19980720023939A

Accident · Substantial damage

FAA accident report · Amtr GLASAIR II FT · Vernoia, OR · July 20, 1998

Date
July 20, 1998 · 14:24 local
Place
Vernoia, OR
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N31066
NTSB investigation
NTSBSEA98LA145
Reported as
Amtr Glasairiift
Reported engine
Lycoming O320A2B
People aboard
1
Fatal injuries
1
Pilot’s flight hours
300 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.

Builder changed fixed prop to a constant speed prop. Unauthorized. No conditions inspection. (.4)the pilot departed about 1030 on a 57-nautical-mile visual flight rules (VFR) flight, and failed to arrive at his destination. The wreckage of the aircraft was discovered about 1424 by a private landowner approximately 37 nautical miles from the departure airport, generally on the direct route from the departure point to the destination. The pilot was dead at the scene. The aircraft had impacted into a tree farm at approximately a 20- to 40-degree impact angle on a southeasterly track (the direct route from the departure point to the destination is northeasterly), and its nose section had separated during the impact sequence. Examinations of the wreckage disclosed no conclusive evidence of pre-impact mechanical problems with the aircraft. Autopsy of the pilot, who held a valid and current FAA third-class medical certificate, disclosed arteriosclerotic cardiovascular disease as a contributing cause of death, with focal severe (greater than 90% occlusion) left anterior descending coronary artery atherosclerosis. It could not b e conclusively estiblished that the pilot had become incapacitated inflight. (-23) an experimental glasair ii aircraft, N31066, built and piloted by Mr. Raymond w. baggerly crashed under unknown circumstances, 2 miles NE of the vernonia, Oregon. Mr. Baggerley, the sole occupant, was found dead at the scene.

As the FAA filed it

BUILDER CHANGED FIXED PROP TO A CONSTANT SPEED PROP. UNAUTHORIZED. NO CONDITIONS INSPECTION. (.4)THE PILOT DEPARTED ABOUT 1030 ON A 57-NAUTICAL-MILE VISUAL FLIGHT RULES (VFR) FLIGHT, AND FAILED TO ARRIVE AT HIS DESTINATION. THE WRECKAGE OF THE AIRCRAFT WAS DISCOVERED ABOUT 1424 BY A PRIVATE LANDOWNER APPROXIMATELY 37 NAUTICAL MILES FROM THE DEPARTURE AIRPORT, GENERALLY ON THE DIRECT ROUTE FROM THE DEPARTURE POINT TO THE DESTINATION. THE PILOT WAS DEAD AT THE SCENE. THE AIRCRAFT HAD IMPACTED INTO A TREE FARM AT APPROXIMATELY A 20- TO 40-DEGREE IMPACT ANGLE ON A SOUTHEASTERLY TRACK (THE DIRECT ROUTE FROM THE DEPARTURE POINT TO THE DESTINATION IS NORTHEASTERLY), AND ITS NOSE SECTION HAD SEPARATED DURING THE IMPACT SEQUENCE. EXAMINATIONS OF THE WRECKAGE DISCLOSED NO CONCLUSIVE EVIDENCE OF PRE-IMPACT MECHANICAL PROBLEMS WITH THE AIRCRAFT. AUTOPSY OF THE PILOT, WHO HELD A VALID AND CURRENT FAA THIRD-CLASS MEDICAL CERTIFICATE, DISCLOSED ARTERIOSCLEROTIC CARDIOVASCULAR DISEASE AS A CONTRIBUTING CAUSE OF DEATH, WITH FOCAL SEVERE (GREATER THAN 90% OCCLUSION) LEFT ANTERIOR DESCENDING CORONARY ARTERY ATHEROSCLEROSIS. IT COULD NOT B E CONCLUSIVELY ESTIBLISHED THAT THE PILOT HAD BECOME INCAPACITATED INFLIGHT. (-23) AN EXPERIMENTAL GLASAIR II AIRCRAFT, N31066, BUILT AND PILOTED BY MR. RAYMOND W. BAGGERLY CRASHED UNDER UNKNOWN CIRCUMSTANCES, 2 MILES NE OF THE VERNONIA, OREGON. MR. BAGGERLEY, THE SOLE OCCUPANT, WAS FOUND DEAD AT THE SCENE.

NTSB investigation

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