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Aviation safety reports, made easier to study

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December 4, 1996 · Hughes 269C · N1105P

Mayfield, KY

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 4, 1996
Injury Outcomes
No injuries (2 uninjured)
Location
Mayfield, KY
Aircraft
Hughes 269C
Tail Number
N1105P
Injuries
None
Aircraft Damage
Substantial
NTSB Number
IAD97LA028

The pilot stated that the purpose of the flight was to ferry the helicopter. The helicopter had been cruising at 1,200 feet MSL for over an hour, when the nose started to yaw to the right. Unable to control the yaw, the pilot entered an autorotation at about 70 mph to a field. During the forced landing, the helicopter collided with a fence. Examination of the helicopter revealed that the aft pinion nut of the main transmission had disengaged, which allowed the tail rotor splined drive sleeve to disengage from the pinion and tail rotor drive shaft. Investigation did not determined why the aft pinion backed off. The last annual inspection was completed on 6/7/96. The helicopter had accumulated 66 hours of flight time, since the annual inspection.

NTSB Probable Cause

disengagement of the main transmission aft pinion nut, allowing the tail rotor splined drive sleeve to disengage from the pinion, which resulted in loss of directional control and an emergency (autorotative) landing.

Full Narrative

On December 4, 1996, at 1635 eastern standard time, a Hughes 269C, N1105P, was substantially damaged when it collided with a fence during a forced landing near Mayfield, Kentucky. The certificated commercial pilot and passenger were not injured. Visual meteorological conditions prevailed and a flight plan was not filed. The ferry flight was conducted under 14 CFR Part 91, and originated in Henning, Tennessee, at 1530. The intended destination was Indianapolis, Indiana. The pilot reported that he was ferrying the helicopter to the new owner. He said that the had been cruising at 1,200 feet MSL for about an hour, when the nose of the helicopter began to yaw to the right, followed by a change in aircraft noise. He attempted to correct the yaw by applying full left pedal, but was unsuccessful. He entered autorotation at about 70 mph, and attempted a forced landing to the middle of a field. During touchdown, the helicopter collided with a fence. The helicopter was examined after the accident by an FAA Inspector. The examination revealed that the aft pinion nut of the main transmission disengaged during flight, which disengaged the tail rotor splined drive sleeve from the pinion, and the tail rotor drive shaft. It was not determined why the aft pinion nut backed off causing the drive spline to disengage. The last annual inspection was completed on June 7, 1996, and the helicopter had accumulated 66 hours since the annual inspection.

Flight

Event TypeAccident
Event Time15:35 CST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 269C
Tail NumberN1105P
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360-D1A · Reciprocating · 190
Seats2

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 32 · Second Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point39 C / 36 C
Altimeter30.00 inHg
Weather SourcePILO

Appendix: Source Data