Incident Sikorsky S-92A N920AL,
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ASN Wikibase Occurrence # 183672
 
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Date:Wednesday 19 January 2011
Time:11:34 LT
Type:Silhouette image of generic S92 model; specific model in this crash may look slightly different    
Sikorsky S-92A
Owner/operator:Bristow US LLC
Registration: N920AL
MSN: 920088
Year of manufacture:2008
Total airframe hrs:1248 hours
Engine model:GE CT7-8A
Fatalities:Fatalities: 0 / Occupants: 18
Aircraft damage: Minor
Location:Galliano, LA -   United States of America
Phase: Approach
Nature:Offshore
Departure airport:Offshore Installation, Gulf of Mexico
Destination airport:Galliano, LA (2LS0)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
During the initial approach, as the airspeed decreased through about 70 knots, the helicopter began an uncommanded right yaw of more than 100 degrees, and the yaw could not be stopped by the application of left pedal. The crew diverted to a nearby airport and performed a successful roll-on landing, touching down at 72 knots using differential braking to maintain the runway heading. An after-landing inspection showed that the tail rotor pitch change beam retaining nut, pitch beam retaining washer, and associated screws and washers were missing. The remainder of the tail rotor assembly remained attached and did not depart the helicopter.

Recent maintenance had been performed to replace the pitch change beam retaining nut and pitch beam retaining washer. According to maintenance personnel, the maintenance had been performed per the existing maintenance procedures, and the mechanics did not notice anything odd or out of place. Evidence of witness marks along with plastic deformation on the end faces of the pitch change shaft splines is consistent with the retaining washer installed with its indexing spline slightly off, resulting in a cocking condition and incomplete engagement of the spline teeth. Accordingly, there was likely an improper alignment of the components during reassembly, which would have prevented the nut from locking in place. Subsequent tests on an exemplar assembly showed that it was possible for the pitch beam retaining washer to be misaligned with the teeth on the shaft splines, which then showed barely visible evidence of the misalignment.
Probable Cause: The misalignment of the retaining washer during routine maintenance, resulting in the subsequent separation of the washer and nut.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN11IA156
Status: Investigation completed
Duration: 2 years
Download report: Final report

Sources:

NTSB

History of this aircraft

Other occurrences involving this aircraft
5 July 2016 LN-OND Bristow Norway AS 0 Stavanger Airport, Sola sub

Location

Revision history:

Date/timeContributorUpdates
17-Jan-2016 23:59 Aerossurance Added
21-Dec-2016 19:30 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
27-Nov-2017 18:06 ASN Update Bot Updated [Cn, Operator, Other fatalities, Departure airport, Destination airport, Source, Narrative]
12-Dec-2017 08:32 Aerossurance Updated [Time, Operator, Other fatalities, Departure airport]

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