Accident Cessna 206A N4605F,
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ASN Wikibase Occurrence # 352810
 
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Date:Sunday 15 August 1999
Time:13:00 LT
Type:Silhouette image of generic C206 model; specific model in this crash may look slightly different    
Cessna 206A
Owner/operator:Alaska Expedition Company
Registration: N4605F
MSN: P206-0205
Year of manufacture:1966
Total airframe hrs:7260 hours
Engine model:Continental IO-520-F
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Cordova, AK -   United States of America
Phase: Initial climb
Nature:Executive
Departure airport:
Destination airport:(PACV)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The commercial certificated pilot departed from his company's fishing lodge to begin a cross-country business flight. About 300 feet above the ground, the engine suddenly quit. The pilot switched fuel tanks, activated the engine boost pump, and began a turn into the wind. The engine did not restart. The pilot selected an open area of marsh for an emergency landing area. When the airplane touched down, the nose wheel separated from the nose wheel strut, and the airplane nosed down in the soft terrain. The airplane received damage to the engine, propeller, and the left wing. A postaccident examination of the engine by a mechanic found corrosion, and blockage of the vent hole of the engine manifold valve housing. The manifold valve is comprised of a fuel inlet, a diaphragm chamber, and outlet ports for fuel lines to each cylinder. The spring loaded diaphragm operates a valve in the central bore of the lower chamber of the valve body. Fuel pressure below the diaphragm opens the valve to allow fuel to flow to each cylinder. A spring above the diaphragm retains the valve in the closed position, absent any fuel pressure. The upper chamber of the valve housing, containing the spring, is vented to the atmosphere.

Probable Cause: A loss of engine power due to corrosion/blockage of the fuel flow divider vent hole. A factor was unsuitable terrain for a forced landing.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ANC99LA114
Status: Investigation completed
Duration: 1 year and 5 months
Download report: Final report

Sources:

NTSB ANC99LA114

Location

Revision history:

Date/timeContributorUpdates
08-Mar-2024 20:04 ASN Update Bot Added

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