FTW86LA164

NTSB accident investigation · Hiller FH-1100 · Abilene, TX · September 6, 1986

Accident · No injuriesLimited investigationFinal report
Date
September 6, 1986, 18:30 local (23:30 UTC)
Place
Abilene, TX
Injuries
6 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N5068FHiller FH-1100
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Safety recommendations
Yes
FAA report
19860906045999A
Case key
22088

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionTakeoff - initial climb
Rotor system,tail rotor blade cuff - contaminationCause
Maintenance - inadequateOther maintenance personnelFactor
Rotor system,tail rotor blade cuff - stress corrosionCause
Rotor system,tail rotor blade - separationCause
Loss of control - in flightTakeoff - initial climb
Directional control - not possible
Forced landingDescent - emergency
Autorotation - attemptedPilot in command
In flight collision with terrain/waterLanding

Analysis

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.

Aircraft

Registration
N5068F
Reported as
Hiller FH-1100
Category
Helicopter
Serial number
227
Airframe hours
2,530
Engine
Allison 250-C18, 274 horsepower, turbo shaft
Damage
Substantial damage
Fire
On-Ground
Flight
Part 91
Registered owner
Jack O. Canon
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · March 22, 1986 · 68 hours before
Departed
AB1
Destination
AB1
Airport
ABI · Abilene

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
60
Certificate
Commercial
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
4,870 total · 236 in this make and model · 4,315 as pilot in command · 39 in the last 90 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
30° at 8 knots
Visibility
30 statute miles
Lowest ceiling
None
Temperature
82 °F, dew point 63 °F
Altimeter
30.00 inHg
Observed at
AB1, 3 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N5068F · 1

Matched to the same aircraft by N-number and date.