Hughes 369 accident near Ash, North Carolina, September 17, 2021
On September 17, 2021 at about 2:30 pm local time, a 1974 Hughes 369 (helicopter), registered N420AT, was substantially damaged in an accident during maneuvering (low-alt flying) near Ash, North Carolina. It was an aerial application (crop spraying) flight under agricultural flying rules (Part 137). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
A partial loss of engine power due to corrosion and erosion damage to the engine’s compressor section components.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- September 17, 2021 · about 2:30 pm local time
- Place
- Ash, North Carolina · map
- Type
- Accident
- Injuries
- No one was hurt; 1 person was on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Hughes 369 HS, built 1974 · all 369s on the register
- Registration
- N420AT · no longer on the register · serial 940648S
- Damage
- Substantial damage
- Flight
- Aerial application (crop spraying) flight · agricultural flying rules (Part 137)
The NTSB's narrative final · quoted from the NTSB record
The pilot flew the helicopter from his home base to a remote aerial application site, where he landed the helicopter on a support truck so that the ground crew could load the chemical hopper. After loading was completed, the pilot increased the throttle until the engine and rotor rpm needles were in the green range of the tachometer. Immediately after liftoff from the truck, the pilot heard the low-rotor rpm warning horn, and the helicopter began to descend. The pilot attempted to add more pitch; however, the helicopter did not respond. The helicopter subsequently descended, impacted a field, and rolled over onto its right side, resulting in substantial damage to the tailboom. Postaccident examination of the engine revealed that it would start and run but could not reach full operating speed. Upon disassembly of the compressor section, significant erosion and corrosion damage was found on the compressor case halves and stator vanes, which also exhibited structural damage that ranged from being fully rolled over to being severely distorted or twisted. Other stator vanes were missing. The polymer coating on the inside of the compressor case was eroded in several places. Many of the rotating blades of the compressor were mechanically damaged. Since 1986, the engine manufacturer has published guidance instructing operators to perform a daily water rinse of engine components if the engine was operating in a corrosive environment, to reduce the possibility of component damage from corrosion and erosion. The aerial application of agricultural chemicals creates such a corrosive environment. The damage to the blades and polymer coating were consistent with a buildup of chemicals that the daily wash would likely have mitigated. The significant erosion and corrosion damage on the blades and the polymer coating likely began at some point before the accident and resulted in a partial loss of engine power during the accident 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
- Loss of engine power (partial) during maneuvering (low-alt flying) defining event
- Off-field or emergency landing during maneuvering (low-alt flying)
- Collision with terrain or object (not controlled flight into terrain) during maneuvering (low-alt flying)
The NTSB's findings
- Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Compressor section › Not serviced/maintained
- Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Compressor section › Damaged/degraded
Pilot
- Certificate: commercial pilot
- Ratings: rotorcraft: helicopter
- Flight time: 2,453 hours in all; 1,926 in this make and model; 145 in the last 90 days; 7 in the last 30 days; 2,403 as pilot in command
- Last flight review: May 28, 2021
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: left
- Injury: no injuries
The aircraft
- Airframe total time: 5,178 hours
- Last inspection: 100-hour inspection, September 1, 2021
- Maximum gross weight: 2,550 lb
- Seats: 4
- Landing gear: fixed
- Engine: Allison 250-C20B (turboshaft); 8,253 hours total
- Operator: Dat Aircraft LLC
The flight
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 020° at 6 knots
- Visibility: 10 statute miles
- Sky: broken clouds at 3,300 ft; scat at 2,400 ft
- Temperature: 82°F (28°C), dew point 72°F (22°C)
- Altimeter: 30.13 inHg
- Observation at 12:35 pm from CPC, 16 miles away
Weather report (METAR): KCPC 171635Z AUTO 02006KT 10SM SCT024 BKN033 BKN041 28/22 A3013 RMK AO2 T02790217
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
9 documents, released by the NTSB on September 14, 2023. 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, 11 pages | View Download |
| 2 | Memorandum for Record - Conversation with Pilot | PDF, 1 page | View Download |
| 3 | Pilot Statement and Interview with FAA | PDF, 3 pages | View Download |
| 4 | Maintenance Records | PDF, 41 pages | View Download |
| 5 | Engine Manufacturer's Commercial Service Letter - Contamination Removal Instructions | PDF, 14 pages | View Download |
| 6 | Investigative Photographs | PDF, 4 pages | View Download |
| 7 | Engine Examination Report - Rolls Royce | PDF, 14 pages | View Download |
| 8 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 1 page | View Download |
| 9 | Statement of Party Representatives to NTSB Investigation | PDF, 11 pages | 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.
