MIA91FA017

NTSB accident investigation · Cessna 150G · Marathon, FL · October 30, 1990

Accident · FatalField investigationFinal report
Date
October 30, 1990, 08:05 local (13:05 UTC)
Place
Marathon, FL
Injuries
1 fatal, 1 serious
Damage
Destroyed
Phase of flight
Takeoff
Aircraft
N3220JCessna 150G
Weather
Visual (VMC) · Day
Status
Completed · report July 10, 1992
Report
Approved by Office Director
Safety recommendations
Yes
FAA report
19901030047409A
Case key
32735

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 pilot-in-command's failure to maintain airspeed, while attempting to make a forced landing following a partial loss of engine power. Fatigue failure of the center rocker boss on the #3 cylinder was a related factor.

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(partial) - mech failure/malfTakeoff
Engine assembly,cylinder - fatigueCause
Forced landingDescent - emergency
Loss of control - in flightDescent - emergency
Airspeed - not maintainedPilot in commandCause
Stall - inadvertentPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

While on a x-wind after a tough-&-go lndg, a partial loss of eng power occurred. The instructor (CFI) took ctl & mnvrd the acft to land. The acft was not aligned with the rwy, so the CFI elected to land in a grass area. He stated that while dscndg thru about 100' AGL, 'the yoke fell backward' into his lap. He believed that the elevator cable had failed, which allowed the acft to crash. However, according to witnesses, a steep turn was made in an atmt to align the acft for landing; then the acft leveled off at about 30' AGL & was at a slow speed. The acft then entered a steep dscnt & crashed. No preimpact mechanical problem was found with the flt ctl sys. A metallurgical exam showed that the elevator up cable had failed under a tensile load while being bent around an edge or corner. An exam of the eng revealed that the center rocker boss on the #3 cylinder had failed in fatigue. The fatigue had originated where numbers were embossed into the boss drg manufacture.

Aircraft

Registration
N3220J
Reported as
Cessna 150G
Category
Airplane
Serial number
15065920
Airframe hours
4,922
Engine
Continental O-200-A, 100 horsepower, reciprocating
Damage
Destroyed
Flight
Instructional · Part 91
Registered owner
Blue Max, Inc.
Airworthiness certificate
Standard, Utility; Standard, Normal
Last inspection
100 hour · August 30, 1990 · 57 hours before
Airport
MTH · Marathon, runway 7, 5,008 × 100 ft, grass/turf

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
27
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Toxicology
Performed
Flight hours
320 total · 23 in this make and model · 209 as pilot in command · 53 in the last 90 days · 47 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
30° at 15 knots
Visibility
10 statute miles
Lowest ceiling
9,000 ft broken
Temperature
73 °F, dew point 64 °F
Altimeter
30.00 inHg
Observed at
MTH

FAA reports on this event · 1

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

Other investigations on N3220J · 1

Matched to the same aircraft by N-number and date.