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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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March 17, 2003 · Bell 430 · N431UM

Highland, MI

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 17, 2003
Injury Outcomes
No injuries (1 uninjured)
Location
Highland, MI
Aircraft
Bell 430
Tail Number
N431UM
Operator
Cj System Aviation Group
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI03LA084

The helicopter was substantially damaged when the tail rotor impacted a roadway sign while repositioning at night for departure. The medical evacuation flight had landed on a roadway to pick-up a patient. The medical crew had departed the helicopter prior to the reposition. The pilot was the only occupant on-board at the time. The pilot reported he began to taxi. He stated he "cleared the tail to move left into the turn around along M-59. I started to move the aircraft which now was facing south into M-59 ... when the tail rotor hit a steel reflector post. The aircraft became airborne to around five or six feet when I lowered the collective and rolled the throttles to idle to stop the aircraft rotation." The aircraft impacted on the left rear skid first and came to rest one-hundred eighty degrees from its initial heading. A post-accident examination revealed the tail rotor and gearbox had departed the helicopter. The pilot reported there were no mechanical malfunctions with the helicopter prior to the accident.

NTSB Probable Cause

The pilot's failure to maintain clearance to the roadway sign. Contributing factors were the failure of the tail rotor gearbox, the roadway sign and the low lighting conditions (night).

Full Narrative

On March 16, 2003, at 2015 eastern standard time, a Bell 430 helicopter, N431UM, piloted by an airline transport pilot, was substantially damaged when the tail rotor impacted a roadway sign during an aerial taxi. The accident occurred on Highway M-59, east of US Highway 23, near Highland, Michigan. Visual meteorological conditions prevailed at the time of the accident. The medical evacuation flight was operating under the provisions of 14 CFR Part 135 and was not on a flight plan. The pilot was the sole occupant at the time of the accident. He reported no injuries. The flight departed the University of Michigan Medical Center Heliport (MI32), Ann Arbor, Michigan, at 1959 est, with the intention of returning to MI32 after picking up a patient. According to the pilot's statement, he overflew the area from west to east to review the landing site. He stated that he reversed course and approached the landing site from the east. Prior to touchdown the pilot reported he rotated the aircraft and landed on an easterly heading, at which point the medical crew departed the helicopter. The pilot decided to reposition the aircraft to face west for departure. After notifying local authorities and clearing the helcopter, he reported he began to taxi to the east. He stated he "cleared the tail to move left into the turn around along M-59. I started to move the aircraft which now was facing south into M-59 ... when the tail rotor hit a steel reflector post. The aircraft became airborne to around five or six feet when I lowered the collective and rolled the throttles to idle to stop the aircraft rotation." The aircraft impacted on the left rear skid first and came to rest one-hundred eightly degrees from its initial heading. A post-accident examination revealed the tail rotor and gearbox had departed the helicopter. The pilot reported there were no mechanical malfunctions with the helicopter prior to the accident.

Flight

Event TypeAccident
Event Time20:15 EST
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 430
Tail NumberN431UM
Aircraft CategoryHeli
DamageSubstantial
OperatorCj System Aviation Group
Operating RulePart 135
Engines2
Engine TypeTurboshaft
Engine DetailsRolls-Royce · 250-C40 · Turboshaft · 1300 | Rolls-Royce · 250-C40 · Turboshaft · 1300

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 53 · Second Class · None

Conditions

ConditionsVMC
LightNight
Wind170° @ 4 kt
Visibility6 sm
CeilingOvercast 22000 ft
Temperature / Dew Point55 / 52
Altimeter29.81 inHg
Observation Time00:53
Weather SourceWFAC

Appendix: Source Data