N93018

Substantial
Minor

CESSNA 185 S/N: 18503161

Accident Details

Date
Thursday, July 1, 1993
NTSB Number
ANC93FA107
Location
WASILLA, AK
Event ID
20001211X12735
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

THE PILOT IN COMMAND'S FAILURE TO USE ALL OF THE AVAILABLE RUNWAY (WATERWAY). A FACTOR IN THE ACCIDENT WAS THE PILOT IN COMMAND'S LACK OF RECENT EXPERIENCE IN THE TYPE OF OPERATION.

Aircraft Information

Registration
Make
CESSNA
Serial Number
18503161
Engine Type
Reciprocating
Year Built
1976
Model / ICAO
185 C185
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
A185F

Registered Owner (Current)

Name
JOY AUSTIN J JR
Address
PO BOX 111073
City
ANCHORAGE
State / Zip Code
AK 99511-1073
Country
United States

Analysis

On July 1, 1993, at approximately 1315 Alaska daylight time, a float equipped Cessna 185 airplane, N93018, registered to and operated by the pilot in command, crashed during takeoff from the Anderson Lake Seaplane Strip in Wasilla, Alaska. The airline transport certificated pilot and the one passenger on board received minor injuries, and the airplane sustained substantial damage. The local pleasure flight was being conducted under 14 CFR Part 91 and a VFR flight plan had not been filed. Visual meteorological conditions prevailed.

The pilot in command told the NTSB investigator during the on scene investigation that prior to commencing the takeoff, he performed a preflight and engine run up check and found everything to be in proper working order. The airplane's wing fuel tanks were full and the cargo/baggage consisted of a fishing tackle box and a small bag containing survival gear. The on scene investigation verified this information. The pilot said that the takeoff was commenced from the other side of the lake in the general area that he normally began his takeoffs from. Not all of the available lake area was used for the takeoff run. The plane's takeoff acceleration and engine instrument indications were normal. The pilot said that he believed that the airplane became airborne in the approximate area that it normally did. The pilot did not recall the airspeed at which the airplane became airborne nor the speed at which the plane was flown during the initial climb out. The pilot said that as the airplane climbed to the height of the trees at the rapidly approaching shoreline, a gust of wind from the right was encountered which required some pilot input to correct. The pilot said that this was the only wind induced event that was experienced during the flight and that he did not experience the sensation that the plane was sinking or that it had entered a downdraft. The pilot said that upon correcting for the gust, he realized that he did not have sufficient altitude to avoid colliding with the trees. He then slightly reduced engine power and maneuvered the plane away from a nearby house.

The pilot reported that he did not experience any problems with the plane's engine or flight controls. The on scene investigation collaborated the comments made by the pilot.

Based upon the empty weight of the airplane, and the known fuel, cargo and weights of the pilot and passenger, the airplane's weight and center of gravity (CG) at the time the takeoff was commenced was approximately 3000 pounds and 42 inches, respectively. The forward and aft CG limits at 3000 pounds are 40 inches and 46.5 inches, respectively. The plane's maximum authorized weight is 3350 pounds.

The pilots log book showed that prior to July 1993, his most recent flight in N93018 occurred in June 1992.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC93FA107