N7370N

Substantial
None

Cessna 206 S/N: U20603639

Accident Details

Date
Sunday, July 19, 1998
NTSB Number
ANC98LA103
Location
PALMER, AK
Event ID
20001211X10456
Coordinates
61.620159, -148.980773
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

The pilot's inadequate compensation for wind conditions, and inadequate clearance from mountainous terrain. Factors were the downslope winds and downdrafts.

Aircraft Information

Registration
N7370N
Make
CESSNA
Serial Number
U20603639
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
206 C206
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HITCHINGS JEANNE L
Address
4915 DE ARMOUN RD
Status
Deregistered
City
ANCHORAGE
State / Zip Code
AK 99516-3625
Country
United States

Analysis

On July 18, 1998, at 1828 Alaska daylight time, a float equipped Cessna 206 airplane, N7370N, sustained substantial damage when it collided with terrain about 3,000 feet msl at 61 degrees 24.38 minutes North latitude, 148 degrees 14.09 minutes West longitude. The commercial pilot and the three passengers were not injured. The flight was operated under 14 CFR Part 91 as a personal flight to view glaciers. The flight departed from Six Mile Lake Seaplane Base, Anchorage, Alaska, at 1755. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed.

The pilot told the NTSB investigator-in-charge (IIC) during a telephone interview on July 18, 1998, that while cruising at 95 knots, in an up glacier direction about 700 feet above the glacier surface, the airplane began to descend rapidly. The pilot stated he added power, but was unable to arrest the descent before colliding with slightly rising terrain near the glacier's edge. The pilot indicated that he did not attempt to turn because the most favorable landing terrain was ahead of the airplane. He said in the interview, and wrote in his pilot/operator report, that the winds on the surface were flowing down the glacier approximately 15 knots, and the temperature was 55 degrees Fahrenheit.

The pilot calculated the airplane's weight to be 3,312 pounds. The Cessna Model U206G rate of climb table shows a maximum rate of climb at 3,300 pounds and 2,000 feet pressure altitude, given a temperature between 0 and 20 degrees C, to be between 915 feet per minute (fpm) and 1,005 fpm.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC98LA103