N9507U

Substantial
None

STOL UC-1 S/N: 017

Accident Details

Date
Tuesday, July 16, 1996
NTSB Number
FTW96LA305
Location
PRINCETON, TX
Event ID
20001208X06227
Coordinates
33.180267, -96.500694
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

improper adjustment of the left propeller governor which resulted in uncommanded feathering of the left propeller. Factors were: the airplane's inadequate engine out performance and the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N9507U
Make
STOL
Serial Number
017
Engine Type
None
Year Built
1975
Model / ICAO
UC-1 FEST
No. of Engines
0

Registered Owner (Historical)

Name
ERMAKOV BULAT
Address
612 JOHN THOMAS AVE
Status
Deregistered
City
DELAND
State / Zip Code
FL 32724-2995
Country
United States

Analysis

On July 16, 1996, at 0720 central daylight time, a Stol UC-1, N9507U, registered to and operated by a private owner under Title 14 CFR Part 91, was substantially damaged during a forced landing near Princeton, Texas. The airline transport rated pilot and his pilot rated passenger were not injured. Visual meteorological conditions prevailed for the cross-country flight and a flight plan was not filed. The flight originated from Gladewater, Texas, at 0610, and the intended destination was Childress, Texas.

According to the pilot, the airplane was in cruise flight at 4,500 feet MSL when the left engine propeller "went into feather, causing the engine to stall." The pilot's attempts "to unfeather the propeller and restart the engine" were unsuccessful. The pilot reported that "the aircraft's single engine performance was inadequate to maintain altitude." A forced landing was made to an open field with the landing gear up. During the landing roll, the airplane impacted a drainage ditch, resulting in substantial damage to the right lift strut and the fuselage.

The accident flight was the continuation of a trip which started on July 13, 1996, in Hollywood, Florida, with a planned final destination of Lake Havasu City, Arizona. The pilot had purchased the airplane in Florida and was flying it to his home in Arizona. According to the pilot, "through-out the entire flight (7-13 to 7-16)," he "had difficulty keeping the props in synch." He further stated that "the longest period of time they would remain synchronized was approximately one minute." Both the pilot and the passenger held mechanic certificates with airframe and powerplant ratings.

The left engine propeller governor was removed and bench tested under the supervision of an FAA inspector. The manufacturer's specifications called for the feather stop on the governor to be set at 1,690 rpm. Testing revealed that the stop was set at 2,000 rpm.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW96LA305