LAX92FA289

NTSB accident investigation · Cessna T210N · Superior, AZ · July 9, 1992

Accident · FatalField investigationFinal report
Date
July 9, 1992, 07:50 local (14:50 UTC)
Place
Superior, AZ
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N6483CCessna T210N
Weather
Visual (VMC) · Day
Status
Completed · report June 30, 1993
Report
Approved by Office Director
FAA report
19920709024559A
Case key
27441

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

On this page

Probable cause

An inadequate major engine overhaul procedure, during which previous crankshaft damage was not detected. Contributing to the accident was a surface initiated fatigue failure of the engine crankshaft.

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,crankshaft - fatigue
Maintenance,overhaul,major - inadequateOther maintenance personnelCause
Forced landingDescent - emergency
In flight collision with terrain/waterLanding - flare/touchdown
Terrain condition - rough/uneven
Proper touchdown point - not attainedPilot in command

Analysis

The certificated private pilot, the sole occupant, was on a cross country business flight when the engine quit. The pilot made a forced landing about 250 feet short of a dirt airstrip. The airplane was destroyed by impact and a post impact fire, and the pilot was fatally injured. Examination of the engine revealed a broken crankshaft on the crankcheek adjacent to the number 1 cylinder. The crankshaft had been replaced 42 hours prior to the accident. The crankshaft was supplied from an engine with an accumulated total time of about 1,000 hours of operation that had previously sustained a separation of the number 1 cylinder from the engine case. After an inspection, the crankshaft was determined to be serviceable and installed in the accident airplane's engine. Metallurgical examination revealed a high cycle fatigue failure consistent with surface initiated cracking. A metallurgical report indicated that surface cracking would not be expected in the area of failure unless prior damage to the surface had occurred.

Aircraft

Registration
N6483C
Reported as
Cessna T210N
Category
Airplane
Serial number
21063900
Airframe hours
2,894
Engine
Continental TSIO-520-R, 285 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Business · Part 91
Operator
Edward Curtis
Registered owner
Edward Curtis
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 17, 1992 · 35 hours before
Departed
SAD · Safford, AZ
Destination
PHX · Phoenix, AZ
Airport
E81 · Superior

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
51
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
1,000 total · 600 in this make and model · 20 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
60° at 3 knots
Visibility
30 statute miles
Lowest ceiling
25,000 ft broken
Temperature
88 °F, dew point 61 °F
Altimeter
30.00 inHg
Observed at
IWA, 32 nm away

FAA reports on this event · 1

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