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April 8, 2005 · Bell OH-58C · N198PD

Colorado Sprngs, CO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 8, 2005
Injury Outcomes
No injuries (3 uninjured)
Location
Colorado Sprngs, CO
Aircraft
Bell OH-58C
Tail Number
N198PD
Injuries
None
Aircraft Damage
Substantial
NTSB Number
DEN05TA072

According to the pilot, he was orbiting over a campus when the "engine out light illuminated in the cockpit," followed by an "audible engine out alarm" and the "N1 gauge dropped." The pilot elected to perform a precautionary landing to a field. The pilot stated that the terrain sloped uphill and the helicopter stopped "abruptly" and rock back and forth. A postaccident examination revealed that the N1 Tachometer Generator had failed. Further examination revealed that the N1 tachometer generator wire was not connected to the cannon plug and frayed. Examination of the helicopter's remaining systems revealed no anomalies.

NTSB Probable Cause

the failure of the N1 tachometer generator which resulted in a precautionary landing. Contributing factors include the frayed wire and the unsuitable terrain for a precautionary landing.

Full Narrative

On April 7, 2005, approximately 1815 mountain daylight time, a Bell OH-58C, N198PD, operated by the City of Colorado Springs Police Department, was substantially damaged during a forced landing 10 miles north of Colorado Springs, Colorado. Visual meteorological conditions prevailed at the time of the accident. The local public use flight was being operated under the provisions of Title 14 CFR Part 91 without a flight plan. The commercial certificated pilot and two passengers reported no injuries. The local flight originated approximately 1800. According to the accident report submitted by the pilot, he was orbiting over a college campus when the "engine out light illuminated" in the cockpit. This light was followed by an "audible engine out alarm" and the "N1 gauge dropped." The pilot elected to perform a precautionary landing west of Interstate 25 on Air Force Academy property. The pilot stated that the terrain sloped uphill and the helicopter stopped "abruptly" and rock back and forth. Approximately 30 inches aft from the boom attach point, the boom buckled, leaving a wrinkle approximately 9 inches in length and approximately 2 inches at its deepest point. A postaccident examination revealed that the N1 tachometer generator had failed. Further examination revealed that the N1 tachometer generator wire was not connected to the cannon plug and frayed. Examination of the helicopter's remaining systems revealed no anomalies.

Flight

Event TypeAccident
Event Time18:15 MDT
Nearest Airport0nm
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell OH-58C
Tail NumberN198PD
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsRolls-Royce · Allison 250 · Turboshaft · 420
Seats4

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 41 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind30° @ 18 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point54 / 21 C
Altimeter30.29 inHg
Observation Time00:54
Weather SourceWFAC

Appendix: Source Data