LAX92LA108

NTSB accident investigation · Sikorsky S55B · Richvale, CA · February 4, 1992

Accident · Serious injuriesLimited investigationFinal report
Date
February 4, 1992, 09:30 local (17:30 UTC)
Place
Richvale, CA
Injuries
1 serious, 1 uninjured; on the ground: 1 serious
Damage
Substantial damage
Phase of flight
Standing
Aircraft
N1033Sikorsky S55B
Weather
Visual (VMC) · Day
Status
Completed · report June 11, 1993
Report
Approved by Office Director
FAA report
19920204001839A
Case key
27550

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 failure of the lateral control arm in the cyclic control system.

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.

Airframe/component/system failure/malfunctionStanding - engine(s) operating
Rotorcraft flight control,cyclic control rod - fracturedCause
Roll overStanding - engine(s) operating
Aircraft control - not possiblePilot in command

Analysis

As the helicopter was being refueled in preparation for an aerial application flight, the pilot was in the helicopter and the main rotor blades were rotating at 'flight RPM.' According to the pilot, the helicopter suddenly 'jumped about two feet in the air and at the same time rolled to the right and moved forward.' The main rotor blades struck the fuel truck and the helicopter rolled over. An examination of the helicopter's structure revealed that the lateral control arm component in the cyclic control system had fractured at a taper pin hole. Thereafter, the disconnected cyclic control system permitted the main rotor blades to tilt down, and the roll over was unavoidable. No pre-existing defect was reported observed in the lateral control arm when the helicopter was previously inspected, about 14 operational hours prior to the accident.

Aircraft

Registration
N1033
Reported as
Sikorsky S55B
Category
Helicopter
Serial number
1328
Airframe hours
5,616
Engine
Curtis Wright R-1300, 800 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Operator
Avag Corporation
Registered owner
Avag Corporation
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · October 10, 1991 · 89 hours before
Airport
O97 · Richvale

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
Certificates
Airline transport, Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
22,020 total · 6,200 in this make and model · 20,500 as pilot in command · 120 in the last 90 days · 50 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
340° at 10 knots, gusting 10
Visibility
50 statute miles
Lowest ceiling
None
Temperature
57 °F
Altimeter
30.00 inHg

FAA reports on this event · 1

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