Deadhorse – Nuiqsut
Flight / Schedule
Deadhorse – Nuiqsut
Aircraft
Piper PA-31 CheyenneRegistration
N220CS
MSN
31-8275013
Year of Manufacture
1982
Operator
Cape Smythe Air ServiceDate
September 18, 2000 at 03:10 PM
Type
CRASHFlight Type
Charter/Taxi (Non Scheduled Revenue Flight)
Flight Phase
Landing (descent or approach)
Crash Site
Airport (less than 10 km from airport)
Crash Location
Nuiqsut Alaska
Region
North America • United States of America
Coordinates
70.2168°, -151.0030°
Crash Cause
Human factor
Narrative Report
On September 18, 2000 at 03:10 PM, Deadhorse – Nuiqsut experienced a crash involving Piper PA-31 Cheyenne, operated by Cape Smythe Air Service, with the event recorded near Nuiqsut Alaska.
The flight was categorized as charter/taxi (non scheduled revenue flight) and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.
10 people were known to be on board, 5 fatalities were recorded, 5 survivors were identified or estimated. This corresponds to an estimated fatality rate of 50.0%.
Crew on board: 1, crew fatalities: 1, passengers on board: 9, passenger fatalities: 4, other fatalities: 0.
The listed crash cause is human factor. The airline transport certificated pilot was landing at a remote village on a scheduled domestic commuter flight with nine passengers. The accident airplane, a twin-engine turboprop certified for single-pilot operations, was equipped with a fuselage-mounted belly cargo pod. Witnesses saw the airplane touch down on the gravel runway with the landing gear retracted. The belly pod lightly scraped the runway for about 40 feet before the airplane transitioned to a climb. The propeller tips did not contact the runway. As the airplane began climbing away from the runway, the landing gear was extended. The airplane climbed to about 100 to 150 feet above the ground, and then began a descending left turn, colliding with tundra-covered terrain. A postcrash fire destroyed the fuselage, right wing, and the right engine. The flaps were found extended to 40 degrees. The balked landing procedure for the airplane states, in part: "power levers to maximum, flaps to 15 degrees, landing gear up, and then retract the flaps." Five passengers seated in the rear of the airplane survived the crash. The survivors did not recall hearing a gear warning horn before ground contact. The airplane was landed gear-up eight months before the accident. The airplane was nearly landed gear-up four months before the accident. Each time, a landing gear warning horn was not heard by the pilot or passengers. A postcrash examination of the airplane and engines did not locate any preimpact mechanical malfunction. The FAA's Fairbanks, Alaska, FSDO conducted an inspection of the operator six months before the accident, and recommended the operator utilize two pilots in the accident airplane. Following the accident, the Fairbanks FSDO required the operator to utilize two pilots for passenger flights in the accident airplane make and model.
Aircraft reference details include registration N220CS, MSN 31-8275013, year of manufacture 1982.
Geospatial coordinates for this crash are approximately 70.2168°, -151.0030°.
Fatalities
Total
5
Crew
1
Passengers
4
Other
0
Crash Summary
The airline transport certificated pilot was landing at a remote village on a scheduled domestic commuter flight with nine passengers. The accident airplane, a twin-engine turboprop certified for single-pilot operations, was equipped with a fuselage-mounted belly cargo pod. Witnesses saw the airplane touch down on the gravel runway with the landing gear retracted. The belly pod lightly scraped the runway for about 40 feet before the airplane transitioned to a climb. The propeller tips did not contact the runway. As the airplane began climbing away from the runway, the landing gear was extended. The airplane climbed to about 100 to 150 feet above the ground, and then began a descending left turn, colliding with tundra-covered terrain. A postcrash fire destroyed the fuselage, right wing, and the right engine. The flaps were found extended to 40 degrees. The balked landing procedure for the airplane states, in part: "power levers to maximum, flaps to 15 degrees, landing gear up, and then retract the flaps." Five passengers seated in the rear of the airplane survived the crash. The survivors did not recall hearing a gear warning horn before ground contact. The airplane was landed gear-up eight months before the accident. The airplane was nearly landed gear-up four months before the accident. Each time, a landing gear warning horn was not heard by the pilot or passengers. A postcrash examination of the airplane and engines did not locate any preimpact mechanical malfunction. The FAA's Fairbanks, Alaska, FSDO conducted an inspection of the operator six months before the accident, and recommended the operator utilize two pilots in the accident airplane. Following the accident, the Fairbanks FSDO required the operator to utilize two pilots for passenger flights in the accident airplane make and model.
Cause: Human factor
Occupants & Outcome
Crew On Board
1
Passengers On Board
9
Estimated Survivors
5
Fatality Rate
50.0%
Known people on board: 10
Operational Details
Schedule / Flight
Deadhorse – Nuiqsut
Operator
Cape Smythe Air ServiceFlight Type
Charter/Taxi (Non Scheduled Revenue Flight)
Flight Phase
Landing (descent or approach)
Crash Site
Airport (less than 10 km from airport)
Region / Country
North America • United States of America
