N407GV

Substantial
None

Cessna 208B S/N: 208B0616

Accident Details

Date
Saturday, March 4, 2000
NTSB Number
ANC00LA033
Location
HOLY CROSS, AK
Event ID
20001212X20576
Coordinates
62.180061, -159.839447
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

An in-flight separation of a main landing gear tire mud flap, and subsequent impact with the horizontal stabilizer.

Aircraft Information

Registration
Make
CESSNA
Serial Number
208B0616
Engine Type
Turbo-prop
Year Built
1997
Model / ICAO
208B C208
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
12
FAA Model
208B

Registered Owner (Current)

Name
AVION CAPITAL CORP
Address
7251 SAND LAKE RD
City
ANCHORAGE
State / Zip Code
AK 99502-1827
Country
United States

Analysis

On March 4, 2000, about 1230 Alaska standard time, a wheel equipped Cessna 208B airplane, N407GV, sustained substantial damage during cruise flight between Holy Cross, Alaska, and Aniak, Alaska. The location of the occurrence was about 18 miles south of Holy Cross, about latitude 61 degrees, 54 minutes north, and longitude 159 degrees, 40 minutes west. The airplane was being operated as a visual flight rules (VFR) scheduled flight under Title 14, CFR Part 135, when the accident occurred. The airplane was operated as Flight 2602 by Hageland Aviation Services Inc., Anchorage, Alaska. The commercial certificated pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed. VFR company flight following procedures were in effect. The flight originated at the Holy Cross airport, about 1215.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on March 6, 2000, the director of operations for the company reported the flight was carrying U.S. mail. The pilot was in cruise flight when he heard a bang. After landing at Aniak, damage was discovered to the horizontal stabilizer. The left mud flap, normally positioned at the aft side of the main landing gear tire, was missing. The horizontal stabilizer was dented, and had damage to the auxiliary spar.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC00LA033