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Accidents · NTSB CEN13FA122 · Final report

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

  1. Structural icing during enroute
  2. Loss of control in flight during enroute defining event
  3. 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

FatalSeriousMinorNone
Flight crew3

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.

#DocumentWhat it is
1 Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 PDF, 9 pages View Download
2 Witness Statements PDF, 12 pages View Download
3 Plot of GPS Track Data PDF, 3 pages View Download
4 GPS Track Data Log text file View Download
5 Accident Flight - Risk Assessment/weight & Balance PDF, 1 page View Download
6 Pilot Training Records PDF, 15 pages View Download
7 Helicopter Inspection Status Report PDF, 18 pages View Download
8 Operations/discrepancy Logbook - Excerpt PDF, 10 pages View Download
9 Helicopter Inspection Records - Excerpt PDF, 66 pages View Download
10 Helicopter Airworthiness Directive Listing PDF, 7 pages View Download
11 Helicopter Service Bulletin Listing PDF, 17 pages View Download
12 Helicopter Weight and Balance Record PDF, 7 pages View Download
13 Engine Control Unit - Download Summary/data Files PDF, 10 pages View Download
14 Documentation of Caution Warning Panel Light Bulb Filaments PDF, 6 pages View Download
15 Aircraft Flight Manual - Caution/warning Panel Description PDF, 1 page View Download
16 Meteorology 5 - Factual Report of Group Chairman PDF, 23 pages View Download
17 Release of Aircraft Wreckage/evidence Control PDF, 6 pages View Download
18 Statement of Party Representatives to NTSB Investigation PDF, 7 pages View Download
19 Toxicology Report PDF, 1 page View Download
20 Photo 1. Accident Site PDF, 1 page View Download
21 Photo 2. Accident Site PDF, 1 page View Download
22 Photo 3. Tail Rotor Assembly PDF, 1 page View Download
23 Photo 4. Tailboom PDF, 1 page View Download
24 Photo 5. Tail Rotor Assembly PDF, 1 page View Download
25 Photo 6. Main Rotor Hub PDF, 1 page View Download
26 Photo 7. Main Rotor Hub/transmission (Blades Removed) PDF, 1 page View Download
27 Photo 8. Hydraulic Actuators PDF, 1 page View Download
28 Photo 9. Engine PDF, 1 page View Download
29 Photo 10. Landing Skid Layout PDF, 1 page View Download
30 Revised Factual Report PDF, 6 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.