Tag Archives: Lockheed L-1049H Super Constellation

24 November 1959

Trans World Airlines’ Lockheed L-1049H Super Constellation N102R at Frankfurt, Germany, 1959. (Erich Marek)

24 November 1959: At 5:35 a.m., Central Standard Time, Trans World Airlines Flight 595, a Lockheed L-1049H Super Constellation freighter, N102R, crashed into a residential area about ¼-mile (0.4 kilometer) to the southeast of Midway Airport (MDW), Chicago, Illinois.

“How disabled plane, whose pilot tried to return to airport, crashed into homes on southwest side in holocaust of destruction.” —Chicago Tribune, Vol. CXVIII, No. 282, Wednesday, 25 November 1959, Page 3, columns 5–8)
(L–R) Auge, Helwig, Watters.

N102R had departed Midway Airport at approximately 5:31 a.m., Central Standard Time (11:31 UTC), en route to Los Angeles, California. The flight crew were Captain Claude Wilbert Helwig, First Officer Delmas Earl Watters, and Flight Engineer Aerion Lyman Auge, Jr.

A weather observation made ten minutes before takeoff reported the sky partially obscured, scattered clouds at 600 feet (183 meters), measured 900 foot (274 meters) overcast; visibility 3 miles (4.8 kilometers), with light rain, fog and smoke. The wind was 10 knots (5.14 meters per second) temperature 39 °F. (3.8 °C.) and dew point 38 °F. (3.3 °C.).

1 minute, 20 seconds after takeoff, the flight crew reported to the control tower that that they had a fire warning for the airplane’s number 2 engine (inboard, left wing) and that they would return to the airport. The tower cleared Flight 595 to land on Runway 31L. [Today, this runway is 31C.] The controller asked if they wanted to use a localizer approach, and received the answer, “I think we’ll make it VFR, OK,” meaning that the crew intended to remain in visual conditions below the overcast.

Ground track of TWA Flight 595, 24 November 1959. (Civil Aeronautics Board)

According to the accident investigation report,

      In the turn to final approach to runway 31 the aircraft banked in excess of 45 degrees during which it developed an excessive rate of sink. When the aircraft reached the tops of the trees its wings were nearly level and its nose was raised in a climbing attitude; however, the descent continued. The wing flaps were being retracted during the last 5 to 10 seconds of the final descent and were found to be symmetrically extended at 24 percent upon impact.

A controller saw the airplane crash into the residential area. The time was established by the time of the power failure caused when the Super Constellation hit the Commonwealth Edison Company power lines.

The three members of the flight crew and 11 people of the ground were killed. Another 11 people were injured.

Investigators found that the number 2 engine had been shut down and its propeller feathered, but there was no evidence of any inflight fire.

The investigative board found the the flight crew’s decision to remain below the clouds was reasonable under the circumstances.

     In anticipation of landing, a gear-down, flap-extended configuration was established on the downwind portion of the traffic pattern. The wing flaps were at least in the takeoff position of 60 percent and had been allowed, presumably to remain so extended since takeoff, because less than one minute had elapsed from the start of the takeoff roll until the fire warning, and at that time the captain planned to return to land. The track over the ground on the “downwind” curved toward the runway. When the aircraft was positioned to start the turn to final approach a sharp turn was needed to avoid overshooting the extended centerline of runway 31L.

     The Board believes the captain attempted such a turn, and in doing so combined a very steep bank with high gross weight ¹ and three-engine aircraft configuration in such a manner that the aircraft entered a regime of flight describable as being on the backside of the power curve. More power and altitude than was available to him was needed to safely recover the aircraft At some point in this turn the captain very probably decided to discontinue the landing approach and attempted to “go-around.” Hence, he called for gear up at or near this same point, but for an unexplained reason the wing flap controls were positioned for flap retraction.

The nose landing gear and left main gear assemblies were found to be in the up position but unlocked, and the right main gear was up and locked. The wing flaps were extended symmetrically at about 24 percent of their full travel. The flap control valve and follow-up mechanism were positioned to raise the flaps. The cockpit flap control lever was found to be about 1/8-inch (3.2 millimeters) aft of the full up position, with the lever bent over 80 degrees to the left. There was no indication that the lever had been forcibly moved fore or aft.

