Lockheed L-1049 Super Constellation

Flight 401 was a scheduled domestic flight between Madrid, Spain and Santa Cruz de Tenerife, Canary Islands. At 2053 hours the aircraft was cleared for approach to runway 30 at the Santa Cruz de Tenerife/Los Rodeos Airport. At this time it was informed by the approach controller that the airport was below meteorological minima and that the following weather conditions prevailed:
Wind : 330/variable 10 to 12 kt, gust to 14 kt
Visibility: 100 to 500 m, reduced to zero over the runway by a bar of stratus
Present weather: distant fog, intermittent fog banks
Clouds: 6/8 stratus from 0 to 30 m
QNH: 30.03 in of Hg
QFE: 942.9 mb
Temperature: 14°
Dew-point : 14°.
This was acknowledged by the flight. The pilot, who saw the beginning of runway 30 clearly but not the rest of it, decided to make a very low run after which he re-applied power for a go-around at 2106 hours. He circled the aerodrome, apparently intending to land, and at 2115 hours reported on final. At 2117 hours he reported to the tower: "401 pulling up to go around", and this was the last communication received from the aircraft. It was subsequently found that, when starting its go-around, the aircraft struck a scraper and tractor located 50 m from the runway edge, with one leg of the undercarriage and the lower aft part of the fuselage. It left various debris scattered about and finally crashed on the western edge of the diversion canal of the Rodeo gorge. From there, it slid about 100 m across private farmland and finally burst into flames. The accident occurred at 2117 hours.

Flight 282 was a scheduled domestic cargo flight from San Francisco International Airport, California, to John F. Kennedy International Airport, New York. It was originally scheduled to depart at 2100 hours, Pacific Standard Time, on 23 December, but the flight was delayed because of the non-availability of a flight engineer. An engineer obtained from Los Angeles arrived in San Francisco at 2315 hours and the flight departed at 0028 hours on 24 December. At 0015 hours, while taxiing to runway 28L, the flight advised Ground Control that because of a heavy load, they would like to proceed out past the GAP Radio Beacon to the Golden Gate Intersection, and thence via Victor 150 to Sacramento instead of direct to Sacramento as originally filed. The request was coordinated with Oakland Air Route Traffic Control Centre and approval obtained. The crew was then advised that for take-off on runway 28L there would be a 'heavy' left crosswind from 210° at 18 to 25 knots which they acknowledged. After having switched to clearance delivery frequency, the flight was cleared to Kennedy Airport via Victor one fifty Sacramento, Victor six north, and requested to climb out on the San Francisco two eight seven radial for a vector to Golden Gate Intersection to intercept Victor one fifty. This was acknowledged. The Clearance Delivery Controller then stated: " You can disregard the vector, climb outbound San Francisco 287° radial to Golden Gate Intersection, then Victor 150, and, depending on your altitude, they probably will give you a vector to intercept (Victor) 150 before you get to Golden Gate". This was also acknowledged. The Local Controller, who was also Tower Supervisor, noted the time of 0030 on his clock as the aircraft became airborne and passed the tower. An eyewitness observed the landing lights retracting as the aircraft crossed the end of the runway. However, several witnesses along the flight path, including some located at points just prior to the crash, saw both landing lights on. Landing lights of the L-1049H may be retracted flush with the lower wing surface and remain on until switched off. After take-off, witnesses stated the aircraft made a slight turn to the right, then a steeper turn to the left, and then was observed returning to a wings-level attitude as it entered the clouds. At 0030:22, the flight was advised to contact Departure Control and did so immediately. The Departure Controller advised the flight at 0030:57 that he had radar contact with it and requested it to report leaving thousand-foot altitudes. At 0031:05, the crew asked how they were tracking toward the GAP. The Departure Controller switched his radar scope from the 30 to the 10-mile setting and requested the flight's altitude. The crew!replied they were at 900 ft. At 0031:20, the Departure Controller advised that they were left of the San Francisco 287° radial. As he received no acknowledgement he repeated his message. The Departure Controller stated that within seconds after the second transmission, the target stopped, bloomed, and disappeared from the radar scope. Repeated attempts to communicate with the flight after its disappearance from the scope were unsuccessful. At this time, 0032:30, the controller placed a time hack on the communications tape. Ground impact was computed to have occurred at approximately 0031:30. Main impact occurred 860 ft above sea level on Sweeney's Ridge, at approximately 4.3 miles on the 257° radial of the SFO TVOR. The coordinates of the impact area were 122° 28' 00" W longitude and 37° 38' 28" N latitude. The aircraft disintegrated on impact and all three crew members were killed.

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.

A Slick Airways Lockheed 1049H, N9740Z, crashed and burned during an ILS approach to runway 28R at the San Francisco International Airport at approximately 1207 P.s.t., February 3, 1963. Due to an inoperative glide slope receiver, the crew was listening radar advisories on the localizer receiver for altitude information. The aircraft struck approach lights 1,170 feet from the runway threshold, climbed to about 200 feet and then crashed approximately 1,900 feet beyond the threshold and on the left edge of runway 28L. Of the three crew members and five passengers aboard, the captain, first officer, and two passengers received fatal injuries. The remaining persons aboard received serious injuries. The aircraft was destroyed by subsequent fire.

