Cessna TU206F N922MA

Summary

On 28 August 2021 at about 13:16 local time, a Cessna TU206F registered N922MA, operated by McCall Aviation Inc., was involved in an accident near Bernard, Idaho, United States. 3 people were on board and 2 died, one was seriously injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

28 August 2021 at 13:16

Classification

Accident

Location

Bernard, Idaho, United States

Coordinates

45.0093, -114.8720

Aircraft

Cessna TU206F

Registration

N922MA

Category

Airplane

Year built

1976

Engines

1

Operator

McCall Aviation Inc.

Operating rule

Part 135: Air Taxi & Commuter

Phase of flight

Not recorded

Route

McCall → Unknown

Aircraft damage

Substantial

Weather

VMC

Light

Day

NTSB number

WPR21FA330

2 people died.

The pilot’s decision to continue the flight into a canyon that exceeded the performance capabilities of the airplane, which resulted in an impact with trees an terrain.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot departed on a scenic air tour flight with two passengers over an area of mountainous terrain. After surveying the desired location, the pilot chose to fly up a canyon (drainage) to return to the departure airport. The pilot stated that he could not completely recall the events of the accident flight but reported that as the airplane neared the top of the canyon, he realized that the rate of climb was insufficient to clear the terrain ahead, and he initiated a 180° turn. He stated that he remembered extending the wing flaps but did not remember when. After starting the turn, the airplane encountered a downdraft and descended into trees. Data from an onboard GPS device indicated that the airplane entered the canyon at an altitude about 6,000 ft about 4 minutes before the impact. The airplane continued to climb until the final 3 seconds of recorded data. During the last approximate 2 minutes of recorded data, the airplane climbed from an altitude about 7,000 ft to about 8,300 ft. The airplane’s pitch attitude, which had not previously exceeded about 9° nose-up during the flight, exceeded 10° nose-up for much of the final minute of the flight and increased to a maximum of 17° nose-up about 5 seconds before the end of the data. During the final minute of the flight, the speed remained below 80 knots, ultimately decreasing to below 65 knots during the final 15 seconds of recorded data. A performance analysis indicated that, given the airplane’s gross weight and the atmospheric conditions present at the time of the accident, the airplane would have required nearly 2 additional minutes to reach and clear the top of the canyon. Postaccident examination of the wreckage did not reveal any preimpact mechanical anomalies. The wing flaps were found fully extended at the accident site. Full flap extension would have adversely affected the airplane’s climb performance; however, the point at which the flaps were fully extended could not be determined. The pilot had extensive low-level flight experience in military jets; however, he had about 28 total hours and about 3 months of experience in the accident airplane, and the accident flight was his first scenic flight with passengers. Review of weather conditions indicated light wind conditions with no evidence of mountain wave activity. The density altitude in the area of the accident site was near 10,000 ft. The circumstances of the accident are consistent with the pilot’s decision to continue into a canyon that exceeded the climb performance of the airplane, which resulted in impact with terrain during an attempted course reversal.

Quoted verbatim from the NTSB record.