Wreckage of Lockheed L-1049H Super Constellation N102R in a hangar at Chicago Midway Airport 25 November 1959. (Civil Aeronautics Board)

The Civil Aeronautics Board determined that the Probable Cause of the accident was

     . . . the maneuvering of the aircraft in a manner that caused it to develop an excessive rate of sink in the turn to final approach.

Lockheed L-1049 Super Constellation three-view illustration with dimensions. (Lockheed Aircraft Corporation)

The L-1049 series was 18 feet, 4 inches (5.588 meters) longer than the preceding L-749 Constellation, with cylindrical “plugs” installed fore and aft of the wing. The L-1049H was the final commercial variant of the Super Constellation series. It could be converted from a passenger airliner to an air freighter configuration in a few hours. The L-1049 was 113 feet, 3.7 inches (34.536 meters) long, with a wingspan of 123 feet, 0 inches (37.490 meters), and overall height of 24 feet, 9.5 inches (7.557 meters). The fuselage had a maximum diameter of 11 feet, 7½ inches ( meters).

The total wing area was 1,650 square feet (153.3 square meters). The wings’ leading edges were swept aft 7° 28.7′, while the trailing edges swept forward 3° 13′. They had 7° 36.6′ dihedral.

Factory cutaway Wright Aeronautical Division 988TC18 turbocompound engine. (Aircraft Engine Historical Society)

N102R was powered by four air-cooled, direct-fuel-injected, 3,347.662 cubic-inch-displacement (54.858 liters) Wright Aeronautical Division 988TC18EA3 Duplex Cyclone turbocompound engines with a compression ratio of 6.70:1. The turbocompound engine used captured exhaust gases to drive three Power Recovery Turbines. These PRTs were coupled to the engine’s crankshaft. This system added approximately 450 horsepower to the engine’s total power output.

The 988RC18EA3 had Normal Power ratings of 2,860 horsepower at 2,650 r.p.m. at Sea Level; 2,920 horsepower at 2,650 r.p.m. at 4,800 feet (1,463 meters); 2,450 horsepower at 2,600 r.p.m. at 16,400 feet (4,999 meters). Its Maximum Power ratings were 3,400 horsepower at 2,900 r.p.m. to 4,000 feet (1,219 meters) for Take Off; and 2,600 horsepower at 2,600 r.p.m. at

The engines turned three-bladed Hamilton Standard propellers through a 0.4375:1 propeller gear reduction. The reduction gears were strengthened to support 4,000 horsepower. The Wright 988TC18EA3 was 7 feet, 5.53 inches (2.274 meters) long, 4 feet, 8.59 inches (1.473 meters) in diameter, and weighed 3,640 pounds, ± 1% (1,651 kilograms).15,200 feet (4,633 meters). 115/145-octane aviation gasoline was required.

The L-1049 had a maximum speed for normal operations (VNO) of 260 knots (299 miles per hour/482 kilometers per hour) and a maximum speed (VNE) of 293 knots (337 miles per hour/543 kilometers per hour) up to 11,000 feet (3,353 meters). VNO was reduced by 9 knots, and VNE reduced by 11 knots, for each 2,000 foot (610 meters) increase in altitude above 11,000 feet.

The maximum operating altitude for the L-1049 was 25,000 feet (7,620 meters). Its maximum range was 4,140 miles (6,663 kilometers).

N102R had a manufacture date of 6 June 1957. When it went through a scheduled overhaul 8 March 1959, it had accumulated 3,432:08 hours of flight time.

Claude Wilbert Helwig was born 9 July 1919 in San Francisco, California. He was the son of Henry Wilbert Helwig, a truck driver, and Mina Helwig Borchard. He attended Balboa High School in San Francisco, graduating in 1937.

Helwig enlisted in the United States Army Air Forces 12 March 1941. He had brown hair, gray eyes, a light complexion, was 5 feet, 8 inches (178 centimeters) tall and weighed 133 pounds (60 kilograms). Helwig was honorably discharged 9 March 1943 and was commissioned as a second lieutenant, Air Corps, Army of the United States (AUS), 10 March 1943. he was assigned to in the 14th Troop Carrier Squadron, 61st Troop Carrier Group.

