N9876D

Substantial
None

Rotorway Rotorway Exec 90S/N: R15160

Accident Details

Date
Monday, February 25, 2002
NTSB Number
LAX02LA096
Location
Phoenix, AZ
Event ID
20020227X00266
Coordinates
33.276668, -112.118057
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The student's inadvertent over control of the throttle mechanism, which resulted in the bending of the throttle mechanical stop and binding the linkage in the idle position. Also causal was the CFI's inadequate supervision. A factor in the accident was the CFI's inability to add engine power due to the bent throttle mechanism during a practice autorotation.

Aircraft Information

Registration
N9876D
Make
ROTORWAY
Serial Number
R15160
Engine Type
Reciprocating
Year Built
1992
Model / ICAO
Rotorway Exec 90EXEC
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
ROTORWAY HELICOPTER MANUFACTURING CO
Address
4140 W MERCURY WAY
Status
Deregistered
City
CHANDLER
State / Zip Code
AZ 85226-3707
Country
United States

Analysis

On February 25, 2002, at 1430 mountain standard time, a Rotorway Exec 90 experimental helicopter, N9876D, made a hard landing following a loss of power during cruise about 5 miles south of Phoenix, Arizona, on the Gila River Indian Reservation. The helicopter was operated by Cobb International, Inc., under the provisions of 14 CFR Part 91 as an instructional flight, and sustained substantial damage. The certified flight instructor (CFI) and student pilot were not injured. Visual meteorological conditions prevailed for the local area flight that departed the Chandler Stellar Airpark (P19), Chandler, Arizona, at 1410. The flight was scheduled to terminate at P19. A flight plan had not been filed.

In the CFI's written statement, he stated that he and his student were on a training flight to practice autorotations. During the third practice autorotation from 500 feet agl, the student performed the maneuver "without problems until the aircraft was straight and level after flaring" about 30 feet agl. Attempts were made to reintroduce power without success. The CFI stated he was on the controls "lightly" with the student, when the student told the CFI he could not reintroduce power. The CFI then came fully onto the controls and attempted to roll on the throttle only to discover it would not roll any further. The collective was raised to cushion the landing at 10 feet agl; however, the aircraft made hard contact with the ground, collapsing the left skid, and rolling onto its left side.

The Federal Aviation Administration Inspector, who responded to the accident site, informed the National Transportation Safety Board that the mechanical stop for the throttle was bent. He stated once the linkage is driven "over center," it can't be brought back, and it remains at ground idle. The engine was started after the accident and ran "with no problems."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX02LA096