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Medal of Honor, Major Charles Joseph Loring, Jr., United States Air Force

Major Charles Joseph Loring, Jr., United States Air Force (1918–1952)
Major Charles Joseph Loring, Jr., United States Air Force (1918–1952)

MEDAL OF HONOR

LORING, CHARLES J., JR.

The President of the United States of America, in the name of Congress, takes pride in presenting the Medal of Honor (Posthumously) to Major Charles Joseph Loring, Jr. (AFSN: 13008A), United States Air Force, for conspicuous gallantry and intrepidity at the risk of his life above and beyond the call of duty while serving with the 80th Fighter-Bomber Squadron, 8th Fighter-Bomber Wing, Fifth Air Force in aerial combat at Sniper Ridge, North Korea, on 22 November 1952. While leading a flight of four F-80 type aircraft on a close support mission, Major Loring was briefed by a controller to dive-bomb enemy gun positions which were harassing friendly ground troops. After verifying the location of the target, Major Loring rolled into his dive bomb run. Throughout the run, extremely accurate ground fire was directed on his aircraft. Disregarding the accuracy and intensity of the ground fire, Major Loring aggressively continued to press the attack until his aircraft was hit. At approximately 4,000 feet, he deliberately altered his course and aimed his diving aircraft at active gun emplacements concentrated on a ridge northwest of the briefed target, turned his aircraft 45 degrees to the left, pulled up in a deliberate, controlled maneuver, and elected to sacrifice his life by diving his aircraft directly into the midst of the enemy emplacements. His selfless and heroic action completely destroyed the enemy gun emplacement and eliminated a dangerous threat to United Nations ground forces. Major Loring’s noble spirit, superlative courage, and conspicuous self-sacrifice in inflicting maximum damage on the enemy exemplified valor of the highest degree and his actions were in keeping with the finest traditions of the U.S. Air Force.

Action Date: November 22, 1952

Service: Air Force

Rank: Major

Company: 80th Fighter-Bomber Squadron

Regiment: 8th Fighter-Bomber Wing

Division: 5th Air Force

This Lockheed F-80C-10-LO Shooting Star, 49-1826, (marked FT-826)  of the 8th Fighter Bomber Wing is the same type as F-80C-10-LO, 49-1830, flown by Major Loring. (U.S. Air Force)

Charles Joseph Loring, Jr., was born at Portland, Maine, 2 October 1918. He was the first of four children of Charles Joseph Loring, a laborer, and Mary Irene Cronin Loring. Charles Loring, Sr., served in the United States military during World War I.

Lieutenant Charles J. Loring, Jr.

Charley Loring attended Cheverus High School, a private religious school in Portland, graduating in 1937.

Loring enlisted in the Air Corps, United States Army, at Cumberland, Maine, 16 November 1942. He was trained as a pilot at Greenville, Mississippi, and Napier Field, Alabama. He was commissioned a second lieutenant, Air Reserve, 16 February 1943.

During World War II, Lieutenant Charles J. Loring, Jr., had been a Republic P-47D Thunderbolt fighter pilot assigned to the 22nd Fighter Squadron, 36th Fighter Group, 9th Air Force, in Europe. Loring was promoted to first lieutenant, Army of the United States (A.U.S.), 24 June 1944. He was awarded the Distinguished Flying Cross for actions in support of the D-Day invasion of Normandy.

Lieutenant Loring flew 55 combat missions before his P-47D-28-RE, 44-19864, was shot down by ground fire near Rocherath-Krinkelt, Belgium, on Christmas Eve, 24 December 1944. Captured, Lieutenant Loring was taken to the garrison hospital at Hemer, then transferred to an interrogation center at Frankfurt, Germany. He remained a prisoner of war until Germany surrendered in May 1945.

Lieutenant Charles J. Loring, Jr., stands next to a Republic P-47 Thunderbolt. (World War II Flight Training Museum)

Loring was promoted to captain, A.U.S., 23 October 1945. He was awarded the Distinguished Flying Cross for actions in support of the D-Day invasion of Normandy. He was also awarded the Air Medal with ten oak leaf clusters, and the Purple Heart.

In 1945, Charles J. Loring, Jr. married Miss Elsie P. Colton of Beverly, Massachusetts, in Boston. They would have two daughters, Aldor Rogers Loring and Charlene Joan Loring.

