA
Serial Number
185-03335
Engine Type
Reciprocating
Model / ICAO
185 C185
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
A185F

Registered Owner (Current)

Name
SAMARITANS PURSE
Address
PO BOX 3000
City
BOONE
State / Zip Code
NC 28607-3000
Country
United States

Analysis

On November 3, 1994, at 1500 eastern standard time, a Cessna 185, N6688H, went off the right side of runway 24 during an attempted landing at Elizabethton Municipal Airport, Elizabethton, Tennessee. The instructional flight operated under 14 CFR Part 91, with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane sustained substantial damage, and the instructor pilot and three other pilots were not injured. The flight departed Elizabethton at 1300 hours.

According to the certified flight instructor, he and three other private pilots were conducting routine training when he lost control of the airplane during a landing attempt. The airplane had rolled 500 feet when the left pedal collapsed. The airplane veered off the right side of runway and collided with the ground. A preliminary examination of the airplane disclosed that the instructor's left pedal unlocked and collapsed.

Examination of the rudder pedal assembly failed to disclose any failed components. The examination disclosed some deformation to the locking assembly. The steering and braking systems operated normally, after the pedal assembly was restored to the normal operational position. The company maintenance inspector concluded that heavy braking caused the locking components to flex enough to collapse the left pedal assembly. The company maintenance inspector stated that rudder pedal malfunctions experienced by mission pilots were corrected by disabling the stow feature.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL95LA011