Lieutenant Helwig married Miss Josephine Crull at Crow Creek Township, North Carolina, 20 May 1943. The ceremony was performed by J.W. Johnson, Justice of the Peace.

Following World War II, Helwig remained in the U.S. Air Force Reserve, serving with the rank of captain. He was discharged 1 April 1953. Captain Helwig had been awarded the Air Medal with 13 oak leaf clusters (14 awards). Captain Helwig’s remains were interred at Glen Oaks Memorial Park, Chico, California.

Delmas Earl Watters was born at Estill Springs, Tennessee, 30 November 1922. He was the son of Earl Watters, a locomotive fireman,  and Annabelle Smith Watters.

He attended Tennessee Technological University, Cookeville, Tennessee.

Watters enlisted as an aviation cadet in the United States Navy, 9 December 1942, at Atlanta, Georgia. He entered pre-flight school at Athens, Georgia, 1 May 1942, then underwent flight training at Corpus Christi, Texas. His enlistment was terminated to accept a commission as an ensign, United States Navy Reserve, 26 December 1944.

Ensign Watters married Miss Theda Jeanne McMillan in King County, Washington, 30 December 1945. The ceremony was performed by J. Robert Walter of the Central Presbyterian Church, Seattle, Washington. They later divorced.

Ensign Watters was promoted to the rank of lieutenant (junior grade), 1 January 1947.

Watters later transferred to the United States Air Force with the rank of first lieutenant. During the Korean War, he was awarded the Distinguished Flying Cross with one oak leaf cluster (two awards).

Watters married Miss Jean Ruth Cleere at the Chapel of Roses, Pasadena, California, California, 30 December 1951. They would have one son.

First Officer Watters’ remains were interred at the Mountain View Cemetery and Mausoleum, Altadena, California.

Aerion Lyman Auge, jr., was born 8 June 1924 in Jefferson, Kentucky. He was the son of Aerian Lyman Auge, an electrician, and Isabelle Veronica Jahn Auge.

Auge served in the United States Navy during World War II.

Auge married Yvonne Easton in Pierce County, Washington, 19 April 1946. They would have three daughters. Flight Engineer Auge’s remains were interred at the Inglewood Park Cemetery, Inglewood, California.

Thanks to TDiA reader George Firis for suggesting this subject. Mr. Firis’s aunt lived in an apartment building that was destroyed.

¹ The computed allowable gross takeoff weight for this flight was 127,400 pounds (57,788 kilograms). At departure, the aircraft weighed 126,606 pounds (57,428 kilograms). The allowable landing weight was 115,000 pounds (52,163 kilograms).

© 2024, Bryan R. Swopes

15 March 1962

Color photograph of Flying Tiger Line’s Lockheed L-1049H Super Constellation N6921C. (Pinterest)

15 March 1962: Flying Tiger Line Flight 7815/13 was a chartered flight for the Military Air Transport Service (M.A.T.S. Flight 739/14), from Travis Air Force Base, Fairfield, California, to Saigon, Republic of Vietnam, with scheduled refueling stops at Honolulu, Hawaii; Wake Island; Naval Air Station Agana, Guam; and Clark Air Force Base, Luzon, Philippine Islands. The flight departed Travis at 0545 G.M.T., 14 March.

The airliner was a Lockheed L-1049H Super Constellation, N6921C, under the command of Captain Gregory P. Thomas. The flight crew consisted of three pilots, two flight engineers, and two navigators/radio operators. There were four stewardesses in the passenger cabin, with 96 passengers. Three of the passengers were Vietnamese military personnel, while the remainder were U.S. Army electronics and communications specialists.

The Super Constellation departed Guam for Luzon at 1257 G.M.T, 15 March. It climbed to 18,000 feet (5,486 meters). The estimated flight time for this leg was 6 hours, 19 minutes. The airplane carried sufficient fuel for 9 hours, 30 minutes of flight.

