Amateur-built EXEC 162F accident near Mt. Comfort, Indiana, June 21, 2014
On June 21, 2014 at about 2:30 pm local time, a 2000 amateur-built EXEC 162F (helicopter), registered N6828D, was substantially damaged in an accident during landing (flare/touchdown) near Mt. Comfort, Indiana (Indianapolis Rgnl airport). It was a personal 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 installation of an unauthorized main rotor belt and his subsequent failure to properly inspect the belt, which resulted in inadequate belt tension, the belt’s failure, and the subsequent loss of engine power.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 21, 2014 · about 2:30 pm local time
- Place
- Mt. Comfort, Indiana · Indianapolis Rgnl · map
- Type
- Accident
- Injuries
- No one was hurt; 2 people were on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built EXEC 162F, built 2000
- Registration
- N6828D · no longer on the register · serial 6460
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot reported that, while the experimental, amateur-built helicopter was climbing through 300 feet, he heard a loud "bang" come from the rear compartment and that the helicopter subsequently yawed right. He made an emergency autorotation landing to a field. During the landing, the helicopter's skids sunk into the mud, and the main rotor blades contacted the ground. The helicopter then came to rest on its side. A postaccident examination of the helicopter revealed that the main rotor belt was not approved for aircraft use and that it was broken straight across in a crimp-type failure. According to the belt manufacturer, belt crimping damage is "commonly associated with belt mishandling, inadequate belt installation tension, sub-minimal sprocket diameters, and/or entry of foreign objects within the belt drive." No foreign object preimpact damage was found. Further, although the belt was an unapproved part, it should have been inspected during each 25-hour standard inspection and the belt tension was to be tested during each annual inspection. At the time of the accident, the belt had accumulated 215.9 total hours. Based on this evidence, the pilot installed an unauthorized main rotor drive belt and then failed to properly inspect the belt, which resulted in inadequate belt tension, the belt's failure, and the subsequent loss of engine power.
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
- Abnormal runway contact during landing (flare/touchdown)
- Roll over during landing (flare/touchdown) defining event
- Loss of engine power (total) during initial climb
- Powerplant sys/comp malf/fail during initial climb
The NTSB's findings
- cause Aircraft › Aircraft propeller/rotor › Main rotor drive › (general) › Failure
- cause Aircraft › Aircraft handling/service › Maintenance/inspections › (general) › Incorrect service/maintenance
- cause Personnel issues › Task performance › Maintenance › Installation › Pilot
- Environmental issues › Physical environment › Terrain › Wet/muddy › Contributed to outcome
Pilot
- Certificate: private
- Ratings: rotorcraft: helicopter
- Flight time: 478 hours in all; 423 in this make and model; 7 in the last 90 days; 6 in the last 30 days; 405 as pilot in command
- Last flight review: May 21, 2014
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: no injuries
The aircraft
- Last inspection: annual inspection, January 14, 2014; 371 hours since
- Maximum gross weight: 1,500 lb
- Seats: 2
- Landing gear: fixed
- Engine: Rotorway RW-145 (piston); 371 hours total
The flight
- Departed from: MQJ Mt. Comfort IN at 2:30 pm
- Destination: GSH Goshen IN
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 350° at 5 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 79°F (26°C), dew point 70°F (21°C)
- Altimeter: 29.95 inHg
- Observation at 1:53 pm from KGEZ, 17 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
9 documents, released by the NTSB on August 7, 2014. 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 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 9 pages | View Download |
| 2 | FAA Inspector - Accident Information | PDF, 3 pages | View Download |
| 3 | Memorandum for Record - Pilot Letter to FAA | PDF, 1 page | View Download |
| 4 | Aircraft Maintenance Logbook Excerpts | PDF, 4 pages | View Download |
| 5 | Gates Belt Failure Analysis Report | PDF, 8 pages | View Download |
| 6 | Gates Part Catalog Introduction | PDF, 5 pages | View Download |
| 7 | Rotorway EXEC162F Helicopter Manual | PDF, 91 pages | View Download |
| 8 | Photo 1. Broken Belt (Photo Courtesy of FAA) | PDF, 1 page | View Download |
| 9 | Photo 2. Main Wreckage (Photo Courtesy of FAA) | 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.
