Accident Hiller FH-1100 N5068F,
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ASN Wikibase Occurrence # 374259
 
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Date:Saturday 6 September 1986
Time:18:30 LT
Type:Silhouette image of generic FH11 model; specific model in this crash may look slightly different    
Hiller FH-1100
Owner/operator:Private
Registration: N5068F
MSN: 227
Total airframe hrs:2530 hours
Engine model:Allison 250-C18
Fatalities:Fatalities: 0 / Occupants: 6
Aircraft damage: Substantial
Category:Accident
Location:Abilene, TX -   United States of America
Phase: Initial climb
Nature:Unknown
Departure airport:(AB1)
Destination airport:(AB1)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
THE PLT WAS CONDUCTING SIGHT-SEEING FLTS FROM A RODEO/FAIRGROUND AREA. DURING A CRITICAL PART OF A TAKEOFF, A TAIL ROTOR BLADE SEPARATED & THE PLT LOST DIRECTIONAL CONTROL. HE ATTEMPTED AN AUTOROTATIVE LANDING. AFTER SPINNING AROUND ABOUT 3 TIMES, THE PLT PULLED FULL COLLECTIVE, JUST BEFORE THE HELICOPTER CRASHED, BUT IT WAS STILL BADLY DAMAGED. AN INVESTIGATION REVEALED THAT A TAIL ROTOR TENSION-TORSION (T-T) BAR ASSEMBLY, PN 24-55106, HAD FAILED WHERE THE ATTACHMENT BOLT GOES THRU THE T-T STRAPS. A METALLURGICAL EXAM REVEALED CHLORINE RICH DEPOSITS IN THE FRACTURE AREA. THE GREASE FROM THE T-T BAR CAVITY HAD DARKENED & THE CAVITY FOR THE OTHER SET OF T-T STRAPS CONTAINED A SMALL AMOUNT OF FLUID WITH AN UNPLEASANT ODOR. AN ANALYSIS OF THE GREASE REVEALED EXCESSIVE AMOUNTS OF CHLORINE. THERE WAS EVIDENCE THAT WATER & CHLORINE CONTAMINATION HAD RESULTED IN STRESS CORROSION & EVENTUAL FAILURE OF THE T-T BAR ASSEMBLY.

Probable Cause:

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: FTW86LA164
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB FTW86LA164

Revision history:

Date/timeContributorUpdates
28-Mar-2024 07:34 ASN Update Bot Added

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