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Aviation safety reports, made easier to study

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May 3, 2011 · Aerospatiale AS350B2 · N916AM

Camden, SC

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 3, 2011
Injury Outcomes
No injuries (2 uninjured)
Location
Camden, SC
Aircraft
Aerospatiale AS350B2
Tail Number
N916AM
Operator
Air Methods
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ERA11LA278

The instructor pilot had completed two night training flights in the helicopter, which included rapid decelerations, autorotations (including standard, hovering, and turning), sloping ground landings, and simulated hydraulic failures. The instructor pilot reported that at no time during the flights did he experience a hard landing or ground contact with the lower fin tail guard; however, a subsequent inspection revealed damage to the tailboom and tail rotor gearbox that was consistent with a hard landing. In addition, the lower fin tail guard contained fresh ground-contact marks, which were not present prior to the training flights.

NTSB Probable Cause

The instructor pilot did not maintain adequate helicopter control while maneuvering, which resulted in a hard landing.

Full Narrative

On May 3, 2011, sometime between 0130 and 0355 eastern daylight time, an Aerospatiale AS350B2, N916AM, operated by Air Methods Corp., was substantially damaged while maneuvering at Woodward Field, Camden, South Carolina. The two certificated airline transport pilots were not injured. Night visual meteorological conditions prevailed and no flight plan was filed for the local flight. The training flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. According to a Federal Aviation Administration (FAA) inspector and the Operator, the helicopter was being utilized for night vision goggle training. Two training flights were conducted between 2130 on May 2, and 0355 on May 3, 2011. According to the instructor pilot, both training flights comprised of similar maneuvers and profiles, which included rapid decelerations, standard autorotations, hovering autorotations, autorotations with turns, sloping ground landings, and simulated hydraulic failures. The instructor pilot stated that the helicopter was inspected prior to the second training flight, which began about 0130, and no discrepancies were noted. He further stated: "…At no time during both training flights did any maneuver feel nor indicate either a heavy landing, or contact between the tail fin stinger and the ground. No abnormal vibrations were experienced throughout the evening training events…." Subsequent inspection of the helicopter by an FAA inspector and a company mechanic revealed that the tail boom was buckled about 42-inches in front of the horizontal stabilizer. In addition, the tail rotor gearbox input seal was excessively leaking oil, and the tail fin stinger, which is reference by Eurocopter as the lower fin tail guard, contained fresh ground contact marks. The mechanic noted that no damage was present during an inspection he performed about 1900 on May 2, 2011. In addition, the mechanic reported that a postaccident landing gear "spread check" was within manufacturer specifications; however, there were no previous measurements taken on the accident helicopter that could be used for comparison purposes.

Flight

Event TypeAccident
Event Time02:45 EDT
Nearest AirportWoodward Field (0nm)
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftAerospatiale AS350B2
Tail NumberN916AM
Aircraft CategoryHeli
DamageSubstantial
OperatorAir Methods
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsTurbomeca · Arriel 1D1 · Turboshaft · 712
Seats6

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 49 · Second Class · None
Crew 2Age 49 · Second Class · None

Conditions

ConditionsVMC
LightNight
Wind190° @ 4 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point70 F / 64 F
Altimeter30.17 inHg
Observation Time06:35
Weather SourceWFAC

Appendix: Source Data