N5316D

Substantial
None

Cessna 180 S/N: 50214

Accident Details

Date
Tuesday, September 7, 1999
NTSB Number
ANC99LA134
Location
DILLINGHAM, AK
Event ID
20001212X19662
Coordinates
58.820194, -157.859970
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 inadequate preflight planning. Factors associated with the accident were a short runway, and the pilot's failure to use available performance data.

Aircraft Information

Registration
Make
CESSNA
Serial Number
50214
Engine Type
Reciprocating
Year Built
1958
Model / ICAO
180 C180
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
180A

Registered Owner (Current)

Name
ERICKSON TODD E
Address
7362 W PARKS HWY # 811
City
WASILLA
State / Zip Code
AK 99623-9300
Country
United States

Analysis

On September 6, 1999, about 1830 Alaska daylight time, a float equipped Cessna 180 airplane, N5316D, sustained substantial damage when it did not become airborne during takeoff and collided with level terrain at the end of the Shannon's Pond seaplane base, Dillingham, Alaska. The accident occurred at 59 degrees 03.54 minutes north latitude, 158 degrees 34.63 minutes west longitude. The commercial pilot and the one passenger on board were not injured. The visual flight rules (VFR) personal flight was being conducted under 14 CFR Part 91 by the airplane's owner. The flight was departing for the Tikchik Lakes, Alaska. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed.

During a telephone interview with the NTSB investigator-in-charge (IIC) on September 8, and in his NTSB Pilot/Operator report, the pilot stated he water taxied to the southwest end of the 1,400 feet long by 100 feet wide, northeast-southwest water lane and began the takeoff run. He said the winds were north about four knots, and the water surface was lightly rippled. The flaps were set to 20 degrees. The pilot indicated that the airplane came up "on step" normally, but did not lift off the water before colliding with the northeast end of the lake. The airplane came to rest several hundred feet beyond the lake edge, and sustained substantial damage to several fuselage stringers aft of the rear float attachments.

The pilot stated that the airplane contained full standard fuel tanks, about 100 pounds of equipment, and that he and the passenger weigh 450 pounds combined. He stated in his Pilot/Operator report that he could have managed his fuel better. The allowable maximum takeoff weight for the airplane is 2,820 pounds. The NTSB IIC estimated the actual takeoff weight to be 2,813 pounds. The Cessna 180A pilot operating handbook states the takeoff water run on floats, at 2,820 pounds is 1,356 feet with zero knots of headwind.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC99LA134