N9855X

Substantial
None

Cessna 185 S/N: 185-0055

Accident Details

Date
Tuesday, June 9, 1998
NTSB Number
ANC98LA067
Location
CHICKALOON, AK
Event ID
20001211X10206
Coordinates
61.739162, -148.219589
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's inadvertent activation of the fuel boost pump selector switch during final approach, which resulted in an overly rich mixture and subsequent loss of engine power.

Aircraft Information

Registration
Make
CESSNA
Serial Number
185-0055
Engine Type
Reciprocating
Year Built
1961
Model / ICAO
185 C185
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
185

Registered Owner (Current)

Name
MCGEE JACOB QUINTON
Address
13 ALASKA PENINSULA HIGHWAY
PO BOX 31
City
KING SALMON
State / Zip Code
AK 99613
Country
United States

Analysis

On June 9, 1998 about 1200 Alaska daylight time, a wheel/ski equipped Cessna 185 airplane, N9855X, sustained substantial damage during a forced landing on the Matanuska Glacier, about 50 miles southeast of Chickaloon, Alaska. The airplane was being operated as a visual flight rules (VFR) on-demand passenger flight under Title 14 CFR Part 135 when the accident occurred. The airplane was operated by Hudson Air Service, Talkeetna, Alaska. The certificated commercial pilot, and the sole passenger aboard were not injured. Visual meteorological conditions prevailed, and a VFR flight plan was filed. The flight originated at the Talkeetna Airport, about 0719.

During a telephone conversation with the National Transportation Safety Board investigator-in-charge on June 11, the pilot reported that he was transporting personnel and cargo to a base camp located at 6900 feet msl on the Matanuska Glacier. The pilot reported that while on short final for landing, all engine power was lost. Attempts to restore engine power were unsuccessful, and the airplane landed hard, about 500 feet short of the intended touch down point. The airplane's fuselage sustained substantial damage.

The pilot reported in his written statement that after landing he discovered that the fuel boost pump switch had been placed in the "high boost" position. The Cessna Pilot's Operating Handbook, states, in part: "If the engine-driven fuel pump switch is placed in the ON position, a fuel/air ratio considerably richer than best power is produced unless the mixture is leaned."

The pilot said that wind conditions at the time of the accident were calm.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC98LA067