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June 7, 2023 · Cessna A188B · N731UF

Chillicothe, MO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 7, 2023
Injury Outcomes
1 injury (1 minor injury)
Location
Chillicothe, MO
Aircraft
Cessna A188B (1978)
Tail Number
N731UF
Injuries
Minor
Aircraft Damage
Destroyed
NTSB Number
WPR23LA218

The airplane sustained a partial loss of engine power while maneuvering to apply fertilizer to a corn field. The pilot initiated a forced landing to a clearing, during which the airplane struck trees and powerlines before it came to rest upright in an open field; a postaccident fire ensued. Examination of the of the airplane revealed that the cockpit and fuselage structure was mostly destroyed by thermal and impact damage. Examination of the engine revealed a tear on the fuel manifold assembly diaphragm. The tear in the diaphragm likely result in the fuel manifold’s inability to provide sufficient fuel pressure to maintain engine power, resulting in a partial loss of engine power.

NTSB Probable Cause

A partial loss of engine power due to a tear in the fuel manifold diaphragm, which prevented sufficient fuel flow to the engine.

Full Narrative

On June 7, 2023, about 1415 central daylight time, a Cessna A188B, N731UF, was destroyed when it was involved in an accident near Chillicothe, Missouri. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 agricultural flight. The pilot reported that the airplane sustained a partial loss of engine power while he was maneuvering to apply fertilizer to a corn field about ½ mile from the departure airport. He ensured the throttle was in the full forward position and turned on the emergency electric auxiliary fuel pump to no avail. Unable to maintain altitude, the pilot elected to conduct an off-airport landing and, during the descent, the airplane struck trees and powerlines before it came to rest upright in an open field; a postaccident fire ensued. Postaccident examination of the airplane revealed that the cockpit and fuselage structure was mostly destroyed by thermal and impact damage. The engine, engine mount, firewall, main landing gear, instrument panel, flight controls, and seats were separated and exhibited varying degrees of thermal and impact damage. Examination of the fuel manifold revealed it remained attached to its respective mount and was undamaged. The No. 6 fuel injector line and the nozzle pressure gauge fitting were fracture separated. The fuel manifold assembly was removed and subsequently disassembled. The internal diaphragm exhibited an approximate 1-inch tear and the spring was undamaged. No additional anomalies were noted with the engine or airframe. No reference to any maintenance performed on the fuel manifold was observed within the engine and airframe logbooks. The engine was last overhauled on July 10, 2009.

Flight

Event TypeAccident
Event Time14:15 CDT
Nearest Airport0nm
Flight Plan FiledNone
Aircraft FireGrd
Aircraft ExplosionNo

Aircraft

AircraftCessna A188B
Tail NumberN731UF
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 137
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-540-K1A5 · Reciprocating · 300
Seats1

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 51 · Second Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind10° @ 5 kt
CeilingNone
Temperature / Dew Point63 F
Altimeter29.84 inHg
Observation Time13:51
Weather SourceWFAC

Appendix: Source Data