N7509E

Substantial
None

Schweizer 269-C S/N: 1436

Accident Details

Date
Wednesday, April 8, 1998
NTSB Number
MIA98LA127
Location
ORMOND BEACH, FL
Event ID
20001211X09913
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The CFI's inadequate supervision and poor communication which led the rated student pilot to roll the throttle off, and the CFI's subsequent failure to apply forward cyclic to increase airspeed which resulted in the subsequent hard landing and roll over.

Aircraft Information

Registration
N7509E
Make
SCHWEIZER
Serial Number
1436
Engine Type
Reciprocating
Year Built
1990
Model / ICAO
269-C H269
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
TOMLINSON AVIATION INC
Address
1860 OLD TOMOKA RD W
Status
Deregistered
City
ORMOND BEACH
State / Zip Code
FL 32174-6715
Country
United States

Analysis

On April 8, 1998, about 1130 eastern daylight time, a Schweizer 269-C, N7509E, registered to Tomlinson Aviation Inc., operating as a 14 CFR Part 91 instructional flight, experienced a hard landing at the Ormond Beach Municipal Airport, Ormond Beach, Florida. Visual meteorological conditions prevailed and no flight plan was filed. The helicopter sustained substantial damage. The commercial pilot flight instructor (CFI), and the airline transport-rated student pilot (SP) reported no injuries. The flight originated from Ormond Beach about 20 minutes before the accident.

The CFI stated he was conducting training with the SP on obtaining a CFI in helicopters. They had completed two normal approaches and a max performance takeoff from the sod area adjacent to runway 17. They departed the sod area with the SP flying the helicopter at 500 feet. He was asking the SP questions and told him to make a steep approach. The SP turned base and final. He descended to 300 feet and was maintaining about 35 knots. He asked the SP, can you roll the throttle off? The SP replied, " roll the throttle off," and immediately rolled the throttle off. The CFI noticed an immediate drop in rotor rpm, and took over the flight controls with the helicopter in a vertical rate of descent. He lowered the collective pitch in an attempt to regain rotor rpm, but not apply forward cyclic to increase airspeed due to low altitude. The helicopter collided with the sod area hard, and rolled over onto its left side.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA98LA127