LAX92LA124

NTSB accident investigation · Cessna 150 · San Jose, CA · February 23, 1992

Accident · Minor injuriesLimited investigationFinal report
Date
February 22, 1992, 19:40 local (Feb 23, 1992, 03:40 UTC)
Place
San Jose, CA
Injuries
2 minor
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N126NKCessna 150
Weather
Visual (VMC) · Day
Status
Completed · report August 26, 1993
Report
Approved by Office Director
FAA report
19920222003379A
Case key
27563

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

That the certified flight instructor's (CFI) misjudged approach which resulted in a long landing, the cfi's in-flight decision to a go-around with partial power, and the failure of the CFI to maintain aircraft control in the initial climb segment of the partial power go-around resulting in an inadvertent stall. Contributing to the accident was the inadequate maintenance inspection performed by the operator's maintenance management personnel after the initial stuck valve deficiency and the decision of the CFI to operate the airplane with a known discrepancy.

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 - initial climb
Maintenance,inspection - inadequateCompany/operator managementFactor
Engine assembly,rocker arm/tappet - fracturedFactor
Operation with known deficiencies in equipment - intentionalPilot in command(cfi)Factor
Loss of control - in flightGo-around (vfr)
Proper touchdown point - not attainedPilot in command(cfi)Cause
Go-around - attemptedPilot in command(cfi)Factor
Aircraft performance,climb capability - loss,partial
In-flight planning/decision - poorPilot in command(cfi)Cause
Stall/spin - inadvertentPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - rising

Analysis

A Cessna 150 crashed after experiencing an in flight loss of control. During the initial takeoff on runway 31R the CFI transmitted a 'may day' call to the air traffic control tower stating the airplane had a partial loss of engine power. The local controller cleared the flight to land on any runway. The pilot executed a 180 degree turn and landed long on runway 13L. The CFI then attempted a go-around. Witnesses observed the airplane climb to 50 feet and then enter a right skidding turn, stall, and spin, impacting the ground outside of the airport boundary. The CFI indicated that the airplane's engine had previously malfunctioned with a sticking valve and thought the valve was sticking again. The post accident examiation of the engine revealed the number 4 cylinder rocker arm valve malfunctioned as a result of a fractured rocker arm shaft boss.

Aircraft

Registration
N126NK
Reported as
Cessna 150
Category
Airplane
Serial number
15073390
Airframe hours
3,565
Engine
Continental O-200-A, 100 horsepower, reciprocating
Damage
Destroyed
Flight
Instructional · Part 91
Operator
Veda Corporation
Registered owner
Veda Corporation
Airworthiness certificate
Standard, Normal; Standard, Utility
Last inspection
Annual · December 31, 1991 · 68 hours before
Airport
RHV · Reid-Hillview, runway 13, 3,101 × 75 ft, asphalt

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
24
Certificates
Private, Flight instructor, Commercial
Airplane ratings
Single-engine sea, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
1,090 total · 150 in this make and model · 700 as pilot in command · 30 in the last 90 days · 13 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
300° at 7 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
57 °F, dew point 54 °F
Altimeter
30.00 inHg
Observed at
RHV, 1 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.