GAA17CA178

NTSB accident investigation · Schweizer 269C · Ormond beach, FL · February 21, 2017

Accident · No injuriesData collectionFinal report
Date
February 21, 2017, 12:37 local (17:37 UTC)
Place
Ormond beach, FL
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N614TASchweizer 269C
Defining event
Enroute: Flight control sys malf/fail
Weather
Visual (VMC) · Day
Status
Completed · report May 15, 2017
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA
FAA report
20170221001479A
Case key
94837

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

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.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Engine controls: power leverAircraft › Aircraft power plant · MalfunctionSchweizer 269C-1: 2 casesAll aircraft: 95 casesProbable cause
Performance/control parameters: landing flareAircraft › Aircraft oper/perf/capability · Attain/maintain not possibleSchweizer 269C-1: 5 casesAll aircraft: 1,285 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

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 postaccident examination revealed that 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 flex outside of the housing.

Factual narrative

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.

Aircraft

Registration
N614TA
Reported as
Schweizer 269C (1)
Category
Helicopter
Serial number
0080
Built
1998
Airframe hours
5,655.1
Engine
Lycoming HO-360, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · January 6, 2017
Departed
OMN · Ormond beach, FL
Destination
OMN · Ormond beach, FL
Airport
OMN · Ormond Beach Muni, runway 8, 4,005 × 75 ft, asphalt
Equipment
None

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
27
Injuries
None
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Without waivers/limitations
Last flight review
February 13, 2017
Seat
Left
Restraint
4-point
Flight hours
1,175 total · 630 in this make and model · 1,070 as pilot in command · 175 in the last 90 days · 75 in the last 30 days · 4 in the last 24 hours
Role
Student pilot
Age
25
Injuries
None
Certificate
Private
Medical
Class 1, Without waivers/limitations
Last flight review
December 19, 2016
Seat
Right
Restraint
4-point
Flight hours
118 total · 118 in this make and model · 35 as pilot in command · 26 in the last 90 days · 21 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
140° at 11 knots, gusting 16
Visibility
10 statute miles
Temperature
73 °F, dew point 59 °F
Altimeter
30.06 inHg
Observed at
KOMN

Docket · 2

The files NTSB released with the investigation on April 4, 2017, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.2 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.