After World War II came to an end, Captain Loring reverted to the rank of first lieutenant, Air Reserve, 16 February 1946. Loring was appointed first lieutenant, Air Corps, 19 June 1947 with date of rank retroactive to 16 February 1946. In September 1947, the United States Air Force was established as a separate military service, with standing equivalent to the United States Army and United States Navy. Charles Loring was appointed a first lieutenant, United States Air Force, with date of rank again 16 February 1946.

Lieutenant Charles J. Lorig was flying this Republic P-47D-28-RE Thunderbolt, 44-19864, marked 3T W, when he was shot down near Hotten, Belgium, 24 December 1944. (U.S. Air Force photograph via Jim Sterling)

Flying the Lockheed F-80C Shooting Star with the 80th Fighter Bomber Squadron, 8th Fighter Bomber Wing, during the Korean War, Major Loring served as the squadron operations officer. According to his father, Charles J. Loring, Sr., “Charley was a stubborn man. He said he would never be a prisoner again. He was the kind of man who kept his word about everything.”

Major Charles J. Loring, Jr., United States Air Force, Operations Officer, 80th Fighter Bomber Squadron ("Headhunters"), at K-13, Suwon, South Korea, Fall 1950. (U.S. Air Force)
Major Charles J. Loring, Jr., United States Air Force, Operations Officer, 80th Fighter Bomber Squadron (“Headhunters”), at K-13, Suwon, South Korea, Fall 1950. (U.S. Air Force)

The Medal of Honor was awarded by President Dwight D. Eisenhower, 5 May 1953, but this was kept secret by the Air Force “to protect him from enemy reprisal” in the event that Major Loring had not died in the crash of his fighter, but had been captured. The Medal was presented to Mrs. Loring and her two daughters, Aldor and Charlene, by Secretary of the Air Force Harold E. Talbott, during a ceremony held at Bolling Air Force Base, Washington, D.C., 17 April 1954. Limestone Army Airfield in Maine was renamed Loring Air Force Base, 1 October 1954.

Secretary of the Air Force Harold E. Talbott shows the Medal of Honor to the daughters of Major Charles Joseph Loring, Jr., during a presentation ceremony at Bolling Air Force Base, 17 April 1954. Left to right, Secretary Talbott; Charlene Joan Loring, age 4; Aldor Rogers Loring, age 5; Mrs. Loring. (NEA Wirephoto)

A cenotaph memorializing Major Loring is at the Arlington National Cemetery, Arlington, Virginia.

Medal of Honor

© 2017, Bryan R. Swopes

4 November 1941

Lockheed YP-38 Lightning 39-689, manufacturer's serial number 122-2202. (Lockheed)
Lockheed YP-38 Lightning 39-689, manufacturer’s serial number 122-2202. (Lockheed Martin)
Ralph Burwell. Virden (Los Angeles Times)

4 November 1941: Lockheed test pilot Ralph Burwell Virden was conducting high speed dive tests in the first Lockheed YP-38 Lightning, Air Corps serial number 39-689 (Lockheed’s serial number 122-2202).

As the airplane’s speed increased, it approached what is now known as its Critical Mach Number. Air flowing across the wings accelerated to transonic speeds and began to form shock waves. This interrupted lift and caused a portion of the wing to stall. Air no longer flowed smoothly along the airplane and the tail surfaces became ineffective. The YP-38 pitched down into a steeper dive and its speed increased even more.

Designed by famed aeronautical engineer Clarence L. “Kelly” Johnson, the YP-38 had servo tabs on the elevator that were intended to help the pilot maintain or regain control under these conditions. But they increased the elevator’s effectiveness too well.

The Los Angeles Times described the accident:

     Witnesses said the twin-engined, double-fuselaged ship was booming westward at near maximum speed (unofficially reported to be between 400 and 500 miles an hour) when the duralumin tail assembly “simply floated away.”

     A moment afterward the seven-ton craft seemed to put on a burst of speed, the the high whine of its engines rising.

     It then went into a downward glide to about 1500 feet, then into a flat spin, flipped over on its back and shot earthward.

     Several persons said that they thought they had heard an explosion during the dive, but qualified observers doubted it. . .

     . . . Fellow pilots at Lockheed said, “Ralph was the best we had, especially in power dives.”

      Robert E. Gross, president of Lockheed, said, “Ralph Virden was a great pilot but an even greater man. If anyone ever had national defense at heart it was he, who every day was carrying the science of aviation into new and higher fields.”

