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ASN Wikibase Occurrence # 215944
Last updated: 18 November 2019
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Date:01-JUL-1986
Time:15:00
Type:Silhouette image of generic BE58 model; specific model in this crash may look slightly different
Beechcraft 58
Owner/operator:
Registration: VH-REH
C/n / msn:
Fatalities:Fatalities: 0 / Occupants: 4
Other fatalities:0
Aircraft damage: Substantial
Location:5km E of Lawlers, WA -   Australia
Phase: Landing
Nature:Domestic Non Scheduled Passenger
Departure airport:YLAW
Destination airport:YPKG
Investigating agency: BASI
Narrative:
As the aircraft was accelerating to the normal climbing speed after takeoff, the pilot lost elevator control. The nose continued to pitch up until the pilot closed the throttles. He then discovered that he could maintain limited pitch control by the judicious use of power. A successful gear-up forced landing was made, however, during the landing slide one wing was torn off after it struck a tree. An inspection of the elevator control system revealed that its control cable had been incorrectly engaged into the control column fork. While the locking pin was fitted correctly, it was rendered ineffective due to the incorrect fitment of the cable. Despite numerous maintenance inspections this error went undetected. Due to the location of the control column fork, the pilot would not have been expected to notice the unserviceability on his daily inspection.

Sources:

https://www.atsb.gov.au/publications/investigation_reports/1986/aair/aair198600141/
https://www.atsb.gov.au/media/32335/aair198600141.pdf

Accident investigation:
cover
  
Investigating agency: BASI
Status: Investigation completed
Duration:
Download report: Final report


Revision history:

Date/timeContributorUpdates
02-Oct-2018 12:55 Pineapple Added

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