Bradley Lakes Airstrip Airport
Aircraft Accident/Incident Report

Homer, Alaska 99603
Friday, February 28, 2003 17:10 AKD

NTSB Narrative Summary Released at Completion of Accident

The airline transport certificated pilot was landing a nose wheel-equipped airplane at a remote gravel surfaced airstrip during a VFR air taxi flight. The airplane landed hard, and the right main landing gear, a spring steel strut, fractured and separated from the fuselage just outboard of the landing gear fuselage support clamp. The airplane settled onto the belly-mounted cargo pod and sustained minor damage. The airplane had accrued about 17,120 total flight hours. The right main gear was replaced in 1994, at an aircraft total time of 11,848 hours, with a "serviceable unit." Visual examination of the fracture surface revealed beach marks radiating in successive arc patterns from mulitple locations, along the underside of the gear strut. A metallurgical examination revealed that the landing gear spring had two different layers of paint. Multiple fatigue crack initiation sites, coinciding with corrosion pits, were found along the lower surface of the gear. Particles in the pits contained titanium, a component of paint, indicating the corrosion pits were present at the time the gear was painted. Periodic visual inspection of the landing gear is required by 14 CFR Part 43. Neither the manufacturer nor the FAA have established time in service limits (hours or cycles) for the main landing gear strut. Removal of the gear strut for inspection, or the use of nondestructive inspection techniques is not required by the manufacturer or the FAA. On March 16, 2001, the NTSB recommended that the FAA issue an airworthiness directive (AD) to require an initial and recurring inspection of Cessna main landing gear spring steel struts, using nondestructive inspection techniques. On August 31, 2001, the FAA reported to the NTSB that the current inspection criteria outlined in the Cessna Maintenance Manual are adequate to detect cracks in the main landing gear struts, and that additional airworthiness action is not warranted. On March 25, 2002, the NTSB responded by stating, in part: "The Safety Board continues to believe that a visual inspection alone will not detect cracks in the Cessna main landing gear spring struts. However, the Safety Board acknowledges that the statistical evidence does not warrant issuance of ADs at this time as called for in the Board's recommendation." The safety recommendation was then classified as: "Closed-Reconsidered."

NTSB Probable Cause Narrative

The separation of the main landing gear spring strut during landing touchdown due to corrosion and fatigue. Factors contributing to the accident were the manufacturer's and the FAA's insufficient standards/requirements for inspection procedures.

Event Information

Type of Event Incident
Event Date 2/28/2003
Event Day of the Week Friday
Time of Event 1710
Event Time Zone --
Event City HOMER
Event State ALASKA
Event Country --
Zipcode of the event site 99603
Event Date Year 2003
Event Date Month 2
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 594500N
Event Location Longitude 1504500W
Event Location Airport BRADLEY LAKES AIRSTRIP
Event Location Nearest Airport ID --
Indicates whether the acc/inc occurred off or on an airport On Airport
Distance from airport in statute miles --
Degrees magnetic from airport --
Airport Elevation 20
Weather Briefing Completeness Partial - limited by pilot
Investigator's weather source Pilot
Time of the weather observation
Direction of event from weather observation facility (degrees) --
Weather Observation Facility ID --
Elevation of weather observation facility --
Distance of event from weather observation facility (units?) --
Time Zone of the weather observation --
Lighting Conditions Day
Lowest Ceiling Height --
Lowest Non-Ceiling Height --
Sky/Lowest/Cloud Conditions Clear
Sky Condition for Lowest Ceiling None
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) 30
Air Temperature at event time (in degrees celsius) 5
Dew Point at event time (in degress fahrenheit) 0
Wind Direction (degrees magnetic) 60
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 15
Wind Velocity Indicator --
Wind Gust Indicator Gusting
Wind Gust (knots) 25
Altimeter Setting at event time (in. Hg) 29.92
Density Altitude (feet) --
Intensity of Precipitation --
METAR weather report --
Event Highest Injury None
On Ground, Fatal Injuries --
On Ground, Minor Injuries --
On Ground, Serious Injuries --
Injury Total Fatal --
Injury Total Minor --
Injury Total None 2
Injury Total Serious --
Injury Total All --
Investigating Agency NTSB
NTSB Docket Number (internal use) 14120
NTSB Notification Source FAA REGIONAL OPERATIONS CENTER
NTSB Notification Date Feb 28 2003 12:00AM
NTSB Notification Time 1756
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Nov 25 2003 11:36AM
User who most recently changed record NTSB\MONR
Basic weather conditions Visual Meteorological Cond
FAA District Office FAA-AL-ANC FSDO 03

Aircraft Involved

Aircraft #1

Aircraft Registration Number N8337Q
NTSB Number ANC03IA037
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 135: Air Taxi & Commuter
Type of Flight Plan filed Company VFR
Flight plan Was Activated? No
Damage Minor
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name Cessna
Aircraft Model 206
Aircraft Series Identifier --
Aircraft Serial Number U20603198
Certified Max Gross Weight 3600
Aircraft Category Airplane
Aircraft Registration Class U.S. Registered/U.S. Soil
Aircraft is a homebuilt? No
Flight Crew Seats --
Cabin Crew Seats --
Passenger Seats --
Total number of seats on the aircraft 4
Number of Engines 1
Fixed gear or retractable gear Fixed
Aircraft, Type of Last Inspection 100 Hour
Date of Last Inspection Feb 7 2003 12:00AM
Airframe hours since last inspection 71
Airframe Hours 7050
ELT Installed Yes
ELT Activated No
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name HOMER AIR INC.
Aircraft Owner Street Address 2190 KACHEMAK DR.
Aircraft Owner City HOMER
Aircraft Owner State AK
Aircraft Owner Country USA
Aircraft Owner Zipcode 99603
Operator is an individual? No
Operator Name --
Operator Same as Owner? Yes
Operator Is Doing Business As --
Operator Address Same as Owner? Yes
Operator Street Address --
Operator City --
Operator State --
Operator Country --
Operator Zip code --
Operator Code ENEC
Owner has at least one certificate --
Other Operator of large aircraft? --
Certified for Part 133 or 137 Operation --
Operator Certificate Number --
Indicates whether an air carrier operation was scheduled or not Non-scheduled
Indicates Domestic or International Flight Domestic
Operator carrying Pax/Cargo/Mail Passenger Only
Type of Flying (Per_Bus / Primary) --
Second Pilot on Board No
Departure Point Same as Event No
Departure Airport Code PAHO
Departure City HOMER
Departure State AK
Departure Country USA
Departure Time 1700
Departure Time Zone AST
Destination Same as Local Flt --
Destination Airport Code --
Destination City BRADLEY LAKE
Destination State AK
Destination Country USA
Specific Phase of Flight Landing - flare/touchdown
Report sent to ICAO? No
Evacuation occurred --
Date of most recent change to record Aug 12 2003 3:39PM
User who most recently changed record PETL
Since inspection or accident Last Inspection
Event Location Runway Number and Location 06
Runway Length 2000
Runway Width 75
Sight Seeing flight No
Air Medical Flight No
Medical Flight --