     Various witnesses said the ill-fated ship’s tail assembly could be followed easily as its bright surfaces glinted in the sun during its drop to earth. It landed several blocks from the scene of the crash.

     Mrs. Jack Davenport of 1334 Elm Ave., left her ironing board when she heard the unfamiliar roar of the plunging plane’s engines.

     “I ran out and saw it passing over us, very low. It disappeared among the trees and then zoomed back into sight just before crashing in the next block,” she said. “It looked just like a toy airplane. I knew the pilot didn’t have a chance, as the ship was too low and going too fast.”

Los Angeles Times, Vol. LX, Wednesday, 5 November 1941, Page 1, Column 6, and Page 2, Column 5.

The YP-38 crashed into the kitchen of Jack Jensen’s home at 1147 Elm Street, Glendale, California. Fire erupted. Ralph Virden was killed. The airplane’s tail section was located several blocks away.

Another view of Lockheed YP-38 Lightning 39-689. It's factory serial number, "2202," is stenciled on the nose. (Lockheed Martin)
Another photograph of Lockheed YP-38 Lightning 39-689. The factory serial number, “2202,” is stenciled on the nose. (Lockheed Martin)

39-689 was the first of thirteen YP-38 service test aircraft that had been ordered by the U.S. Army Air Corps shortly after the XP-38 prototype, 37-457, had crashed on a transcontinental speed record attempt, 11 February 1939. 39-689 made its first flight 16 September 1940 with test pilot Marshall Headle at the controls. With hundreds of production P-38s being built, Lockheed continued to use the YP-38 for testing.

Newspaper phototograph of the wreckage of Lockheed YP-38 Lightning 39-689 at 1147 Elm Street, Glendale, California. (Los Angeles Times)
Newspaper photograph of the wreckage of Lockheed YP-38 Lightning 39-689 at 1147 Elm Street, Glendale, California. (Los Angeles Times)

The YP-38s were service test prototypes of a single-place, twin engine long range fighter with a unique configuration. There was not a fuselage in the normal sense. The cockpit, nose landing gear, and armament were contained in a central nacelle mounted to the wing. Two engines and their turbochargers, cooling systems and main landing gear were in two parallel booms. The booms end with vertical fins and rudders, with the horizontal stabilizer and elevator between them. The P-38 was 37 feet, 9–15/16 inches (11.530 meters) long, with a wingspan of 52 feet, 0 inches (15.850 meters) and height of 12 feet, 10 inches (3.952 meters).

The P-38’s wings had a total area of 327.50 square feet (30.43 square meters). Their angle of incidence was 2° and there was 5° 40′ dihedral. The leading edges were swept aft 5° 10′.

The YP-38 had an empty weight 11,171 pounds (5,067 kilograms). The gross weight was 13,500 pounds (6,123 kilograms) and the maximum takeoff weight 14,348 pounds (6,508 kilograms).

The YP-38 was powered by two counter-rotating, liquid-cooled, turbosupercharged 1,710.597-cubic-inch displacement (28.032 liter) Allison V-1710-27 right-hand tractor and V-1710-29 left-hand tractor, single overhead cam (SOHC) 60° V-12 engines (Allison Engineering Co. Models F2R and F2L) with a Normal Power rating of 1,000 horsepower at 2,600 r.p.m., and 1,150 horsepower at 3,000 r.p.m. for takeoff. They drove three-bladed Curtiss Electric constant-speed propellers with a diameter of 11 feet, 6 inches (3.505 meters) through a 2.00:1 gear reduction. In a change from the XP-38, the propellers rotated outboard at the top of their arc. The V-1710-27/-29 engines were 7 feet, 1-5/8 inches (2.175 meters) long, 2 feet, 5-9/32 inches (0.744 meters) wide and 3 feet, 0-17/32 inches (0.928 meters) high. The V-1710-27/-29 weighed 1,305 pounds (592 kilograms)

The YP-38 had a maximum speed of 405 miles per hour (651.8 kilometers per hour) at 10,000 feet (3,048 meters) and it could climb  from the surface to 20,000 feet (6,096 meters) in six minutes. Normal range 650 miles (1,046 kilometers).

Lockheed built one XP-38, thirteen YP-38s, and more than 10,000 production fighter and reconnaissance airplanes. At the end of World War II, orders for nearly 2,000 more P-38 Lightnings were cancelled.

