20040625011589A

Accident · Substantial damage

FAA accident report · Beech 36BEECH · Cantwell, AK · June 25, 2004

Date
June 25, 2004 · 16:00 local
Place
Cantwell, AK
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N7673N
NTSB investigation
NTSBANC04FA070
Reported as
Beech 36BEECH
Reported engine
Continental IO520*
People aboard
1
Fatal injuries
1
Pilot’s flight hours
4,700 total4,500 in this make and model50 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) On scene investigation suggests that the aircraft contacted the steeply rising and grass and shrub covered terrain in level flight and at cruise power and speed. At first impact, the propeller cut a furrow in the terrain for approximately 15 yards before the propeller separated and the aircraft apparently bounced into the air before hitting the ground again in a direct line from the first impact. The aircraft came to rest approximately 110 yards upslope from impact and turned approximately 120 degrees to the right from its flight path where it burned. The charred body of the pilot was found adjacent to the right side of the fuselage behind the right wing.

As the FAA filed it

(-23) ON SCENE INVESTIGATION SUGGESTS THAT THE AIRCRAFT CONTACTED THE STEEPLY RISING AND GRASS AND SHRUB COVERED TERRAIN IN LEVEL FLIGHT AND AT CRUISE POWER AND SPEED. AT FIRST IMPACT, THE PROPELLER CUT A FURROW IN THE TERRAIN FOR APPROXIMATELY 15 YARDS BEFORE THE PROPELLER SEPARATED AND THE AIRCRAFT APPARENTLY BOUNCED INTO THE AIR BEFORE HITTING THE GROUND AGAIN IN A DIRECT LINE FROM THE FIRST IMPACT. THE AIRCRAFT CAME TO REST APPROXIMATELY 110 YARDS UPSLOPE FROM IMPACT AND TURNED APPROXIMATELY 120 DEGREES TO THE RIGHT FROM ITS FLIGHT PATH WHERE IT BURNED. THE CHARRED BODY OF THE PILOT WAS FOUND ADJACENT TO THE RIGHT SIDE OF THE FUSELAGE BEHIND THE RIGHT WING.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.