Aviation Crash Map

Cessna 172S N184NW

10 May 2022 · Traverse City, Michigan, United States · No injuries

Summary

On 10 May 2022 at about 21:26 local time, a Cessna 172S registered N184NW, operated by Northwestern Michigan College, was involved in an accident near Traverse City, Michigan, United States. 2 people were on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 21:26
Classification
Accident
Location
Traverse City, Michigan, United States
Coordinates
44.7608, -85.5925
Aircraft
Cessna 172S
Registration
N184NW
Category
Airplane
Year built
2010
Engines
1
Operator
Northwestern Michigan College
Operating rule
Part 91: General Aviation
Purpose of flight
Instructional
Phase of flight
Not recorded
Route
Gaylord → Unknown
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
CEN22LA194

People

Nobody was injured.

On board Died Serious Minor Uninjured
2 0 0 0 2

Probable cause

The failure of maintenance personnel to properly torque a fuel line “B” nut, which resulted in a total loss of engine power.

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

Read the full NTSB narrative

The pilot receiving instruction was on a visual approach to the runway during an instructional flight, at which time the engine lost total power. The flight instructor took control of the airplane and made multiple attempts to restart the engine, which were unsuccessful. The flight instructor declared an emergency and executed a forced landing to a park area about 1 mile north of the runway. During the forced landing, the airplane impacted terrain and a perimeter fence. Postaccident examination of the airplane revealed substantial damage to the right wing and engine mount. Examination of the engine and fuel system revealed a loose “B” nut fitting on the fuel line between the fuel injector and fuel manifold. The engine had recently been installed by maintenance personnel; the airplane had flown about 2.7 hours after the installation and before the accident. There was no visible impact damage to the “B” nut on the line or the fitting. Given this evidence, the “B” nut on the fuel line was likely not properly tightened during engine installation, which allowed the nut to loosen with normal engine vibration and allowed air to enter the system which resulted in total loss of engine power.

Quoted verbatim from the NTSB record.

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All 12,209 records for this type

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