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NTSB accident investigation · Robinson Helicopter R44 II · Devine, TX · October 5, 2015

Accident · No injuriesData collectionFinal report
Date
October 5, 2015, 15:50 local (20:50 UTC)
Place
Devine, TX
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N174CDRobinson Helicopter R44 II
Defining event
Takeoff: Collision during takeoff/land
Weather
Visual (VMC) · Day
Status
Completed · report December 17, 2015
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA San Antonio FSDO
FAA report
20151005018309A
Case key
92127

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 failure to maintain obstacle clearance during the takeoff, which resulted in the helicopter striking power lines.

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.

Performance/control parameters: altitudeAircraft › Aircraft oper/perf/capability · Not attained/maintainedRobinson Helicopter R44 II: 39 casesAll aircraft: 1,310 casesProbable cause
Object/animal/substance: wireEnvironmental issues › Physical environment · Awareness of conditionRobinson Helicopter R44 II: 26 casesAll aircraft: 588 cases
Object/animal/substance: wireEnvironmental issues › Physical environment · Effect on operationRobinson Helicopter R44 II: 26 casesAll aircraft: 588 cases

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 during takeoff from a field next to an office building, the helicopter came in contact with one or two power lines, which caught on the left skid, and pulled the helicopter to the left. The main rotor blades contacted two power lines, and cut both of them. The pilot attempted to maintain control of the helicopter but it rolled to the left and impacted the ground. He reported that "the wires hit were invisible to me at the time of departure." A postflight inspection revealed substantial damage to the fuselage, the main rotor blade system, the tail boom, and the tail rotor blade system. The pilot reported there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation.

Factual narrative

The pilot reported that during takeoff from a field next to an office building, the helicopter came in contact with one or two power lines, which caught on the left skid, and pulled the helicopter to the left. The main rotor blades contacted two power lines, and cut both of them. The pilot attempted to maintain control of the helicopter but it rolled to the left and impacted the ground. He reported that "the wires hit were invisible to me at the time of departure." A postflight inspection revealed substantial damage to the fuselage, the main rotor blade system, the tail boom, and the tail rotor blade system. The pilot reported there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The pilot also stated as a safety recommendation, it would be "Best to walk the entire departure path, look for poles, wires, and guy wires prior to departure, especially with trees present, and a dark day which conceals the presence of wires. Don't get locked into one departure route. Turn the cellphone off when evaluating sites, and look 360 degrees." ADDITIONAL INFORMATION Robinson Helicopter Company Safety Notice SN-16 Robinson Helicopter Company has published Safety Notice SN-16 Power Lines Are Deadly (revised June 1994). This safety notice discusses wire strike mitigation techniques. The safety notices states; Flying into wires, cables, and other objects is by far the number one cause of fatal accidents in helicopters. Pilots must constantly be on the alert for this very real hazard. Watch for the towers; you will not see the wires in time. Fly directly over the towers when crossing power lines. Allow for the smaller, usually invisible, grounding wire(s) which are well above the larger more visible wires. Constantly scan the higher terrain on either side of your flight path for towers. Always maintain at least 500 feet above ground level (AGL) except during takeoff and landing. By always flying above 500 feet AGL, you can virtually eliminate the primary cause of fatal accidents.

Aircraft

Registration
N174CD
Reported as
Robinson Helicopter R44 II (II)
Category
Helicopter
Serial number
13863
Built
2015
Airframe hours
33.4
Engine
Lycoming IO-540-AE1A5, 225 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Operator
Over & Out Inc.
Registered owner
Over & Out Inc.
Airworthiness certificate
Standard, Normal
Departed
DZB · Horseshoe Bay, TX
Destination
23R · Devine, TX
Equipment
ADS-B

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
63
Injuries
None
Certificates
Private, Commercial, Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Without waivers/limitations
Last flight review
April 12, 2015
Seat
Front
Restraint
3-point
Flight hours
14,244 total · 366.8 in this make and model · 14,244 as pilot in command · 92 in the last 90 days · 38 in the last 30 days · 2.5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 5 knots
Visibility
10 statute miles
Temperature
86 °F, dew point 45 °F
Altimeter
30.03 inHg
Observed at
KHDO, 19 nm away

Docket · 3

The files NTSB released with the investigation on December 14, 2015, on NTSB’s docket system: statements, records, photos and specialists’ reports.

FAA reports on this event · 1

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