Sikorsky 269C accident near Burnham, Maine, July 3, 2013
On July 3, 2013 at about 8:48 pm local time, a Sikorsky 269C (helicopter), registered N888ZW, was substantially damaged in an accident during maneuvering (low-alt flying) near Burnham, Maine. It was an aerial observation flight under general aviation rules (Part 91). 1 person was seriously injured and 1 person had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's failure to maintain yaw control while operating out of ground effect at a low airspeed, which resulted in the loss of tail rotor effectiveness, an uncontrolled descent, and an in-flight collision with trees and terrain. Contributing to the accident was the pilot's failure to recognize that the low-altitude maneuvering during the aerial observation flight could lead to a loss of tail rotor effectiveness.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- July 3, 2013 · about 8:48 pm local time
- Place
- Burnham, Maine · map
- Type
- Accident
- Injuries
- 1 person was seriously injured and 1 person had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Sikorsky 269C
- Registration
- N888ZW · no longer on the register · serial S1497
- Damage
- Substantial damage
- Flight
- Aerial observation flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
**This report was modified on February 23, 2015. Please see the public docket for this accident to view the original report.** The pilot reported that, during a black bear-tracking flight while flying the helicopter about 50 feet above tree tops at an airspeed of between 10 and 20 knots with a "fairly calm" wind and the engine instruments reading normal, he began a "fading right turn" (that is, a right turn with a sideways component of flight leading into it.) During the turn, the pilot input a "modicum" of left antitorque pedal while slowing. About 2 seconds after initiating the right turn and while the helicopter was about 30 to 40 feet above the trees, the turn escalated into a right (or clockwise) spin about the main rotor axis despite the pilot's left pedal inputs, which is consistent with a sudden loss of tail rotor authority. The helicopter subsequently impacted trees and terrain. The passenger, who had only been flown once previously in a helicopter, reported that the helicopter spun counterclockwise. Postaccident examinations of the airframe, flight controls, main and tail rotor drive system components, engine, and engine accessories revealed no evidence of preimpact failure or malfunction. Although the pilot and passenger descriptions of the direction of the spin were inconsistent, the lack of any mechanical issue with the helicopter or its engine, the pilot's comment that the engine readings were normal at the start of the turn, and the helicopter's flight condition when the loss of control occurred (operating out of ground effect and turning right at a low airspeed) were consistent with a loss of tail rotor effectiveness during the right turn, resulting in a right (clockwise) spin.
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
- Loss of tail rotor effectiveness during maneuvering (low-alt flying) defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Directional control › Not attained/maintained
- factor Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Not specified
- factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
Pilot
- Certificate: commercial pilot, private
- Ratings: multi-engine land; single-engine land; single-engine sea; instrument: airplane; rotorcraft: helicopter
- Flight time: 1,165 hours in all; 419 in this make and model; 27 in the last 90 days; 6 in the last 30 days; 1,024 as pilot in command
- Last flight review: March 15, 2012
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: left
- Injury: serious injuries
The aircraft
- Airframe total time: 2,233 hours
- Last inspection: annual inspection, May 30, 2013
- Maximum gross weight: 2,050 lb
- Seats: 3
- Landing gear: fixed
- Engine: Lycoming HIO-360-D1A (piston); 0 hours total
- Operator: Point Of View Helicopter Services LLC
The flight
- Departed from: WVL Waterville ME at 7:44 pm
- Destination: WVL Waterville ME
- Flight plan: none
Weather at the time
- Light: daylight
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 79°F (26°C), dew point 72°F (22°C)
- Altimeter: 30.07 inHg
- Observation at 8:55 pm from WVL, 14 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.
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.
