ERA11CA201

NTSB accident investigation · Schweizer 269C-1 · Mount Pocono, PA · March 20, 2011

Accident · No injuriesData collectionFinal report
Date
March 20, 2011, 14:39 local (18:39 UTC)
Place
Mount Pocono, PA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N153HTSchweizer 269C-1
Defining event
Landing: Dynamic rollover
Weather
Visual (VMC) · Day
Status
Completed · report June 20, 2011
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20110320003319A
Case key
78614

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 flight instructor's selection of an unsuitable landing site to practice autorotations, which resulted in an inadvertent dynamic rollover during touchdown.

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.

Action: incorrect action performancePersonnel issues › Action/decision · Instructor/check pilotSchweizer 269C-1: 7 casesAll aircraft: 1,386 casesProbable cause
Performance/control parameters: lateral/bank controlAircraft › Aircraft oper/perf/capability · Capability exceededSchweizer 269C-1: 3 casesAll aircraft: 390 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 certified flight instructor (CFI) stated that during a local training flight, the helicopter was at a hover and he reduced power to simulate an engine failure. He said that upon ground contact, the aft portion of helicopter's left skid sank into the mud, the helicopter began to roll to the left, and he attempted corrective action for a dynamic rollover. However, the helicopter rolled over on to its left side resulting in substantial damage to the main rotor blades and fuselage. The CFI and student pilot both stated that there were no mechanical malfunctions with the helicopter prior to the accident.

Factual narrative

The certificated flight instructor (CFI) stated that during a local training flight, the helicopter was at a hover and he "rolled off power" to simulate an engine failure. According to the CFI, upon ground contact, the aft portion of helicopter's left skid "sank into the mud," the helicopter began to roll to the left, and he attempted corrective action as taught for a dynamic rollover. However, the helicopter rolled over on to its left side resulting in substantial damage to the main rotor blades and fuselage. The CFI and student pilot both stated that there were no mechanical malfunctions with the helicopter prior to the accident.

Aircraft

Registration
N153HT
Reported as
Schweizer 269C-1
Category
Helicopter
Serial number
0240
Airframe hours
1,766
Engine
Lycoming HIO-360-G1A, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Hi-Tech Helicopters Inc
Registered owner
Hi-Tech Helicopters Inc
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · March 17, 2011 · 5 hours before
Departed
MPO · Mount Pocono, PA
Destination
MPO · Mount Pocono, PA
Airport
MPO · Pocono Mountains Municipal Air

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
22
Injuries
None
Certificate
Commercial
Instrument ratings
Helicopter
Medical
Class 2, Without waivers/limitations
Last flight review
September 5, 2010
Seat
Left
Flight hours
205 total · 190 in this make and model
Role
Student pilot
Age
39
Injuries
None
Certificate
Student
Medical
Class 3, Without waivers/limitations
Seat
Right
Flight hours
33 total · 33 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
160° at 9 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
45 °F, dew point 12 °F
Altimeter
30.45 inHg
Observed at
MPO, 8 nm away

Docket · 5

The files NTSB released with the investigation on April 13, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.3 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.