BEECH C35 near Weslaco, TX — 2009-07-03
- Date
- 2009-07-03
- Location
- Weslaco, TX, USA
- Airport
- T65
- Aircraft
- BEECH C35
- Registration
- N2043D
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Go-around
Probable cause
The pilot's failure to maintain aircraft control while operating with a fuel imbalance. Contributing to the accident was the pilot/owner's decision to fly the airplane outside of the operating limitations.
Contributing factors
Contributing to the accident was the pilot/owner's decision to fly the airplane outside of the operating limitations.
NTSB narrative
Both main tanks and the left tip tank were filled with fuel prior to departure. When attempting to fuel the right tip tank, the fuel nozzle broke loose and fell into the tip tank. The pilot was unable to retrieve the broken nozzle, and no fuel was added to the tip tank, therefore the aircraft took off with a fuel imbalance between the tanks. The pilot occupied the right seat and another occupant who poissessed a student pilot certificate occupied the left seat. The supplemental type certificate (STC) directive regarding tip tank balance had not been complied with. During flight, the fuel imbalance resulted in a left rolling tendency. The pilot attempted to land at the nearest airfield, and configured the airplane with 10 degrees of flaps, which was contrary to the STC. During the landing, the airplane bounced and began to drift to the left towards the edge of the runway surface. The pilot performed a go-around and elected to turn left to enter the downwind pattern. During the left turn, directional control of the airplane was lost, and the airplane descended and impacted terrain. An examination of the airframe and engine did not reveal any pre-impact anomalies. Fracture and bending signatures on the throwover style control column and hub were consistent with the controls being positioned toward the left seat during the accident sequence. It is unknown whether the flight was instructional, and it could not be conclusively determined which occupant was at the controls at the time of the accident.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot could have aborted the landing due to left-rolling tendency before go-around.
NTSB coding
Evidence available
- Photos
- 7 docket documents
Docket documents7
Related mishaps
- CESSNA 195
2025-11-28 · Downers Grove, IL
- CIRRUS DESIGN CORP SR22
2025-11-17 · Eastpoint, FL
- CESSNA R172
2025-10-05 · Mount Carroll, IL
- TOCI GABE C G SUPA
2025-09-19 · Palmer, AK
- CIRRUS DESIGN CORP SR22
2025-08-13 · Cleburne, TX
- CIRRUS DESIGN CORP SR22
2025-06-25 · Unionville, MO