N3180G

Substantial
None

MAULE M 7-235CS/N: 25002C

Accident Details

Date
Sunday, October 11, 2015
NTSB Number
GAA16CA019
Location
Mankato, MN
Event ID
20151019X70023
Coordinates
44.218887, -93.919441
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's failure to maintain directional control during the go-around, which resulted in a collision with terrain.

Aircraft Information

Registration
Make
MAULE
Serial Number
25002C
Engine Type
Reciprocating
Model / ICAO
M 7-235C
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
M-7-235C

Registered Owner (Current)

Name
EDWARDS THOMAS E
Address
15689 HARVEST CT
City
BRIGHTON
State / Zip Code
CO 80603-3889
Country
United States

Analysis

The pilot reported that he was landing in gusting wind conditions, and that while on final, "the wind let off causing us to sink faster than I wanted so I added power." He reported that the airplane drifted to the left side of the runway, he attempted to correct the drift, and then he decided to execute a go-around. He reported that during the go around, he encountered a large gust of wind while in a nose high attitude, and added full right rudder and full left aileron. The right main landing gear struck the ground and was severed, and the airplane impacted the ground. A postflight inspection revealed substantial damage to the fuselage and right wing.

The pilot reported there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation.

The pilot stated as a safety recommendation, he should have "Come in a little faster and used 1 or 2 notches of flaps versus 3."

Visual meteorological conditions prevailed in the area at the time of the accident. The local automated weather observing system was reporting; wind 180 degrees at 16 knots gusting to 22 knots.

The Maule M-7-235C airplane flight manual describes the normal flight operations for crosswind landings and takeoffs. This manual does not have a maximum safe crosswind velocity chart. This manual states in part;

Maximum demonstrated crosswind component is 12 knots (14 miles per hour) and flap extension should be limited to 0 degrees (first notch) with such crosswind or higher. 12 knots (14 miles per hour) is the maximum demonstrated for certification of the airplane and is not considered limiting with flaps at 0 degrees.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# GAA16CA019