Lockheed YP-38 39-692 in flight.(Hans Groenhoff Photographic Collection, Smithsonian Institution National Air and Space Museum NASM-HGC-967)

Ralph Burwell Virden was born 11 June 1898, at Audobon Township, Illinois. He was the second child of Hiram R. Virden, a farmer, and Nancy Carrie Ivy Virden.

Virden attended Bradley Polytechnic Institute at Peoria, Illinois. At the age of 17, 15 October 1918, Ralph Virden enlisted in the U.S. Army. With the end of World War I less than one month later, he was quickly discharged, 7 December 1918.

In 1919, Ralph Virden married Miss Florence I. McCullers. They would have two children, Kathryn and Ralph, Jr. Kathryn died in 1930 at the age of ten years.

Ralph Burwell Virden with a Boeing Model 40 mail plane, circa late 1920s. As a U.S. Air Mail pilot, Virden is armed with a .45-caliber Colt M1911 semi-automatic pistol. (San Diego Air and Space Museum Archives)
Boeing Airplane Company President Clairmont L. Egvtedt and United Air Lines Captain Ralph B. Virden examine a scale model of the Boeing 247D airliner. (Boeing)

During the mid-1920s, Virden flew as a contract mail pilot. He held Airline Transport Pilot Certificate No. 628, and was employed by Gilmore Aviation and Pacific Air Transport. For thirteen years, Virden was a pilot for United Air Lines. He joined Lockheed Aircraft Company as a test pilot in 1939. He had flown more than 15,000 hours.

Virden lived at 4511 Ben Ave., North Hollywood, California, with his  family. Ralph, Jr., now 19 years of age, was also employed at Lockheed. (Following his father’s death, the younger Virden enlisted in the United States Navy.)

After the accident, Lockheed, the Air Corps and the National Advisory Committee on Aeronautics (NACA) undertook an extensive test program of the P-38.

The Lockheed YP-38 Lightning, 39-690, was sent to the NACA Research Center at Langley Field, Virginia. This photograph is dated 4 February 1942. (NASA)
The second Lockheed YP-38 Lightning, 39-690, was sent to the NACA Langley Research Center at Langley Field, Virginia. This photograph is dated 4 February 1942. (NASA)
Lockheed YP-38 39-690 in the NACA Full Scale Tunnel, December 1944. (NASA)
Lockheed YP-38 39-690 in the NACA Full Scale Tunnel, December 1944. (NASA)
Lockheed YP-38 Lightning 39-690, serial number 122-2203. (NASA)
Lockheed YP-38 Lightning 39-690, serial number 122-2203. (NASA)
Lockheed YP-38 #2 in the NACA full-scale wind tunnel at Langley, Virginia. (NASA)
Lockheed YP-38 Lightning, 39-690 (122-2203), in the NACA Langley Research Center’s full-scale wind tunnel at Langley Field, Virginia, December 1944. (NASA)
Lockheed YP-38 Lightning 39-690. (NASA)
Lockheed YP-38 Lightning 39-690. (NASA)
Lockheed YP-38 Lightning 39-690. (NASA)
Lockheed YP-38 Lightning 39-690. (NASA)
Lockheed YP-38 Lightning 39-690. (NASA)
Lockheed YP-38 Lightning 39-690. (NASA)
Lockheed YP-38 Lightning 39-690, 122-2203. (NASA)
Lockheed YP-38 Lightning 39-690, 122-2203. (NASA)

© 2018, Bryan R. Swopes

3 November 1950

Mont Blanc, western face. The summit was most recently measured at 4,810.06meters. 18 meters of snow and ice cover the actual rock peak, at 4,792 meters.
Mont Blanc, western face. The summit was most recently measured at 4,810.06 meters (15,781.04 feet). 18 meters (59 feet) of snow and ice cover the actual rock peak, at 4,792 meters.

3 November 1950: Air India Flight 245, a Lockheed L-749A Constellation, VT-CQP, Malabar Princess, was on a flight from Bombay, India, to London, England, with intermediate stops at Cairo, Egypt and Geneva, Switzerland. The aircraft was under the command of Captain Alan R. Saint, with co-pilot Vijay Yeshwant Korgaokar, three navigators and a radio operator.

