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Accidents · NTSB WPR24LA109 · Final report

Raytheon Aircraft Company B200 accident near Billings, Montana, March 12, 2024

On March 12, 2024 at about 2:05 pm local time, a 1999 Raytheon Aircraft Company B200, registered N299AV, was substantially damaged in an accident during enroute near Billings, Montana (Billings Logan Intl airport). It was a positioning flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's improper engine start, resulting in the engine starters remaining engaged and the generators not being activated, which led to the discharge of the airplane’s battery and subsequent total electrical failure after takeoff. Contributing to the accident were generator caution lights not illuminating and the pilot’s inadequate manual landing gear extension, resulting in a landing with the gear not down and locked.

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

What the record shows

Date
March 12, 2024 · about 2:05 pm local time
Place
Billings, Montana · Billings Logan Intl · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Raytheon Aircraft Company B200, built 1999
Registration
N299AV · registry record · serial BB-1680
Damage
Substantial damage
Flight
Positioning flight · general aviation rules (Part 91)

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

The pilot stated that shortly after departure, the airplane lost all electrical power. While descending and returning to the airport, the pilot attempted to manually extend the landing gear but could not verify they were in the down-and-locked position because the landing gear indicator lights were not operational. With the flaps retracted, the airplane touched down on the runway and the landing gear collapsed. According to the airplane’s Pilot’s Operating Handbook (POH), the engine start procedure required sequencing to ignite the engine before placing each generator online. To turn the generator on, the generator control switch must first be held upward in the spring-loaded “GEN RESET” position for a minimum of one second, then released to the “ON” position. The electrical system is designed so that the starter circuit has priority over the generator circuit, prohibiting a generator from coming online until the starter is fully disengaged. Placing the ignition and engine start switch into any position except “OFF” results in the same-side generator shutting off, and it is not possible to bring the generator online until the ignition and engine start switch is moved to the “OFF” position. The POH also instructs the pilot to unstow and pump the alternate extension handle to perform a manual gear extension. It states, “If one or more green gear-down annunciators do not illuminate for any reason and a decision is made to land in this condition,” the pilot should continue pumping the handle “until maximum resistance is felt.” Postaccident examination of the airplane revealed that the generator caution lights were not operational and it is unlikely that the pilot tested them. Capacity testing of the battery indicated that its condition was slightly less than that of a normally functioning battery, which is likely partially the reason the battery lasted just 18 minutes after start, rather than the specified 30 minutes. Additionally, the 30-minute battery life assumes that only essential electrical equipment is operating. No mechanical anomalies were found during the postaccident manual extension of the landing gear. The pilot stated that, during training for emergency manual landing gear extension procedures, he consistently verified illumination of three green indicator lights, confirming that the landing gear was in the down-and-locked position. During the accident flight, he was unable to obtain this visual confirmation due to the complete electrical power loss, which rendered the gear position indicator lights inoperative. It is likely that the pilot inadvertently turned on the starter switches or did not reset the generators, which led to depletion of the battery and loss of electrical power to the airplane's systems. If the pilot had followed the emergency procedures and had continued to pump the manual landing gear extension handle, he likely could have lowered the landing gear.

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. Electrical system malf/failure during enroute defining event

The NTSB's findings

  • Personnel issues › Action/decision › Action › Incorrect action sequence › Pilot
  • Aircraft › Aircraft systems › Landing gear system › Gear extension and retract sys › Incorrect use/operation
  • Aircraft › Aircraft systems › Electrical power system › DC generation system › Incorrect use/operation
  • Aircraft › Aircraft systems › Electrical power system › DC indicating system › Inoperative

Pilot

  • Certificate: airline transport pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instrument: airplane
  • Flight time: 10,559 hours in all; 204 in this make and model; 74 in the last 90 days; 33 in the last 30 days; 6,454 as pilot in command; 2,521 on instruments
  • Last flight review: October 19, 2023
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

Pilot

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 930 hours in all; 4 in this make and model; 100 in the last 90 days; 17 in the last 30 days; 413 as pilot in command
  • Last flight review: October 23, 2023
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: rgt
  • Injury: no injuries

The aircraft

  • Airframe total time: 13,801.9 hours
  • Last inspection: continuous airworthiness programme, March 5, 2024; 12.5 hours since
  • Maximum gross weight: 12,590 lb
  • Landing gear: retractable
  • Engine 1: Pratt & Whitney Canada PT6A-61 (turboprop); 21,831 hours total
  • Engine 2: Pratt & Whitney Canada PT6A-61 (turboprop); 21,831 hours total
  • Operator: Teton Leasing LLC

The flight

  • Departed from: KBIL Billings MT at 1:45 pm
  • Destination: M46 Colstrip MT
  • Flight plan: IFR
  • Runway 28R, 10,518 ft by 150 ft
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 210° at 5 knots
  • Visibility: 10 statute miles
  • Sky: overcast at 11,000 ft
  • Temperature: 37°F (3°C), dew point 25°F (-4°C)
  • Altimeter: 29.75 inHg
  • Observation at 7:53 am from KBIL

Weather report (METAR): KBIL 121353Z 21005KT 10SM OVC110 03/M04 A2975 RMK AO2 SLP085 ACSL N-S T00281044

Injuries

FatalSeriousMinorNone
Flight crew2

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

8 documents, released by the NTSB on February 11, 2026. 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.

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.