Casualties unknown

Helicopter Suffers Main Rotor Separation During Low-Level Flight (N1345Q)

Stevensville, MD, US

On April 26, 1998, a Fairchild Hiller FH-1100 (registration N1345Q) was involved in an aviation accident near Stevensville, MD. Investigators recorded the probable cause as: The pilot's abrupt, low-g maneuver, which resulted in mast bumping and separation of the main rotor system. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

A helicopter on a local photo flight experienced a main rotor hub separation after abrupt maneuvers, with the rotor assembly found 190 feet from the main wreckage. The mast fracture showed overload and no fatigue; records indicated unqualified maintenance and missing caution panel bulbs.

Accident Overview

Two pilots departed on a local flight to photograph waterfront real estate. Witnesses described the helicopter performing abrupt maneuvers at low level near their homes. A witness in close proximity to the accident site reported, "The rotor flew off and the blade hit the cabin side...It was at a hover. The nose angled up, the rotor hit the cabin, and the person came out. The nose pitched up before the blade hit the cabin...There was engine noise all along."

Wreckage Examination

The main rotor hub and blade assembly, with the top portion of the main rotor mast attached, was located approximately 190 feet prior to the main wreckage. The mast fracture was aligned with the bottom of the hub at the static stops and exhibited overload fractures with no evidence of fatigue.

Maintenance and Documentation Issues

No historical records existed for the helicopter. Examination of records revealed the annual inspection and airworthiness certificate were signed and produced by an unqualified person. The owner/operator signed off overhaul of time-limited components with no evidence of work performed.

Equipment Anomalies

Examination of the master caution annunciator panel revealed that the PRIMARY HYDRAULICS and MAIN GENERATOR segments had no light bulbs installed.

Previous Accident History

Examination of NTSB accident records revealed the helicopter was 'demolished' and de-registered after an accident in 1988.

Frequently asked questions

What happened in the 26 Apr 1998 Fairchild Hiller FH-1100 accident near Stevensville, MD?

A helicopter on a local photo flight experienced a main rotor hub separation after abrupt maneuvers, with the rotor assembly found 190 feet from the main wreckage. The mast fracture showed overload and no fatigue; records indicated unqualified maintenance and missing caution panel bulbs.

What aircraft was involved and where did it happen?

The accident on 26 Apr 1998 involved a Fairchild Hiller FH-1100, registration N1345Q, at Stevensville, MD.

What was the probable cause of the accident?

The pilot's abrupt, low-g maneuver, which resulted in mast bumping and separation of the main rotor system.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X09878. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.