SEA94LA218

NTSB accident investigation · Beech 99 · Helena, MT · August 20, 1994

Accident · No injuriesLimited investigationFinal report
Date
August 20, 1994, 02:10 local (08:10 UTC)
Place
Helena, MT
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Taxi
Aircraft
N14MVBeech 99
Weather
Visual (VMC) · Night/dark
Status
Completed · report May 16, 1995
Report
Approved by Office Director
FAA report
19940820022259A
Case key
42005

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

Landing gear locking mechanism overload and improper rigging.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Gear collapsedTaxi - from landing
Landing gear,gear locking mechanism - overloadCause
Maintenance,adjustment - improperOther maintenance personnelCause

Analysis

After landing and exiting on to the taxiway, the left main landing gear collapsed. Metallurgical examination of the broken down lock hook, link, fitting, and pin revealed fractures typical of an overstress separation. These failures were the 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.

Factual narrative

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.

Aircraft

Registration
N14MV
Reported as
Beech 99
Category
Airplane
Serial number
U59
Engine
P&W PT6A-28, 680 horsepower, turbo prop
Damage
Substantial damage
Flight
Part 135
Operator
Alpine Aviation
Registered owner
Precision Airlease Inter.
Airworthiness certificate
Standard, Normal
Departed
BIL · Billings, MT
Destination
HLN
Flight plan
IFR
Airport
HLN · Helena Regional, runway 27, 9,000 × 150 ft, asphalt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
49
Certificates
Commercial, Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
4,620 total · 100 in this make and model · 3,000 as pilot in command · 120 in the last 90 days

Weather

Conditions
Visual (VMC) · Night/dark
Wind
70° at 5 knots
Visibility
15 statute miles
Lowest ceiling
None
Temperature
54 °F, dew point 37 °F
Altimeter
30.00 inHg
Observed at
HLN

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.