United States of America

After touchdown at Seldovia Airport, the airplane encountered difficulties to stop within the remaining distance, overran, hit obstacles and went down an embankment before coming to rest. All four occupants were rescued while the aircraft was damaged beyond repair.

A Mohawk Airlines, Inc., Martin 404, N449A, operating as Flight 112 from Rochester, New York, to Newark, New Jersey, crashed on the Rochester-Monroe County Airport July 2, 1963, at approximately 1649 e d t. Seven of the forty-three persons aboard, including both pilots, were fatally injured. Flight 112 commenced a takeoff on runway 28 as a thunderstorm approaching from the west-northwest, moved over the takeoff runway. After becoming airborne and almost immediately after entering heavy rain and shifting wind conditions, the left wing of the aircraft made contact with the ground. In the ensuing Cartwheel to a stop, the aircraft was destroyed by impact and fire.

The crew was completing a local training flight at Westover AFB and encountered poor visibility due to heavy rain falls. On final, the airplane was too low, struck trees and crashed on a hilly and wooded terrain (777 feet high) located 5 miles short of runway and one mile to the left of the approach path. Three crew members were injured and the fourth occupant was killed. For unknown reason, the aircraft passed below the decision height and was not properly aligned.

Flight 388C was a nonstop flight from Daggett, California, to Manhattan, Kansas. The crew consisted of Captain David R Brown, First Officer Joseph A. Merlo, Flight Engineer Peter H. Raymon, Stewardesses Sandra R. wise, and Ann H. Allen, and Pilot/Observer Penrod Rideout who was assigned to this flight to observe operating procedures preparatory to transitioning to L-1049 type aircraft. The aircraft was serviced with fuel and oil at the company's maintenance base in Long Beach, California, and departed for Daggett at 1210. The only maintenance required prior to departure was the replacement of the Y-lead, high tension ignition leads, and spark plugs of cylinders Nos. 12 and 13 on the No. 3 engine. Upon arrival at Daggett at 1245, Federal Aviation Agency (TAA) and Military Air Transport Service (MATS) inspectors conducted a visual ramp inspection of the aircraft and interrogation of the crew. The only discrepancy noted was small area of corrosion on the underside of the aft fuselage in the vicinity of the lavatory service area. Sixty-four U. S. Army personnel boarded at Daggett and were briefed by a stewardess regarding emergency exit locations, emergency equipment and procedure The aircraft required no servicing or maintenance and there were no carry-over maintenance items reported. Takeoff gross weight was computed to be 116,520 pounds. This weight and the center of gravity (e.g.) were both within prescribed limit. Following an uneventful flight, the crew started the descent to Manhattan Municipal Airport when the observer/pilot, who was standing between the captain's and first off seats, recalled that shortly after entering the final approach he observed the propeller rpm increase approximately 100 rpm and then return to the setting of 2400 rpm, This fluctuation occurred three times. Then, following extension of full flaps, he observed the captain reduce power to approximately inches hg and almost immediately the rate of descent increased and the aircraft yawed to the right. The aircraft, was at an altitude of approximately 75 feet a.g l. when he observed the No 3 propeller reverse indicating the light 3 come on and shouted, "No. 3 is in reverse". This shouted warning was concurrent with the application of engine power and was not heard by the captain. None of the other flight crew members saw the reverse light illuminate. Persons on the ground who witnessed the accident generally agreed that the approach appeared normal until the aircraft reached a point approximately 1/3 of a mile from the airport. It was then observed to settle abruptly and contact the ground several hundred feet short of the runway. Initial impact occurred in a wheat field, 546 feet from the approach end of runway 21. At, this point the aircraft was in a right bank of approximately 15 degrees and aligned slightly to the right of the runway centerline The aircraft bounced once, then continued through the wheat field on all three landing gears until it struck an earth embankment. 3-1/2 feet high, located 176 feet from the end of the runway. This impact sheared the right main landing gear and the nose gear from the aircraft. The right wing separated from the fuselage when the aircraft contacted the end of the runway. The aircraft slid a distance of 774 feet down the runway during which time the left main landing gear failed followed by separation of the left wind. The fuselage came to rest on a heading of approximately 270 degrees, 72 feet from the right side of the runway. There were no fatalities and only one passenger was seriously injured. The aircraft was totally destroyed by a post crash fire.

Suffered an unclear accident upon landing at Andrews AFB. There were no injuries but the aircraft was written off.

The crew was performing a secret mission from Andrews AFB to March AFB. While overflying New Mexico, he encountered severe icing conditions. A wing fell off and the aircraft crashed in the Sandia Mountain Range located northeast of Albuquerque. All nine occupants were killed and the aircraft was destroyed. All USAF C-47's were grounded following this accident, until the struts had been replaced.

The crew was completing a local training flight at Travis AFB. After few circuits, the pilot-in-command started a new approach to runway 21L in poor weather conditions when control was lost. The airplane crashed in a huge explosion 0,8 mile short of runway threshold and was destroyed. All nine crew members were killed.

The approach to Millington was completed by night and in poor weather conditions. On final, the pilot declared an emergency as an engine failed. As the aircraft was not properly aligned with the runway, the crew elected to make a go around. A second attempt to land was completed in thunderstorm activity when the airplane stalled, hit a pecan tree and crashed in Hill Street, just near some houses. On ground, it lost its right wing and came to rest in flames. All 33 occupants evacuated safely while the aircraft was destroyed by fire.

The crew departed Eielson AFB, engaged in a routine refueling mission. Just after liftoff, while in initial climb, the engine number one failed. The airplane banked left and crashed in a huge explosion onto several buildings. All seven crew members and two people on the ground were killed. The aircraft and two buildings (the crew rest house and a guard local) were destroyed.

Zantop Air Transport, Inc., LOGAIR Flight 60-16 (VK060), a Curtiss C-40F, N616Z, crashed following an attempt to land on runway 17 at Thun Field, near Puyallup, Washington, at 1826 P.s.t., February 16, 1963. Both crew members survived the crash but were severely injured. There were no other occupants. The aircraft was destroyed by the impact and post-impact fire. An engine malfunction seven minutes after takeoff from McChord AFB, Washington, was followed by an unsuccessful attempt to feather the propeller and by intermittent overspeeding. During an attempted go-around from the landing approach the pilot lost control of the aircraft and crashed in a pasture approximately one-half tile northeast of Thun Field.