Tag Archives: Distinguished Flying Cross

12 February 1971

MEDEVAC FROM THE FOG – SS STEEL EXECUTIVE
By Sean M. Cross, CAPT, USCG (retired)

“Lewis had to make what he considered to be one of the most crucial decisions of his life. Peering at the fog below him, he remembers asking himself a question to plunge or not to plunge…”

TODAY IN COAST GUARD AVIATION HISTORY – 12 FEBRUARY 1971: an HH-3F assigned to Air Station San Diego, CA and crewed by LCDR Paul R. Lewis (AC), LT Joseph O. Fullmer (CP), ASM3 Larry E. Farmer (FM), AT3 Charles Desimone (AV) and HM3 Richard M. McCollough (AMS) launched in response to an injured or ill “seaman in need of an operation” ¹ from the 492-foot freighter STEEL EXECUTIVE, approximately 220 miles south of San Diego. The WWII-era Type C3-class cargo ship owned by Isthmian Lines, Inc. of New York was on an extended trip from Saigon, South Vietnam to New York City via the Panama Canal with stops in Astoria, OR and various east coast ports. They departed Saigon on 29 January 1971 and on 12 February were southbound for the Panama Canal.² After requesting assistance, the ship reversed course back toward San Diego to reduce transit distance for the helicopter. This is their story.

A United States Coast Guard Sikorsky HH-3F Pelican over Air Station San Diego. (U.S. Coast Guard)

Friday afternoon at around 4:00 PM, Rescue Coordination Center Long Beach launched the off-going Air Station San Diego HH-3F duty crew on a long range medical evacuation or MEDEVAC. The maintenance crew had to stop downtown vehicle traffic so that could taxi from the unit’s waterfront location across Harbor Drive to Lindberg Field in order to utilize the runway for a running takeoff – as the aircraft could not get airborne from a hover with a maximum fuel load.³ According to LCDR Lewis, taking off “out of San Diego, it was a clear afternoon,” ⁴ but the sun was lowering in the sky with official sunset at 5:31 PM.

Photo caption: profile view of generic Type C3-S-A2 cargo ship built by Ingalls – a development of the C3 basic design. During WWII these ships stood the test as cargo vessels and transports and after the war as cargo liners sold under Merchant Sales Act of 1946. These ships were widely used by U.S. and Foreign Steamship Companies into the 1970s.

After two hours of night overwater navigation and using a combination of radio direction finding, helicopter radar, and guidance from the STEEL EXECUTIVE, arrived in the vessel’s vicinity, but was unable to make visual contact through the dense fog which extended from the surface to about 700 feet above the water.

Flight mechanic Larry Farmer described the scene, “We flew over the estimated position at 1,500 feet and it was beautiful, you could see stars clear to either horizon, but glancing down – it looked like a huge layer of thick cotton blanketing the water below us.” ⁵

Chartlet Caption: Approximate route of flight to STEEL EXECUTIVE’s last known position “about 220 miles southeast of San Diego” en route to the Panama Canal.

With visibility less than 1/8 mile, the helicopter directed the vessel to turn on all available topside lighting and dropped two MK-58 marine location markers (floating cylinder that produces smoke and flames for 40-60 minutes) approximately two miles downwind to assist in executing an instrument approach to a hover above the water’s surface. ⁶

Lewis had to make a crucial decision. Peering at the fog below him, he remembers asking himself a question to plunge or not to plunge. ⁷ Lewis knew that the answer could spell a chance at life for the seriously ill merchant seaman. However, there was also his crew, his co-pilot, a radio operator, a corpsman and the aviation survivalman who operated the rescue hoist. Their lives and his own also were at stake. “I decided to lower the helicopter down to the water,” he said in an interview. “By then it was pitch dark. I flew away from where our radar told us the ship was and then went down to about 40 feet from the ocean.” ⁸

Diagram Caption: overhead view of the HH-3F PATCH (Precision Approach to a Coupled Hover) a procedure very similar to the “beep-to-hover”.

To transition from forward flight to a hover, executed a challenging “beep-to-hover” maneuver, which enabled them to safely approach the water and the ship. The “beep-to-hover” maneuver was developed by LCDR Frank Shelley, test pilot and program manager for HH-52A acquisition testing, to help pilots safely transition to an overwater hover at night and/or in instrument conditions. The HH-3F PATCH (precision approach to a coupled hover) eventually replaced the “beep-to-hover” in late-1971. ⁹ Interestingly, both procedures most closely mimic the ‘early’ MATCH (manual approach to a controlled hover) in the H-60 and H-65 series aircraft – the PATCH and CATCH in these aircraft utilize auto-pilot and trim functions to perform a ‘hands off’ coupled approach to the water.

This “beep-to-hover” maneuver can be disorienting in the clouds at night, particularly when low over the water with little room for error. Both pilots must continuously scan and interpret the flight instruments – this is critically important – while smoothly manipulating the controls to ensure they are hitting various airspeed and altitude windows to fly the correct profile.

