ERA14CA080

NTSB accident investigation · Schweizer 269C · White Plains, NY · December 28, 2013

Accident · Minor injuriesData collectionFinal report
Date
December 28, 2013, 08:30 local (13:30 UTC)
Place
White Plains, NY
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N2056JSchweizer 269C
Defining event
Landing-flare/touchdown: Hard landing
Weather
Visual (VMC) · Day
Status
Completed · report February 4, 2014
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FSDO/FAA
FAA report
20131228024809A
Case key
88597

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 flight instructor's failure to maintain airspeed during a practice autorotation, which resulted in a hard landing and subsequent loss of control

Findings · 4

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.

Attention/monitoring: monitoring equip/instrumentsPersonnel issues › Psychological · Instructor/check pilotSchweizer 269C: 1 caseAll aircraft: 142 casesProbable cause
Performance/control parameters: airspeedAircraft › Aircraft oper/perf/capability · Not attained/maintainedSchweizer 269C: 1 caseAll aircraft: 1,681 casesProbable cause
Use of equip/info: use of equip/systemPersonnel issues › Task performance · Instructor/check pilotSchweizer 269C: 1 caseAll aircraft: 1,391 casesProbable cause
Performance/control parameters: landing flareAircraft › Aircraft oper/perf/capability · Incorrect use/operationSchweizer 269C: 3 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 (CFI) was demonstrating a 180-degree autorotation to a student pilot while performing an instructional flight. The CFI reported entering the autorotation when, at about 100 feet agl, the indicated airspeed suddenly dropped to about 40 knots. He pushed the cyclic forward in an attempt to regain airspeed and flared at about 50 feet agl in an attempt to slow down the helicopter's rate of descent. The helicopter landed on the edge of the runway on the back of the skids, bounced back into the air, and began an accelerated yaw to the right. According to the CFI, he lowered the collective and reduced throttle while the helicopter spun four or five times. The helicopter subsequently impacted the ground, and came to rest on its left side. A postaccident examination by a Federal Aviation Administration inspector revealed substantial damage to the cabin and the tail boom. The CFI reported no preaccident mechanical malfunctions or failures that would have precluded normal operation.

Factual narrative

The flight instructor (CFI) was demonstrating a 180-degree autorotation to a student pilot while performing an instructional flight. The CFI reported entering the autorotation when, at about 100 feet agl, the indicated airspeed suddenly dropped to about 40 knots. He pushed the cyclic forward in an attempt to regain airspeed and flared at about 50 feet agl in an attempt to slow down the helicopter's rate of descent. The helicopter landed on the edge of the runway on the back of the skids, bounced back into the air, and began an accelerated yaw to the right. According to the CFI, he lowered the collective and reduced throttle while the helicopter spun four or five times. The helicopter subsequently impacted the ground, and came to rest on its left side. A postaccident examination by a Federal Aviation Administration inspector revealed substantial damage to the cabin and the tail boom. The CFI reported no preaccident mechanical malfunctions or failures that would have precluded normal operation.

Aircraft

Registration
N2056J
Reported as
Schweizer 269C
Category
Helicopter
Serial number
S1820
Built
2001
Airframe hours
7,504
Engine
Lycoming HIO-360-D1A, 190 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Wings Air LLC
Registered owner
Wings Air LLC
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · December 6, 2013
Departed
HPN · White Plains, NY
Destination
HPN · White Plains, NY
Airport
HPN · Westchester County, runway 29, 4,451 × 150 ft, asphalt

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
Pilot
Age
20
Injuries
Minor
Certificates
Flight instructor, Commercial
Instrument ratings
Helicopter
Medical
Class 2, Without waivers/limitations
Last flight review
June 19, 2013
Seat
Right
Restraint
4-point
Flight hours
446 total · 257 in this make and model · 367.7 as pilot in command · 88 in the last 90 days · 24.7 in the last 30 days · 0.8 in the last 24 hours
Role
Student pilot
Age
16
Injuries
None
Certificate
Student
Medical
Class 2, With waivers/limitations
Seat
Left
Restraint
4-point
Flight hours
96.8 total · 96.8 in this make and model · 9.6 as pilot in command · 21.3 in the last 90 days · 7 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
250° at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
37 °F, dew point 19 °F
Altimeter
30.18 inHg
Observed at
HPN

Docket · 6

The files NTSB released with the investigation on January 21, 2014, on NTSB’s docket system: statements, records, photos and specialists’ reports. 736 KB 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.