19990428004179A

Accident · Destroyed

FAA accident report · Beech B24R · Boone, NC · April 28, 1999

Date
April 28, 1999 · 12:50 local
Place
Boone, NC
Airport
Boone Inc Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N12RF
NTSB investigation
NTSBATL99LA077
Reported as
Beech B24R
Reported engine
Lycoming IO360A1B6
Fatal injuries
0
Pilot’s flight hours
625 total

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.

Acft crashed shortly after take-off 1.6 miles from the arpt, other circumstances are unknown. (.4) according to witnesses, the ceiling was about 50 feet above the ground, and the takeoff appeared to be normal until the collision with trees. According to the FAA inspector on-scene, the aircraft collided with trees and rising terrain and subsequently the ground in a wooded area about 1.6 miles south of the airport. Examination of the wreckage revealed that the airplane had collided with trees up-slope on the north side of a ridge, at the 3800 foot level. The slope of the ridge was approximately 25 degrees. The initial crash path through the trees was inclined 3-5 degrees. Examination of the engine found it heat damaged from the post-impact fire. All of the accessory components were destroyed. Engine examination and partial disassembly found no evidence of any pre-impact mechanical deficiencies that would have prevented the engine from developing power.

As the FAA filed it

ACFT CRASHED SHORTLY AFTER TAKE-OFF 1.6 MILES FROM THE ARPT, OTHER CIRCUMSTANCES ARE UNKNOWN. (.4) ACCORDING TO WITNESSES, THE CEILING WAS ABOUT 50 FEET ABOVE THE GROUND, AND THE TAKEOFF APPEARED TO BE NORMAL UNTIL THE COLLISION WITH TREES. ACCORDING TO THE FAA INSPECTOR ON-SCENE, THE AIRCRAFT COLLIDED WITH TREES AND RISING TERRAIN AND SUBSEQUENTLY THE GROUND IN A WOODED AREA ABOUT 1.6 MILES SOUTH OF THE AIRPORT. EXAMINATION OF THE WRECKAGE REVEALED THAT THE AIRPLANE HAD COLLIDED WITH TREES UP-SLOPE ON THE NORTH SIDE OF A RIDGE, AT THE 3800 FOOT LEVEL. THE SLOPE OF THE RIDGE WAS APPROXIMATELY 25 DEGREES. THE INITIAL CRASH PATH THROUGH THE TREES WAS INCLINED 3-5 DEGREES. EXAMINATION OF THE ENGINE FOUND IT HEAT DAMAGED FROM THE POST-IMPACT FIRE. ALL OF THE ACCESSORY COMPONENTS WERE DESTROYED. ENGINE EXAMINATION AND PARTIAL DISASSEMBLY FOUND NO EVIDENCE OF ANY PRE-IMPACT MECHANICAL DEFICIENCIES THAT WOULD HAVE PREVENTED THE ENGINE FROM DEVELOPING POWER.

NTSB investigation

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