N84787

Substantial
None

AERONCA 7ACS/N: 7AC-3504

Summary

On August 07, 2009, a Aeronca 7AC (N84787) was involved in an incident near Broadus, MT. All 2 people aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The pilot’s failure to maintain sufficient airspeed during low altitude maneuvering, which resulted in an inadvertent stall.

The pilot reported that he initiated a descending right turn at a slow airspeed to check on livestock. As he added power to arrest the descent rate, he felt the right wing stall, and the airplane impacted terrain. Examination of the airplane by the pilot revealed structural damage to the right wing, fuselage, and empennage. The pilot stated that he had no time to recover due to the low altitude, and reported no mechanical anomalies with the airplane or flight control systems.

This incident is documented in NTSB report WPR09CA388. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N84787.

Accident Details

Date
Friday, August 7, 2009
NTSB Number
WPR09CA388
Location
Broadus, MT
Event ID
20090807X11952
Coordinates
45.470275, -105.457221
Nearest Airport
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 sufficient airspeed during low altitude maneuvering, which resulted in an inadvertent stall.

Aircraft Information

Registration
Make
AERONCA
Serial Number
7AC-3504
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
7ACCH7A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
7AC

Registered Owner (Current)

Name
BOWERS JAMES H
Address
230 E RIVER RD
City
BROADUS
State / Zip Code
MT 59317-9528
Country
United States

Analysis

The pilot reported that he initiated a descending right turn at a slow airspeed to check on livestock. As he added power to arrest the descent rate, he felt the right wing stall, and the airplane impacted terrain. Examination of the airplane by the pilot revealed structural damage to the right wing, fuselage, and empennage. The pilot stated that he had no time to recover due to the low altitude, and reported no mechanical anomalies with the airplane or flight control systems.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR09CA388