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NTSB Report

October 8, 2009 · Schweizer 269C-1 · N1835E

Lewiston, ME

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
October 8, 2009
Injury Outcomes
No injuries (2 uninjured)
Location
Lewiston, ME
Aircraft
Schweizer 269C-1
Tail Number
N1835E
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ERA10CA010

The pilot of a helicopter was conducting a non-revenue sightseeing flight for one passenger. After lifting off, the pilot stated that he was hovering eastbound with the winds out of the west. A METAR taken on the airport approximately 5 minutes before the accident indicated the wind was from 340 degrees at 11 knots with gusts to 16 knots. The pilot further stated that the helicopter’s nose made a sudden yaw to the right, which could not be corrected with reduction of throttle and full left pedal application. The helicopter touched down after a 270 degree turn, came to rest upright, with substantial damage to the main rotor blades, skids and tailboom. According to a Federal Aviation Administration Advisory Circular (AC) 90-95 titled "Unanticipated Right Yaw in Helicopters", operation of a helicopter with a tailwind as reported by the pilot or with a left quartering tailwind as determined by the METAR and the pilot's statement can result in unanticipated right yaw or loss of tail rotor effectiveness (LTE).

NTSB Probable Cause

Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Yaw control-Attain/maintain not possible

Full Narrative

The pilot of a helicopter was conducting a non-revenue sightseeing flight for one passenger. After lifting off, the pilot stated that he was hovering eastbound with the winds out of the west. A METAR taken on the airport approximately 5 minutes before the accident indicated the wind was from 340 degrees at 11 knots with gusts to 16 knots. The pilot further stated that the helicopter’s nose made a sudden yaw to the right, which could not be corrected with reduction of throttle and full left pedal application. The helicopter touched down after a 270 degree turn, came to rest upright, with substantial damage to the main rotor blades, skids and tailboom. According to a Federal Aviation Administration Advisory Circular (AC) 90-95 titled "Unanticipated Right Yaw in Helicopters", operation of a helicopter with a tailwind can result in unanticipated right yaw or loss of tail rotor effectiveness (LTE).

Flight

Event TypeAccident
Event Time09:00 EDT
Nearest AirportAuburn/Lewiston Municipal Airp (0nm)
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftSchweizer 269C-1
Tail NumberN1835E
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360-G1A · Reciprocating · 180
Seats3

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 62 · None · None

Conditions

ConditionsVMC
LightDaylight
Wind340° @ 11 kt, gusting 16 kt
Visibility10 sm
CeilingOvercast 3700 ft
Temperature / Dew Point52 / 39 C
Altimeter29.86 inHg
Observation Time12:55
Weather SourceWFAC

Appendix: Source Data