NYC99LA072

NTSB accident investigation · Miner Rotorway Exec 162F · Mechanicsburg, PA · March 14, 1999

Accident · Minor injuriesLimited investigationFinal report
Date
March 14, 1999, 10:38 local (15:38 UTC)
Place
Mechanicsburg, PA
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N124CFMiner Rotorway Exec 162F
Weather
Visual (VMC) · Day
Status
Completed · report August 10, 2000
Report
Approved by Office Director
FAA report
19990314028399A
Case key
45902

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 pilot's inadvertent induced dynamic rollover. A factor in the accident was the pilot's lack of helicopter experience.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - in flightHover - in ground effect
Dynamic rollover - inadvertentPilot in commandCause
Lack of total experience in kind of aircraftPilot in commandFactor
Roll overHover - in ground effect

Analysis

This was the pilot's first solo flight in a helicopter. He brought the helicopter to about a 6 inch hover and then drifted left and settled. The left rear skid contacted the ground and the helicopter rolled over on its left side. The pilot held a private pilot certificate for single engine airplanes but had not flown in several years. He had received 9.9 hours of dual instruction in the same model of helicopter, and was signed off for solo flight, but had not flown in the 44 days that preceded the accident flight.

Factual narrative

On March 14, 1999, at 1038 eastern standard time, a homebuilt Rotorway Exec 162F, N124CF, was substantially damaged while the pilot was practicing hovering in an open field in Mechanicsburg, Pennsylvania. The certificated private pilot received minor injuries. Visual meteorological conditions prevailed and no flight plan had been filed for the flight conducted under 14 CFR Part 91.

In an interview, the pilot reported that he was on his first solo flight when the accident occurred. He had brought the helicopter to what he estimated was a 6 inch hover. After a few seconds, the helicopter drifted left and settled. The left rear skid caught on the ground and the helicopter rolled over on its left side. The frame and main rotor drive shaft were bent, and the main rotor blades were destroyed. The landing surface was a flat, hard packed field, about 5 acres in size which had recently been rolled.

According to the pilot, he held a single engine land rating for airplanes, and had logged 69.3 hours in airplanes; however, he had not flown in several years. As the construction of the helicopter neared completion, the pilot went to the kit manufacturer's facility in Arizona, where he received 9.9 hours of dual helicopter instruction in the same model. The pilot had been signed-off for solo flight on January 29, 1999, and had not flown again until the accident flight. The pilot's total flight time, including his recent helicopter dual instruction, was 79.2 hours.

The flight instructor who signed the pilot off for solo flight reported the pilot was "good" and did not remember him as having any specific problems.

According to Federal Aviation Administration Advisory Circular 90-87 HELCIOPTER DYNAMIC ROLLOVER:

"...During normal or slope takeoffs and landings with same degree of bank angle or side drift with one skid/wheel on the ground, the bank angle or side drift can place the helicopter in a situation where it is pivoting (rolling) about a skid/wheel which is still in contact with the ground. When this happens, lateral cyclic control response becomes more sluggish and less effective than for a free hovering helicopter. Consequently, if a roll rate is permitted to develop, a critical bank angle (the angle between the helicopter and the horizon) may be reached where roll cannot be corrected, even with full lateral cyclic, and the helicopter will roll over onto its side. As the roll rate increases, the angle at which recovery is still possible is significantly reduced...."

Aircraft

Registration
N124CF
Reported as
Miner Rotorway Exec 162F (ROTORWAY E)
Category
Helicopter, amateur-built
Serial number
6165
Airframe hours
13
Engine
Rotorway RI 162F, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
William A. Newhart, doing business as Two Way Traffic Inc
Registered owner
Two Way Traffice, Inc.
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · February 18, 1999 · 13 hours before
Departed
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

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
53
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
79 total · 10 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
110° at 6 knots
Visibility
7 statute miles
Lowest ceiling
9,000 ft broken
Temperature
36 °F, dew point 25 °F
Altimeter
30.00 inHg
Observed at
CXY, 6 nm away

FAA reports on this event · 1

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