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Aviation safety reports, made easier to study

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NTSB Report

October 24, 1998 · Hiller UH-12C · N9739C

Clinton, IA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
October 24, 1998
Injury Outcomes
No injuries (2 uninjured)
Location
Clinton, IA
Aircraft
Hiller UH-12C
Tail Number
N9739C
Operator
Aerocraft Helicopter
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI99LA012

During cruise flight the helicopter suffered a loss of tail rotor authority. The pilot initiated an autorotational landing; however, during the approach he lost all control of the aircraft. An inspection of the tail rotor gearbox after the accident revealed a failure of the 90 degree gearbox. The log books indicated an overhaul 195 hours prior to the accident with no other maintenance on the gearbox noted. An inspection of the helicopter was conducted one month prior to the accident and the helicopter had accumulated about 33 hours since that inspection.

NTSB Probable Cause

the failure of the 90 degree gearbox for reasons undetermined. Factors were the failure of the gearbox, and it not being possible for the pilot to maintain control of the aircraft.

Full Narrative

On October 24, 1998, at 1130 central daylight time, a Hiller UH-12C, N9739C, owned by a corporation and operated by a commercial pilot, sustained substantial damage during a forced landing four miles east of the Clinton Municipal Airport, near Clinton, Iowa. The pilot said that he lost tail rotor control and initiated an autorotational landing into a field. He and the passenger reported no injuries. The 14 CFR Part 91 sightseeing flight was operating in visual meteorological conditions. No flight plan was on file. The local flight departed Clinton about 1120. An examination of the helicopter after the accident revealed that the "90 degree" gearbox had suffered a failure of the internal gears. When disassembled it was determined that the drive gear and the pinion gear in the transmission were both missing teeth. A check of the maintenance log books for the helicopter indicated that the last overhaul and maintenance on the "90 degree" gearbox occurred 195 hours prior to the failure. The helicopter had received an inspection the month prior to the accident with no note of maintenance on the gearbox or gears. The helicopter had accumulated about 33 hours since the most recent inspection.

Flight

Event TypeAccident
Event Time11:30 CDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHiller UH-12C
Tail NumberN9739C
Aircraft CategoryHeli
DamageSubstantial
OperatorAerocraft Helicopter
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsFranklin · 6V335-50 · Reciprocating · 210

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 26 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind210° @ 6 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point64 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data