Plane Crash List

Cessna 210M N9139M

20 November 1990 · Fallbrook, California, United States · Serious injuries

Summary

On 20 November 1990 at about 20:00 local time, a Cessna 210M registered N9139M, operated by Self Enterprises, was involved in an accident near Fallbrook, California, United States. One person was on board and one was seriously injured. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 20:00
Classification
Accident
Location
Fallbrook, California, United States
Coordinates
33.3892, -117.2105
Aircraft
Cessna 210M
Registration
N9139M
Category
Airplane
Engines
1
Operator
Self Enterprises
Operating rule
Part 91: General Aviation
Purpose of flight
Business
Phase of flight
Not recorded
Route
Unknown → Unknown
Aircraft damage
Destroyed
Weather
VMC
Light
Day
NTSB number
LAX91LA035

People

1 person was seriously injured.

On board Died Serious Minor Uninjured
1 0 1 0 0

Probable cause

THE FAILURE OF THE NUMBER 5 CYLINDER PISTON CONNECTING ROD DUE TO BENDING AND SUBSEQUENT FATIGUE FRACTURE. CONTRIBUTING TO THE ACCIDENT WAS THE IMPROPER STARTING PROCEDURE ACCOMPLISHED BY AN UNIDENTIFIED PERSON WHICH RESULTED IN EXCESSIVE FUEL IN THE CYLINDER RESULTING IN A HYDRAULIC LOCK WITHIN THE NUMBER 5 CYLINDER.

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

Read the full NTSB narrative

A CESSNA 210M LOST ENG POWER AND COLLIDED WITH A POLE AFTER A FORCED LANDING ON A CITY STREET. THE ENGINE CRANKCASE WAS FRACTURED AND THE #5 PISTON CONNECTING ROD HAD SEPARATED FROM THE ENG AND WAS FOUND ALONG THE WRECKAGE PATH. EXAM OF THE NUMBER 5 CYLINDER WALL DISCLOSED EVIDENCE OF THE AREA BELOW THE NORMAL PISTON STROKE BEING SCRAPED BY THE PISTON RINGS. ACCORDING TO THE METALLURGIC REPORT, THE PISTON'S CONNECTING ROD FAILED DUE TO A FATIGUE CRACK. THE CONNECTING ROD WAS BENT SOME TIME AFTER INITIAL ENG OPERATION. THE BENDING THAT OCCURRED TO THE NO. 5 CONNECTING ROD IS CHARACTERISTIC OF AN HYD LOCK CONDITION WHERE THE PISTON IS FORCED AGAINST INCOMPRESSIBLE FLUIDS BETWEEN THE PISTON AND CYLINDER HEAD. NO INDICATION OF METALLURGICAL DEFECT WAS OBSERVED IN THE CONNECTING ROD. HARDNESS READINGS ON THE CONNECTING ROD, WHICH INDICATES THE STRENGTH, CONFORMED TO MATERIAL SPECIFICATIONS. THE MAINTENANCE RECORDS NOTE THAT A MAJOR OVERHAUL WAS ACCOMPLISHED 207.8 HOURS BEFORE THE ACCIDENT.

Quoted verbatim from the NTSB record.

Other Cessna 210 accidents

Date Aircraft Location Operator Outcome Died
30 Sep 1990 Cessna 210
N6523X
White Plains, Georgia, United States Grecol Aviation, Inc. No injuries -
26 Feb 1990 Cessna 210-M
N525CW
Sarasota, Florida, United States
no coordinates
Flight Express Serious injuries -
25 Jun 1990 Cessna 210L
N732BL
Fort Lauderdale, Florida, United States - No injuries -
12 Jan 1990 Cessna 210M
N9064M
Ocala, Florida, United States
no coordinates
Cherokee Express No injuries -
22 Nov 1990 Cessna 210G
N5819F
Indianapolis, Indiana, United States Larry E. Bailey Minor injuries -
16 Apr 1990 Cessna 210
N6182R
Eden Prairie, Minnesota, United States Olsen, Loren T Minor injuries -

All 2,022 records for this type

Other accidents in this area

Date Aircraft Location Operator Outcome Died
15 Apr 1990 Cessna 180
N9394C
Soledad, California, United States - No injuries -
10 Oct 1990 Cessna 150
N68350
Riverside, California, United States PAR Flight No injuries -
17 Apr 1990 Piper PA46
N4387S
Paso Robles, California, United States Piper Aircraft Corp. No injuries -
7 Oct 1990 Cessna 182M
N70892
Bakersfield, California, United States - No injuries -
1 Apr 1990 Piper J-3
N7363H
Creston, California, United States - Minor injuries -
11 Oct 1990 Bell 47G4
N477JM
Merced, California, United States John W. Myers Serious injuries -

All 170,864 records in United States