DEN04LA001

NTSB accident investigation · Elliott Mustang II · Cedar City, UT · October 1, 2003

Accident · No injuriesLimited investigationFinal report
Date
October 1, 2003, 12:55 local (18:55 UTC)
Place
Cedar City, UT
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N9XQElliott Mustang II
Weather
Visual (VMC) · Day
Status
Completed · report March 2, 2004
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20031001025049A
Case key
58068

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 inadequate preflight planning/preparation which led to fuel exhaustion and subsequent loss of engine power.

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) - nonmechanicalDescent
Preflight planning/preparation - inadequatePilot in commandCause
Fluid,fuel - exhaustionFactor
Forced landingEmergency descent/landing
Emergency procedure - attemptedPilot in command
In flight collision with terrain/waterEmergency descent/landing
Terrain condition - roadway/highway

Analysis

The pilot reported that he had just begun his descent when the airplane's engine suddenly lost power. The pilot attempted a restart without success. He said he declared an emergency, and established a best glide speed. The pilot set up for a forced landing to a state highway. He said he set "full flap" and "let the airplane stall at about 25-30 [feet], which resulted in a sudden drop ..." The airplane impacted on the road. The landing gear collapsed and the airplane slid on the road, substantially damaging both wings and the forward fuselage. The airplane came to a stop within 200 feet of its initial impact point. The pilot said he fueled the 28 gallon tank to full before leaving on his trip. The pilot reported that since the refueling he had flown a total of 2 hours and 20 minutes. The pilot said that the airplane's engine burns approximately 8 to 8-1/2 gallons per hour. An examination of the fuel tanks, lines, sump, and fuel filter showed no evidence of fuel. No other anomalies with the airplane were found.

Factual narrative

On October 1, 2003, at approximately 1255 mountain daylight time, an Elliott Mustang II, N9XQ, was substantially damaged when it impacted on a road during a forced landing, following a loss of engine power, 5 miles east of Cedar City, Utah. The private pilot, the sole person on board the airplane, reported no injuries. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The cross-country flight originated at Monument Valley, Arizona, at 1200, and was en route to the pilot's private airstrip near Cedar City.

The pilot reported that he had just begun his descent into Cedar City when the airplane's engine suddenly quit. The pilot attempted a restart without success. He said he called Cedar City Flight Service, declared an emergency, and established best glide speed. The pilot set up for a forced landing on Utah State Highway 14. He said he set "full flap" and "let the airplane stall at about 25-30 [feet], which resulted in a sudden drop ..." The airplane impacted on the road. The landing gear collapsed and the airplane slid on the road, coming to a stop within 200 feet of its initial impact point.

The pilot stated he had fully fueled the airplane at Cedar City before flying to Monument Valley. He said the fuel tank held 28 gallons The pilot said the trip to Monument Valley takes about an hour and the airplane's engine burns approximately 8 to 8-1/2 gallons per hour. The pilot said he had flown about 2 hours and 20 minutes since the fueling, when the engine quit.

The airplane was examined at the accident site. It rested upright on the right edge of the highway, up against a rock face. The lower cowling and bottom of the fuselage at the cockpit area were crushed upward. The upper cowling was buckled outward. The left wing was crushed upward. The outboard-third of the left wing was bent upward approximately 70 degrees. The outboard section of the right wing was bent and broken upward and aft. The landing gear legs were broken out. One of the three propeller blades was broken aft. Flight control continuity was confirmed. An examination of the fuel tanks, lines, sump, and fuel filter showed no evidence of fuel. No other anomalies with the airplane were found.

The pilot did not return the Safety Board Form 6120.1/2. The pilot did provide a written statement and copies of his pilot and airplane records.

Aircraft

Registration
N9XQ
Reported as
Elliott Mustang II
Category
Airplane, amateur-built
Serial number
1684
Airframe hours
132
Engine
Lycoming IO-360, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Lynne E. Elliott
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · November 16, 2002 · 48 hours before
Departed
Monument Valley, AZ
Destination
CDC · Cedar City, UT

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
59
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3
Last flight review
November 30, 2001
Seat
Left
Flight hours
1,175 total · 84 in this make and model · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
210° at 20 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 36 °F
Altimeter
30.21 inHg
Observed at
CDC, 5 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.