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CHI97GA103 · Bell OH-58A

10 Apr 1997 · Seymour, IN, United States

Bell OH-58A · Accident: loss of control in flight while maneuvering

From Sélibaby Airport (SEY) to Sélibaby Airport (SEY)

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Event

NTSB case
CHI97GA103
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
0 · all aircraft and ground
Ground fatalities
0
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Bell OH-58A

Aircraft type
Bell OH-58
Category
Helicopter
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N132SP
Operator
Unknown
Onboard fatalities
Unknown
Route
From Sélibaby Airport (SEY)To Sélibaby Airport (SEY)
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Maneuvering · hover
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Loss of control in flight
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Aircraft weight and balance › Exceeded
  • Ground personnel › Condition(s)/step(s) in improper sequence

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

State Police personnel were using the helicopter in connection with an Emergency Response Team (ERT) static drill. The helicopter was hovering about 1 foot above ground level as 4 ERT members (2 on each side) awaited hand signals from the lead member (first) to stabilize & then (second) to board the helicopter. According to the lead member, the first signal was given for each member to grab a strap & place 1 foot on a skid to stabilize (but not board) the helicopter; however, before the second signal was given, the helicopter began quickly moving to the right. The 2 ERT members on the left side were unable 'keep up' with the helicopter as it banked/climbed, and they fell to the ground. Both right side ERT members climbed aboard the helicopter when they were unable to remain clear of its path. The helicopter continued moving right & rolled into a steep bank. It gained about 10 feet of altitude before it entered a descent & crashed. Weight & balance calculations by Bell Helicopter showed that with the weight of 2 ERT members on the right skid (& no weight on the left), the helicopter's lateral center-of-gravity (CG) limit would have been exceeded by 4.3 inches. There was a flight step above & inboard from each skid. With weight of the 2 ERT members on the right step, the CG would have been exceeded by 3.2 inches). Bell reported the pilot would not have been able to maintain lateral control in either case.

Probable cause

improper action(s) by one or more of the emergency response team members, during a hovering/loading sequence, which resulted in the helicopter's lateral center-of-gravity (CG) limitations to be exceeded. A factor associated with the accident was: the pilot's inability to maintain lateral control of the helicopter, once the lateral CG limits had been exceeded.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record CHI97GA103
Event ID
20001208X07674
Case number
CHI97GA103
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: 1eb1bade323ca9a6b94e8fd4e929948e0d61e16965d91a29fd1a5a456cb197dd; retrieved 2026-09-21T12:10:56.533Z.