Collier Q200 N200CQ
29 October 1996 · Estacada, Oregon, United States · Fatal
Summary
On 29 October 1996 at about 22:30 local time, a Collier Q200 registered N200CQ was involved in an accident near Estacada, Oregon, 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 22:30
- Classification
- Accident
- Location
- Estacada, Oregon, United States
- Coordinates
- 45.1996, -122.0610
- Aircraft
- Collier Q200
- Registration
- N200CQ
- Category
- Airplane
- Engines
- 1
- Operator
- Not recorded
- Operating rule
- Part 91: General Aviation
- Purpose of flight
- Unknown
- Phase of flight
- Not recorded
- Aircraft damage
- Substantial
- Weather
- VMC
- Light
- Day
- NTSB number
- SEA97LA022
People
1 person died.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 1 | 1 | 0 | 0 | 0 |
Probable cause
inadequate maintenance adjustment by the owner/pilot/mechanic, by not using safety wire to secure the throttle arm clamping screw, which resulted in a loose clamping screw and rotation of the throttle arm with respect to the butterfly valve shaft. The lack of suitable terrain for an emergency landing was a factor.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
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.
Quoted verbatim from the NTSB record.
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 5 Aug 1996 | Piper PA-12 | Astoria, Oregon, United States | - | Minor injuries | - |
| 20 Oct 1996 | Garlick UH-1H | Detroit, Oregon, United States | Usfs | Minor injuries | - |
| 6 Aug 1996 | Grumman American AA-5A | Klamath Falls, Oregon, United States | Sweet, David, N. | No injuries | - |
| 12 Aug 1996 | Jonas EXEC 90 | Hermiston, Oregon, United States | - | Minor injuries | - |
| 18 Aug 1996 | Piper PA-20 | Mulino, Oregon, United States | James K. Warnock | No injuries | - |
| 22 Aug 1996 | Piper PA-38-112 | Sisters, Oregon, United States | Jack's Aircraft | Serious injuries | - |