Air India’s Lockheed L-749A Constellation, VT-CQP, Malabar Princess. (ETH Zurich)

At 9:43 a.m., Malabar Princess crashed into the Rochers de la Tournette (Tournette Spur) on the west side of Mont Blanc at an approximate elevation of 15,344 feet (4,677 meters). All 48 persons on board were killed.

Air India International was the national airline of India, having been formed from Tata Airlines. On 8 June 1948, Air India’s first scheduled flight departed Bombay for Cairo, Geneva and London. The airliner was Malabar Princess.

On 24 January 1966, Air India Flight 101, a Boeing 707-437, VT-DMN, named Kanchenjunga,¹ crashed at almost the same location on Mount Blanc. All 117 persons on board were killed.

The Lockheed L-749A Constellation was operated by a flight crew of four, with two to four flight attendants. It could carry up to 81 passengers. The airplane was 97 feet, 4 inches (29.667 meters) long with a wingspan of 123 feet (37.490 meters) and an overall height of 22 feet, 5 inches (6.833 meters). It had an empty weight of 56,590 pounds (25,669 kilograms) and maximum takeoff weight of 107,000 pounds (48,534 kilograms).

The L-749A was powered by four air-cooled, supercharged and fuel-injected 3,347.66-cubic-inch-displacement (54.858 liter) Wright Aeronautical Division Cyclone 18 (also known as the Duplex-Cyclone) 749C18BD1 two-row 18-cylinder radial engines with a compression ratio of 6.5:1. They had a Normal Power rating of 2,100 horsepower at 2,400 r.p.m., and Takeoff Power rating 2,500 horsepower at 2,800 r.p.m. (five minute limit). The engines drove three-bladed Curtiss-Electric propellers through a 0.4375:1 gear reduction. This engine featured “jet stacks” which converted the piston engines’ exhaust to usable jet thrust, adding about 15 miles per hour (24 kilometers per hour) to the airplane’s speed. The 749C18BD1 was  6 feet, 6.52 inches (1.994 meters) long, 4 feet, 7.62 inches (1.413 meters) in diameter, and weighed 2,915 pounds (1,322 kilograms).

The L-749 had a cruise speed of 345 miles per hour (555 kilometers per hour) and a range of 4,995 miles (8,039 kilometers). Its service ceiling was 24,100 feet (7,346 meters).

A sister ship of Malabar Princess, this is Air India's Lockheed L-749A Constellation VT-CQS. (Lockheed via R.A. Schofield. Photograph used with permission.)
A sister ship of Malabar Princess, this is Air India’s Lockheed L-749A Constellation VT-CQS. (Lockheed via R.A. Schofield. Photograph used with permission.)

The Air India Flight 245 crash was the basis for a novel, La neige en deuil (“The Snow in Mourning”), written by Henri Troyat (née Lev Aslanovic Tarassov), which in turn inspired the 1956 Edward Dymtryk motion picture, “The Mountain.” The film starred Spencer Tracy, Robert Wagner and Anna Kashfi.² Tracy was nominated by the British Academy of Film and Television Arts for an award for his performance.

The great American actor Spencer Tracy starred as a mountain guide in Edward Dmytryk's 1956 motion picture, "The Mountain." (Paramount)
The great American actor Spencer Tracy starred as Alpine mountain guide “Zachary Teller” in Edward Dmytryk’s 1956 motion picture, “The Mountain.” (Paramount)

¹ Kanchenjunga is the name of the world’s third highest mountain, an “eight thousander” located 125 kilometers (78 miles) east-southeast of Mount Everest in the Himalayas. Its summit is 8,598 meters (28,209 feet) above Sea Level. It is considered to be a sacred mountain. Climbers are not allowed there.

² Anna Kashfi (née Joan O’Callaghan) was the first Mrs. Marlon Brando.

© 2018, Bryan R. Swopes

10 October 1956: Lockheed L-1649 Starliner

—Los Angeles Times, Vol. LXXV, Thursday, 11 October 1956, Part 1, Page 3.

10 October 1956: At 4:15 p.m., after a 20-second ground run, the prototype L-1649 Starliner lifted off from Lockheed Air Terminal, Burbank, California. On the flight deck were company test pilots Herman Richard (“Fish”) Salmon and Roy Edwin Wimmer. The flight engineer was Glenn Fisher, and John Stockdale served as the flight test engineer.

  “The ground shook as the big Connie climbed gracefully away. Its wings glistened in the late-afternoon sunlight like long, slender knife blades. They measure 150 feet, or 27 feet more than on previous Super Constellations. Gross takeoff weight is 156,000 pounds. The plane is powered by four 3400 h.p. turbo-compound engines.”

