- Date
- July 10, 2011, 13:25 local (19:25 UTC)
- Place
- Cedar City, UT
- Injuries
- 1 minor
- Damage
- Substantial damage
- Phase of flight
- Enroute
- Aircraft
- N2075ULeineke Walter L Thorp T-211
- Defining event
- Enroute: Fuel exhaustion
- Weather
- Visual (VMC) · Day
- Status
- Completed · report October 6, 2011
- Report
- Approved by Office Director
- NTSB office
- Western Pacific Region
- Parties
- Federal Aviation Administration
- FAA report
- 20110710015069A
- Case key
- 81067
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 pilot's misjudgment of the fuel consumption, which lead to fuel exhaustion. Contributing to the accident was the pilot's lack of experience in the accident airplane.
Findings · 4
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
The pilot reported that he was ferrying the homebuilt airplane to its new owner when the accident occurred. Having no prior time in the airplane, he flew it around the pattern to familiarize himself with the airplane's controls. The pilot stated that since he was not sure what the fuel burn of the airplane was he made an estimate using a similar aircraft with the same engine. After refueling the airplane to its 24 gallon maximum capacity, the pilot departed for the cross country flight to the destination airport. En route he climbed the airplane to 9,500 feet, leaned the mixture, and set the engine rpm to 2500. He estimated that the engine was using 4 to 4 1/2 gallons per hour, which by his calculations would give him 5 hours of flight time at that altitude. After 3.8 hours of flight, the pilot noticed the fuel gauge read 1/4 of a tank. About 6 minutes later, the engine lost power and the pilot initiated an off-airport landing. During the landing attempt, the airplane impacted a fence, struck the ground with its left wing, and tumbled. The airplane sustained substantial damage to both wings and the fuselage. The pilot stated that the fuel gauge acted normally during flight, but remained between 1/8 to 1/4 of a tank even after the airplane ran out of gas. An inspection of the fuel gauge by a mechanic showed that the gauge was functional; however, the mechanic described the type of fuel gauge as typically being difficult to calibrate and that they tend to only read accurately when the tank is full. Examination of the airplane's fuel tanks showed they were empty and the fuel system was intact.
Factual narrative
The pilot reported that he was tasked with ferrying the homebuilt airplane to its new owner. Having no prior time in the airplane, he flew it around the pattern to familiarize himself with the airplane's controls. The pilot stated that since he was not sure what the fuel burn of the airplane was he made an estimate using a similar aircraft with the same engine. After refueling the airplane to its 24 gallon maximum capacity, the pilot took off for the cross country to the destination airport. En route he climbed the airplane up to 9,500 feet, leaned the mixture, and set the engine RPM to 2500. He estimated that the engine was using 4 to 4 1/2 gallons per hour, which by his calculations would give him 5 hours of flight time at that altitude. After 3.8 hours of flight, the pilot noticed the fuel gauge read 1/4th of a tank. About 6 minutes later, the engine quit and the pilot was forced to initiate an off airport forced landing. During the landing attempt, the pilot hit a fence which caused the airplane to impact the ground with its left wing and tumble. The airplane suffered substantial damage to both wings and part of the fuselage. The pilot stated that the fuel gauge acted normally during flight, but remained between 1/8th to 1/4th of a tank even after the airplane ran out of gas. An inspection of the fuel gauge by an A&P mechanic showed that the gauge was functional; however, the mechanic described the type of fuel gauge as typically being difficult to calibrate and that they tend to only read accurately when the tank is full. Examination of the airplane's fuel tanks showed they were empty and the fuel system was intact.
Aircraft
- Registration
- N2075U
- Reported as
- Leineke Walter L Thorp T-211
- Category
- Airplane, amateur-built
- Serial number
- 08
- Engine
- Cont Motor O-200-A, 100 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Operator
- Randal S Dippold
- Registered owner
- Charles Lee
- Airworthiness certificate
- Special, Experimental (Special); Special, Experimental light sport (Special)
- Last inspection
- Condition · June 13, 2011 · 2 hours before
- Departed
- KCXP · Carson City, NV
- Destination
- KCOC · Cedar City, UT
- Airport
- CDC · Cedar City
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
- 57
- Injuries
- None
- Certificate
- Commercial
- Airplane ratings
- Multi-engine land, Single-engine sea, Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, With waivers/limitations
- Last flight review
- September 11, 2009
- Seat
- Left
- Flight hours
- 6,000 total · 7 in this make and model · 6,000 as pilot in command · 60 in the last 90 days · 20 in the last 30 days · 4 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 81 °F
Docket · 2
The files NTSB released with the investigation on August 17, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 408 KB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.