Trenton

Following an uneventful flight from RCAF Trenton on behalf of the RCAF, the twin engine aircraft apparently landed hard at Thunder Bay Airport. After touchdown on runway 25, it went out of control and veered off runway into a snow covered area. All three crew members evacuated safely while the aircraft suffered severe damages to wings and tail. The fuselage also broke in two.

The multi-engine airplane rolled inverted and dove into the ground on a landing approach. According to witnesses, the airplane made two approaches to runway 23. During the first approach the airplane was observed, "fish tailing" while about 30' feet over the runway. The airplane appeared to regain control and continued flying over the runway until passing the air traffic control tower, at which time the airplane began a climbing left turn. The witnesses stated that they heard the pilot tell the air traffic controller that he was doing a go-around. The controller asked the pilot if he had problems with the sea fog. The pilot responded back to the controller "no that his left engine kept power up a little too much and would not come back." The witnesses observed the airplane circle the airport to the left, and watched it line up on runway 23 for the second time. The witnesses stated that as the airplane descended to the runway and without any indication of trouble, the airplane "climbed and rolled left, went inverted and nosed down into the grass to the left of the runway and burst into flames." Examination of the airplane, airplane systems, engines, and propellers found no abnormal preimpact conditions that would have interfered with the normal operation of the airplane. No recorded radar data for the flight was located that captured the airplane's two attempted landings. Information contained in the Super King Air 200 Pilot's Operating Handbook (POH) and FAA Approved Flight Manual (AFM) showed the stall speed with gear extended, 40-degrees flaps, and zero bank angle as 84 knots Indicated Air Speed.

The pilot departed on a night cross-country flight without obtaining a weather briefing or flight plan. Arriving in the area of the destination airport, the weather was reported as, 2 statute miles of visibility and mist; overcast cloud layer at 100 feet. The pilot requested an instrument flight rules clearance from the approach controller, and was vectored and cleared for the ILS 24 approach. The clearance included an altitude restriction of 1,500 feet msl, until the airplane was established on the localizer. As the pilot contacted the control tower, the tower controller issued a low altitude alert to the pilot. The pilot replied that he was climbing and the tower controller cleared the pilot to land, which the pilot acknowledged. No further pertinent radio transmissions were received from the airplane. The airplane came to rest in a wooded area about 3/4-mile from the runway threshold, and about 50 feet right of the extended centerline. Review of the approach plate for the ILS 24 approach revealed that the minimum glide slope intercept altitude at the beginning of the final approach segment on the precision approach was 1,500 feet. The glide slope altitude at the final approach fix for the non-precision approach, which was located about 4 miles from the approach end of the runway, was 1,407 feet. The glide slope altitude at the middle marker, which was located about 0.6 miles from the approach end of the runway, was 299 feet. Review of radar data revealed that the airplane was observed at 700 feet, about 4 miles from the airport, and at 300 feet, about 1.5 miles from the airport. The pilot had accumulated about 1,946 hours of total flight experience, with about 252 hours in make and model. The pilot had attended initial and recurrent training for the make and model airplane; however, did not complete the training. The pilot, aged 61, was Charles B. Yates, member of the New Jersey Senate, who was flying to Martha's Vineyard with his wife and two of his three children.

Air traffic control had cleared the airplane for the ILS approach to runway 24, circle to land on runway 06. The airplane broke off the approach to runway 24, and was observed by a witness at a low altitude, on a left downwind for runway 06, flying in and out of clouds. On the base leg, the airplane turned to the left, and a witness saw the left wing make contact with the ground. One witness said that before the crash, the engine sounded 'like they were at full rpm. Several pilots from the air national guard (ang) at the airport went to the crash site minutes after the crash, and observed ice on the airplane's wings and empennage. One of the ang pilot reported his observation of the ice on the aircraft: 'It appeared to be approximately 1/8 inch in thickness throughout the left and right wing surfaces and the rear empennage sections . . .' Another ang pilot described the weather at the time of the accident as, visibility less then one mile with 'freezing rain and sleet.' The examination of the airplane did not disclose evidence of mechanical malfunction. Both occupants were killed.

The crew was dispatched out from Trenton on a SAR operation for a missing helicopter. While flying at low height, the four engine airplane crashed in a wooded area located about 13 km west of Chapais. Eight crew members were killed while two others were seriously injured.
Crew:
Cpt Dave Salmons, pilot, †
Cpt Ron Kavanagh, †
M/Cpl Allan Woodham, †
Sgt J. R. O'Neill, †
Cpl R. W. Fisher, †
Cpl R. J. Cocks, †
Cpl R. J. Taylor, †
Pvt W. D. Minnis, †
Cpt Dahl Manthorpe,
Mst W/O Bing Crosby.

The four engine airplane departed Brunswick NAS, Maine, at 1205LT on a flight to Trenton, Ontario, where it was dispatched to an airshow. While climbing, the crew encountered poor weather conditions with stormy weather when the engine n°1 went in whirl mode and detached. 11 feet of the left wing separated and struck the left horizontal stabilizer that was torn off as well. Out of control, the airplane entered a dive and partially disintegrated before crashing near Poland. All eight occupants were killed.
Crew:
Lt Cdr Francis William Dupont Jr.,
Lt Jg Donald Edward Merz,
Lt Jg George D. Nuttelman,
Lt Jg Ernest A. Smith,
Aw2 James Allen Piepkorn,
Awan Paul G. Schulz,
Ad3 Robert Lewis Phillips Jr.,
Adc Larry Miller.

While on a night approach to Trenton Airport, one of the engine failed. The crew decided to initiate a go-around when the airplane stalled and crashed in flames few miles short of runway. The aircraft was destroyed and all four occupants were killed.

While in cruising altitude and approaching Indianapolis from the east, the pilot encountered very bad weather conditions. He informed ATC about severe turbulences when control was lost. The twin engine airplane entered a spin and eventually crashed in a field located in Arlington. The aircraft was totally destroyed and all nine occupants were killed, among them seven employees of the United States Auto Club.

On approach to Hot Springs-Ingalls Field Airport, the crew encountered very poor weather conditions. On final, he failed to realize his altitude was too low when the airplane struck a mountain and crashed short of runway 24. The aircraft disintegrated on impact and all 11 occupants were killed. The wreckage was found 500 feet below the runway elevation. At the time of the accident, weather was poor with clouds down to 100 feet and fog.

The crew was engaged in a local training flight at Trenton Airport. Shortly after a night takeoff, while climbing, the four engine airplane crashed in unknown circumstances in a field located 2,5 km from the airport. All six crew members were killed.