Originally posted by SunTracker F3F designed to fly sustained inverted flight for 30 minutes.
Lubricating oil was carried in amagnesium tank of 28.6 U.S. gallons capacity, strapped to supports on the engine mount. A pendulum was in-corporated in the tank to insure ade-quate lubrication for inverted flightsof limited duration
Show proof please.
powered by a Wright Cyclone R-1820-GI 1,000 hp engine and a three-blade Hamilton Standard propeller the aircraft was equipped for inverted flying for periods of up to half an hour.
A second scavenger pump and five drain lines enabled the plane to sustain inverted flight for up to 30 minutes.
Originally posted by SunTracker Look what I found about the P-47 while searching for one of Bodhis endless questions:
Originally posted by SunTracker P-51http://nasaui.ited.uidaho.edu/nasaspark/safety/process/flight.htm P-38http://home.tiscali.dk/winthrop/p38op1.html The F3F had a scavanger pump to allow for sustained inverted flight, but the F6F, F4U, and P47 did not.