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NTSB Report

April 26, 2004 · Hiller UH-12E · N9785C

Haines, OR

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 26, 2004
Injury Outcomes
1 injury (1 minor injury)
Location
Haines, OR
Aircraft
Hiller UH-12E
Tail Number
N9785C
Operator
Sundance Helicopters
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
SEA04LA073

The pilot was descending through about 100 feet above the ground at 60 knots airspeed on approach to landing when he heard a loud bang. He immediately transitioned into an autorotation but as he flared prior to touchdown he had insufficient rotor RPM and the helicopter landed hard with the main rotor blades severing the tailboom. The pilot reported that as the helicopter impacted the ground he noted the Rolls Royce (Allison) 250-C20B engine spooling up. He also stated that he did not hear any audible engine out alert during the entire sequence and that the helicopter was not equipped with an auto-relight system. A post-crash test run of the engine revealed no abnormalities. The height-velocity diagram for the helicopter indicated that a successful auto-rotation could be accomplished at an elevation of 100 feet for airspeeds of 41 knots and above.

NTSB Probable Cause

A momentary partial loss of power for undetermined reason(s) and the pilot's failure to maintain adequate RPM during his autorotation landing.

Full Narrative

On April 26, 2004, approximately 1615 Pacific daylight time, a Hiller UH-12E, N9785C, registered to/operated by Sundance Helicopters, Inc. and being flown by a commercial pilot sustained substantial damage during a hard landing following a mechanical malfunction while on short approach to landing near Haines, Oregon. The pilot suffered minor injuries. Visual meteorological conditions existed and no flight plan had been filed. The flight, which was returning from an agricultural spray run, was operated under 14 CFR 137, and had departed Elgin, Oregon, approximately 40 nautical miles north a short time before the accident. The pilot reported to the Safety Board's investigator that he departed Elgin with about 20 gallons of fuel aboard and as he was descending through about 100 feet above ground at 60 knots airspeed (refer to Attachment HV-I and HV-II) and approaching his base of operations he heard a loud bang. He immediately transitioned into an autorotation but as he flared prior to touchdown he had insufficient rotor RPM and the helicopter landed hard with the main rotor blades severing the tailboom. The pilot reported that as the helicopter impacted the ground he noted the Rolls Royce (Allison) 250-C20B engine spooling up and suspected a transmission malfunction. He also stated that he did not hear any audible engine out alert during the entire sequence and that the helicopter was not equipped with an auto-relight system. An inspector assigned to the Federal Aviation Administrations (FAA) Boise Flight Standards District Office (FSDO) examined the helicopter following the accident and found no outward evidence of any mechanical malfunction. The engine was shipped to the facilities of Rolls Royce in Indianapolis, Indiana, where it was examined. It was noted that there was no "O" ring at the base of the anti-ice valve and there was no rubber seal within the valve. The valve was replaced with a functional unit and the engine was test run. Engine performance during the test run was normal. The engine was subsequently returned to the Operator.

Flight

Event TypeAccident
Event Time16:00 PDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHiller UH-12E
Tail NumberN9785C
Aircraft CategoryHeli
DamageSubstantial
OperatorSundance Helicopters
Operating RulePart 137
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20 · Turboshaft · 400
Seats3

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 50 · Second Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind80° @ 7 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point39 C
Altimeter30.26 inHg
Observation Time22:53
Weather SourceWFAC

Appendix: Source Data