Los Angeles Times, Vol. LXXV, Thursday, 11 October 1956, Part 1, Page 5, Column 5

After a 50-minute flight, the new airliner returned to Burbank. When asked, one of the pilots said, “It handles real smooth.”

The prototype Lockheed L-1649 Starliner, c/n 1001, registered N60968, was a major improvement over the previous model the L-1049 Super Constellation. Using the fuselage of the L-1049G variant, a new low-drag wing was used. The wing was about 16% thinner than the previous design, and had a span increased to 150 feet. By designing the main landing gear to retract into the inner engine nacelles rather than into openings in the lower surface of the wing, the wing could be built much stronger. The wing tips were squared.

The airliner’s fuel capacity, 9,600 gallons (36,340 liters), was sufficient for it to stay aloft for 24 hours. It was designed to carry 58 passengers 6,300 miles (10,139 kilometers) at 350 miles per hour (563 kilometers per hour).

The first production L-1649A, c/n 1002, was built for Trans World Airlines and registered N7301C. TWA called its Starliners “Jetstreams.”

The first production aircraft, Trans World Airlines’ Lockheed L-1649A Starliner, N7301C, c/n 1002. (NACA Ames Imaging Library System A83-0499-18)

Lockheed and TWA had considered using turboprop engines (this would have been designated L-1549), but reliability, poor fuel efficiency and cost resulted in continuing to use Wright’s reciprocating Duplex-Cyclone radials.

The L-1649A was powered by four air-cooled, supercharged and fuel-injected 3,347.662-cubic-inch-displacement (54.858 liter) Wright Aeronautical Division Turbo Compound 988TC18EA2 18-cylinder radial engines. The engine’s high-velocity exhaust gases drove three “blow down” turbines which were geared to the engine’s crankshaft. (Gear reduction is 6.52:1.). Energy that would otherwise be wasted added as much as 600 horsepower to each engine. The Turbo Compound used the same nose section, power section and rear section as the standard Cyclone 18CB. The 988TC18EA2 was rated at 2,800 horsepower at 2,600 r.p.m., and 3,400 horsepower at 2,900 r.p.m. for takeoff. It had a compression ratio of 6.7:1 and required 115/145-octane aviation gasoline. The Turbo Compound engine was 7 feet, 5.53 inches (2.274 meters) long, 4 feet, 8.59 inches (1.437 meters) in diameter, and weighed 3,745 pounds (1,699 kilograms). The engines drove three-bladed Hamilton Standard propellers with a diameter of 16 feet, 10 inches (5.131 meters) through a 0.355:1 gear reduction.

A Trans World Airlines Lockheed L-1649A Starliner, c/n 1016, N7314C, at Los Angeles International Airport, 1964. (Photograph courtesy of Jon Proctor)

44 production L-1649A Starliners were built by Lockheed in 1957 and 1958. The original L-049 prototype, NC25600, having previously modified as the prototype L-749 Constellation, L-1049 Super Constellation and PO-1W Warning Star, was also converted to the L-1649A configuration.

The prototype L-1649 was retained by Lockheed until withdrawn from service in 1971. Sold to M-K Aerospace Industries, in January 1973, it was re-registered as a L-1649A-98, N1102, and exported to Japan. It is reported to have been scrapped in December 1982.

The second Lockheed L-1649A Starliner, delivered to Trans World Airlines in September 1957. (Lockheed Martin)

© 2020, Bryan R. Swopes

9 October 1999

9 October 1999: At a Saturday air show at Edwards Air Force Base, California, NASA Research Pilot Rogers E. Smith and Flight Test Engineer Robert R. Meyer, Jr., flew Lockheed SR-71A-LO 61-7980, NASA 844, on what would be the very last flight of a Blackbird. Although it was scheduled to fly again for the Sunday air show, a serious fuel leak prevented that flight.

61-7980 (Lockheed serial number 2031) was the final SR-71A to be built.

NASA 844 was retired after the final flight and placed in flyable storage, but in 2002, it was placed on static display at the Dryden Flight Research Center,¹ Edwards Air Force Base, California. EC92-02273  

¹ In 2014, DFRC was renamed the NASA Neil A. Armstrong Flight Research Center (AFRC).

© 2017, Bryan R. Swopes