2 fatalities

Commuter Flight Crashes Near Merrill Field; Two Killed (N967JW)

Anchorage-Merrill Field, United States of AmericaLanding (descent or approach)

On April 1, 1987, a Cessna 402 (registration N967JW) operated by Wilbur's Flight Operations was involved in an aviation accident near Anchorage-Merrill Field, United States of America during landing or approach. 2 people were killed. Investigators recorded the probable cause as: Occurrence #1: loss of engine power (total) - nonmechanical Phase of operation: approach - vfr pattern - base turn Findings 1. (c) fluid, fuel - starvation 2. (f) inattentive - pilot in command 3. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

A scheduled commuter flight crashed while on a VFR approach to Merrill Field, Alaska, killing the captain and one passenger. The aircraft struck the ground inverted in a near-vertical attitude, and fuel starvation is suspected.

Accident Overview

A commuter aircraft on the final leg of a scheduled flight crashed in a heavily wooded area while conducting a visual flight rules (VFR) approach to Merrill Field in Anchorage, Alaska. The captain and the sole passenger were killed in the crash. The airplane struck the ground upside-down in a near-vertical attitude.

Flight History

The flight was the last leg of a scheduled commuter route. The airplane's copilot, who had deplaned minutes before the accident flight, reported that he did not observe the captain select or use the aircraft's auxiliary fuel tanks at any point during the evening's earlier flights.

Fuel System and Consumption

The aircraft's main fuel tanks have a usable capacity of 100 gallons. Investigators estimated that the airplane had consumed slightly more than 100 gallons of fuel at the time of the accident. Sufficient fuel remained in the auxiliary tanks, but the engine cannot be readily restarted if the auxiliary tanks are not selected before the engine quits.

Findings

The official investigation determined that the accident involved multiple occurrences. The first occurrence was a total loss of engine power due to non-mechanical reasons, specifically fuel starvation, attributed to the pilot in command's inattentiveness and improper in-flight planning and decision-making. This led to a forced landing, during which the pilot lost control because airspeed and directional control were not maintained. The final occurrence was an uncontrolled descent resulting in collision with terrain.

Probable cause

Occurrence #1: loss of engine power (total) - nonmechanical Phase of operation: approach - vfr pattern - base turn Findings 1. (c) fluid, fuel - starvation 2. (f) inattentive - pilot in command 3. (f) in-flight planning/decision - improper - pilot in command ---------- Occurrence #2: forced landing Phase of operation: descent - emergency ---------- Occurrence #3: loss of control - in flight Phase of operation: descent - emergency Findings 4. (c) airspeed (vmc) - not maintained - pilot in command 5. (c) directional control - not maintained - pilot in command ---------- Occurrence #4: in flight collision with terrain/water Phase of operation: descent - uncontrolled