On December 14, 1962, at 2212 P.s.t., a Flying Tiger Line Inc., Super Constellation, N6913C, crashed about 1-1/4 miles west of the Lockheed Air Terminal, Burbank California, during an ILS approach to runway 7. All five persons on board the aircraft and three persons on the ground sustained fatal injuries. The last radio communication with N6913C was the flight's acknowledgement of its radar-observed position two miles from the end of the runway on the localizer course. Twenty seconds later the aircraft crashed Into a fog-shrouded residential/industrial area.

he Super Constellation departed Gander at 17:09 GMT for a military (MATS) charter flight to Frankfurt. Three hours later, at FL210 a fire developed in the no. 3 engine, which was shut down and the propeller feathered. The no. 1 engine oversped 5 minutes later when the flight engineer closed the no. 1 engine firewall shut-off valve in error. The crew were not able to restart the engine, and wanted to divert to Shannon with METO power on the no. 4 engine and reduced power on engine no. 2. The no. 2 engine lost power and finally failed, forcing the crew to carry out a ditching. The left wing broke off, but the fuselage remained intact. The cabin filled with water fast and the aircraft sank nose first in about 10 minutes. The Swiss merchant ship christened 'Celerina' was the first to be on site and its crew was able to evacuate 48 wounded people while 28 others, among them five crew members, were killed. The aircraft sank and was lost.

On approach to Patuxent River NAS, the crew encountered poor weather conditions with heavy rain falls. In low visibility, the aircraft was too low and struck the ground before coming to rest in flames few hundred yards short of runway threshold. Five occupants were killed while 14 others were injured. The aircraft was destroyed.

The aircraft departed Frankfurt-Main on a special flight, carrying a crew of four, 22 passengers and thousands of confidential documents of the US Army. While cruising at an altitude of 18,000 feet, the crew contacted ATC twice, declared an emergency and elected to divert to Munich-Riem Airport. Shortly later, the aircraft exploded and crashed in a field located in Markt Schwaben, 17 km south of Munich Airport. The aircraft was totally destroyed and all 26 occupants were killed. Debris and documents were scattered on an area over 65 km2.

On March 15, 1962, sometime after its last position report at 1422 G.m.t. (22 minutes past midnight, local time), a Flying Tiger Line Inc., Lockheed 1049H, N6921C, operated as Military Air Transport Service Flight 739/14, disappeared west of the position 13 degrees 14' North Latitude and 140 degrees 00' East Longitude en route from Agana Naval Air Station, Guam, to Clark Air Force Base, Philippine Islands. A widespread and intensive search was initiated after the aircraft failed to arrive at Clark Air Force Base at 1916 G.m.t., its estimated time of arrival. The flight was officially declared missing at 2227 G.m.t. which was the estimated fuel exhaustion time for the aircraft. All occupants, 96 military passengers and a crew of 11, are missing and presumed dead. Crew members of a surface vessel witnessed what appeared to have been a midair explosion at 1530 G.m.t., near the position and at the time estimated by the pilot of N6921C for his next scheduled position report. No wreckage or debris which could be definitely associated with the aircraft has been found.

A Lockheed Constellation, model L-1049H, N 6911C, owned by The Flying Tiger Line Inc., and being operated under contract with the Military Air Transport Service, crashed during the hours of darkness at Adak, Alaska, March 15, 1962, at 1214 G.m.t. Impact and subsequent fire destroyed the aircraft. There were seven occupants, all crew members. Six received minor injuries and one, the duty flight engineer, was trapped in the cockpit and died in the fire. This was a scheduled cargo flight, designated by the carrier as Flight No. FTL 7816/14. It originated at Travis Air Force Base, California, for Kadena Air Force Base, Okinawa, with stops planned at Cold Bay, Alaska, Adak, Alaska, and Misawa, Japan. Shortly after departure from Travis Air Force Base, buffeting developed and the aircraft was landed back at Travis. Inspection disclosed an open hydraulic reservoir access door. This was closed and secured and the flight proceeded uneventfully to Cold Bay, Alaska. The flight from Cold Bay to the vicinity of Adak was also uneventful, with the copilot flying the aircraft from the left seat and the captain acting as copilot in the right seat. Instrument weather prevailed at Adak and a ground controlled approach (GCA) was started. The flight was advised several times that it was below the glide slope and then was advised to execute a missed approach. The aircraft’s captain replied that the field was in sight. The approach continued, visually. At a point 328 feet short of the runway threshold and four feet below its level the landing gear struck rocks. The main landing gear was torn off and the aircraft slid about 2,000 feet on the runway coining to rest just off its edge. A severe fire developed.