No fatalities

Engine Failure and Stall During Emergency Landing at Morris Airport (N420D)

Morris, United States of AmericaTakeoff (climb)

On April 16, 1970, a De Havilland DH.104 Dove (registration N420D) operated by Mid-Continent Airlines was involved in an aviation accident near Morris, United States of America during takeoff. No fatalities were reported. Investigators recorded the probable cause as: Powerplant failure for undetermined reason. Contributing factors: pilot-in-command failed to follow approved procedures; improper emergency procedures; complete failure on one engine; propeller not feathered; flaps 20°; landing gear extended. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 5 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

While climbing after takeoff, the pilot reported an engine failure. Cleared for emergency landing, the airplane stalled on final and crashed short of the runway. The aircraft was destroyed; the pilot was seriously injured.

Accident Sequence

Shortly after takeoff from Morris Airport, while in initial climb, the pilot informed air traffic control about an engine failure. The pilot was cleared to return for an emergency landing. On final approach, the airplane stalled and subsequently crashed in a field located short of the runway threshold.

Aircraft and Pilot Information

The sole occupant and pilot was Fred Irwin. No further details regarding the aircraft type, registration, or operator were provided in the investigation source.

Damage and Injuries

The aircraft was destroyed in the crash. The pilot sustained serious injuries.

Probable Cause

According to the official findings, the probable cause of the accident was a powerplant failure for an undetermined reason. The following factors were considered as contributing: the pilot-in-command failed to follow the approved procedures; improper emergency procedures; complete failure on one engine; propeller not feathered; flaps 20°; landing gear extended.