19840716032779A

Accident · Substantial damage

FAA accident report · Hiller OH23G · Redmond, OR · July 16, 1984

Date
July 16, 1984 · 07:20 local
Place
Redmond, OR
Phase of flight
Low Level Operations
Operating rules
Agricultural (Part 137)
Damage
Substantial damage
Aircraft
N1043L
NTSB investigation
NTSBSEA84LA174
Reported as
Hiller OH23G
Reported engine
Lycoming VO540C2A
Fatal injuries
0
Pilot’s flight hours
5,400 total5,400 in this make and model100 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Main rotor blade seperated from the helicopter during a spray run. Cause high stress and low cycle fatigue.

As the FAA filed it

MAIN ROTOR BLADE SEPERATED FROM THE HELICOPTER DURING A SPRAY RUN. CAUSE HIGH STRESS AND LOW CYCLE FATIGUE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.