Bell Helicopter 407 accident near Clear Lake, Iowa, January 3, 2013
On January 3, 2013 at about 2:57 am local time, a 2009 Bell Helicopter 407, registered N445MT, was destroyed in an accident during enroute near Clear Lake, Iowa (Mason City Municipal airport). It was a positioning flight under general aviation rules (Part 91). 3 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s inadvertent encounter with localized icing conditions and his subsequent in-flight loss of helicopter control.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- January 3, 2013 · about 2:57 am local time
- Place
- Clear Lake, Iowa · Mason City Municipal · map
- Type
- Accident
- Injuries
- 3 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Bell Helicopter 407, built 2009 · all 407s on the register
- Registration
- N445MT · no longer on the register · serial 53959
- Damage
- Destroyed
- Flight
- Positioning flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
GPS tracking data revealed that, after departure, the helicopter proceeded westbound about 600 ft above ground level (agl), following a roadway. About 6 minutes after liftoff, when the helicopter was about 3/4 mile south of the accident site, it turned right and became established on a northerly course. The helicopter subsequently turned left and appeared to be on a southerly heading at the final data point. Shortly before beginning the left turn, the helicopter entered a climb, reached an altitude of about 1,800 ft agl, and then entered a descent that continued until impact. Weather observations from the nearest Automated Surface Observing System, located about 7 miles east of the accident site, indicated that the ceilings and visibility appeared to be adequate for nighttime helicopter operations and did not detect any freezing precipitation. Although an airmen's meteorological information advisory for icing conditions was current for the route of flight, and several pilot reports of icing conditions had been filed, none of the reports were in the immediate vicinity of the intended route of flight. Witnesses and first responders reported mist, drizzle, and icy road conditions at the time of the accident. It is likely that the pilot inadvertently encountered localized icing conditions, which resulted in his subsequent in-flight loss of helicopter control. A postaccident examination of the helicopter revealed no preimpact failures or malfunctions. The engine control unit recorded engine torque, engine overspeed, and rotor overspeed events; however, due to their timing and nature, the events were likely a result of damage that occurred during the impact sequence. Evidence also indicated that the cyclic centering, engine overspeed, and hydraulic system warning lights illuminated; it is also likely that their illumination was associated with the impact sequence. Further, the engine anti-ice status light was illuminated, which was consistent with the activation of the anti-ice system at some point 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
- Structural icing during enroute
- Loss of control in flight during enroute defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Environmental issues › Conditions/weather/phenomena › Ceiling/visibility/precip › Freezing rain/sleet › Awareness of condition
- cause Environmental issues › Conditions/weather/phenomena › Ceiling/visibility/precip › Freezing rain/sleet › Effect on equipment
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
Pilot
- Certificate: airline transport pilot
- Ratings: single-engine land; instructor: helicopter; instrument: helicopter; rotorcraft: helicopter
- Flight time: 2,808 hours in all; 29 in this make and model; 29 in the last 90 days; 6 in the last 30 days; 2,697 as pilot in command
- Last flight review: September 29, 2012
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 953 hours
- Last inspection: approved inspection programme, December 28, 2012; 3 hours since
- Maximum gross weight: 5,252 lb
- Seats: 5
- Landing gear: fixed
- Engine: Rolls-Royce 250-C47B (turboshaft); 956 hours total
- Fire on the ground
- Operator: Med-Trans Corporation
The flight
- Departed from: Mason City IA at 2:49 am
- Destination: IA76 Emmetsburg IA
Weather at the time
- Light: night
- Wind: from 300° at 8 knots
- Visibility: 8 statute miles
- Sky: broken clouds at 1,700 ft
- Temperature: 27°F (-3°C), dew point 23°F (-5°C)
- Altimeter: 30.04 inHg
- Observation at 2:53 am from MCW, 7 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 3 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
30 documents, released by the NTSB on August 11, 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.
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.
