Investigation Report

Super Puma Rejected Takeoff Following Rotor Spindle Fatigue Failure

AAIBAir Accidents Investigation BranchAAR 7/2010

AAR 7-2010 G-PUMI

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Summary

Investigation of a Super Puma takeoff rejection at Aberdeen Airport following rotor spindle fatigue failure. Metallurgical examination, finite element modelling, fatigue tests and flight-load measurements examined assembly preload, wear and interference-fit stresses. The report describes revised spindle assembly arrangements and recommends reviewing options to extend helicopter health and usage monitoring into rotating systems.

Topics

About This Record
Original title
AAR 7-2010 G-PUMI
Publisher
Air Accidents Investigation Branch
Type
Investigation Report
Reference
AAR 7/2010
Date
10 December 2014
Topic
Material Fatigue, Mechanical Failure
Activity
Helicopter Operations, Inspection and Maintenance
Equipment
Helicopter, Rotating Machinery
Control
Operating and Work Procedures, Preventive Maintenance
Sector
Upstream Oil and Gas
Setting
Onshore Facility
Link
Checked , working
Record
aaib-aar-7-2010 · added 2 October 2026

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