- Date
- February 4, 2011, 14:22 local (22:22 UTC)
- Place
- Elverta, CA
- Injuries
- 2 minor
- Damage
- Substantial damage
- Phase of flight
- Maneuvering
- Aircraft
- N416WCMcDonnell Douglas Helicopters 369E (MD500E)
- Defining event
- Maneuvering-hover: Low altitude operation/event
- Weather
- Visual (VMC) · Dawn
- Status
- Completed · report March 28, 2012
- Report
- Approved by Office Director
- NTSB office
- Western Pacific Region
- Parties
- Wilson Construction, Rolls-Royce, FAA FSDO, Boeing
- FAA report
- 20110204002599A
- Case key
- 78282
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 did not maintain rotor blade clearance from an installation rope while maneuvering to install 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.
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
A lineman was on the skid of the helicopter installing high-power electrical lines on a power line structure. The pilot positioned the helicopter about 30 to 50 feet from the structure. The main rotor blades made contact with an installation rope, which then wrapped around the mast as the blades pulled it in. The pilot lost control of the helicopter, and it began an uncontrolled descent to the ground. A postaccident examination of the airframe and engine revealed no mechanical anomalies that would have precluded normal operation. It is likely that the pilot misjudged the distance between the rotor blades and the installation rope.
Factual narrative
HISTORY OF FLIGHT On February 4, 2011, about 1422 Pacific standard time, a McDonnell Douglas Helicopters 369E (MD500E), N416WC, became entangled with a sock line rope used to string power lines near Elverta, California. Wilson Construction Company was operating the helicopter under the provisions of 14 Code of Federal Regulations (CFR) Part 133. The commercial pilot and one passenger sustained minor injuries; the helicopter sustained substantial damage to the airframe and main rotor blades. Visual meteorological conditions prevailed, and no flight plan had been filed. The operator reported that the helicopter was working on a project to construct 30 miles of high power electrical lines, which are oriented north-south. It is not possible to pull the conductor wire through bundled travelers unless the sock line is actually in contact with the roller. Construction crews install a hold down, which is a temporary block that they secure to a ground anchor. They adjust the anchor rope to force the sock line to rest in the bundle block traveler when in tension. The operator noted that it is standard industry practice to use a helicopter to install a hold down. A lineman was on the skid of the helicopter, which was in position to install a hold down at a power line structure. The pilot positioned the helicopter about 30-50 feet south of the structure; his flagman was facing the west. The pilot believed that he was properly positioned near the sock line so that they could perform the task safely. The lineman on the skid placed the larger of the two hold down ropes over the sock line, and allowed it to fall onto the west side. The lineman allowed the hold down block to hang by the large rope just below and on the east side of the sock line. The large rope tangled as it fell to the ground. The lineman on the ground grabbed the end of the rope, and tried to clear the tangle. The lineman on the skid had one hand on the hold down, and was preparing to release the second, smaller rope downward on the western side of the sock line with the other hand. The main rotor blades made contact with the sock line rope, which wrapped around the mast as the blades pulled it in. The pilot lost control of the helicopter, and it began an uncontrolled descent to the ground. The helicopter came to rest upright about 10 feet south of the power line structure. The lineman on the skid was lying on the ground, but still attached to the helicopter by her fall restraint and positioning belt. The pilot extricated himself from the helicopter. TESTS AND RESEARCH Investigators from the FAA, Boeing, and Rolls-Royce Allison (RR) examined the wreckage at the operator’s facilities at McLellan Airfield, Sacramento, California, on February 9, 2011. The investigators examined the airframe and engine, with no mechanical anomalies identified that would have precluded normal operation.
Aircraft
- Registration
- N416WC
- Reported as
- McDonnell Douglas Helicopters 369E (MD500E)
- Category
- Helicopter
- Serial number
- 0268E
- Airframe hours
- 6,256
- Engine
- Rolls-Royce Allison 250-C20B, 420 horsepower, turbo shaft
- Damage
- Substantial damage
- Flight
- Other work use · Part 133
- Operator
- Wilson Construction Company
- Registered owner
- Wilson Construction Company
- Airworthiness certificate
- Standard, Normal
- Last inspection
- 100 hour · January 26, 2011
- Departed
- Elverta, CA
- Destination
- Elverta, CA
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 57
- Injuries
- Minor
- Certificate
- Commercial
- Instrument ratings
- Helicopter
- Medical
- Class 2, With waivers/limitations
- Last flight review
- February 11, 2010
- Seat
- Left
- Flight hours
- 22,500 total · 17,600 in this make and model · 22,500 as pilot in command · 75 in the last 90 days · 20 in the last 30 days · 5 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Dawn
- Wind
- Calm
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 59 °F, dew point 43 °F
- Altimeter
- 30.30 inHg
- Observed at
- KSMF, 6 nm away
Docket · 4
The files NTSB released with the investigation on February 13, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.4 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.