WPR14CA006

NTSB accident investigation · Siemens Rotorway Exec 162F · Nampa, ID · October 5, 2013

Accident · Minor injuriesData collectionFinal report
Date
October 5, 2013, 09:15 local (15:15 UTC)
Place
Nampa, ID
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N104BJSiemens Rotorway Exec 162F
Defining event
Enroute-cruise: Flight control sys malf/fail
Weather
Visual (VMC) · Day
Status
Completed · report December 2, 2013
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
FAA-FSDO
FAA report
20131005018459A
Case key
88175

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

A flight control malfunction during cruise flight for reasons that could not be determined. No follow-up examination was conducted due to a lapse in agency funding and subsequent government shutdown.

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.

Not determinedNot determined › Not determined · Unknown/Not determinedSiemens Jim ROTORWAY EXEC 162F: 1 caseAll aircraft: 2,247 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 pilot reported that while in cruise flight, about 500 feet above ground level (agl), the cyclic control seemed to require a higher than normal input. He changed speed, however, that seemed to make it worse. The pilot was over a field and entered a 180 degree autorotation to lose altitude. At the completion of the autorotation, forward velocity had dissipated and the lateral movement to the left increased even with full right cyclic input. The helicopter collided with trees that bordered the field and subsequently rolled over onto its left side after touchdown. The fuselage and tailboom were substantially damaged.

Factual narrative

The pilot reported that while in cruise flight, about 500 feet above ground level (agl), the cyclic control seemed to require a higher than normal input. He changed speed, however, that seemed to make it worse. The pilot was over a field and entered a 180 degree autorotation to lose altitude. At the completion of the autorotation, forward velocity had dissipated and the lateral movement to the left increased even with full right cyclic input. The helicopter collided with trees that bordered the field and subsequently rolled over onto its left side after touchdown. The fuselage and tailboom were substantially damaged.

Aircraft

Registration
N104BJ
Reported as
Siemens Rotorway Exec 162F (F)
Category
Helicopter, amateur-built
Serial number
6194
Built
1997
Engine
Rotorway RI 162F, 150 hp, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Departed
EUL · Caldwell, ID
Destination
EUL · Caldwell, ID

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
49
Injuries
Minor
Certificates
Airline transport, Flight engineer, Flight instructor
Airplane ratings
Multi-engine land, Single-engine sea, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, With waivers/limitations
Last flight review
June 19, 2013
Seat
Left
Restraint
3-point
Flight hours
30,000 total · 100 in this make and model · 22,000 as pilot in command · 220 in the last 90 days · 60 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
15 statute miles
Lowest ceiling
None
Temperature
55 °F
Altimeter
30.10 inHg
Observed at
EUL, 7 nm away

Docket · 1

The files NTSB released with the investigation on November 15, 2013, on NTSB’s docket system: statements, records, photos and specialists’ reports. 643 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 N104BJ · 1

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