Enstrom 280 accident near Hayden, Idaho, June 24, 2020
On June 24, 2020, a 2003 Enstrom 280 (helicopter), registered N280MM, was destroyed in an accident during maneuvering (low-alt flying) near Hayden, Idaho. It was an instructional 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
The total loss of power while maneuvering at low altitude due to the detonation of two engine cylinders and damaged spark plugs.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 24, 2020
- Place
- Hayden, Idaho · map
- Type
- Accident
- Injuries
- 1 person was killed and 1 person was seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Enstrom 280 FX, built 2003 · all 280s on the register
- Registration
- N280MM · no longer on the register · serial 2099
- Damage
- Destroyed
- Flight
- Instructional flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
Shortly after takeoff on an instructional flight, a helicopter was maneuvering at a low altitude when the engine rpm “skyrocketed,” and the engine lost total power; the flight instructor (who was at the controls) reported hearing “backfiring” at the time, although the engine was still running. The flight instructor then had to maneuver the helicopter to avoid nearby power lines, but the helicopter impacted terrain. The main rotor blades struck the tailboom, and the helicopter subsequently spun around about 180° before coming to rest. A postcrash fire then ensued, which consumed most of the helicopter. Additionally, the student pilot stated to a witness after the accident that the helicopter was losing power. An engine examination revealed that detonation had occurred in two of the four engine cylinders. (Detonation in a piston engine occurs when the fuel-air mixture in a cylinder detonates or explodes prematurely instead of being ignited by spark plugs and burning evenly and smoothly, as occurs with normal combustion.) Furthermore, damaged spark plugs were observed in one of the detonated cylinders as well as another cylinder. The combined effects of the detonation and damaged spark plugs likely caused the loss of engine power. Because the loss of power occurred at a low altitude, the flight instructor likely did not have enough altitude to adequately establish a steady-state autorotation to avoid the helicopter’s impact with terrain.
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
- Unknown or undetermined during maneuvering (low-alt flying) defining event
The NTSB's findings
- Aircraft › Aircraft power plant › Engine (reciprocating) › Recip eng cyl section › Damaged/degraded
- Aircraft › Aircraft power plant › Ignition system › Spark plugs/igniters › Damaged/degraded
Dual student
- Certificate: student
- Flight time: 157 hours in all
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: left
- Injury: fatal
Flight instructor
- Certificate: flight instructor, commercial pilot
- Ratings: instructor: helicopter; instrument: helicopter; rotorcraft: helicopter
- Flight time: 365 hours in all
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: rgt
- Injury: serious injuries
The aircraft
- Airframe total time: 1,793.4 hours
- Last inspection: annual inspection, July 15, 2019
- Maximum gross weight: 2,600 lb
- Landing gear: fixed
- Engine: Lycoming HI0-360 SER (piston); 0 hours total
- Fire on the ground
The flight
- Departed from: COE Coeur D' Alene ID at 11:59 pm
- Destination: COE Coeur D' Alene ID
- Flight plan: none
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 280° at 8 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 86°F (30°C), dew point 55°F (13°C)
- Altimeter: 29.96 inHg
- Observation at 11:56 pm from KCOE, 3 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
11 documents, released by the NTSB on July 28, 2022. 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 | Record of Email - Witnesses | PDF, 2 pages | View Download |
| 2 | Record of Conversations | PDF, 3 pages | View Download |
| 3 | Record of Emails | PDF, 6 pages | View Download |
| 4 | Engine Examination Summary Report | PDF, 6 pages | View Download |
| 5 | Annual Inspection | PDF, 2 pages | View Download |
| 6 | Transmission Examination Report | PDF, 11 pages | View Download |
| 7 | Detonation - Lycoming | PDF, 1 page | View Download |
| 8 | FAA Aviation Maintenance Technician Handbook Powerplant Volume 2 Excerpt | PDF, 2 pages | View Download |
| 9 | Enstrom 280FX Height and Velocity Diagram | PDF, 1 page | View Download |
| 10 | Memorandum for Record | PDF, 1 page | View Download |
| 11 | Statement of Party Representatives to NTSB Investigation | 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.
