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Accidents · NTSB WPR17FA179 · Final report

Amateur-built Lancair IV-TP accident near Rio Linda, California, August 3, 2017

On August 3, 2017 at about 10:03 pm local time, a 2004 amateur-built Lancair IV-TP, registered N420M, was substantially damaged in an accident during enroute (cruise) near Rio Linda, California (Mc Clellan Airfield). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A loss of engine power for reasons that could not be determined based on available evidence.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
August 3, 2017 · about 10:03 pm local time
Place
Rio Linda, California · Mc Clellan Airfield · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built Lancair IV-TP, built 2004
Registration
N420M · no longer on the register · serial LIV 071
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The pilot departed on a visual flight rules cross-country flight in his turboprop-equipped experimental airplane. Onboard data indicated that, upon reaching about 6,500 ft mean sea level, about 5 minutes after takeoff, the airplane pitched down about 25° and entered an approximate 35° left bank; the engine power reduced to idle with a simultaneous decrease in fuel flow. Several seconds later, the voltage began to slowly decrease, consistent with the generator turning off. The airplane continued to descend toward the nearest airport and ultimately impacted powerlines and terrain about 1.3 nautical miles from the approach end of the runway. The pilot made no radio transmissions that indicated that he was experiencing an emergency. Examination of the fuel system and engine revealed no mechanical malfunctions or failures, and the reason for the reduction of engine power could not be determined. The propeller was found in a low pitch position. The propeller was not equipped with a feathering pump; therefore, unless the propeller control was moved to the feather position immediately following a loss of engine power, the speed of the counterweights and the aerodynamic loads on the blades would quickly degrade to a point where feathering would become impossible. It is likely that, had the pilot immediately placed the propeller control into the feather position following the loss of engine power, significantly less drag would have been produced by the propeller and the airplane would likely have been able to reach the intended runway. The first responders reported that the pilot stopped breathing shortly after being extricated from the wreckage. Given that the pilot diverted the airplane and initially survived the impact, it is unlikely that he experienced sudden incapacitation during the flight.

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

  1. Loss of engine power (total) during enroute (cruise) defining event
  2. Emergency descent initiated during enroute (cruise)
  3. Controlled flight into terrain or object (CFIT) during emergency descent

The NTSB's findings

  • Not determined › Not determined › (general) › (general) › Unknown/Not determined

Pilot

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 7,300 hours in all
  • Last flight review: February 1, 2016
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 934.7 hours
  • Last inspection: condition inspection, August 4, 2016; 61 hours since
  • Seats: 4
  • Landing gear: retractable
  • Engine: Diemech Turbines M601D (turboprop); 935 hours total

The flight

  • Departed from: AUN Auburn CA at 9:54 pm
  • Destination: SQL San Carlos CA
  • Flight plan: VFR
  • Runway 16, 10,599 ft by 150 ft

Weather at the time

  • Light: daylight
  • Wind: from 240° at 6 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 99°F (37°C), dew point 45°F (7°C)
  • Altimeter: 29.87 inHg
  • Observation at 9:55 pm from KMCC, 2 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

8 documents, released by the NTSB on August 28, 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.

#DocumentWhat it is
1 Powerplants Factual Report PDF, 64 pages View Download
2 Other Electronic Devices Factual Report PDF, 11 pages View Download
3 Other Electronic Devices Factual Report - Attachment 1 Tabular Data data file Download
4 Maps and Diagrams with Test and Research PDF, 21 pages View Download
5 Records of Conversation PDF, 2 pages View Download
6 Excerpts Comparing Prior Flight to and from the Same Airports PDF, 5 pages View Download
7 EFIS Configuration PDF, 1 page View Download
8 Toxicological Report 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.