NTSB CAROL · Event
Event DEN06LA063
Registry · N7JC
FAA Aircraft Registry record.
Make / Model
VAN'S AIRCRAFT RV-9A
Year of manufacture
2001 · 5 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20020122
ADS-B equipped
Yes — Mode-S A950A7
Registrant of record
JCMC INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Vapor lock which resulted in total engine failure and the pilot's abrupt brake application on touchdown. Factors contributing to the accident were the improper design of the fuel system resulting in the misrouting of the fuel lines close to the exhaust pipes, and the short landing area.
Factual narrative
On April 13, 2006, about 1945 central daylight time, a Rumble/Williams/Boomhower Starduster II, amateur-built airplane, N7JC, was substantially damaged when the airplane nosed over during a forced landing at the Junction City Airport, Junction City, Kansas. 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 private pilot on board the airplane was not injured. The flight was originating at the time of the accident and was en route to Chapman, Kansas. The pilot reported taking off from runway 5 (1,927 feet by 200 feet, dry grass) at Junction City. He said he "Checked engine instruments as normal, applied power and everything was normal on take off. At approximately 150 - 200 feet agl (above ground level) the engine stopped suddenly with no indication of roughness or power drop of any kind." the pilot said he verified the throttle's position and pumped it with no resumption of power. The pilot attempted a forced landing on the remaining runway ahead of him. He said that on touchdown he attempted to stop the airplane before reaching a ravine in front of him. The pilot said he applied "hard brakes and held the tail high to increase braking effectiveness. Initially I could feel the wheels skidding on the grass. As speed began to bleed off, weight loaded on the tires, the brakes became more effective, and the aircraft nosed over onto its back adjacent to the end of the runway." An examination of the airplane showed substantial damage to the top wing and vertical stabilizer and rudder. The propeller was bent and the spinner was crushed aft. Flight control continuity was confirmed. An examination of the engine showed that the fuel lines had been routed to within 1-1/4 inches of the dual exhaust pipes. FAA requirements for certificated airplanes requires a minimum of 6 inches separation due to the potential for fuel in the lines to boil and subsequently cause a vapor lock in the lines. No other anomalies were found. The pilot reported making a normal takeoff and climb out. At about 200 feet above the ground, the pilot said the engine lost power without any prior warning. The pilot immediately executed a forced landing. On touchdown, the pilot applied "hard brakes" to avoid a ravine at the end of the grass strip. The airplane subsequently nosed over on its back causing substantial damage to the top wing, vertical stabilizer, and rudder. An examination of the engine showed that the fuel lines had been routed within 1-1/4 inches of the dual exhaust pipes. FAA requirements for certified airplanes requires a minimum of 6 inches separation due to the potential for fuel in the lines to boil and subsequently cause a vapor lock in the lines. No other anomalies were found. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_DEN06LA063.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
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