LAX92LA258

NTSB accident investigation · Cessna T210N · Georgetown, CA · June 24, 1992

Accident · Minor injuriesLimited investigationFinal report
Date
June 23, 1992, 16:20 local (Jun 24, 1992, 00:20 UTC)
Place
Georgetown, CA
Injuries
2 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N9933NCessna T210N
Weather
Visual (VMC) · Day
Status
Completed · report August 26, 1993
Report
Approved by Office Director
FAA report
19920623021569A
Case key
27657

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The under torque of the crankcase through bolts during overhaul causing; 1) the number 2 main bearing to spin, 2) the resultant blockage of the internal oil passage, and 3) the oil starvation induced failure of the number 2 connecting rod and cap. A factor in the accident was the unsuitable nature of the terrain which made a successful forced landing impossible.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - mech failure/malfCruise - normal
Engine assembly,other - undertorquedCause
Maintenance,overhaul - improperOther maintenance personnelCause
Engine assembly,bearing - slippedCause
Lubricating system,oil port/passage,internal - blocked(total)Cause
Fluid,oil - starvationCause
Engine assembly,connecting rod cap - failure,totalCause
Forced landingDescent - emergency
Terrain condition - none suitableFactor
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - uphill
Terrain condition - rough/uneven
Terrain condition - high obstruction(s)

Analysis

The pilot said he was in cruise at 10,500 feet when the oil pressure went to zero and the oil temperature rose. The engine quit shortly thereafter. The aircraft then collided with ground obstructions during a uphill forced landing attempt in mountainous terrain. External examination of the engine revealed that the number 2 connecting rod had failed and was sticking up through the case. Internal examination of the engine revealed that the number 2 main bearing had spun in the journal, with severe abrasion noted under the bearing inserts. The oil channel in the number 2 main bearing journal was found totally plugged with metal particles. Progressive heat discoloration and component distress was found downstream in the oiling path of the number 2 main bearing. The engine and bearings was examined by a technical representative from Continental engines who opined that the bearing had been intermittently spinning on the journal for 10 hours and that the failure of the number 2 connecting rod was due to oil starvation caused by the restrictions in the oil path. He stated that the most likely cause of the bearing spin condition was under torque of the case through bolts at the number 2 main bearing area. The engine was overhauled 70 hours prior to the accident.

Aircraft

Registration
N9933N
Reported as
Cessna T210N
Category
Airplane
Serial number
21063255
Airframe hours
2,721
Engine
Continental TSIO-520-R, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Operator
Glacier Ice Company, Inc.
Registered owner
Glacier Ice Company, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · October 26, 1991 · 19 hours before
Departed
TRK · Truckee, CA
Destination
LVK · Livermore, CA

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
26
Certificates
Airline transport, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
3,400 total · 200 in this make and model · 3,000 as pilot in command · 90 in the last 90 days · 30 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
30° at 10 knots
Visibility
40 statute miles
Lowest ceiling
22,000 ft overcast
Temperature
70 °F, dew point 50 °F
Altimeter
29.00 inHg

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.