N8724F

Substantial
Serious

Hughes 269AS/N: 12-0039

Accident Details

Date
Monday, June 25, 2001
NTSB Number
LAX01LA219
Location
Paso Robles, CA
Event ID
20010703X01301
Coordinates
35.672779, -120.626945
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
1
Total Aboard
2

Probable Cause and Findings

the pilot's failure to maintain rotor rpm during a practice autorotational landing, which resulted in a hard landing.

Aircraft Information

Registration
Make
HUGHES
Serial Number
12-0039
Engine Type
Reciprocating
Model / ICAO
269A
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
2
FAA Model
269A

Registered Owner (Current)

Name
DEL RIO AVIATION INC
Address
5062 WING WAY
City
PASO ROBLES
State / Zip Code
CA 93446-9528
Country
United States

Analysis

On June 24, 2001, approximately 1930 Pacific daylight time, a Hughes 269A single engine helicopter, N8724F, was substantially damaged during a hard landing following an autorotational landing at the Paso Robles Municipal Airport, Paso Robles, California. The flight instructor sustained serious injuries and the student was not injured. The helicopter was registered to and operated by Del Rio Aviation, Paso Robles, under the provision of 14 CRR Part 91 as an instructional flight. Visual meteorological conditions prevailed for the flight, and a flight plan had not been filed. The local instructional flight originated about 1845.

According to the instructor pilot, he was demonstrating a simulated loss of engine power and ensuing autorotational landing to the student. He reduced the throttle and lowered the collective. He then pointed out an area to land to the student. As he looked back into the cockpit (approximately 400 feet agl), he noticed the rotor rpm had decreased "drastically" and was dropping even lower. The instructor then ensured the collective was lowered all the way and put the cyclic forward; however, he was unable to regain the lost rotor rpm in time. The instructor then flared the helicopter, but it impacted the ground hard. The main rotor blades severed the tail boom and the helicopter rolled over.

The flight instructor indicated he was not sure how the rotor rpm got so low, but commented there were no problems with the engine or the freewheeling unit. The instructor pilot reported having accumulated approximately 2,000 total hours in helicopters, of which about 300 hours were flown in the accident helicopter make and model.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX01LA219