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Accidents · NTSB WPR20FA016 · Final report

Enstrom 280F accident near Jordan Valley, Oregon, October 25, 2019

On October 25, 2019 at about 9:41 pm local time, a 1981 Enstrom 280F (helicopter), registered N280F, was substantially damaged in an accident during maneuvering (low-alt flying) near Jordan Valley, Oregon. It was a personal flight under general aviation rules (Part 91). 1 person was killed and 1 person was seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A partial loss of engine power due to a worn engine air induction hose, and a subsequent uncontrolled descent into terrain. Contributing to the accident was the failure of maintenance personnel to adequately inspect the hose, and the pilot’s decision to fly the helicopter at a speed and altitude that provided limited time to enter and establish an autorotation following the loss of power.

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

What the record shows

Date
October 25, 2019 · about 9:41 pm local time
Place
Jordan Valley, Oregon · map
Type
Accident
Injuries
1 person was killed and 1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
Enstrom 280F, built 1981 · all 280Fs on the register
Registration
N280F · no longer on the register · serial 1501
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot was performing low-level flight over high desert terrain. The passenger reported that, during the flight, the pilot became concerned over a low “rpm” indication. The pilot began to manipulate the flight controls, and the helicopter rapidly descended, yawed to the right, and impacted terrain. Examination revealed that significant sections of the outer liner of the engine’s air induction hose were abraded, consistent with long-term wear, and had worn away from the supporting structure, allowing the hose liner to collapse and restrict airflow into the engine. Given this condition, the engine would have experienced a partial power loss due to the restricted airflow; damage signatures indicated that the engine was producing some power at the time of impact. The helicopter’s most recent annual inspection was completed about three months before the accident, and the worn hose should have been apparent at the time of the inspection. Automatic Dependent Surveillance-Broadcast (ADS-B) data indicated that, before the accident, the helicopter was traveling at a speed and altitude such that, in the event of an engine failure, the pilot would have had limited time to enter and establish a controlled autorotative descent. The helicopter’s operating handbook stated that, at low altitude and low speed, sufficient altitude may not be available to increase rotor rpm following a loss of engine power. Impact damage to the helicopter was consistent with an uncontrolled collision with terrain. The helicopter was equipped with a current emergency locator transmitter (ELT), but it had been incorrectly installed inside the metal baggage compartment in a portable configuration and was not equipped with the required external antenna. Therefore, although the ELT activated, it’s signal was likely shielded by the metal compartment, and not received by search and rescue personnel. As a result, the helicopter was not discovered until the following morning. Even if the ELT signal had been received, the unit was not registered with the current owner; this could potentially have resulted in a delay as search and rescue personnel attempted to track down the owner and ascertain the validity of the alert.

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 (partial) during maneuvering (low-alt flying) defining event
  2. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • Aircraft › Aircraft power plant › Power plant › Air intake › Fatigue/wear/corrosion
  • Personnel issues › Task performance › Inspection › Scheduled/routine inspection › Maintenance personnel
  • Personnel issues › Task performance › Maintenance › Replacement › Maintenance personnel
  • Aircraft › Aircraft systems › Equipment/furnishings › Emergency locator beacon › Incorrect use/operation

Pilot

  • Certificate: commercial pilot
  • Ratings: single-engine land; rotorcraft: helicopter
  • Flight time: 950 hours in all; 100 in this make and model
  • Last flight review: March 1, 2018
  • Medical certificate: BasicMed (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 1,504 hours
  • Last inspection: annual inspection, July 1, 2019; 21.8 hours since
  • Maximum gross weight: 2,350 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Lycoming HIO-360-F1AD (piston); 173 hours total

The flight

  • Departed from: EUL Caldwell ID at 9:20 pm
  • Destination: EUL Caldwell ID
  • Flight plan: none
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 350° at 5 knots
  • Visibility: 9 statute miles
  • Sky: clear
  • Temperature: 64°F (18°C), dew point 27°F (-3°C)
  • Altimeter: 30.09 inHg
  • Observation at 10:55 pm from KMAN, 25 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

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

15 documents, released by the NTSB on December 16, 2021. 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.