Aviation Crash Map

Aero Commander AC-690 N690AC

12 February 2001 · Eugene, Oregon, United States · No injuries

Summary

On 12 February 2001 at about 01:20 local time, a Aero Commander AC-690 registered N690AC was involved in an accident near Eugene, Oregon, United States. 2 people were on board and nobody was injured. 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 01:20
Classification
Accident
Location
Eugene, Oregon, United States
Nearest airport
Mahlon Sweet Field (EUG)
Coordinates
44.0604, -123.0792
Aircraft
Aero Commander AC-690
Registration
N690AC
Category
Airplane
Engines
2
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Redmond → Eugene
Aircraft damage
Substantial
Weather
IMC
Light
Dusk
NTSB number
SEA01LA049

People

Nobody was injured.

On board Died Serious Minor Uninjured
2 0 0 0 2

Probable cause

an undetermined malfunction of the nose gear system which resulted in the failure of the nose gear to fully extend and lock prior to landing.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

After taxiing and taking off in "very icy conditions," the pilot was unable to get the nose gear to fully retract even after multiple recycle attempts. Because of the severe weather at his point of departure, the pilot elected to continue to his planned destination. At the destination ILS final approach fix, the pilot moved the gear handle to the DOWN position, but the nose gear did not fully extend. He therefore recycled the gear a number of times, with and without full rudder pedal application, but the nose gear would not fully extend and lock. During the landing, the initial touchdown was successful, but as the nose gear was lowered to the runway, it collapsed back into the wheel well. During a post-accident inspection, after prying the nose wheel loose from the well with a bar, it rotated to the full down and locked position. After the bushing collar bolts at the base of the gear strut oleo body were loosened, the nose gear was able to be centered. The post-accident inspection did not reveal any anomalies in the extension and retraction assembly, and it could not be positively determined why the gear did not fully retract or extend.

Quoted verbatim from the NTSB record.

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