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NTSB Report

September 11, 2013 · Bell 47G5 · N7836S

King City, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 11, 2013
Injury Outcomes
No injuries (1 uninjured)
Location
King City, CA
Aircraft
Bell 47G5 (1967)
Tail Number
N7836S
Operator
Wilbur-Ellis
Injuries
None
Aircraft Damage
Substantial
NTSB Number
WPR13LA404

The pilot reported that he was flying low over a field when he heard a "loud bang." He initiated a precautionary landing, during which, the helicopter started to spin. The pilot lowered the collective, and the helicopter subsequently landed hard on a road. Postaccident examination of the helicopter structure revealed that one of the center frame tubes, located just aft of the cabin, had separated due to a fracture. Examination of the fracture surface revealed that a fatigue fracture initiated in the tube at the root of a fillet weld associated with a reinforcing fillet welded axially along the tube. The fatigue crack propagated through the thickness of the tube and circumferentially around the tube from both sides of the weld root. Darker corrosion product found on the fracture face indicated that the preexisting fatigue crack had been exposed to atmospheric elements. The tube fracture occurred in single-sided bending consistent with in-flight airframe loads. The helicopter's most recent 100-hour inspection occurred about 1 month before the accident. According to manufacturer's guidance, the 100-hour inspection required, in part, an inspection of all structural tubing and fittings for cracks, cuts, bends, corrosion, distortion, and damage. If maintenance personnel had adequately inspected this area, they might have identified the degradation of the tube.

NTSB Probable Cause

The failure of the helicopter’s center frame tube due to a fatigue crack and corrosion originating from a welded surface. Contributing to the accident was maintenance personnel’s inadequate inspection of the helicopter during its most recent 100-hour inspection.

Full Narrative

On September 11, 2013 about 0715 Pacific daylight time, a Bell 47G5 helicopter, N7836S, sustained substantial damage during a precautionary landing about 6 miles southeast of King City, California. The pilot, the sole occupant, was not injured. The helicopter's lower center frame and tailboom sustained substantial damage. The helicopter was registered to and operated by Wilbur-Ellis Corporation as an agricultural spray flight under the provisions of 14 Code of Federal Regulations Part 137. Visual meteorological conditions prevailed for the flight and no flight plan was filed. The pilot reported that he was spraying a field about 3-4 feet above the ground when he heard a loud bang. The pilot elected to make a precautionary landing; during the landing flare, the helicopter started to spin. The pilot lowered the collective and the helicopter landed hard onto a road; subsequently, the helicopter's skids spread, and the lower center frame and tailboom were bent. Postaccident examination by a Federal Aviation Administration (FAA) inspector revealed that one of the helicopter's center frame tubes, located just aft of the cabin, had fracture separated. A senior metallurgist at the National Transportation Safety Board (NTSB) materials laboratory reviewed photographs of the fractured surfaces and reported that a fatigue fracture initiated in the tube at the root of a fillet weld associated with a reinforcing filet welded axially along the tube. The fatigue crack propagated through the thickness of the tube and circumferentially around the tube from both sides of the weld root. Darker corrosion product on the fracture face is indicative of a pre-existing fatigue crack that had been exposed to atmospheric elements. The fracture in the tube occurred in single-sided bending consistent with inflight airframe loads. On August 8, 2013 the helicopter underwent a 100 hour inspection. According to manufacturer's guidance, the 100 hour inspection requires in part: to "Inspect all structural tubing and fittings for cracks, cuts, bends, corrosion, distortion and damage."

Flight

Event TypeAccident
Event Time07:15 PDT
Nearest AirportMesa Del Rey Airport (6nm SE)
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 47G5
Tail NumberN7836S
Aircraft CategoryHeli
DamageSubstantial
OperatorWilbur-Ellis
Operating RulePart 137
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · VO-435 SERIES · Reciprocating · 260
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 58 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind320° @ 4 kt
Visibility10 sm
CeilingOvercast 1700 ft
Temperature / Dew Point63 F / 55
Altimeter30.00 inHg
Observation Time14:53
Weather SourceWFAC

Appendix: Source Data