LAX91LA090

NTSB accident investigation · Riddell Lancair 235 · Agua Caliente, CA · February 1, 1991

Accident · Serious injuriesLimited investigationFinal report
Date
February 1, 1991, 12:30 local (20:30 UTC)
Place
Agua Caliente, CA
Injuries
2 serious
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N17SRiddell Lancair 235
Weather
Visual (VMC) · Day
Status
Completed · report March 31, 1993
Report
Approved by Office Director
FAA report
19910201003529A
Case key
27107

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

The failure of the propeller blades due to a weakening of the wood structure due to acid hydrolysis. A factor in the accident was the inadequate maintenance of the propeller assembly by allowing exposure to excessive moisture and heat.

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.

Airframe/component/system failure/malfunctionClimb - to cruise
Propeller system/accessories,blade - delaminationCause
Propeller system/accessories,blade - failure,totalCause
Maintenance,service of aircraft/equipment - inadequateOther maintenance personnelFactor
Forced landingDescent - emergency

Analysis

The aircraft was on climb out when a loud bang was heard, followed by an engine overspeed then engine stoppage. After the forced landing, the pilots found that both wooden propeller blades had separated from the steel hub assembly. The propeller hub was removed from the engine and sent to the manufacturer for functional analysis and disassembly under the supervision of FAA inspectors. The manufacturer stated that all internal components were functional, however, the cam adjustment for the high and low pitch stop settings had been altered from the factory settings. The blade butt ends retained in the hub were removed and submitted to the forest products laboratory of the us department of agriculture for analysis. According to the laboratory the wooden blades fractured and separated due to a hydrolysis interaction between the wood and the adhesive caused by excess moisture and heat. The hydrolysis is a chemical decomposition process of the wood and glue relationship.

Aircraft

Registration
N17S
Reported as
Riddell Lancair 235 (LANCAIR 23)
Category
Airplane, amateur-built
Serial number
OJ-1988
Engine
Lycoming O-320, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Kenneth E. Parks
Registered owner
Kenneth E. Parks
Last inspection
Unknown · January 2, 2000
Departed
MYF · San Diego, 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
47
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Flight hours
1,500 total · 400 in this make and model · 4,500 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
90° at 15 knots
Visibility
10 statute miles
Lowest ceiling
None

FAA reports on this event · 1

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