Cessna 177 accident near Moneta, Virginia, September 13, 2015
On September 13, 2015 at about 8:30 pm local time, a 1967 Cessna 177, registered N2835X, was substantially damaged in an accident during approach (VFR go-around) near Moneta, Virginia (Smith Mountain Lake airport). It was an aerial observation flight under general aviation rules (Part 91). 2 people were seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's premature retraction of the wing flaps and his subsequent failure to maintain pitch control during an attempted go-around, which resulted in the airplane exceeding its critical angle-of-attack and an aerodynamic stall. Contributing to the accident were the pilot’s inadequate in-flight fuel planning; his internal pressure to reach the airport expediently due to low fuel, which led to a high and fast approach; and his subsequent decision to go around when low on fuel.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- September 13, 2015 · about 8:30 pm local time
- Place
- Moneta, Virginia · Smith Mountain Lake · map
- Type
- Accident
- Injuries
- 2 people were seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Cessna 177 UNDESIGNAT, built 1967 · all 177s on the register
- Registration
- N2835X · no longer on the register · serial 17700235
- Damage
- Substantial damage
- Flight
- Aerial observation flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The commercial pilot was conducting an aerial photographic flight with one passenger on board. The airplane had been filled with fuel the day before the accident flight. On the day of the accident, the airplane was flown to and landed at two airports before it departed for the accident flight. The airplane was not refueled before the accident flight. According to the passenger, during the accident flight, the pilot chose to land because the airplane was "low on fuel." Two witnesses stated that the airplane was high and fast on the approach. One witness stated that the airplane had a high groundspeed on the runway. The passenger stated that, during the landing, the wind "pushed" the airplane too far down the runway and that, when the airplane was about 80 percent of the way down the runway, the pilot attempted to perform a go-around. The passenger added that, during climbout, the engine did not sound normal, the stall horn sounded, and the airplane then impacted trees and that, after the airplane came to rest, fuel was "pouring onto them." A postcrash fire ensued. Examination of the airframe and engine did not find any abnormalities that would have precluded normal operation. The examination revealed that one propeller blade was fractured in at least three segments, which was indicative of rotation at the time of impact. Although it is likely that the engine was developing power at the time of impact, the investigation could not determine the amount of power that was being developed or applied at that time. Although the pilot stated that the airplane was low on fuel and the passenger reported that the engine did not sound normal during the go-around, the amount of available fuel could not be determined. However, if the airplane was in a very low fuel state, the pilot might have felt a sense of urgency to get the airplane on the ground before the fuel was exhausted. He may have then rushed the approach to the airport, which led to the airplane being high and fast as it neared the runway and resulted in the need to go around late in the ground roll. The flap position was found at less than 10 degrees; however, according to the go-around checklist in the Pilot's Operating Handbook (POH), the flaps should be retracted to "1/2," which correlates to 15 degrees, until the airplane reaches an airspeed of about 75 mph. Therefore, it is likely that the flaps were in transit at the time of impact because the pilot had prematurely retracted the flaps. Further, the POH states that "application of maximum allowable power [during a go-around] will require considerable control pressure to maintain a climb pitch attitude. The addition of power will tend to raise the airplane's nose suddenly and veer to the left. Forward elevator pressure must be anticipated and applied to hold the nose in a safe climb attitude…" It is likely that the combination of the premature retraction of the flaps and insufficient forward pressure led to the pilot's inability to maintain pitch control, which resulted in the airplane exceeding its critical angle-of-attack and a subsequent aerodynamic stall.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Miscellaneous/other during approach (VFR pattern final)
- Fuel starvation during approach (VFR go-around)
- Loss of engine power (partial) during approach (VFR go-around)
- Aerodynamic stall/spin during approach (VFR go-around) defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
- Fire/smoke (post-impact) during post (impact)
The NTSB's findings
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Capability exceeded
- cause Personnel issues › Task performance › Use of equip/info › Use of equip/system › Pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Pitch control › Not attained/maintained
- factor Personnel issues › Task performance › Planning/preparation › Fuel planning › Pilot
- factor Aircraft › Fluids/misc hardware › Fluids › Fuel › Fluid level
- factor Personnel issues › Psychological › Personality/attitude › Motivation/respond to pressure › Pilot
- factor Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Landing flare › Incorrect use/operation
- factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
Pilot
- Certificate: commercial pilot
- Ratings: single-engine land; instrument: airplane; instrument: helicopter; rotorcraft: helicopter
- Flight time: 779 hours in all; 20 in this make and model
- Last flight review: March 30, 2015
- Medical certificate: Class 1 (with waivers/limitations)
- Seat: left
- Injury: serious injuries
The aircraft
- Airframe total time: 3,777 hours
- Last inspection: annual inspection, September 1, 2015
- Maximum gross weight: 2,350 lb
- Seats: 4
- Landing gear: retractable
- Engine: Lycoming O-320-E2D (piston); 3,777 hours total
- Fire on the ground
- Operator: Dap Imaging, Inc.
The flight
- Departed from: ORF Norfolk VA
- Destination: W91 Moneta VA
- Flight plan: none
- Runway 23, 3,058 ft by 50 ft
Weather at the time
- Light: daylight
- Wind: from 330° at 9 knots
- Visibility: 10 statute miles
- Sky: broken clouds at 6,000 ft; scat at 5,000 ft
- Temperature: 66°F (19°C), dew point 46°F (8°C)
- Altimeter: 29.98 inHg
- Observation at 8:54 pm from ROA, 22 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
Other NTSB records under N2835X the same tail number, which may have belonged to a different aircraft at the time
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
