N980FE

Substantial
None

Cessna 208B S/N: 208B0108

Accident Details

Date
Wednesday, February 3, 1999
NTSB Number
DEN99LA036
Location
CODY, WY
Event ID
20001205X00148
Coordinates
44.509677, -109.049674
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's inability to maintain aircraft control due to unfavorable winds conditions.

Aircraft Information

Registration
Make
CESSNA
Serial Number
208B0108
Engine Type
Turbo-prop
Year Built
1988
Model / ICAO
208B C208
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
12
FAA Model
208B

Registered Owner (Current)

Name
FEDERAL EXPRESS CORPORATION
Address
3630 HACKS CROSS ROAD
BUILDING C 2ND FLOOR
City
MEMPHIS
State / Zip Code
TN 38125
Country
United States

Analysis

On February 2, 1999, at 1711 mountain standard time, a Cessna 208B, N980FE, was substantially damaged when the airplane nosed down during taxi for takeoff at Yellowstone Regional Airport, Cody, Wyoming. The airline transport rated pilot, the sole occupant in the airplane, was not injured. The airplane was being operated by Corporate Air of Billings, Montana, dba Federal Express Corporation under Title 14 CFR Part 135. Visual meteorological conditions prevailed for the cross-country cargo flight which was taxiing for departure at the time of the accident. A company VFR flight plan had been filed with the destination of Riverton, Wyoming.

FAA records indicated that the pilot got a weather briefing at 1521, and the winds were 250 degrees at 21 knots, gusting to 38 knots. The pilot reported that taxied out for a departure on runway 22 at approximately 1708. The pilot said that as he was taxiing out, he was monitoring the airport's Automatic Weather Observation Station (AWOS), and it was reporting the maximum wind velocity of 34 to 36 knots. The pilot reported that as he turned the airplane from northwest to northeast, the wind lifted the airplane's left wing. The airplane nosed down with its left main landing gear off the ground and the engine's propeller in the ground. The right wing spar was bent.

The AWOS wind report at 1714 (approximately 3 minutes after the accident), was 250 degrees, at 27 knots gusting to 43 knots. The manufacturer's Information Manual for this airplane states that the maximum demonstrated crosswind velocity is 20 knots (not a limitation).

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN99LA036