Amateur-built CIRRUS VK 30 accident near Agua Dulce, California, February 11, 2018
On February 11, 2018 at about 6:59 pm local time, a 1999 amateur-built CIRRUS VK 30, registered N52TH, was substantially damaged in an accident during enroute (cruise) near Agua Dulce, California. It was a personal flight under general aviation rules (Part 91). 4 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The driveshaft fracture due to overstress loading and rotational bending as a result of the under-torqued nuts on the elastomeric couplings backing off and the subsequent in-flight separation of the horizontal fairing due to contact with the separated end of the driveshaft, which led to a loss of control. Contributing to the accident was inadequate maintenance.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- February 11, 2018 · about 6:59 pm local time
- Place
- Agua Dulce, California · map
- Type
- Accident
- Injuries
- 4 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built CIRRUS VK 30 NO SERIES, built 1999
- Registration
- N52TH · no longer on the register · serial 143
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The private pilot, who was the builder of the experimental amateur-built airplane, and three passengers departed on a cross-country flight. A witness about 2 miles from the accident site saw the airplane in cruise flight about 2,000 to 3,000 ft above the ground when the right wing rose, and he heard what he perceived as the engine advancing to full power as the airplane entered a vertical descent that continued to ground contact. The wreckage was mostly contained within an area about 100 ft in diameter except for the left horizontal stabilizer fairing, which was found about 2,500 ft west of the main wreckage. The airplane's engine was mounted mid-fuselage and drove an aft-mounted, "pusher" configuration, constant-speed propeller. A torque tube (driveshaft) equipped with forward and aft elastomeric couplings was used to transfer power from the propeller flange located on the front of the engine crankshaft to the propeller. The driveshaft was found fractured about 2 ft forward of the propeller. A metallurgical examination revealed that the driveshaft fractured due to overstress loads in torsion and rotational bending. Deformation of the forward side of the fracture was consistent with continued rotation in the clockwise direction relative to the aft portion of the shaft, indicating that the shaft was being powered by the engine at the time of the fracture. Further examination of the driveshaft revealed that one of eight nuts from the forward coupling and one of two nuts from the aft coupling were backed off (4 mm and 2.11 mm, respectively) of their respective bolts. It is likely that the bolts were under torqued and, at some point, the driveshaft developed a vibration which caused the nuts to back off, which lead to the catastrophic in-flight separation of the driveshaft. Review of the airplane's maintenance records revealed that, about 8 years and 300 flight hours before the accident, the entry indicated that an unspecified coupling was replaced, and the engine drive system was balanced. The entry did not detail the work accomplished. A further review of the records revealed that, 5.1 flight hours before the accident flight, the bolts on the flywheel and couplings were retorqued. The entry did not detail the work accomplished nor indicate the torque values, but it is likely that the nuts were not properly torqued at that time, allowing them to back off during flight. Following the driveshaft failure, the engine likely began to overspeed, consistent with the increased engine sound reported by the witness. In addition, the forward portion of the driveshaft likely contacted the bottom of the horizontal stabilizer, and the horizontal fairing subsequently separated in flight, resulting in an inflight upset and loss of control. The three-bladed propeller was found with two of the three blades broken, indicating that at the time of impact, there was no power to the propeller. The propeller spinner remained attached to the propeller and displayed little damage. The left elevator was found about 80 ft from the empennage and red paint transfer marks were found on the trailing edge of the elevator, consistent with propeller tip contact. Thus, it is likely that the propeller blade struck the elevator during the rapid descent, separating both from the airplane. Although the level of diphenhydramine detected in specimens from the pilot's cavity blood (even accounting for post-mortem redistribution) may have been in a range where it may have resulted in psychoactive effects, there is no direct evidence of impaired judgment or decision-making and no evidence of psychomotor slowing. Therefore, it is unlikely that the pilot's use of diphenhydramine contributed to this accident. In addition, the pilot had moderate coronary artery disease without evidence of ever having an acute cardiac event. Given the circumstances of the accident, the pilot's heart disease was not a contributing factor.
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
- Aircraft maintenance event during prior to flight
- Powerplant sys/comp malf/fail during enroute (cruise) defining event
- Inflight upset during enroute (cruise)
- Part(s) separation from AC during enroute (cruise)
- Loss of control in flight during enroute (cruise)
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Aircraft › Aircraft propeller/rotor › Main rotor drive › Engine/transmission coupling › Failure
- cause Aircraft › Aircraft propeller/rotor › Main rotor drive › Engine/transmission coupling › Incorrect service/maintenance
- factor Personnel issues › Task performance › Maintenance › Scheduled/routine maintenance › Maintenance personnel
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 1,240 hours in all
- Last flight review: August 28, 2016
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 1,037.7 hours
- Last inspection: condition inspection, January 1, 2018; 5 hours since
- Maximum gross weight: 3,600 lb
- Seats: 5
- Landing gear: retractable
- Engine: Continental IO-550-GIB (piston); 1,038 hours total
The flight
- Departed from: HND Las Vegas NV at 6:00 pm
- Destination: VNY Van Nuys CA
- Flight plan: not recorded
Weather at the time
- Light: daylight
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 68°F (20°C), dew point 25°F (-4°C)
- Altimeter: 29.94 inHg
- Observation at 6:55 pm from KWHP, 13 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 3 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
15 documents, released by the NTSB on July 15, 2019. 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 | Materials Laboratory Factual Report 18-072 | PDF, 5 pages | View Download |
| 2 | Weather Study | PDF, 23 pages | View Download |
| 3 | Weather Study - Attachment 1 | PDF, 5 pages | View Download |
| 4 | Weather Study - Attachment 2 | PDF, 227 pages | View Download |
| 5 | Weather Study - Attachment 3 | PDF, 6 pages | View Download |
| 6 | Weather Study - Attachment 4 | PDF, 3 pages | View Download |
| 7 | Witness Statements | PDF, 6 pages | View Download |
| 8 | Air Traffic Control Communications | PDF, 5 pages | View Download |
| 9 | On-scene Diagrams | PDF, 7 pages | View Download |
| 10 | Exam Diagrams W/photos | PDF, 11 pages | View Download |
| 11 | Airframe Log Book Excerpt | PDF, 2 pages | View Download |
| 12 | Engine Log Excerpt | PDF, 6 pages | View Download |
| 13 | Statement of Party Representatives to NTSB Investigation – Continental Motors | PDF, 1 page | View Download |
| 14 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 1 page | View Download |
| 15 | Toxicological Report (Pilot) | PDF, 1 page | 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.
