N5246E

Substantial
None

Cessna 185 S/N: 185-03943

Accident Details

Date
Saturday, August 9, 1997
NTSB Number
ANC97LA120
Location
CHICKALOON, AK
Event ID
20001208X08531
Coordinates
61.739234, -148.220458
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

inadequate maintenance inspection and failure of the left main landing gear attachment due to fatigue. A factor was continuous use of the airplane for rough area, off-airport landings.

Aircraft Information

Registration
N5246E
Make
CESSNA
Serial Number
185-03943
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
185 C185
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
JOHNSON FRED E
Address
PO BOX 521170
Status
Deregistered
City
BIG LAKE
State / Zip Code
AK 99652-1170
Country
United States

Analysis

On August 9, 1997, at 1100 Alaska daylight time, a Cessna 185 tundra tire equipped airplane, N5246E, sustained substantial damage when it contacted terrain during landing roll on a Chickaloon River off airport landing site, 30 miles north of Chickaloon, Alaska. The commercial certificated pilot and two passengers were uninjured. The airplane was operated by Talkeetna Air Taxi, Inc., of Talkeetna, Alaska. The flight was conducted under 14 CFR Part 135 as an on demand air taxi from Palmer to the Chickaloon River. Visual meteorological conditions prevailed at the time of the accident, and a company VFR flight plan was filed.

The pilot stated that during landing roll, while decelerating through 25 knots, the left main wheel separated at the axle mounting bolts. The airplane ground looped, and the propeller and wing contacted the ground.

Metallurgical inspection conducted at the NTSB laboratory revealed multiple fatigue crack origin sites on the attaching bolt hole walls of the left hand main landing gear leg. Scanning electron microscope inspection revealed a fatigue crack originating from corrosion pits. Metallurgical composition was consistent with 6150 steel specified by Cessna. Hardness was tested to be 50.8 to 52.7 HRC. The specified HRC range is 48.3 to 50.0 HRC.

The operator reported that this landing gear leg had been damaged during a lake landing in February 1996. It was removed, arched, heat treated, and reinstalled on April 12, 1996. At this time, landing gear leg serial number 814048 underwent a magnaflux inspection for cracks at 5437 airframe hours. This was 806 hours prior to the accident. Previous magnaflux inspections had been performed at 5086 airframe hours, and 5415 airframe hours.

Cessna maintenance procedures do not have required inspections, or life limits, on landing gear legs. The FAA does not mandate any inspection interval for landing gear in off airport use. Landing gear legs are replaced "on condition." The air taxi company maintains the airplane on an FAA approved continuing airworthiness inspection schedule, and voluntarily performs non-destructive magnaflux inspections of landing gear legs for cracks. These inspections are performed due to the use of the airplane for off-airport wheel and ski landings.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC97LA120