Bell Helicopter Textron 206B accident near Arcadia, Iowa, August 1, 2022
On August 1, 2022 at about 2:15 pm local time, a 1973 Bell Helicopter Textron 206B, registered N169AA, was substantially damaged in an accident during maneuvering near Arcadia, Iowa. It was an aerial application (crop spraying) flight under agricultural flying rules (Part 137). 1 person had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
Maintenance personnel’s failure to properly torque a fuel control unit B-nut, which resulted in a loss of engine power at low altitude and an impact with terrain.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- August 1, 2022 · about 2:15 pm local time
- Place
- Arcadia, Iowa · map
- Type
- Accident
- Injuries
- 1 person had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Bell Helicopter Textron 206B, built 1973 · all 206Bs on the register
- Registration
- N169AA · registry record · serial 990
- 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 reported that he was completing an aerial application flight about 6 ft above the corn field when the engine sustained a loss of power. The helicopter descended into the corn and impacted the field. A small postcrash fire ensued near the engine and was extinguished. Postaccident examination revealed all external air, fuel, and oil line connections were tight except for the pneumatic air line (Pc line) B-nut connecting the power turbine governor (PTG) to the fuel control unit (FCU). The Pc line was not connected to the FCU and a gap was noted between the B-nut and FCU union. Residual torque paint was identified; however, there was no new-effective torque paint identified on any B-Nut. It appeared the B-nut had backed off the FCU fitting. This Pc is one of several that use air pressure to communicate fuel scheduling demands between the PTG and FCU. The security of this line is necessary for proper engine operation. Operation of the engine without the B-nut properly connected would result in the FCU reducing fuel to a sub-idle condition, with the engine not capable of producing power for continued flight. There were no other mechanical functions or failures that would have precluded normal operation. Maintenance was performed on the helicopter 23 days and 12 flight hours before the accident. It is likely that the maintenance personnel did not properly torque this B-but or apply torque stripe paint, which resulted in a disconnection of the B-nut and a 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
- Loss of engine power (total) during maneuvering defining event
The NTSB's findings
- Aircraft › Aircraft power plant › Engine fuel and control › Fuel controlling system › Incorrect service/maintenance
Pilot
- Certificate: commercial pilot
- Ratings: multi-engine land; single-engine land; instrument: airplane; rotorcraft: helicopter
- Last flight review: July 21, 2020
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: rgt
- Injury: minor injuries
The aircraft
- Airframe total time: 13,248 hours
- Last inspection: inspection type not recorded, July 10, 2022
- Seats: 5
- Landing gear: fixed
- Engine: Rolls-Royce 250-C20 (turboshaft); 12,141 hours total
- Fire on the ground
The flight
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 030° at 4 knots
- Visibility: 9 statute miles
- Sky: a few clouds at 10,000 ft
- Temperature: 72°F (22°C), dew point 66°F (19°C)
- Altimeter: 29.98 inHg
- Observation at 9:15 am from KCIN, 11 miles away
Weather report (METAR): KCIN 011415Z AUTO 03004KT 9SM FEW100 22/19 A2998 RMK AO2
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
6 documents, released by the NTSB on June 20, 2024. 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 | NTSB Investigation Summary | PDF, 6 pages | View Download |
| 2 | Reports from Parties to the Investigation - Rolls-royce | PDF, 3 pages | View Download |
| 3 | Correspondence - Pilot Emails | PDF, 3 pages | View Download |
| 4 | Maintenance Records | PDF, 12 pages | View Download |
| 5 | Statement of Party Representatives to NTSB Investigation | PDF, 1 page | View Download |
| 6 | Release of Aircraft Wreckage, NTSB Form 6120.15 | 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.
