N2064J

Substantial
None

BELL 206-L4 S/N: 52028

Accident Details

Date
Thursday, September 30, 1993
NTSB Number
FTW93LA273
Location
HURST, TX
Event ID
20001211X13413
Coordinates
32.830513, -97.169166
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

THE EXCESSIVE FLARE AND THE CONTROL INTERFERENCE BY THE PILOT UNDERGOING INSTRUCTION AND INADEQUATE SUPERVISION BY THE CFI. FACTORS WERE THE PILOT'S FAILURE TO UNDERSTAND THE INSTRUCTOR'S DIRECTIONS DUE TO HIS LIMITED KNOWLEDGE OF THE ENGLISH LANGUAGE.

Aircraft Information

Registration
N2064J
Make
BELL
Serial Number
52028
Engine Type
Turbo-shaft
Year Built
2002
Model / ICAO
206-L4 B06
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
UI PROJEKTOWANA 1
05-400 OTWOCK
Status
Deregistered
City
WOJ MAZOWICKIE
Country
United States

Analysis

On September 30, 1993, at 1450 central daylight time, a Bell 206-L4, N2064J, was substantially damaged during a simulated autorotative landing near Hurst, Texas. Neither the airline transport rated pilot, nor the foreign airline transport rated pilot undergoing instruction were injured. Visual meteorological conditions prevailed for the instructional flight.

According to the instructor, the pilot flared in an excessively nose high attitude following a simulated engine failure during takeoff. The instructor pilot announced to the pilot receiving instruction that he was taking the controls of the aircraft, but the pilot did not understand his command and stayed on the controls. The instructor stated that he had to forcibly overcome the other pilot's control inputs while he attempted to level the attitude of the helicopter to a landing attitude. The pilot said that he was attempting to keep the helicopter airborne.

In the enclosed instructor pilot's statement he reported that "due to language problem with the Japanese student the student did not recognize or acknowledge my stating, "I have it."

The instructor further stated that the helicopter did not touch down hard, but the rotor RPM decayed to the point that pylon rock was encountered during touchdown, resulting in substantial damage to the tailboom.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW93LA273