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Atlas / NTSB / CEN10LA478

NTSB CAROL · Event

Event CEN10LA478

2010-08-14 Justin, Texas, United States Airport · 16X None 1 aircraft Status: Completed

Registry · N85065

FAA Aircraft Registry record.

Make / Model

AERONCA 7CCM

Year of manufacture

1946 · 64 years old at event

Engine

CONT MOTOR C90 SERIES (95 hp)

Seats / Engines

2 seats · 1 engine

Last airworthiness date

19561217

ADS-B equipped

Yes — Mode-S ABAAA0

Registrant of record

WADE TIMOTHY K

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

A loss of engine power due to fuel starvation as a result of the pilot's delay in transferring fuel from the gravity feed wing tanks to the main tank.

Factual narrative

On August 14, 2010, approximately 1045 central daylight time, an Aeronca 7CCM, N85065, registered to and operated by the pilot, was substantially damaged when it impacted terrain during a forced landing following a loss of engine power near Justin, Texas. Visual meteorological conditions (VMC) prevailed at the time of the accident. The personal flight was being conducted under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91 without a flight plan. The pilot and passenger on board the airplane were not injured. The local flight originated from Roanoke, Texas, at 1030, and was returning to that airport when the accident occurred. According to the FAA inspector who went to the scene, the pilot said he had flown over to Prop Wash Airstrip (16X), Justin, where he made a full-stop landing. He taxied back and took off. During climb out, the engine "sputtered" and lost power. The pilot made a forced landing on a grass field near the airstrip. During the landing, the right main collapsed and the right wing and lift strut were bent. The pilot said in his written statement that accident could have been prevented if he had "Start[ed] fuel transfer from gravity feed wing tanks to [the] main tank earlier." An examination of the airplane showed substantial damage to the right main landing gear, right lower fuselage, right outboard wing and lift strut, and fracture damage to the propeller. Flight control continuity was confirmed. An examination of the engine and other airplane systems revealed no anomalies. The pilot made a full-stop landing, taxied back, and took off. During the climb out, the engine "sputtered" and lost power. The pilot made a forced landing on a grass field. During the landing, the right main landing gear fractured aft and collapsed, and the right wing and lift strut were bent. When asked how this accident could have been prevented, the pilot said he should have transferred fuel from the gravity feed wing tanks to the main tank sooner. An examination of the airplane's engine and other systems revealed no anomalies. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • C Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid management - C
  • C Personnel issues-Action/decision-Action-Delayed action-Pilot - C

Verbatim from NTSB's published report. Source file NTSB_2010_CEN10LA478.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (fuel starvation). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