LAX93LA041

NTSB accident investigation · Litchford Falcon XP · Palm Springs, CA · November 15, 1992

Accident · FatalLimited investigationFinal report
Date
November 15, 1992, 13:43 local (21:43 UTC)
Place
Palm Springs, CA
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
UNREGLitchford Falcon XP
Weather
Visual (VMC) · Day
Status
Completed · report August 26, 1993
Report
Approved by Office Director
Case key
27866

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's inflight loss of control for reasons related to the improper installation and functioning of the rudder control system, and, the pilot's inadvertent entry into a stall spin.

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 control - in flightTakeoff - initial climb
Flt control syst,rudder controlCause
Maintenance,installation - improperPilot in commandCause
Aircraft control - not maintainedPilot in commandCause
Stall/spin - inadvertentPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The pilot of the unregistered and unlicensed experimental homebuilt requested a high speed taxi test from the ATCT controllers with an option to takeoff for closed traffic. Witnesses said the aircraft became airborne after about a 150 foot ground roll and entered a steep climb. The pilot then reported to ATCT that 'I've just lost a rudder pedal.' The aircraft then fell off on a wing and entered a steep nose down spin or spiral to ground impact. Earlier in the day a airline pilot who also holds an a & p mechanic's certificate talked to the pilot and looked over the aircraft. The pilot told the witness that the aircraft had not flown in two or three years. The witness said he saw many discrepancies on the aircraft as he watched the pilot work on the rudder cables in the rear seat area. Some items noted by the witness were: 1) rudder cables not routed correctly on the pulleys in the cockpit area, 2) rear cockpit right rudder pedal was collapsed on the floor, and 3) rudder cables connected to the winglet rudders with bungee cords which were tied together. The witness said he recommended to the pilot that it not be flown. FAA inspectors examined the aircraft and reported that control system continuity could not be established due to cockpit impact damage.

Aircraft

Registration
UNREG
Reported as
Litchford Falcon XP
Category
Airplane, amateur-built
Serial number
600188
Engine
Rotax 503, 65 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Operator
Wayne R. Litchford
Last inspection
Unknown · January 2, 2000
Departed
PSP
Destination
PSP
Airport
PSP · Palm Springs Muni, runway 13, 8,500 × 150 ft, asphalt

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
42
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Front
Toxicology
Performed
Flight hours
1,100 total

Weather

Conditions
Visual (VMC) · Day
Wind
80° at 10 knots
Visibility
50 statute miles
Lowest ceiling
15,000 ft broken
Temperature
73 °F
Altimeter
30.00 inHg
Observed at
PSP, 1 nm away