Aircraft Accident/Incident Report

Cordova, Alaska 99574
Saturday, November 5, 2005 10:30 AST

NTSB Narrative Summary Released at Completion of Accident

A commercial certificated pilot in a tundra tire-equipped airplane from a CFR Part 135 operator, under contract to the Federal Aviation Administration (FAA) as a public use flight, was transporting FAA personnel to a navigational facility on a remote island. During the landing roll on a dirt surface runway, the lower end of the left main landing gear strut fractured at the axle bolt holes, where the axle is bolted onto the strut. The fractured end of the left gear strut dug into the ground, the airplane swerved 90 degrees to the left and nosed down, receiving structural damage to the left wingtip and the right main landing gear. The main landing gear is a spring steel strut that is shot peened during manufacture, and is bolted to the fuselage at its upper end. Photographs of the point of separation revealed a vertical fracture, oriented 90 degrees to the span of the gear strut, through the upper axle retaining bolt holes. The fractured surface of the lower end of the strut, containing the axle and brake assembly, had a rough, crystalline appearance with darkening of the metal surface along the outer edges of the strut. The fractured surface of the upper end of the strut, where it dug into the ground, had a smooth polished appearance. Periodic visual inspection of the landing gear is required by 14 CFR Part 43. Neither the manufacturer or the FAA have established 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." In the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1), the pilot indicated that the landing gear strut, Part number 0741001-5, had accrued about 9,000 hours of service. In the optional area of the report: Recommendation (How Could This Accident Have Been Prevented), the pilot wrote: "Put time life [limit] on gear legs."

NTSB Probable Cause Narrative

A fracture and separation of the main landing gear strut during the landing roll, which resulted in a loss of control, and subsequent nose down. Factors contributing to the accident were the manufacturer's and the FAA's insufficient standards/requirements regarding inspection procedures for the main landing gear struts.

Event Information

Type of Event Accident
Event Date 11/5/2005
Event Day of the Week Saturday
Time of Event 1030
Event Time Zone Atlantic Standard Time
Event City Cordova
Event State ALASKA
Event Country --
Zipcode of the event site 99574
Event Date Year 2005
Event Date Month 11
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 602321N
Event Location Longitude 1460644W
Event Location Airport --
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 --
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) 10
Air Temperature at event time (in degrees celsius) -2
Dew Point at event time (in degress fahrenheit) --
Wind Direction (degrees magnetic) --
Variable Wind Indicator Variable
Wind Speed (knots) --
Wind Velocity Indicator Light and Variable
Wind Gust Indicator Not Gusting
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) --
Density Altitude (feet) --
Intensity of Precipitation --
METAR weather report --
Event Highest Injury Minor
On Ground, Fatal Injuries --
On Ground, Minor Injuries --
On Ground, Serious Injuries --
Injury Total Fatal --
Injury Total Minor 1
Injury Total None 2
Injury Total Serious --
Injury Total All 1
Investigating Agency NTSB
NTSB Docket Number (internal use) 19797
NTSB Notification Source Operator
NTSB Notification Date Nov 7 2005 12:00AM
NTSB Notification Time --
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Jun 28 2006 1:30PM
User who most recently changed record NTSB\JOHB
Basic weather conditions Visual Meteorological Cond
FAA District Office FAA-AL-ANC FSDO 03

Aircraft Involved

Aircraft #1

Aircraft Registration Number N771X
NTSB Number ANC06TA009
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 91: General Aviation
Type of Flight Plan filed Company VFR
Flight plan Was Activated? --
Damage Substantial
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name Cessna
Aircraft Model 185
Aircraft Series Identifier --
Aircraft Serial Number 1851336
Certified Max Gross Weight 3350
Aircraft Category Airplane
Aircraft Registration Class --
Aircraft is a homebuilt? No
Flight Crew Seats --
Cabin Crew Seats --
Passenger Seats --
Total number of seats on the aircraft 5
Number of Engines 1
Fixed gear or retractable gear Fixed
Aircraft, Type of Last Inspection 100 Hour
Date of Last Inspection Aug 1 2005 12:00AM
Airframe hours since last inspection 90
Airframe Hours 11299
ELT Installed Yes
ELT Activated No
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name Dorothy Galye Ranney
Aircraft Owner Street Address --
Aircraft Owner City Cordova
Aircraft Owner State AK
Aircraft Owner Country --
Aircraft Owner Zipcode 99574
Operator is an individual? No
Operator Name Federal Aviation Administration
Operator Same as Owner? No
Operator Is Doing Business As --
Operator Address Same as Owner? No
Operator Street Address 301 E. 56th
Operator City Anchorage
Operator State AK
Operator Country --
Operator Zip code 99518
Operator Code --
Owner has at least one certificate None
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 --
Indicates Domestic or International Flight --
Operator carrying Pax/Cargo/Mail --
Type of Flying (Per_Bus / Primary) --
Second Pilot on Board No
Departure Point Same as Event Yes
Departure Airport Code PACV
Departure City Cordova
Departure State AK
Departure Country USA
Departure Time 1010
Departure Time Zone AST
Destination Same as Local Flt crash at destination city
Destination Airport Code --
Destination City Cordova
Destination State AK
Destination Country USA
Specific Phase of Flight Landing - roll
Report sent to ICAO? --
Evacuation occurred --
Date of most recent change to record Jun 23 2006 10:02AM
User who most recently changed record JOHB
Since inspection or accident Last Inspection
Event Location Runway Number and Location 090
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --