LAX96LA281

NTSB accident investigation · Graham Falcon XP · Mesa, AZ · July 20, 1996

Accident · No injuriesLimited investigationFinal report
Date
July 20, 1996, 09:20 local (16:20 UTC)
Place
Mesa, AZ
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N647AAGraham Falcon XP
Weather
Visual (VMC) · Day
Status
Completed · report December 20, 1996
Report
Approved by Office Director
FAA report
19960720018989A
Case key
29516

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

blockage of the fuel system vent in the fuel cap, when the pilot overtorqued the fuel cap during his preflight check, which restricted fuel flow to the engine. The pilot's lack of experience in the make and model of airplane 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(total) - nonmechanicalTakeoff - initial climb
Fuel system,cap - overtorqueCause
Fuel system,vent - blocked(total)Cause
Aircraft preflight - inadequatePilot in commandCause
Lack of total experience in type of aircraftPilot in commandFactor
Forced landingEmergency descent/landing
In flight collision with objectEmergency landing
Object - tree(s)

Analysis

After takeoff, the pilot remained in the traffic pattern and initiated a go-around after the first landing. During the initial climb, the engine decelerated to idle, then lost all power. The pilot attempted to return to the airport, but was unable. The airplane was damaged during a forced landing in an orange grove. During an examination after the accident, no mechanical failure or malfunction was found with the engine or any of the engine components. The airplane's fuel system tank vent in the fuel cap was found closed. The design of the cap consisted of a rubber stopper that was squeezed by a threaded wing bolt. A small hole in the stopper served as a vent. When squeezing pressure was applied to the rubber stopper by turning the wing nut, the wall would expand, decreasing the size of the fuel system vent. Excessive tightening of the wing nut would squeeze the vent closed. The pilot had only about 4 hours of flight time in this make/model of airplane.

Factual narrative

On July 20, 1996, at 0920 hours mountain standard time, an experimental Graham Falcon XP, N647AA, collided with terrain after an in-flight loss of control after takeoff from Falcon Field, Mesa, Arizona. The airplane was substantially damaged and the certificated private pilot was not injured. The airplane was being operated by the pilot/owner as a personal flight. The local flight originated from Falcon Field at 0915. Visual meteorological conditions prevailed at the time.

The pilot remained in the traffic pattern after takeoff and initiated a go-around during the first landing. During the climb, the engine lost power and decelerated to idle. The pilot reported to the Falcon Field air traffic control tower he was having engine problems and asked to return to the airport. As the pilot turned the airplane to return to the airport, the engine lost all power. The airplane subsequently landed in an orange grove about .5 miles northwest of the airport.

The engine was examined by the Federal Aviation Administration (FAA) with the assistance of a mechanic familiar with Rotax engines. There was no evidence of mechanical failure or malfunction found with the engine or any of the engine components.

Examination of the airplane's fuel system revealed the tank vent in the fuel cap was closed. According to the mechanic, the design of the cap consisted of a rubber stopper that was squeezed by a threaded wing bolt. A small hole in the stopper served as a vent. When the squeezing pressure was applied to the rubber stopper by turning the wing nut, the wall would expand decreasing the diameter of the vent hole. He indicated that excessive tightening of the wing nut would also squeeze the vent closed.

According to the FAA, the pilot should have determined the airplane's fuel quantity and secured the fuel cap during his preflight check.

The pilot indicated in his accident report his total flight experience was 82 hours, of which 4 were in the Graham Falcon XP.

Aircraft

Registration
N647AA
Reported as
Graham Falcon XP
Category
Airplane, amateur-built
Serial number
600137
Engine
Rotax 503, 55 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Lawrence M. Mcdermott
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Unknown · May 26, 1996 · 4 hours before
Departed
FFZ
Airport
FFZ · Falcon Field

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
50
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Front
Flight hours
82 total · 4 in this make and model · 82 as pilot in command · 16 in the last 90 days · 3 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Visibility
20 statute miles
Lowest ceiling
25,000 ft broken
Temperature
99 °F, dew point 50 °F
Altimeter
29.00 inHg
Observed at
FFZ, 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.