Casualties unknown

1994-09-28: Mcdonnell Douglas 520N (N520NT) — Mesa, AZ

Mesa, AZ, US

On September 28, 1994, a Mcdonnell Douglas 520N (registration N520NT) was involved in an aviation accident near Mesa, AZ. Investigators recorded the probable cause as: FAILURE OF THE CHASE HELICOPTER PILOT TO MAINTAIN CLEARANCE FROM THE LEAD HELICOPTER DURING A NIGHT APPROACH TO LAND. POSSIBLE FACTORS RELATING TO THE ACCIDENT WERE: DARKNESS, AND INADEQUATE RADIO COORDINATION BETWEEN FLIGHT CREWS OF THE TWO HELICOPTERS. 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 1781061362Data APIEditorial standards

During a night VFR flight, a chase helicopter collided with the lead test helicopter near Falcon Field, Arizona. The lead landed safely; the chase crashed after its main rotor separated.

Overview

Two helicopters, a McDonnell Douglas AH-64D (the test aircraft, referred to as 'lead') and a McDonnell Douglas 520N (the chase aircraft), were involved in a midair collision during a night visual flight rules (VFR) operation. The flight originated from Chandler, Arizona, and was destined for the McDonnell Douglas Heliport in Mesa, Arizona.

Flight Details

The chase crew's mission was to surveil the area for the test crew and provide information about other air traffic or hazards. The destination heliport was located just north of Falcon Field. During the arrival, the lead crew notified the chase of a VHF frequency change to the Falcon Field Tower (ATCT) frequency. The chase acknowledged, which was the last known transmission from that aircraft. The lead then switched to the heliport's 'Apache Ramp Control' frequency. The ground control radio operator, monitoring that frequency, cleared the helicopter(s) to land on Runway 22 at the heliport.

Collision

Shortly after the clearance, the chase helicopter collided with the lead helicopter. During the midair collision, the main rotor blades of the chase struck the left wing and wing stores of the lead. The lead helicopter continued to a safe landing. However, the main rotor separated from the chase helicopter, and it crashed.

Investigation

An investigation revealed that the chase helicopter had converged on the lead helicopter from the left rear quadrant. An expletive of unknown source was transmitted on the ATCT frequency at about the time of the midair collision. Tests of the radios from the chase helicopter showed that both radios were set to the ATCT frequency.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001206X02276. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.