Nevada

After liftoff at McCarran Airport, while in initial climb, the crew raised the landing gear when two engines suffered a simultaneous loss of power. The captain initiated an immediate landing and the airplane belly landed on the runway and slid for few dozen yards before coming to rest. All 104 occupants were evacuated safely while the aircraft was damaged beyond repair.

Shortly after a night takeoff from Las Vegas-McCarran Airport, while in initial climb, the airplane went out of control and crashed in flames near the runway end. The aircraft was destroyed by impact forces and a post crash fire and all four occupants were killed.

While cruising at an altitude of 12,000 feet on a flight from Buckley AFB, Denver, and Seattle, the navigator informed ATC about difficulties to maintain the assigned altitude and was cleared to descend to 10,500 feet. Few minutes later, the copilot reported icing conditions to ATC and requested the permission to gain altitude. About 20 minutes later, while cruising at the altitude of 10,000 feet in marginal weather conditions, the four engine airplane struck the slope of Mt Tobin (2,980 meters high). The wreckage was found few hours later about 300 meters below the summit and all 19 occupants have been killed.

Shortly after takeoff from Las Vegas-McCarran Airport, while in initial climb, both engines lost power. The pilot informed ATC and requested permission to return for a safe landing but realized it would not be possible. He raised the undercarriage and attempted a belly landing in an open field. The airplane crash landed near the airport and came to rest. The pilot was killed and all five passengers were seriously injured. The aircraft was destroyed.

Shortly after takeoff from Minden-Douglas County Airport, while in initial climb, the airplane stalled and crashed. Both occupants were injured and the airplane was written off.

A full flap landing was carried out, followed by flap-retraction to practice a no-flap takeoff. The Fairchild veered left upon rotation and cartwheeled off the runway, coming to rest 557 feet left of the runway and 6000 feet from the takeoff end. It appeared that the right inboard and outboard flaps were fully extended; the left inboard flap was extended 17 degrees and the left outboard flap was fully retracted.

En route, weather conditions worsened with snow falls, thunderstorm activity and turbulences. In low visibility, the twin engine aircraft struck the slope of a mountain located in the region of Elko. Due to poor weather conditions, SAR operations were hampered and eventually suspended few days later. The wreckage was found on 13 May 1965 in an isolated area. The pilot was killed. The aircraft was owned by David E. Gast.

Weather was poor near Las Vegas with indefinite ceiling at 500 feet, sky obscured, 900 m visibility and light snow. Flight 114 was flying a VOR/DME-3 approach when the plane descended below altitude minima. At 9.7 DME, at an elevation of 3575 feet msl the plane struck rising terrain and crashed. The flight should have been at 4300 feet msl at that point. It appeared that the VOR/DME-3 approach procedure was relatively new, having become effective on October 3, 1964. Until November 15 no approaches using this procedure had been flown. The approach chart depiction for the segment of the approach from the 15 mile fix to the 6 mile fix displayed no descent information on the profile section. However, the profile did show a solid horizontal line between the 6 mile fix and the 3 mile fix, with an altitude of 3,100 feet. Further, the solid line was defined in the Chart Legend as "Flight Path," which implied that a descent to 3,100 feet was proper once the fix to which the flight has been cleared is reached.

The crew was engaged in a local crop spraying mission on forest located in the region of Austin, Nevada. While flying at low height, the airplane went our of control and crashed in a wooded area. Both crew members were killed.

The DC-3 was cruising at FL115 between Burbank and Hawthorne when a no. 2 engine failure forced the crew to shut the engine down and feathered the propeller. At 20:50 EDT the crew radioed Tonopah, NV and said they wanted to make an emergency landing there. At 20:58 EDT the no. 1 engine lost power. The propeller couldn't be feathered and an emergency glide was initiated towards Mud Lake airfield. A 2000 feet/min rate of descent was necessary to maintain a 110 knots airspeed. All electrical and hydraulic power was lost during the descent. The DC-3 struck the ground in a 10-20 degree nose down attitude during the flareout and overturned. It appeared that there were numerous maintenance irregularities, a.o. improperly adjusted valve clearances, improperly adjusted voltage regulators and improperly installed cylinders. The plane was equipped with 2 28V dc generators and one 12V battery. All electrical components other than the starters were designed for 12V dc operation. It also appeared that all maintenance was performed by companies other than the operator. In many instances inadequate and incomplete records failed to reflect work accomplished.