N14MV

Substantial
None

BEECH 99 S/N: U59

Accident Details

Date
Saturday, August 20, 1994
NTSB Number
SEA94LA218
Location
HELENA, MT
Event ID
20001206X02148
Coordinates
46.530197, -112.210899
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

LANDING GEAR LOCKING MECHANISM OVERLOAD AND IMPROPER RIGGING.

Aircraft Information

Registration
Make
BEECH
Serial Number
U59
Engine Type
Turbo-prop
Year Built
1969
Model / ICAO
99 BE99
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
17
FAA Model
99

Registered Owner (Current)

Name
ALPINE AVIATION INC
Address
1177 ALPINE AIR WAY
City
PROVO
State / Zip Code
UT 84601-8270
Country
United States

Analysis

On August 20, 1994, at 0210 mountain daylight time, a Beech 99, N14MV, collapsed the left main landing gear after turning off the runway at Helena, Montana. Visual meteorological conditions prevailed at the time and an instrument flight rules flight plan was filed. The airplane was substantially damaged and the airline transport pilot and commercial pilot were not injured. The flight had departed from Billings, Montana, on August 20, 1994, at 0115, as a cargo flight conducted under 14 CFR 135.

It was reported that after departing runway 27, via the high speed taxi way, the left main landing gear collapsed. The airplane skidded another 52.5 feet before coming to rest on the taxi way.

The maintenance inspection and subsequent repairs were to the outboard rear spar, ribs and upper and lower skins on the left wing. Other repairs or replacements were to the left main landing gear assembly, fuselage belly and left flap.

During the post crash inspection of the left main landing gear, it was found that the down lock hook, link, fitting and pin were broken. A metallurgical examination of the broken parts revealed fractures typical of an overstress separation. According to the metallurgist's discussions with the manager of the Air Safety group at Beech, the failure was most likely a result of the down lock hook not properly engaging the lock plate on the drag link, either from inadequate rigging or from excessive binding of the fitting. The Beech manager reported that this condition could occur repeatedly and may not be easily detected unless this portion of the gear was inspected directly. The collapse of the gear could then occur under certain loading conditions.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA94LA218