N432L

Substantial
None

Beech BE-50S/N: CH-164

Accident Details

Date
Friday, November 16, 2001
NTSB Number
FTW02LA049
Location
Altus, OK
Event ID
20011212X02392
Coordinates
34.698890, -99.338058
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 improper flare and his failure to maintain directional control. A contributing factor was the ditch.

Aircraft Information

Registration
N432L
Make
BEECH
Serial Number
CH-164
Engine Type
Reciprocating
Year Built
1955
Model / ICAO
BE-50BE50
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
SALE REPORTED
Address
XXX
Status
Deregistered
City
POPLAR BLUFF
State / Zip Code
MO 63160
Country
United States

Analysis

On November 16, 2001, approximately 1500 central standard time, a Beech BE-50 twin engine airplane, N432L, sustained substantial damage during a hard landing at the Altus Mountain Regional Airport (AXS), near Altus, Oklahoma. The aircraft was owned and operated by the pilot under 14 Code of Federal Regulations Part 91. The single-engine land rated private pilot did not receive injuries. Visual meteorological conditions prevailed at Altus; however, the aircraft encountered fog along the planned route and diverted to Altus. The flight originated from Altus Air Force Base. A flight plan was not filed.

The pilot reported that during an instrument flight rules (IFR) flight from Poplar Bluff, Missouri, to Slaton, Texas, a fog bank, which extended to the ground, was encountered about 20 nautical miles from Altus, Oklahoma. The pilot elected to land the airplane at AXS, but inadvertently landed at Altus Air Force Base. Subsequently, the aircraft departed the military base and landed at AXS.

The FAA inspector, who responded to the accident site, reported that the airplane landed hard, bounced, and departed the runway. Subsequently, the airplane rolled through a ditch, collapsing the nose landing gear.

Examination of the airplane by the FAA inspector revealed structural damage to both engine mounts, and the nose landing gear assembly. Additionally, the generator mounting pad for the left engine was damaged, and the propeller blades were bent aft. The hobbs meter reading was 2,383.1 hours.

The previous owner of the airplane reported that the airplane had been sold to the pilot approximately 2 weeks prior to the accident.

Numerous attempts to obtain a completed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) from the pilot were unsuccessful.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW02LA049