Aviation Crash Map

Jenkins RV-7A N742MJ

18 March 2008 · Winslow, Arizona, United States · Fatal

Summary

On 18 March 2008 at about 19:15 local time, a Jenkins RV-7A registered N742MJ was involved in an accident near Winslow, Arizona, United States. One person was on board and one died. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 19:15
Classification
Accident
Location
Winslow, Arizona, United States
Nearest airport
Winslow Muni (INW)
Coordinates
35.0219, -110.7225
Aircraft
Jenkins RV-7A
Registration
N742MJ
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Winslow → Unknown
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
LAX08LA078

People

1 person died.

On board Died Serious Minor Uninjured
1 1 0 0 0

Probable cause

The pilot's failure to maintain an adequate airspeed that resulted in a stall/spin.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

Witnesses observed the airplane take off and climb to 700-800 feet above the ground. The airplane then banked about 90 degrees, the nose dropped, and it descended towards the ground, impacting the taxiway in a nose low attitude. Witnesses reported that it was not apparent that the pilot attempted to recover from the dive. One witness stated that they heard the engine sputter, then the engine sound increased like the pilot "gunned it." The witness saw the airplane "go straight up" after the increase in engine noise, and then roll after the nose dropped so that she was looking at the top of the wings and cockpit of the airplane as it disappeared behind buildings. Another witness reported that the engine was very loud during the dive. Post crash inspection of the wreckage found that both the airframe and engine were severely fragmented. Remains of all flight controls were within the wreckage. Continuity was established for the aileron controls, but extensive damage to the fuselage precluded any determination for the elevator controls. The engine exhibited extensive impact damage and fragmentation; however, signatures consistent with power production were observed on the propeller. This was the pilot's second flight in the airplane.

Quoted verbatim from the NTSB record.

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