- Date
- November 5, 2018, 16:55 local (23:55 UTC)
- Place
- Texico, NM
- Injuries
- 2 minor, 2 uninjured
- Damage
- Substantial damage
- Phase of flight
- Enroute
- Aircraft
- N3214PPiper PA24
- Defining event
- Enroute: Fuel exhaustion
- Weather
- Visual (VMC) · Dusk
- Status
- Completed · report June 10, 2019
- Report
- Approved by Office Director
- NTSB office
- General Aviation Accidents
- Parties
- FAA
- FAA report
- 20181105021519A
- Case key
- 98610
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 improper preflight fuel planning, which resulted in fuel exhaustion and a total loss of engine power.
Findings · 3
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, the day before the accident flight, he had fully refueled the airplane’s fuel tanks (60 gallons of fuel), conducted a run-up of the engine, and conducted a local flight around the pattern to troubleshoot an electrical issue that was later resolved. The pilot reported that, on the day of the accident, during the preflight inspection for the cross-country flight, the airplane was only "two gallons shy of full." About 2.5 hours into the flight, after switching the fuel tanks multiple times en route, he switched to the left main fuel tank to prepare for landing. He added that, about 4 miles south of the destination airport, the engine lost power, the airplane was "too low," and he set up to land on a nearby road. The airplane landed with the gear retracted and struck multiple signs before coming to rest. The airplane sustained substantial damage to the right wing, fuselage, and empennage. During a postaccident examination by a Federal Aviation Administration inspector, both fuel tanks were found empty, and no evidence of fuel leakage was found at the accident site. During a telephone conversation, the pilot reported that the total flight time the day of the accident was about 3.1 hours and that he was not aware of any preaccident mechanical failures. He estimated that the fuel burn was about 14 gallons per hour and that, during the accident flight, there was about a 17-knot headwind. The Pilot’s Operating Handbook for the airplane stated that, while at 75% power, the airplane has about 3.7 hours of fuel endurance. Given the evidence, it is likely that the pilot did not ensure that there was adequate fuel onboard for the accident flight, which led to fuel exhaustion and a total loss of engine power.
Factual narrative
The pilot reported that, the day before the accident flight, he had refueled the airplane to full tanks (60 gallons of fuel), did a runup of the engine, and a local flight around the pattern to trouble shoot an electrical issue, which was later resolved. The day of the accident, during the prefight for the cross country flight, the airplane was only "two gallons shy of full" during his visual inspection. About 2.5 hours into the flight after switching fuel tanks multiple times en route, he switched to the left main fuel tank to prepare for landing. He added that about 4 miles south of the destination airport the engine lost power, the airplane was "too low", and he set up to land on a nearby road. The airplane landed with the gear retracted and struck multiple signs before coming to rest. The airplane sustained substantial damage to the right wing, fuselage, and empennage. The Federal Aviation Administration (FAA) inspector reported that, the pilot stated that the airplane flew approximately one hour on the left tank, and then switched to the right tank. The pilot then flew approximately 1.5 hours on the right tank, then felt some buffeting (engine sputter) and turned the boost pump on and switched back to the left tank. The pilot reported that this occurred about 23 miles southeast of the destination airport. During a telephone conversation with the NTSB IIC, the pilot reported that the total flight time the day of the accident was about 3.1 hours, and that there were no preaccident mechanical failures that he knew of. He added that he estimated the fuel burn at about 14 gallons an hour, and estimated that during the accident flight there was about a 17 knot head wind. The pilot operating handbook for the airplane states under the endurance/range of the 56 gallon tank airplane, that while at 75% power the airplane has about 3.7 hours of fuel. During a post-accident examination by the FAA inspector, both fuel tanks were empty with no usable fuel onboard and no fuel leak indications at the accident site.
Aircraft
- Registration
- N3214P
- Reported as
- Piper PA24 (250)
- Category
- Airplane
- Serial number
- 24-292
- Built
- 1958
- Airframe hours
- 3,433.83
- Engine
- Lycoming O-540-A1A5, 250 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · May 1, 2018
- Departed
- EDC · Austin, TX
- Destination
- CVN · Texico, NM
- Airport
- CVN · Clovis Muni, runway 30, 5,697 × 150 ft, asphalt
- Equipment
- Stall warning system, Handheld GPS, Electronic flight bag or handheld device, ADS-B
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
- 25
- Injuries
- Minor
- Certificate
- Private
- Airplane ratings
- Single-engine land
- Medical
- Class 1, Without waivers/limitations
- Last flight review
- July 28, 2018
- Seat
- Front
- Restraint
- Lap only
- Flight hours
- 153 total · 29 in this make and model · 73 as pilot in command · 28 in the last 90 days · 11 in the last 30 days · 4 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Dusk
- Wind
- 280° at 9 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 61 °F, dew point 27 °F
- Altimeter
- 29.84 inHg
- Observed at
- KCVN, 3 nm away
Docket · 6
The files NTSB released with the investigation on March 18, 2019, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.6 MB 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.