N6288M

Substantial
None

WSK PZL Mielec M18AS/N: 1Z026-13

Accident Details

Date
Friday, November 22, 2002
NTSB Number
FTW03LA047
Location
Votaw, TX
Event ID
20021125X05517
Coordinates
30.303611, -94.323333
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A loss of engine power for undertermined reasons. Contributing factors included the unsuitable terrain for the forced landing and the lack of airspeed.

Aircraft Information

Registration
Make
WSK PZL MIELEC
Serial Number
1Z026-13
Engine Type
Reciprocating
Year Built
1996
Model / ICAO
M18A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
M-18A

Registered Owner (Current)

Name
CROP JET AVIATION LLC
Address
1921 S 1700 E
City
GOODING
State / Zip Code
ID 83330-5183
Country
United States

Analysis

On November 22, 2002, approximately 0900 central standard time, a WSK PZL Mielec M18A single-engine agricultural airplane, was substantially damaged following a forced landing after experiencing a partial loss of engine power near Votaw, Texas. The airplane was registered to and operated by Wakefield Aircraft LLC, of Cooperstown, North Dakota. The commercial pilot, sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed for the 14 CFR Part 137 aerial application flight, and a flight plan was not filed. The airplane departed a private grass airstrip at Wildwood Resort, Texas, at 0845.

According to the Pilot/Operator Accident Report (NTSB Form 6120.1/2), the pilot reported that after making one pass across the field he pulled up to make a "turn-around" when the engine went to idle power. The pilot stated that he dumped the remaining fertilizer and attempted to turn toward a highway to land, but "I did not have enough airspeed. I opted to land straight ahead in a field of small pine trees." The airplane impacted trees and came to rest in an upright position. There was no postimpact fire, and the pilot was not injured. The pilot also reported that approximately 30 minutes prior to departure he conducted a preflight check of the airplane.

The pilot reported that subtantial damage to both wing spars was a result of impact damage with the pine trees. Both horizontal stabilizers were damaged, all propeller blades exhibited bending and twisting deformation, and the propeller spinner was damaged.

On January 10, 2003, Turbines Inc., of Terre Haute, Indiana, disassembled and inspected the airplane's engine, PT6A-65B PCE 32351. The examination failed to reveal any anomalies which would have precluded normal operation of the engine.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW03LA047