Aviation Crash Map

Cessna T210M N761YZ

17 December 2017 · Oldenburg, Indiana, United States · Fatal

Summary

On 17 December 2017 at about 01:57 local time, a Cessna T210M registered N761YZ was involved in an accident near Oldenburg, Indiana, United States. 3 people were on board and 3 died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 01:57
Classification
Accident
Location
Oldenburg, Indiana, United States
Nearest airport
Batesville (HLB)
Coordinates
39.3725, -85.2481
Aircraft
Cessna T210M
Registration
N761YZ
Category
Airplane
Year built
1978
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Columbus → Frederick
Aircraft damage
Destroyed
Weather
VMC
Light
Night/Dark
NTSB number
CEN18FA053

People

3 people died.

On board Died Serious Minor Uninjured
3 3 0 0 0

Probable cause

A total loss of engine power due to the failure of the No. 4 piston, which resulted in an attempted forced landing in dark night conditions and a subsequent in-flight collision with trees and terrain. Contributing to the accident were the pilot's situational stress and fatigue, both of which degraded his performance.

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

Read the full NTSB narrative

The airline transport pilot and two passengers, one of whom was pilot-rated, were conducting a cross-country flight in dark, night visual conditions. During an en route climb to the assigned cruise altitude, the airplane experienced a loss of engine power about 6,600 ft above ground level (agl). The pilot identified a diversionary airport located about 4 miles northeast of the airplane's position and subsequently established a course toward that airport. The air traffic controller immediately informed the pilot that the airport was closed. However, based on the pilot's stated intention to divert to the airport, the controller provided radar vectors to assist the pilot. The airplane subsequently overflew the airport about 3,000 ft agl. However, instead of circling the airport, the pilot continued about 1 1/2 miles north and entered a right gliding turn until the airplane impacted trees and terrain about 2 miles north of the airport. A postaccident airframe examination did not reveal any anomalies consistent with an airframe structural failure or a malfunction of the flight control system. An engine examination revealed that the No. 4 piston had failed. Specifically, the perimeter of the No. 4 piston crown had separated, resulting in the separation of the upper compression ring and compression ring insert. Metallurgical examination determined that the piston failure was caused by the disbonding of the upper piston ring insert from the piston body. Lead deposits were present on parts of the piston body that formed an interface with the insert. The deposits were abraded in areas exposing the underlying piston material. The abraded areas where the deposits had been worn away could only have occurred if the upper piston ring insert had disbonded from the piston body before the piston failed. The disbonding of the insert was likely caused by a manufacturing anomaly; however, due to the extensive damage to the piston and the insert, it was not possible to determine with any more precision where the failure started or the nature of the defect that might have caused it. An airplane performance study revealed that no airports other than the diversionary airport were within the power-off glide range of the airplane at the time of the loss of engine power. Thus, the location of the airplane at the time of the loss of engine power presented the pilot with limited options for a forced landing. Furthermore, the pilot's ability to discern a suitable off-airport landing area was hindered by the dark night lighting conditions. Although, an interstate highway was below the airplane, attempting to execute a forced landing on an unlighted roadway at night presented significant hazards. In contrast, approach paths to an airport are generally free of obstructions. Therefore, the pilot's decision to alter course toward the diversionary airport, even though it was closed and unlighted, was understandable. However, once the airplane was positioned over the airport, the pilot did not circle but continued to fly north into an area with more limited opportunities for a successful forced landing. A review of the available medical information did not reveal the presence of any condition or medication that would have led to an incapacitation or impairment of the pilot. However, the pilot was likely fatigued at the time of the accident due to the length of time he had been awake, and the significant amount of flight time completed on the day of the accident. This may have narrowed the pilot's attention during the emergency. Additionally, situational stress imposed by the engine failure and the necessity to find a forced landing site in dark night conditions further reduced the pilot's ability to maintain situational awareness. The pilot-rated passenger's medical history included conditions and medications that, while unlikely to cause any sudden incapacitation, could potentially be impairing. However, the investigation was unable to determine the extent of impairment, if any, that might have been present at the time of the accident.

Quoted verbatim from the NTSB record.

Other Cessna T210M accidents

Date Aircraft Location Operator Outcome Died
5 Apr 2017 Cessna T210M
N1215M
Detroit Lakes, Minnesota, United States - No injuries -
12 Dec 2016 Cessna T210M
N761SZ
Mecca, California, United States - Serious injuries -
10 Apr 2015 Cessna T210M
N732YQ
Challis, Idaho, United States - Fatal 4
2 Nov 2014 Cessna T210M
N1593M
Jacksonville, Oregon, United States - Minor injuries -
24 Oct 2014 Cessna T210M
N761SU
Bay City, Wisconsin, United States - Fatal 1
6 Apr 2014 Cessna T210M
N761BT
Lee's Summit, Missouri, United States Mar-Tech Engineering, LLC Serious injuries -

All 231 records for this type

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