Cessna 185F accident near Talkeetna, Alaska, June 15, 2002
On June 15, 2002 at about 7:59 am local time, a Cessna 185F, registered N333DG, was substantially damaged in an accident near Talkeetna, Alaska. It was flown under charter and air-taxi rules (Part 135). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
A fracture failure of the lower end of the spring steel landing gear strut. Factors contributing to the accident were the manufacturer's and the FAA's insufficient standards/requirements for inspection procedures.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 15, 2002 · about 7:59 am local time
- Place
- Talkeetna, Alaska · map
- Type
- Accident
- Injuries
- No one was hurt; 2 people were on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Cessna 185F · all 185Fs on the register
- Registration
- N333DG · registry record · serial 18503234
- Damage
- Substantial damage
- Flight
- Flight · charter and air-taxi rules (Part 135)
The NTSB's narrative final · quoted from the NTSB record
The certificated commercial pilot, with one passenger aboard, was departing from a 900 foot long gravel bar in a tail wheel equipped airplane. The flight was operated as an on-demand charter flight. During acceleration for takeoff, after reaching about 45 knots, the left main landing gear strut fractured above the left wheel axle. The upper portion of the gear strut dug into the ground, and the airplane swerved to the left. The airplane continued off the left side of the site, and the right wing struck the ground. The airplane sustained substantial damage to the right wing and fuselage. The operator reported that a visual inspection of the fractured landing gear strut revealed a fracture through the upper two holes in the gear strut. The lower end of the spring steel landing gear strut has four holes drilled through the metal in a box pattern. The axle is attached to the outboard side of the strut. Neither the manufacturer nor the FAA have established a life limit (hours or cycles) for the main landing gear strut. An annual inspection does not require disassembly of the axle from the gear strut. No inspection procedures, other than a general visual inspection of the landing gear, have been specified 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."
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
Pilot
- Certificate: commercial pilot
- Ratings: multi-engine land; single-engine land; single-engine sea; instructor: airplane single-engine; instrument: airplane; rotorcraft: glider
- Flight time: 17,800 hours in all; 13,000 in this make and model; 150 in the last 90 days; 50 in the last 30 days; 17,780 as pilot in command; 1,000 on instruments
- Last flight review: March 30, 2002
- Medical certificate: Class 2 (valid medical--no waivers/lim.)
- Seat: left
- Injury: no injuries
The aircraft
- Airframe total time: 6,042.6 hours
- Last inspection: 100-hour inspection; 146 hours since
- Maximum gross weight: 3,520 lb
- Seats: 6
- Landing gear: fixed
- Engine: Continental IO-520 (piston); 0 hours total
The flight
- Departed from: TKA Talkeetna AK at 2:00 pm
- Destination: TKA Talkeetna AK
Weather at the time
- Light: daylight
- Visibility: 100 statute miles
- Sky: clear
- Temperature: 19°F (-7°C), dew point 0°F (-18°C)
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
Other NTSB records under N333DG the same tail number, which may have belonged to a different aircraft at the time
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.