CEN23LA301

NTSB accident investigation · Schweizer 269C-1 · Titusville, FL · July 10, 2023

Accident · Minor injuriesClass 4 · LimitedFinal report
Date
July 10, 2023, 10:35 local (14:35 UTC)
Place
Titusville, FL
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Standing
Aircraft
N21409Schweizer 269C-1
Defining event
Standing: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 4 - Basic report with no Prelim publish
NTSB office
Central Region
Parties
FAA-FSDO
FAA report
20230710009279A
Case key
192618

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

On this page

Probable cause

The student pilot’s failure to maintain helicopter control while on the ground when his attention was diverted for post flight activities.

Findings · 1

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.

Use of equip/info: aircraft controlPersonnel issues › Task performance · Student/instructed pilotSchweizer 269C-1: 10 casesAll aircraft: 9,295 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

After completion of a local solo flight, the student pilot was conducting the engine cooling shutdown procedure on the dry ramp when the helicopter suddenly became airborne, climbed about 30ft, and entered a nose down attitude impacting the ground. The helicopter came to rest upright, and the pilot was able to egress from the helicopter without further incident. The helicopter sustained substantial damage to the main rotor system, the tail boom, and the tail rotor system. The student pilot reported that he had engaged both the cyclic and collective friction prior to completing other post flight activities. Postaccident examination of the helicopter showed the collective friction to not be fully engaged. The friction was found at an approximate 90-degree angle to the collective lever, which corresponds to the friction not being fully engaged. The helicopter pilot’s flight manual states that the collective friction is to be on for the engine cooling shutdown procedure. No preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal flight operation were reported.

Aircraft

Registration
N21409
Reported as
Schweizer 269C-1
Category
Helicopter
Serial number
0365
Built
2009
Airframe hours
4,947
Engine
Lycoming HIO-360-G1A, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
US Aviation Training Solutions
Registered owner
US Aviation Training Solutions
Airworthiness certificate
Standard, Normal
Last inspection
January 13, 2023
Destination
Same as departure
Airport
TIX · Space Coast Regional Airport
Equipment
ADS-B

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

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
27
Injuries
Minor
Certificate
Student
Medical
Class 2, Without waivers/limitations
Last flight review
June 16, 2023
Seat
Right
Flight hours
36 total

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 9 knots
Visibility
7 statute miles
Temperature
91 °F, dew point 75 °F
Altimeter
30.02 inHg
Observed at
KTIX
METAR
KTIX 101447Z 24009KT 7SM SCT028 33/24 A3002

Docket · 3

The files NTSB released with the investigation on October 5, 2023, on NTSB’s docket system: statements, records, photos and specialists’ reports. 5.2 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.