N2053E

Substantial
None

AERONCA 7CCMS/N: 7AC-5623

Accident Details

Date
Saturday, December 11, 2010
NTSB Number
ERA11LA084
Location
Rochester, NH
Event ID
20101211X70628
Coordinates
43.283889, -70.929168
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The out-of-rig condition of the tailwheel lock, which resulted in a loss of directional control on landing.

Aircraft Information

Registration
Make
AERONCA
Serial Number
7AC-5623
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
7CCMA270
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
7CCM

Registered Owner (Current)

Name
FERWERDA BEECH LLC
Address
37 TARAH DR
City
FREMONT
State / Zip Code
NH 03044-3249
Country
United States

Analysis

On December 11, 2010, about 0800 eastern standard time, an Aeronca 7CCM, N2053E, was substantially damaged following a loss of directional control during landing at Skyhaven Airport (DAW), Rochester, New Hampshire. The airplane was operated by Rochester Aviation. The certificated student pilot and flight instructor were not injured. Day, visual meteorological conditions prevailed at the time, and no flight plan was filed for the local, instructional flight. The flight originated about 0730 was conducted under the provisions of 14 Code of Federal Regulations Part 91.

The flight instructor reported the following. During the first three landings on runway 33, with the student pilot at the controls, and in calm winds, the airplane "...snapped a little left." Each time, a correction was made to maintain directional control. On the fourth landing attempt, the airplane snapped left again. The tailwheel lifted momentarily off the runway surface. When the tailwheel came back down, the airplane "shot hard left." Although the flight instructor was able to regain some directional control, the airplane departed the runway surface. The airplane then struck the surface-mounted precision approach path indicator (PAPI) unit and came to a stop.

An inspector with the Federal Aviation Administration responded to the accident site and examined the wreckage. The horizontal stabilizer and empennage sustained structural damage from the collision with the PAPI unit. During a flight control continuity check, the control surfaces moved normally. When the tailwheel was examined, the tailwheel unlocked easily when shaken manually.

The student pilot had logged about 2.1 hours of flight time at the time of the accident.

Weather, recorded at DAW at 1252, included winds calm, visibility 10 statute miles, sky overcast at 4,400 feet, temperature -3 degrees C, dew point -9 degrees C, an altimeter setting of 30.21 inches Hg.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA11LA084