At 1422 G.M.T., M.A.T.S. flight 739/14 radioed the Guam International Flight Service Station, reporting their position at 1416 hours as North 13° 40′, East 140°, and cruising at 18,000 feet (5,486 meters). The navigator gave the flight’s estimated position at 1530 G.M.T. as N. 14° 00′, E. 135° 00′.

There was no 1530 hours position report from Flight 739. Beginning at 1533 G.M.T., the Guam I.F.S.S. began attempting to contact the airliner, but was unsuccessful. At 1943  hours, the Joint Rescue Coordination Centers at NAS Agana and Clark AFB began search and rescue operations. At 2227 hours, the airliner was declared lost.

S.S. T. L. Lenzen, built by Mitsubishi Zozen K.K., 1959–1960. 42,277 deadweight tons, 16,000 horsepower. Cargo capacity 319,000 barrels. (The Allen Collection)

The crew of the Standard Oil Company tanker S.S. T. L. Lenzen reported that at 1530 G.M.T., (1:30 a.m., local time), five persons on board had witnessed a midair explosion near Flight 739’s estimated position for that time. The flash was bright enough to illuminate the ship’s decks.

It was established, upon interrogation of five of the crew members, that shipboard lookouts had observed a midair explosion at the approximate position and time when N 6921C was expected to reach 14°00′ North and 135°00′ East. It was recalled that a vapor trail, or some phenomenon resembling a vapor trail, was first observed overhead and slightly to the north of the tanker and moving in an east to west direction. The Lenzen was cruising on a heading of 077° at this time. As this vapor trail passed behind a cloud, there occurred an explosion which was described by the witnesses as intensely luminous, with a white nucleus surrounded by a reddish-orange periphery with radial lines of identically colored light. The explosion occurred in two pulses lasting between two and three seconds and from it two flaming objects of unequal brightness and size apparently fell, at different speeds, into the sea. During the last 10 seconds of the fall of the slower of the two objects, a small bright target was observed on the ship’s radar bearing 270°, range 17 miles.

The captain of the Lenzen stated that he arrived on deck in time to observe the fall of the slower object for approximately 10 seconds before it disappeared from view. He estimated its position in reference to a star and ordered the ship’s course reversed and, after aligning the heading of the vessel with the star, found his heading to be 270°—the same as the bearing of the target previously seen on radar. The captain reported that the weather at that time was:  ‘moonlight, clear atmosphere, 1/4 covered sky by small cumulus clouds evenly distributed.’ The ship proceeded to the position of the radar target and searched the area until 2105 at which time the original course was resumed. No signals or unusual sightings were reported.

The subsequent search, one of the most extensive ever conducted in the history of aviation, covered 144,000 square miles and utilized 1,300 people, 48 aircraft, and 8 surface vessels. A total of 377 air sorties were flown which involved over 3,417 flying hours. Despite the thoroughness of the search, nothing was found that could conceivably be linked to the missing aircraft or its occupants.

CIVIL AERONAUTICS BOARD, AIRCRAFT ACCIDENT REPORT, File No. 1-0002, 8 April 1963, at Pages 8–9

Probable Cause: The Board is unable to determine the probable cause of this accident from the evidence now available.

The last known position of Flying Tiger Line M.A.T.S. Flight 739/14. (GIS & Environmental Management Technologies, LLC)

BURBANK, Calif. (AP)—Sabotage, already suspected in the mysterious disappearance of an airliner loaded with American troops, would be considered a stronger possibility than ever if it turns out the plane blew up.

A Flying Tiger Lines official said Sunday experts consider it impossible for a violent explosion to occur about aboard its Super Constellation under normal conditions.

“We’ve gone over it thoroughly the last few days,” said Frank B. Lynott, executive vice president for operation. “The only explosions known to happen would be in empty wing tanks, and none of these would have been empty then. So far as blowing completely apart,” he said, “there’s nothing that powerful aboard: fuel tanks don’t just go off like that.”

Hartford Courant, Hartford, Connecticut, Volume CXXV, Number 78, Monday, 19 March 1962, Page 21 at Column 2

Another speculative theory was that the airliner had been hijacked in order to kidnap the passengers.

