N7304Q

Destroyed
Serious

Higgens RANS S-12 XL S/N: 7950626

Accident Details

Date
Saturday, September 6, 1997
NTSB Number
CHI97LA287
Location
TUSCOLA, IL
Event ID
20001208X08810
Coordinates
39.790718, -88.280990
Aircraft Damage
Destroyed
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

the pilot's failure to maintain adequate airspeed, while maneuvering, which resulted in an inadvertent stall.

Aircraft Information

Registration
N7304Q
Make
HIGGENS
Serial Number
7950626
Model / ICAO
RANS S-12 XL

Registered Owner (Historical)

Name
HIGGINS JAMES R
Address
RR1 BOX 331
Status
Deregistered
City
TUSCOLA
State / Zip Code
IL 61953
Country
United States

Analysis

On September 6, 1997, at 1030 central daylight time (cdt), a Higgens Rans S-12 XL, N7304Q, operated by a private pilot, sustained substantial damage when while maneuvering, it departed controlled flight and impacted the terrain five miles north of Tuscola, Illinois. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under 14 CFR Part 91. There was no flight plan on file. The pilot reported minor injuries. The passenger on board suffered serious injuries. The local flight originated at Tuscola, Illinois, at 1020 cdt.

In his written statement, the pilot said that he and the passenger were maneuvering in the vicinity of the passenger's house. "At a cruise speed of 60 miles per hour and 6,000 rpm, at 500 feet above ground level (agl) and a heading of 300-degrees, we entered a shallow right turn around the west side of the house. After passing the north side and heading down the east side of the house (heading approximately 150 to 180-degrees), we started to lose altitude." The pilot lowered the nose and added full power. He then raised the nose to a level flight attitude, but continued to descend. "At this point, impact with the ground was imminent."

The Federal Aviation Administration (FAA) inspector who examined the airplane observed upward crush damage to the cockpit floor and frame. Both wings were separated at the wing roots. Both wings showed upward bending and heavy skin wrinkling. The boom fuselage was twisted to the right approximately 15-degrees. A 10-inch long gash was observed in the center fuselage metal running 45-degrees outward and aft of a rivet line. The forward vertical stabilizer showed heavy skin wrinkles. One of the three propeller blades was twisted forward and bent outward. Flight control continuity was confirmed. No anomalies were observed in the engine, engine controls, or other airplane 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# CHI97LA287