32 fatalities

Panarctic Flight 416: Lockheed L-188 Crash at Rea Point (CF-PAB)

Rea Point (Melville Island), CanadaLanding (descent or approach)

On October 30, 1974, a Lockheed L-188 Electra (registration CF-PAB) operated by Panarctic Oils was involved in an aviation accident near Rea Point (Melville Island), Canada during landing or approach. 32 people were killed. Investigators recorded the probable cause as: The approach was continued below the company approved minimum descent altitude, the pilot-in-command reacted inappropriately to a visual cue and suddenly initiated the final rapid descent, partial incapacitation of the pilot-in-command was a factor in the… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards

A Lockheed L-188 (CF-PAB) crashed at Rea Point on 29 October 1974 after an uncontrolled descent. The pilot-in-command's inappropriate reaction to a visual cue and partial incapacitation were key factors.

Flight Details and Approach Sequence On 29 October 1974, a Lockheed L-188 with registration CF-PAB, operating as Panarctic Flight 416, departed Calgary International Airport at 18:05. The aircraft completed a routine positioning flight to Edmonton, where it was loaded with 20,000 lb of baggage and freight and 21,000 lb of Jet B fuel. After a crew change, the aircraft departed Edmonton at 20:04 with 30 passengers and four crew members on board, bound for Rea Point. The flight proceeded uneventfully until the final approach, when the aircraft was cleared for a straight-in VOR/DME approach to runway 33. ## Final Approach and Impact During the descent, the crew experienced light turbulence and glare from external lights. The pilot-in-command (PIC) and co-pilot set their radio altimeters to 300 ft and 450 ft, respectively. At 300 ft radio altitude, the co-pilot reported visual contact with an ice ridge. The PIC then retarded the throttles and pushed forward on the control column, causing a rapid descent of 1,700 to 2,000 ft per minute. Despite calls from the co-pilot and flight engineer, the PIC did not respond. The aircraft impacted the ice surface, and the cockpit section broke away, sliding 900 ft before coming to rest. The flight engineer and co-pilot escaped the sinking cockpit section. ## Official Findings The investigation determined that the approach was continued below the company-approved minimum descent altitude. The PIC's inappropriate reaction to a visual cue and partial incapacitation contributed to the failure to recover from the high rate of descent. Additionally, crew coordination was inadequate, and no company Flight Operations Manual was available to prescribe crew duties. The operation was classified as private, and the aerodrome's emergency response procedures were found to be inadequate.

Probable cause

The approach was continued below the company approved minimum descent altitude, the pilot-in-command reacted inappropriately to a visual cue and suddenly initiated the final rapid descent, partial incapacitation of the pilot-in-command was a factor in the failure to recover from the high rate of descent, crew coordination in the cockpit in the final stages of the flight was inadequate, no company Flight Operations Manual or similar document was available to adequately prescribe the aircraft crew's duties and responsibilities, this operation was in the private category and was not operated or required to operate to the established commercial standards, and the established aerodrome emergency response procedures were inadequate.