Lockheed L-1049H Super Constellation N6921C. (Bureau of Aircraft Accident Archives)
Capt. Gregory P. Thomas (Los Angeles Times)

The flight crew of M.A.T.S. Flight 739/14 were all highly experienced airmen. Captain Gregory P. Thomas had been employed by the Flying Tiger Line since 7 July 1950. He held an Airline Transport Pilot certificate, and was type-rated in the Curtiss C-46, Douglas DC-3, DC-4, DC-6, and Lockheed L-1049H. He had flown a total of 19,500 flight hours, with 3,562 hours in the L-1049H. He was 48 years old and lived in Red Bank, New Jersey. According to contemporary news reports, Captain Thomas was “a colorful and heroic flier.” (In 1957, he had ditched a Douglas DC-6 in Jamaica Bay with no loss of life.)

First Officer Robert J. Wish. (Flying Tiger Line)

First Officer Robert J. Wish had worked for FTL since 25 January 1951. He held an ATP certificate, with type ratings for C-46, DC-4 and L-1049H.had a total of 17,500 flight hours, with 3,374 hours in the L-1049H. Wish was also 48 years old, and lived in Hidden Hills, California.

Second Officer Robbie J. Gayzaway [Gazaway or Gazzaway?], 39 years old, from Fillmore, California, was employed by FTL 7 January 1953. He held an ATP certificate with an L-1049H type rating. He had flown 5,500 hours, with 900 in the L-1049H.

Flight Engineer George Nau. (Laura Nau Collection)

Flight Engineer George Michael Nau was hired by the Flying Tiger Line 15 December 1956. He held an F.A.A. Flight Engineer certificate. He had flown 1,235 hours in the L-1049H. Nau was 38 years old and lived in Pacoima, California.

A second flight engineer was Clayton E. McClellan, 33 years old, from San Mateo, California. He was also a certified flight engineer. He had worked for FTL since 4 April 1960. He had approximately 1,090 hours in the L-1049H.

Navigator Grady R. Burt, Jr. (Connie Burt Spolar via Find A Grave)

Navigator William T. Kennedy was hired by FTL 13 February 1962. He was 45 years old, from Braintree, California. He held both navigator and radio operator licenses.

Navigator Grady Reese Burt, Jr., was hired 14 February 1962. He also held both navigator and radio operators licenses. He lived in Baldwin Park, California.

The cabin crew were Senior Flight Attendant Barbara Jean Walmsley from Santa Barbara, California; Hildegard Muller; Christel Diana Reiter of San Mateo; and Patricia Wassum.

The Super Constellation remains missing today, and all 107 persons on board are presumed to have died. With respect to the loss of life, this was the worst accident involving a Lockheed Constellation.

N6921C was the second Lockheed L-1049H Super Constellation lost by Flying Tiger Line on 15 March 1962.

The first was N6911C (Lockheed serial number 4804), under the command of Captain Morgan W. Hughes of San Mateo, California. It was also a M.A.T.S. chartered flight, FTL Flight 7816/14, and, like N6921C, had departed from Travis Air Force Base on the night of 14 March. It was reportedly carrying a “secret military cargo” to Kadena Air Force Base, Okinawa.

While on a Ground Controlled Approach (GCA) approach to NAS Adak Island (in the Aleutian Islands of Alaska) the airliner was consistently below the glide path. Despite seven separate warnings from the ground controller, at 1214 G.M.T., the airplane’s landing gear struck rocks 328 feet (100 meters) short of the runway threshold. It then slid for 2,000 feet (610 meters) along the runway, coming to rest just off its edge. The airliner caught fire and was destroyed. Of the 7 persons on board, 1, James M. Johnstone, a flight engineer, was killed.

Captain Hughes had a total of 13,000 flight hours, with 3,055 hours in the L-1049H. The co-pilot, First Officer Thomas M. Mitchell, had 19,000 flight hours with 1,211 hours in type.

The Civil Aeronautics Board determined that the Probable Cause of this accident was “. . . attributed to the pilots’ misjudgement of distance and altitude during the final approach.”

Flying Tiger Line lost two more L-1049H Super Constellations, N6923C and 6913C, in 1962.

