Dehavilland DHC6 accident near Hyannis, Massachusetts, June 18, 2008
On June 18, 2008 at about 2:01 pm local time, a Dehavilland DHC6, registered N656WA, was substantially damaged in an accident during takeoff near Hyannis, Massachusetts (Barnstable Municipal Airport). It was flown under charter and air-taxi rules (Part 135). 1 person was killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's failure to remove the flight control lock prior to takeoff. Contributing to the accident was the Federal Aviation Administration's failure to issue an airworthiness directive making the manufacturer's previously-issued flight control lock service bulletins mandatory.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 18, 2008 · about 2:01 pm local time
- Place
- Hyannis, Massachusetts · Barnstable Municipal Airport · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Dehavilland DHC6 · all DHC6s on the register
- Registration
- N656WA · registry record · serial 47
- Damage
- Substantial damage
- Flight
- Flight · charter and air-taxi rules (Part 135)
The NTSB's narrative final · quoted from the NTSB record
The pilot contacted air traffic control and requested clearance to taxi for departure approximately an hour after the scheduled departure time. About 4 minutes later, the flight was cleared for takeoff. A witness observed the airplane as it taxied, and found it strange that the airplane did not stop and "rev up" its engines before takeoff. Instead, the airplane taxied onto the runway and proceeded with the takeoff without stopping. The airplane took off quickly, within 100 yards of beginning the takeoff roll, became airborne, and entered a steep left bank. The bank steepened, and the airplane descended and impacted the ground. Postaccident examination of the wreckage revealed that the pilot's four-point restraint was not fastened and that at least a portion of the cockpit flight control lock remained installed on the control column. One of the pretakeoff checklist items was, "Flight controls - Unlocked - Full travel." The airplane was not equipped with a control lock design, which, according to the airframe manufacturer's previously issued service bulletins, would "minimize the possibility of the aircraft becoming airborne when take off is attempted with flight control locks inadvertently installed." In 1990, Transport Canada issued an airworthiness directive to ensure mandatory compliance with the service bulletins; however, the Federal Aviation Administration did not follow with a similar airworthiness directive until after the accident.
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 control in flight during takeoff defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Personnel issues › Task performance › Use of equip/info › Use of equip/system › Pilot
- factor Organizational issues › Development › Design › Policy/procedure development › FAA/Regulator
- cause Aircraft › Aircraft systems › Flight control system › Gust lock or damper › Incorrect use/operation
Pilot
- Certificate: airline transport pilot
- Ratings: multi-engine land; single-engine land; instrument: airplane
- Flight time: 3,607 hours in all; 99 in this make and model; 63 in the last 90 days; 16 in the last 30 days; 3,469 as pilot in command
- Last flight review: May 2, 2008
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 38,185 hours
- Last inspection: approved inspection programme, June 12, 2008
- Maximum gross weight: 11,579 lb
- Seats: 2
- Landing gear: fixed
- Engine 1: Pratt And Whitney Canada PT6A-20 (turboprop); 0 hours total
- Engine 2: Pratt And Whitney Canada PT6A-20 (turboprop); 0 hours total
- Operator: Wiggins Airways INC
The flight
- Departed from: HYA Hyannis MA at 2:01 pm
- Destination: ACK Nantucket MA
- Flight plan: IFR
- Runway 24, 5,425 ft by 150 ft
Weather at the time
- Light: daylight
- Wind: from 260° at 9 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 70°F (21°C), dew point 45°F (7°C)
- Altimeter: 30.00 inHg
- Observation at 1:56 pm from HYA, 1 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 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.
