Mooney M20K accident near Baker City, Oregon, August 11, 2018
On August 11, 2018 at about 5:17 pm local time, a 1979 Mooney M20K, registered N231EC, was substantially damaged in an accident during approach (VFR pattern base) near Baker City, Oregon (Baker City Muni airport). It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's exceedance of the airplane's critical angle of attack during the landing approach as a result of his diversion of attention after a series of non-essential aircraft systems became inoperative following the failure of the engine-driven vacuum pump, which resulted in an aerodynamic stall/spin.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- August 11, 2018 · about 5:17 pm local time
- Place
- Baker City, Oregon · Baker City Muni · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Mooney M20K No Series, built 1979 · all M20Ks on the register
- Registration
- N231EC · no longer on the register · serial 25-0167
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot and student pilot-rated passenger were in a high-performance airplane and inbound for landing. Multiple witnesses saw the airplane on the downwind leg of the airport traffic pattern; one witness estimated that the airplane was lower and closer to the runway than a typical traffic pattern. Witnesses then saw the airplane begin a left turn, and one reported that the airplane then rapidly transitioned to a nose-down descent. The wreckage location corresponded to an extended downwind-to-base turn; there was ample space available for the pilot to initiate the turn to final without excessive flight control inputs. The airplane appeared to be in the landing configuration, and debris distribution and damage indicated a near vertical, nose-down impact, consistent with the airplane impacting the ground while in a spin. Postaccident examination did not reveal any anomalies with the airframe or engine that would have precluded normal operation, and the engine appeared to be operating at the time of impact; however, evidence suggested that the airplane's engine-driven vacuum pump had recently failed. Such a failure would have resulted in multiple visual alerts, caused the vacuum-operated instruments to become inoperative, and prevented operation of the airplane's speed brakes. The airplane was equipped with a backup vacuum system; however, impact damage prevented an accurate assessment of its operational status at the time of the accident. The vacuum pump had exceeded its manufacturer's recommended replacement life and had been subjected to multiple sudden engine stoppage events, each of which required replacement of the pump; however, there was no indication in the airplane's logbooks that the pump had been replaced following these events. Although none of the systems that relied on the vacuum pump were critical for visual flight rules operation, such a failure would have presented an operational distraction to the pilot that would have competed for his attention while flying in the pattern. Based on witness reports and the location of the wreckage, it is possible that he extended the downwind leg to attempt to manage the failure or in an effort to slow the airplane further in order to land without the speed brakes. The presence of a systems failure may have exceeded the pilot's capability to appropriately divide his attention between airplane control and systems management. The pilot had relatively low flight experience and had demonstrated poor situational awareness and pilot resource management during his initial private pilot practical test, which he failed on the first attempt. He was also involved in a hard landing with the accident airplane about 2 months before the accident, resulting in damage to the propeller and landing gear. His flight instructor expressed concern that the complex, high-performance airplane was too fast and advanced for the pilot's level of experience. He recounted how the pilot often struggled with maintaining a stabilized landing approach and often allowed the airplane to "get ahead of him." It is likely that the pilot became distracted during the landing approach and allowed the airplane to slow down and exceed its critical angle of attack during the turn from the downwind to base leg, resulting in an aerodynamic stall and spin at an altitude too low for recovery.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Flight instrument malf/fail during enroute
- Loss of control in flight during approach (VFR pattern base) defining event
- Aerodynamic stall/spin during approach (VFR pattern base)
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Capability exceeded
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Personnel issues › Psychological › Attention/monitoring › Attention › Pilot
- Aircraft › Aircraft systems › Vacuum system › (general) › Fatigue/wear/corrosion
- Personnel issues › Experience/knowledge › Experience/qualifications › Total experience w/ equipment › Pilot
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 248 hours in all; 50.4 in this make and model; 21 in the last 90 days; 3.2 in the last 30 days
- Last flight review: January 5, 2018
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: fatal
Dual student
- Certificate: student
- Flight time: 40 hours in all; 6 in this make and model
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 3,439.3 hours
- Last inspection: annual inspection, January 2, 2018; 56 hours since
- Maximum gross weight: 2,900 lb
- Seats: 4
- Landing gear: retractable
- Engine: Continental Motors TSIO-360LB(1) (piston); 818 hours total
The flight
- Departed from: EUL Caldwell ID at 4:30 pm
- Destination: BKE Baker City OR
- Flight plan: none
- Runway 31, 5,085 ft by 100 ft
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 290° at 6 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 82°F (28°C), dew point 46°F (8°C)
- Altimeter: 30.02 inHg
- Observation at 5:53 pm from KBKE, 2 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
10 documents, released by the NTSB on July 31, 2020. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Witness Statements | PDF, 8 pages | View Download |
| 2 | Airframe and Engine Examination Report | PDF, 23 pages | View Download |
| 3 | Maintenance Logbook Excerpts | PDF, 9 pages | View Download |
| 4 | Vacuum Pump Maintenance Manual and Service Letters | PDF, 64 pages | View Download |
| 5 | Pilot Training Records | PDF, 19 pages | View Download |
| 6 | Fuel Receipt | PDF, 1 page | View Download |
| 7 | Statement of Party Representatives to NTSB Investigation | PDF, 1 page | View Download |
| 8 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 1 page | View Download |
| 9 | Evidence Control Form | PDF, 1 page | View Download |
| 10 | Toxicological Reports | PDF, 2 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
