N121KT

Substantial
None

DEHAVILLAND DHC-2S/N: 1407

Accident Details

Date
Thursday, June 14, 2012
NTSB Number
ANC12LA051
Location
Talkeetna, AK
Event ID
20120614X42820
Coordinates
62.349998, -150.283340
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
7
Total Aboard
7

Probable Cause and Findings

The loss of engine power after departure due to the separation of an engine cylinder.

Aircraft Information

Registration
Make
DEHAVILLAND
Serial Number
1407
Engine Type
Reciprocating
Year Built
1958
Model / ICAO
DHC-2DH2T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
8
FAA Model
DHC-2 MK. I(L20A)

Registered Owner (Current)

Name
RUSTAIR INC
Address
PO BOX 190867
City
ANCHORAGE
State / Zip Code
AK 99519-0867
Country
United States

Analysis

On June 13, 2012, about 1915 Alaska daylight time, a de Havilland DHC-2 airplane, N121KT, sustained substantial damage during a forced landing, following a loss of engine power after takeoff from the Talkeetna Airport (PATK), Talkeetna, Alaska. The certificated commercial pilot, and six passengers were not injured. The airplane was registered to, and operated by Rusts Flying Service, doing business as K2 Aviation, under the provisions of Title 14 Code of Federal regulations Part 135, as a visual flight rules (VFR) sightseeing flight. Visual meteorological conditions prevailed, and company flight following procedures were in effect.

The pilot reported that he had departed runway 18, at PATK, on a scenic tour flight, and had reduced power to a cruise climb setting. At approximately 1200 feet above the ground, the engine began to run rough, and lose power. The pilot turned back toward PATK, and performed emergency procedures to restore power. The engine continued to run rough at reduced power, and the pilot could not maintain altitude, followed by a total loss of engine power. He made a forced landing to a sand bar on the Chulitna River. On landing the airplane bounced over logs and ditches, and sustained substantial damage to the horizontal stabilizer, elevators, empennage, and main landing gear.

After the aircraft was recovered, a Federal Aviation Administration (FAA) inspector from the Anchorage Flight Standards District Office (FSDO), examined the airplane in Talkeetna, on June 14. The inspector reported that the number two cylinder head had cracks radiating from the spark plug hole throughout the cylinder head, and it had begun to separate from the cylinder base.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC12LA051