N210H

Substantial
None

WSK PZL MIELEC M-18 DROMADER S/N: 1Z007-13

Accident Details

Date
Monday, July 10, 1995
NTSB Number
FTW95LA290
Location
DE WITT, AR
Event ID
20001207X03950
Coordinates
34.280376, -91.329566
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

THE PILOT'S FAILURE TO MAINTAIN AIRSPEED AND THE RESULTING INADVERTENT STALL/MUSH.

Aircraft Information

Registration
N210H
Make
WSK PZL MIELEC
Serial Number
1Z007-13
Model / ICAO
M-18 DROMADER

Registered Owner (Historical)

Name
BULLOCK BILLY PAUL DBA
Address
P O BOX 606
Status
Deregistered
City
DEWITT
State / Zip Code
AR 72042
Country
United States

Analysis

On July 10, 1995, at 1704 central daylight time, a WSK PZL Mielec M-18 Dromader, N210H, collided with machinery during takeoff near De Witt, Arkansas. The commercial pilot was not injured and the airplane sustained substantial damage. No flight plan was filed for the aerial application flight conducted by Bullock Flying Service under Title 14 CFR Part 137. Visual meteorological conditions prevailed for the flight which was originating when the accident occurred.

According to the pilot, after a "normal" liftoff, he "started to turn toward field, [and the] aircraft settled." Subsequently, the airplane's left main landing gear "struck [a] barrel and power unit" at the end of the 2,600 foot airstrip. The pilot reported the airplane then "turned sideways knocking out other gear" and came to rest "100 yards from end of runway." Both main landing gear were torn from the airplane and the fuselage and horizontal stabilizer were deformed.

The operator reported the airplane was loaded with approximately 3,000 pounds of dry fertilizer. Based on a temperature of 94 degrees and a pressure altitude of 1,000 feet, the density altitude was calculated at 3,500 feet. Using this data, a review of the performance charts in the aircraft flight manual indicated the airplane was within the prescribed limit for gross weight and required a takeoff ground roll distance of 750 feet. There were no reports of any engine or airframe discrepancies.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA290