CEN12CA402

NTSB accident investigation · Schweizer TH55A/269A · Grinnell, IA · June 26, 2012

Accident · No injuriesData collectionFinal report
Date
June 26, 2012, 14:33 local (19:33 UTC)
Place
Grinnell, IA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N488MCSchweizer TH55A/269A
Defining event
Maneuvering: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed · report October 4, 2012
Report
Approved by Office Director
NTSB office
Central Region
Parties
FAA/FSDO
FAA report
20120626010919A
Case key
84119

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 pilot’s inadequate compensation for the wind during a hovering maneuver, which resulted in a loss of tail rotor effectiveness and directional control.

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.

Use of equip/info: aircraft controlPersonnel issues › Task performance · PilotSchweizer TH55A/269A: 2 casesAll aircraft: 9,295 casesProbable cause
Wind: gustsEnvironmental issues › Conditions/weather/phenomena · Response/compensationSchweizer TH55A/269A: 1 caseAll aircraft: 1,199 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 helicopter pilot and his passenger were returning to the airport after a local flight. In preparation to land, the pilot approached a grassy area adjacent to the runway and entered a hover into a 12-knot wind that was gusting to 16 knots. The pilot then made a right-pedal turn downwind. He said that during the turn the wind caught the tail and the helicopter began to spin. The pilot could not stop the turning; the tailrotor struck a fence, and the main rotor blades hit the ground. A review of photographs of the helicopter taken after the accident revealed that the tail rotor blades, main rotor blades, and fuselage were substantially damaged. The pilot reported no preaccident mechanical malfunctions with the helicopter.

Factual narrative

The pilot and his passenger were returning to the airport after a local flight. In preparation to land, the pilot approached a grassy area adjacent to the runway and entered a hover into a 12 knot wind. The wind was also gusting to 16 knots. The pilot then made a right pedal turn downwind. He said that during the turn, the wind caught the tail and the helicopter began to spin. The pilot did not have enough left pedal to stop turning and the tailrotor struck a fence and the main rotor blades hit the ground. A review of photographs taken of the helicopter after the accident revealed the tail rotor blades, main rotor blades, and fuselage were substantially damaged. The pilot reported no mechanical malfunctions prior to the accident.

Aircraft

Registration
N488MC
Reported as
Schweizer TH55A/269A
Category
Helicopter
Serial number
680885
Airframe hours
11,666
Engine
Lycoming IO360 SER, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Lowry Flying Service
Registered owner
Lowry Flying Service
Airworthiness certificate
Standard, Normal
Last inspection
Annual · April 12, 2012
Departed
None · New Sharon, IA
Destination
GGI · Grinnell, IA
Flight plan
Unknown
Airport
GGI · Grinnell

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
59
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Flight hours
8,718 total · 47 in this make and model · 35 in the last 90 days · 20 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
130° at 12 knots, gusting 16

Docket · 1

The files NTSB released with the investigation on July 26, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 680 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.

Other investigations on N488MC · 1

Matched to the same aircraft by N-number and date.