Flying Tiger Line’s Lockheed L-1049H Super Constellation N6918C, the same type aircraft as N6921C. (Jon Proctor via Wikipedia)

Lockheed L-1049H Super Constellation N6921C (LAC serial number 4817) was delivered to the Flying Tiger Line in 1957. It was a large, four-engine, long-range airliner. The airplane was operated by two pilots, a flight engineer and a navigator.

The L-1049 series was 18 feet, 4 inches (5.588 meters) longer than the preceding L-749 Constellation, with cylindrical “plugs” installed fore and aft of the wing. The L-1049H was the final commercial variant of the Super Constellation series. It could be converted from a passenger airliner to an air freighter configuration in a few hours. The L-1049 was 113 feet, 3.7 inches (34.536 meters) long, with a wingspan of 123 feet, 0 inches (37.490 meters), and overall height of 24 feet, 9.5 inches (7.557 meters). The fuselage had a maximum diameter of 11 feet, 7½ inches ( meters).

The total wing area was 1,650 square feet (153.3 square meters). The wings’ leading edges were swept aft 7° 28.7′, while the trailing edges swept forward 3° 13′. They had 7° 36.6′ dihedral.

The L-1049H had an empty weight of approximately 73,000 pounds (33,122 kilograms. N6921C had a maximum allowable gross weight of 141,845 pounds (64,340 kilograms). When it departed Guam, it carried 25,552 pounds (11,590 kilograms) of 115/145-octane aviation gasoline, and its gross weight was 132,554 pounds (60,125 kilograms).

Lockheed L-1049 Super Constellation three-view illustration with dimensions. (Lockheed Aircraft Corporation)

N6921C was powered by four air-cooled, direct-fuel-injected, 3,347.662 cubic-inch-displacement (54.858 liters) Wright Aeronautical Division 988TC18EA3 turbocompound engines with a compression ratio of 6.70:1. The turbocompound engine used captured exhaust gases to drive three Power Recovery Turbines. These PRTs were coupled to the engine’s crankshaft. This system added approximately 450 horsepower to the engine’s total power output.

The 988RC18EA3 had Normal Power ratings of 2,860 horsepower at 2,650 r.p.m. at Sea Level; 2,920 horsepower at 2,650 r.p.m. at 4,800 feet (1,463 meters); 2,450 horsepower at 2,600 r.p.m. at 16,400 feet (4,999 meters). Its Maximum Power ratings were 3,400 horsepower at 2,900 r.p.m. to 4,000 feet (1,219 meters) for Take Off; and 2,600 horsepower at 2,600 r.p.m. at 15,200 feet (4,633 meters). 115/145-octane aviation gasoline was required.

The engines turned three-bladed Hamilton Standard or Curtiss Electric propellers through a 0.4375:1 propeller gear reduction. The reduction gears were strengthened to support 4,000 horsepower. The Wright 988TC18EA3 was 7 feet, 5.53 inches (2.274 meters) long, 4 feet, 8.59 inches (1.473 meters) in diameter, and weighed 3,640 pounds, ± 1% (1,651 kilograms).

Factory cutaway Wright Aeronautical Division 988TC18 turbocompound engine. (Aircraft Engine Historical Society)

The L-1049 had a maximum speed for normal operations (VNO) of 260 knots (299 miles per hour/482 kilometers per hour) and a maximum speed (VNE) of 293 knots (337 miles per hour/543 kilometers per hour) up to 11,000 feet (3,353 meters). VNO was reduced by 9 knots, and VNE reduced by 11 knots, for each 2,000 foot (610 meters) increase in altitude above 11,000 feet.

The maximum operating altitude for the L-1049 was 25,000 feet (7,620 meters). Its maximum range was 4,140 miles (6,663 kilometers).

N6921C had flown a total 17,224 hours in just under five years. It was properly certified and maintained, and had no known discrepancies. N6911C had 16,038 hours, TTAF.

Flying Tiger Line’s Lockheed L-1049H Super Constellation N6915C, the same aircraft type as N6911C and 6921C. This airplane crashed 24 December 1964 at San Francisco, California. (Bureau of Aircraft Accident Archives)

© 2019, Bryan R. Swopes