19961029041659A

Accident · Substantial damage

FAA accident report · Amtr Q200 · Estacada, OR · October 29, 1996

Date
October 29, 1996 · 14:30 local
Place
Estacada, OR
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N200CQ
NTSB investigation
NTSBSEA97LA022
Reported as
Amtr Q200
Reported engine
Continental O200A
People aboard
1
Fatal injuries
1
Pilot’s flight hours
1,112 total49 in this make and model23 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.

(.4)During a maintenance test flight of a home built aircraft, the pilot apparently initiated an emergency landing on a gravel road. The road was bordered on both sides by tall trees. On the right side of the road, power lines (lower than tree top level) paralleled the road. During the descent, the right canard and right rear wing came in contact with the power lines. The airplane then collided with the road and came to rest off the right side of the road among the trees. Wreckage examination revealed evidence that the butterfly valve in the carburetor was in the closed position, and the throttle stop was positioned approximately 1/8-inch from the stop screw. The throttle arm clamping screw was loose, and the throttle arm rotated easily on the butterfly valve shaft. Mandatory safety wire that was to be applied to the throttle arm clamping screw had not been used, and the safety wire on the throttle arm clamping screw was slack and provided inadequate security. Friends of the pilot reported that approximately one week before the accident, he was having trouble with the fuel mixture; they presumed that the pilot had been making adjustments to the carburetor.

As the FAA filed it

(.4)DURING A MAINTENANCE TEST FLIGHT OF A HOME BUILT AIRCRAFT, THE PILOT APPARENTLY INITIATED AN EMERGENCY LANDING ON A GRAVEL ROAD. THE ROAD WAS BORDERED ON BOTH SIDES BY TALL TREES. ON THE RIGHT SIDE OF THE ROAD, POWER LINES (LOWER THAN TREE TOP LEVEL) PARALLELED THE ROAD. DURING THE DESCENT, THE RIGHT CANARD AND RIGHT REAR WING CAME IN CONTACT WITH THE POWER LINES. THE AIRPLANE THEN COLLIDED WITH THE ROAD AND CAME TO REST OFF THE RIGHT SIDE OF THE ROAD AMONG THE TREES. WRECKAGE EXAMINATION REVEALED EVIDENCE THAT THE BUTTERFLY VALVE IN THE CARBURETOR WAS IN THE CLOSED POSITION, AND THE THROTTLE STOP WAS POSITIONED APPROXIMATELY 1/8-INCH FROM THE STOP SCREW. THE THROTTLE ARM CLAMPING SCREW WAS LOOSE, AND THE THROTTLE ARM ROTATED EASILY ON THE BUTTERFLY VALVE SHAFT. MANDATORY SAFETY WIRE THAT WAS TO BE APPLIED TO THE THROTTLE ARM CLAMPING SCREW HAD NOT BEEN USED, AND THE SAFETY WIRE ON THE THROTTLE ARM CLAMPING SCREW WAS SLACK AND PROVIDED INADEQUATE SECURITY. FRIENDS OF THE PILOT REPORTED THAT APPROXIMATELY ONE WEEK BEFORE THE ACCIDENT, HE WAS HAVING TROUBLE WITH THE FUEL MIXTURE; THEY PRESUMED THAT THE PILOT HAD BEEN MAKING ADJUSTMENTS TO THE CARBURETOR.

NTSB investigation

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