Beechcraft A36TC C-FFIH

Summary

On 27 October 2009 at about 12:42 local time, a Beechcraft A36TC registered C-FFIH was involved in an accident near Kalamazoo, Michigan, United States. One person was on board and one died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

27 October 2009 at 12:42

Classification

Accident

Location

Kalamazoo, Michigan, United States

Nearest airport

Kalamazoo/Battle Creek Intl (AZO)

Coordinates

42.2450, -85.5486

Aircraft

Beechcraft A36TC

Registration

C-FFIH

Category

Airplane

Engines

1

Operator

Not recorded

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

Kalamazoo → Muskoka, ON

Aircraft damage

Destroyed

Weather

IMC

Light

Day

NTSB number

CEN10FA029

1 person died.

The loss of engine power for an undetermined reason.

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

Read the full NTSB narrative

Witnesses and global positioning system data indicated that after takeoff the airplane tracked the runway centerline and climbed approximately 150 feet above ground level before turning to the right and descending. The airplane subsequently impacted the ground, a fence, and a pole about 1,400 feet from the departure end of the runway. A postimpact fire ensued. After acknowledging the takeoff clearance, no further communications were received from the accident airplane. Examination of the airplane’s structure, flight controls, engine controls, and fuel system did not reveal any anomalies consistent with a preimpact failure. The engine manufacturer had issued a Mandatory Service Bulletin (MSB) that was applicable to the accident airplane’s engine. The airplane’s engine was disassembled in order to replace components damaged during the impact sequence. During the disassembly the valve lifters that were the subject of the MSB were examined and found to have pitting. However, the engine was reassembled with the original valve lifters for a functional test run and during the test run the engine produced full rated power and no anomalies were noted. Data retrieved from an engine monitoring system installed on the accident airplane recorded a significant reduction in engine power during the accident takeoff. The monitoring system did not record throttle, mixture, or propeller control positions and the data was consistent with normal power reductions recorded during the landing phase of previous flights. No mechanical reason for the loss of engine power was found.

Quoted verbatim from the NTSB record.