N614TASCHWEIZER 269C2017-02-21 NTSB Accident Report

Substantial
None

SCHWEIZER 269CS/N: 0080

Summary

On February 21, 2017, a Schweizer 269C (N614TA) was involved in an incident near Ormond Beach, FL. All 2 people aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The separation of the throttle cable’s outer housing from the inner housing at the throttle linkage while at a high-power setting, which prevented the pilot from being able to control the throttle and execute a proper landing flare and resulted in a hard landing.

The flight instructor of the helicopter reported that about halfway through the flight he "discovered that the throttle control was inoperative" and stuck in the high RPM setting. He turned the helicopter back to the departure airport and briefed his student on the situation. Upon being cleared to land, he executed a "running landing" and performed a go around on the first try. On the second try, the skids made hard contact with the runway and the helicopter came to a stop.

A post-accident examination revealed the helicopter had sustained substantial damage to the fuselage.

The flight instructor reported that the throttle cable outer housing separated from the inner solid housing at the throttle linkage, and that the internal wire could now flex outside of the housing.

This incident is documented in NTSB report GAA17CA178. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N614TA.

Accident Details

Date
Tuesday, February 21, 2017
NTSB Number
GAA17CA178
Location
Ormond beach, FL
Event ID
20170221X44737
Coordinates
29.301944, -81.113891
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The separation of the throttle cable’s outer housing from the inner housing at the throttle linkage while at a high-power setting, which prevented the pilot from being able to control the throttle and execute a proper landing flare and resulted in a hard landing.

Aircraft Information

Registration
Make
SCHWEIZER
Serial Number
0080
Engine Type
Reciprocating
Model / ICAO
269CH269
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
TOMLINSON AVIATION INC
Address
92 HANGAR WAY
Status
Deregistered
City
ORMOND BEACH
State / Zip Code
FL 32174-6611
Country
United States

Analysis

The flight instructor of the helicopter reported that about halfway through the flight he "discovered that the throttle control was inoperative" and stuck in the high RPM setting. He turned the helicopter back to the departure airport and briefed his student on the situation. Upon being cleared to land, he executed a "running landing" and performed a go around on the first try. On the second try, the skids made hard contact with the runway and the helicopter came to a stop.

A post-accident examination revealed the helicopter had sustained substantial damage to the fuselage.

The flight instructor reported that the throttle cable outer housing separated from the inner solid housing at the throttle linkage, and that the internal wire could now flex outside of the housing.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# GAA17CA178