Alaska

While cruising parallel to the Seward - Anchorage highway at an altitude of 1,000 feet, the twin engine airplane collided with a Kenai Civil Air Patrol Beechcraft A-45 Mentor registered N1406Z. Engaged in a SAR mission after a Cessna 170 was missing, the Mentor was carrying two pilots. Following the collision, both aircraft dove into the ground and crashed. All four occupants were killed.

Few minutes after takeoff from Palmer, the pilot elected to gain height when the single engine airplane struck a mountain ridge and crashed. A passenger was killed while both other occupants were injured. The aircraft was destroyed.

Few minutes after it departed Anaktuvuk Pass Airstrip, while cruising in poor weather conditions, the single engine airplane struck the ground and crashed. The aircraft was destroyed and all five occupants were killed. The flight was completed on behalf of Wien Air Alaska.

While flying along the Aleutian Islands on a charter flight from Kenai to Dutch Harbor, the crew realized his fuel reserve was low and decided to reduce his altitude and to ditch the aircraft off Akutan Island. All five occupants were quickly rescued while the aircraft was lost.

About 0738LT on April 5, 1976, Alaska Airlines, Inc., Flight 60, a B-727-81, N124AS, departed Juneau, Alaska, on a regularly scheduled passenger flight to Seattle, Washington; an en route stop was scheduled for Ketchikan International Airport, Ketchikan, Alaska. There were 43 passengers and a crew of 7 on board. Anchorage air route traffic control center (ARTCC) cleared Flight 60 on an instrument flight rules (IFR) flight plan to the Ketchikan International Airport; the flight was routine en route. At 0805, Anchorage ARTCC cleared Flight 60 for an approach to runway 11 at Ketchikan. At 0807, the flight was 30 DME miles from the airport. At 0811, Flight 60 reported out of 10,000 feet and was cleared to contact Ketchikan Flight Service Station (FSS); the FSS advised the flight that the 0805 weather was: ceiling 800 ft., obscured, visibility 2 mi, light snow, fog, wind 330° at 5 kt. The FSS also advised the flight that braking action on runway 11 was poor; this report was based on braking tests performed by the airport manager. The captain testified that he did not recall hearing the braking condition report. Upon receipt of the clearance, the crew of Flight 60 began an ILS approach to Ketchikan. Near the 17-mile DME fix, as the flight descended through 4,000 feet, the crew acquired visual contact with the ground and water. As the flight approached Guard Island, the captain had the Island in sight and decided to abandon the ILS approach and to continue the approach visually. The captain testified that he established a 'visual glide slope of my own' at an altitude of about 1,000 feet, and stated that his eyes were '... the most reliable thing I have.' Visual contact with the approach lights was established about 2 miles from the runway threshold. The airport was visible shortly thereafter. The captain did not recall the airspeed at touchdown, but estimated that he touched down about 1,500 feet past the threshold of runway 11. He also testified that he did not see the yellow, 1,000-foot markers on the runway; he further testified that the runway '... was just wet.' A passenger on Flight 60, who was seated in seat 5A (just forward of the wing's leading edge), stated that the yellow runway marks were visible to him. The first officer has no recollection of the sequence of events leading to the accident; however, the second officer testified that airspeeds and descent rates were called out during the last 1,000 feet. The captain could not recall the flap setting either on approach or at touchdown. However, the second officer testified that after the landing gear was extended the first officer remarked, 'We're high,' and lowered the flaps from 30° to 40°. None of the cockpit crew remembered the airspeeds, descent rates, or altitudes of the aircraft during the approach and touchdown. Reference speed was calculated to be 117 kns with 40° flaps and 121 kns with 30° flaps. The captain testified that after touchdown he deployed the ground spoilers, reversed the engines, and applied the wheel brakes. Upon discovering that the braking action was poor, he decided to execute a go-around. He retracted the ground spoilers, called for 25° flaps, and attempted to obtain takeoff thrust. The thrust reverser mechanism did not disengage fully and the forward thrust could not be obtained. He then applied full reversing and quickly moved the thrust levers to 'idle.' This attempt to obtain forward thrust also was not successful. The captain then reapplied reverse thrust and again deployed the ground spoilers in an attempt to slow the aircraft. When he realized that the aircraft could not be stopped on the runway, he turned the aircraft to the right, raised the nose, and passed over a gully and a service road beyond the departure end of the runway. The aircraft came to rest in a ravine, 700 feet past the departure end of runway 11 and 125 feet to the right of the runway centerline. Flight attendants reported nothing unusual about the approach and touchdown, except for the relatively short time between the illumination of the no-smoking sign and the touchdown. The two flight attendants assigned to the rear jumpseats and the attendant assigned to the forward jumpseat did not have sufficient time to reach their assigned seats and had to sit in passenger seats. None of the flight attendants felt the aircraft decelerate or heard normal reverse thrust. Many passengers anticipated the accident because of the high speed of the aircraft after touchdown and the lack of deceleration. Two ground witnesses, who are also pilots, saw the aircraft when it was at an altitude of 500 to 700 feet and in level flight. The witnesses were located about 7,000 feet northwest of the threshold of runway 11. They stated that the landing gear was up and that the aircraft seemed to be 'fast' for that portion of the approach. When the aircraft disappeared behind an obstruction, these witnesses moved to another location to continue watching the aircraft. They saw the nose gear in transit and stated that it appeared to be completely down as the aircraft crossed over the first two approach lights. The first two approach lights are located about 3,000 feet from the runway threshold. A witness, who was located on the fifth floor of the airport terminal, saw the aircraft when it was about 25 feet over the runway. The witness stated that the aircraft was in a level attitude, but that it appeared 'very fast.' He stated that the aircraft touched down about one-quarter way down the runway, that it bounced slightly, and that it landed again on the nose gear only. It then began a porpoising motion which continued until the aircraft was past midfield. Most witnesses placed the touchdown between one-quarter and one-half way down the runway and reported that the aircraft seemed faster-than-normal during the landing roll. Witnesses reported varying degrees of reverse thrust, but most reported only a short burst of reverse thrust as the aircraft passed the airport terminal, about 3,800 feet past the threshold of runway 11.

After landing on an frozen lake cleared of snow, the four engine airplane ran off the end of runway, lost its right main gear and came to rest in flames. All three crew members escaped uninjured while the aircraft was damaged beyond repair.

The single engine airplane departed Igiugig Airstrip in poor weather conditions with low clouds and a limited visibility due to snow falls. During climb, the pilot lost control of the airplane that crashed on the slope of a mountain. The aircraft was totally destroyed and all four occupants have been killed.

During a final approach completed in limited visibility due to low clouds and fog, the crew failed to realize that his altitude was too low when the airplane struck the ground and crashed 914 metres short of runway threshold. Both pilots and four passengers were killed while two other passengers were seriously injured.

Shortly after takeoff from Eielson AFB, while climbing, the crew encountered technical problems with the undercarriage when the airplane went out of control and crashed on a frozen lake located five miles south of the airbase. The aircraft was destroyed and all four crew members were killed. They were involved in a local training mission.

While cruising in good weather conditions, the pilot lost control of the airplane that stalled and crashed on the slope of a mountain located about 12 miles from Kijik Lake. The wreckage was found a day later and all eight occupants have been killed.