Landing at Gimli

In line with their planned diversion to Winnipeg, the pilots were already descending through 35,000 feet (11,000 m)[2] when the second engine shut down. They immediately searched their emergency checklist for the section on flying the aircraft with both engines out, only to find that no such section existed.[3] Captain Pearson was an experienced glider pilot, which gave him familiarity with flying techniques almost never used by commercial pilots. To have the maximum range and therefore the largest choice of possible landing sites, he needed to fly the 767 at the "best glide speed". Making his best guess as to this speed for the 767, he flew the aircraft at 220 knots (410 km/h; 250 mph). First Officer Maurice Quintal began to calculate whether they could reach Winnipeg. He used the altitude from one of the mechanical backup instruments, while the distance traveled was supplied by the air traffic controllers in Winnipeg, measuring the distance the aircraft's echo moved on their radar screens. The aircraft lost 5,000 feet (1,500 m) in 10 nautical miles (19 km; 12 mi), giving a glide ratio of approximately 12:1.
http://en.wikipedia.org/wiki/Gimli_Glider

Three minutes later, at 06:26 UTC and approximately 65 nautical miles (120 km) from Lajes Air Base, engine #1 also flamed out.[3] Without engine power, the plane lost its primary source of electrical power. The emergency ram air turbine was deployed automatically to provide essential power for critical sensors and instruments to fly the aircraft. However the aircraft lost its main hydraulic power, which operates the flaps, alternate brakes, and spoilers. The slats would still be powered, however, when the flaps #1 position was selected.

http://en.wikipedia.org/wiki/Air_Transat_Flight_236