GENERAL INFORMATION FOR NTSB REPORT: ANC00LA033
Data Source |
NTSB AVIATION ACCIDENT/INCIDENT DATABASE |
NTSB Report Nbr |
ANC00LA033 |
Event Id |
20001212X20576 |
Local Date |
03/04/2000 |
Local Time |
1230 |
State |
AK |
Event Type |
ACCIDENT |
Injury Severity |
NONE |
Record Status |
FINAL |
Mid Air Collision |
NO |
Event Location |
OFF AIRPORT/AIRSTRIP |
WEATHER INFORMATION
Weather Briefing Complete |
UNKNOWN |
Basic Weather Conditions |
VISUAL METEOROLOGICAL COND |
Light Condition |
DAY |
Cloud Condition |
UNKNOWN |
Cloud Height above Ground Level (ft) |
0 |
Ceiling Height above Ground Level (ft) |
6000 |
Cloud Type |
BROKEN |
Visibility RVR (ft) |
0 |
Visibility RVV (sm) |
0 |
Visibility (sm) |
10 |
Wind Direction (deg) |
0 |
Wind Condition Flag |
U |
Wind Speed (knots) |
0 |
Wind Condition Indicated |
Unknown |
AIRCRAFT INFORMATION
Aircraft 1
Type of Operation |
PART 135: AIR TAXI & COMMUTER |
Registration Number |
N407GV |
Aircraft Make |
CESSNA |
Aircraft Model |
208 |
Aircraft Series |
B |
Aircraft Damage |
SUBSTANTIAL |
Aircraft Fire |
NONE |
Aircraft Explosion |
NONE |
Aircraft Type |
AIRPLANE |
Aircraft Homebuilt |
UNKNOWN |
Phase of Flight |
UNDEFINED |
Aircraft Use |
UNKNOWN |
Category of Operation |
SCHEDULED |
Flight Plan Filed |
COMPANY VFR |
Domestic/International |
DOMESTIC |
Passenger/Cargo |
PASSENGER/CARGO |
Operator Name |
HAGELAND AVIATION SERVICES INC |
Operator Doing Business As |
|
Owner Name |
HAGELAND AVIATION SERVICES INC |
Number of Seats |
2 |
Number of Engines |
1 |
ELT Installed |
YES |
ELT Operated |
NO |
Departure Airport Id |
4Z4 |
Departure City |
HOLY CROSS |
Departure State |
ALASKA |
Last Departure Point |
NO |
Destination Airport Id |
PANI |
Destination City |
ANIAK |
Destination State |
ALASKA |
Runway Id |
0 |
Air Carrier Operating Certificates |
YES |
Air Carrier Other Operating Certificates |
UNKNOWN |
Rotocraft/Agriculture Operating Certificate |
UNKNOWN |
Cert Max Gross Wgt |
8750 |
ENGINE INFORMATION
Aircraft 1 - Engine : #1
Engine Manufactuer
| P&W |
Engine Model
| PT6-114A |
Engine Horsepower
| 650 |
Engine Thrust
| HP |
INJURY INFORMATION
Injury Summary for Aircraft 1
|
Fatal |
Serious |
Minor |
None |
Crew |
0 |
0 |
0 |
0 |
Pass |
0 |
0 |
0 |
0 |
Total |
0 |
0 |
0 |
1 |
Sequence of Events for Aircraft 1
Occurrence #1 AIRFRAME/COMPONENT/SYSTEM FAILURE/MALFUNCTION
Phase of Operation: CRUISE
Events Sequence for Occurrence #1 of Aircraft 1
Event Seq # |
Event Group Code |
Subject |
Modifier |
Personnel |
Cause/Factor |
1 |
1 |
MISC EQPT/FURNISHINGS |
SEPARATION |
|
CAUSE |
2 |
1 |
HORIZONTAL STABILIZER |
FOREIGN OBJECT DAMAGE |
|
CAUSE |
AIRCRAFT 1 PRELIMINARY REPORT
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.
AIRCRAFT 1 FINAL REPORT
The commercial certificated pilot departed on a scheduled flight. During cruise, about fifteen minutes after takeoff, he heard a bang. After landing at the destination airport, 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.
AIRCRAFT 1 CAUSE REPORT
An in-flight separation of a main landing gear tire mud flap, and subsequent impact with the horizontal stabilizer.
END REPORT