N8030P

Substantial
Minor

Aeronca 7AC S/N: 3523

Accident Details

Date
Saturday, June 20, 1998
NTSB Number
SEA98LA107
Location
MURPHY, ID
Event ID
20001211X10433
Coordinates
43.080486, -116.520629
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's decision to initiate an aborted landing at an airport where, due to the high density altitude, his aircraft was unable to outclimb the rising terrain that surrounded airport. Factors include a high density altitude and crosswinds.

Aircraft Information

Registration
N8030P
Make
AERONCA
Serial Number
3523
Engine Type
Reciprocating
Year Built
2001
Model / ICAO
7AC CH7A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
STROINSKI THEODORE J
Address
3611 HOLTON RD
Status
Deregistered
City
ABBOTSFORD
State / Zip Code
WI 54405-9657
Country
United States

Analysis

On June 20, 1998, approximately 0900 mountain daylight time, an Aeronca 7AC, N8030P, impacted the terrain during an attempted VFR go-around at Murphy Airport, Murphy, Idaho. The private pilot, who was the sole occupant, received minor injuries, and the aircraft, which was owned and operated by Rocky Mountain Air Service, sustained substantial damage. The 14 CFR Part 91 personal pleasure flight, departed Nampa Municipal Airport, Nampa, Idaho, about 30 minutes earlier, and was being operated in visual meteorological conditions. No flight plan had been filed, and the ELT, which was activated by the impact, was turned off at the scene.

According to the pilot, after touching down in a 10 to 15 knot crosswind, the aircraft "...moved right very quickly." He therefore elected to execute a go-around. After initiating the go-around, the pilot felt that his aircraft was not climbing fast enough to clear the terrain ahead. He therefore made a crosswind turn in order to head in a direction where it appeared the aircraft might be able to successfully clear the terrain. That turn placed the aircraft on a heading where it had an almost direct tailwind of 10 to 15 knots. The strong tailwind resulted in an increased ground speed and therefore an even greater need for an increased climb rate. As the pilot pulled the nose up in an attempt to keep the aircraft climbing, it stalled and the right wing caught the terrain causing the aircraft to cartwheel.

A post-accident calculation determined that the density altitude at the time of the attempted go-around was approximately 4,800 feet.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA98LA107