Summary
On July 07, 1994, a Robinson R-22M (N42WC) was involved in an incident near Portland, OR. All 2 people aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: TAIL ROTOR GEARBOX FAILURE DUE TO INADEQUATE ASSEMBLY AND INSPECTION PROCEDURES BY THE MANUFACTURER.
On July 7, 1994, at 1125 Pacific daylight time, a Robinson R-22M, N42WC, sustained substantial damage during an autorotational forced landing to Ross Island beach, Portland, Oregon. The student pilot and certified flight instructor sustained minor injuries. No flight plan was filed for the instructional flight, which had departed Hillsboro, Oregon about 1105.
The pilot stated that he had lost tail rotor effectivness and attempted an autorototation from about 75 feet AGL. The pilot stated that the aircraft continued turning through two or three rotations before toching down.
This incident is documented in NTSB report SEA94LA171. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N42WC.
Accident Details
Probable Cause and Findings
TAIL ROTOR GEARBOX FAILURE DUE TO INADEQUATE ASSEMBLY AND INSPECTION PROCEDURES BY THE MANUFACTURER.
Aircraft Information
Registered Owner (Current)
Analysis
On July 7, 1994, at 1125 Pacific daylight time, a Robinson R-22M, N42WC, sustained substantial damage during an autorotational forced landing to Ross Island beach, Portland, Oregon. The student pilot and certified flight instructor sustained minor injuries. No flight plan was filed for the instructional flight, which had departed Hillsboro, Oregon about 1105.
The pilot stated that he had lost tail rotor effectivness and attempted an autorototation from about 75 feet AGL. The pilot stated that the aircraft continued turning through two or three rotations before toching down. The aircraft landed near shoreline, with the tail rotor and boom striking the water.
Inspection revealed that the tail rotor gearbox (P/N A021-1) output shaft pinion (A545-1) retaining key (A114-2) was not installed at the time of factory assembly, allowing the tail rotor hub and blade to become disengaged.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA94LA171