At the completion of this very demanding approach, the helicopter crew found itself in nearly “zero-zero” weather but had executed the approach with such precision that the MK-58s were located. ¹⁰ Barely establishing visual reference with the ocean surface from a 40-foot hover, the helicopter crew was unable to see the vessel’s lights and therefore was hovering at night in a dense fog with minimal visual reference with the ocean surface.

“We made what amounted to an instrument approach to the water,” Lewis explained, “Hovering just over the waves we crawled toward the ship which was about two to three miles away.” ¹¹ At least that’s where a little black box on the instrument panel said the ship was. The aircrew inched forward using the helicopter doppler hover system, the radar, the RDF (radio direction finding, which provided a bearing to a radio signal from the ship). At about one mile out, the STEEL EXECUTIVE’s blip on the helicopter radar was lost in surface clutter – the mood was tense with the aircrew concerned about the combination of low visibility, closure rate, low altitude and vessel rigging obstacles. ¹² At an altitude of 40 feet in extremely limited visibility, the helicopter could literally stumble into the vessel, causing a collision that would doom everyone on board the aircraft and imperil the ship’s crew as well. Eventually, the ship’s surface search radar picked up the helicopter and guided it to her. ¹³ Farmer was on a gunner’s belt leaning out the cabin door and straining to find the ship’s glow. ¹⁴

Lewis praised ASM2 Larry Farmer for far exceeding the scope of duties he’d been trained for – hoisting the injured man off his ship and onto the hovering aircraft. “Farmer actually guided me to the ship.” Lewis said, “I had no visual references so I depended entirely on him. He became our aircraft’s eyes and brought us over the freighter.” ¹⁵

Pucker factor is a slang phrase used by military aviators to describe the level of stress and/or adrenaline response to danger or a crisis situation. The term refers to the tightening of the sphincter caused by extreme concern – on particularly challenging missions, the seat cushions might go missing altogether. The pucker factor had been high since the initial descent into the fog bank, however Farmer remarked that “finally gaining a visual with the ship eased the pucker factor and transformed the aircrew’s outlook from uncertainty of success to ‘we can do this’.” ¹⁶

Huge spotlights pierced the fog, but all Lewis and Farmer could see was the hoist аrеа. Even under ideal weather conditions, positioning a hovering helicopter over the crowded decks of a freighter is a delicate maneuver. “Doing it in pitch darkness while howling 25-mile an hour winds rock ship and aircraft alike is – in the words of the young crewmen who were there with Lewis – something else”. ¹⁷

Diagram Caption: HH-3F #1473’s approximate hoisting position with STEEL EXECUTIVE (represented with a generic Type C3 cargo ship plan of roughly the same arrangement).

The pilot and flight mechanic were still concerned with the helicopter’s low hoisting altitude as they surveyed the vessel obstacles – the ship’s towering rigging literally disappeared in the fog above. ¹⁸ Much of the obstacle clearance judgement and decision making fell on the flight mechanic’s shoulders as the pilot was unable to see the hoisting area behind him. The crew was convinced that a ‘basket with trail line’ was the right technique for the situation as it would allow the helicopter to hoist from a position offset 30-40 feet from the ship and facilitate Lewis’ use of the STEEL EXECUTIVE as a hover reference. A trail line is a 105-foot piece of polypropylene line (similar to a water ski rope) with a 300-pound weak-link at one end and a weight bag at the other. The weight bag end of the trail line is paid out below the helicopter and delivered to the persons in distress (usually vertically, but seasoned flight mechanics can literally ‘cast’ the weight bag to a spot). The weak link is then attached to the hoist hook and the helicopter backs away until the pilot can see the hoisting area. The persons in distress can then pull the basket to their location – creating a hypotenuse or diagonal – as opposed to a purely vertical delivery.

Farmer carefully conned the helicopter over the vessel providing voice commands to the pilot – delivering the trail line and, subsequently, the rescue basket to the stern of the STEEL EXECUTIVE. The semi-ambulatory patient was assisted into the basket by the ship’s crew and then hoisted aboard the helicopter. Lewis and Farmer were able to complete the hoist on the first attempt. Farmer appreciatively described Desimone’s efforts: “he spent most of his time working the radios, but he assisted me during the hoists. He was the extra set of hands getting the rescue basket into the cabin and then clearly directed the patient to the back of the cabin.” ¹⁹ Petty Officer McCollough secured the patient for the flight, administered antibiotics and maintained constant watch on the patient’s condition during the return flight. ²⁰

Often forgotten was the job done by Fullmer as Safety Pilot. He continuously scanned the system instruments to ensure the aircraft was operating normally and monitored the flight instruments to ensure obstacle clearance and safe altitude. He effectively conveyed critical information without interfering with Farmer’s conning commands. ²¹

After completing the hoist, it took a few minutes to secure the cabin – Farmer stowed the basket and secured the hoist hydraulics, then closed the cabin door and reported the cabin was secured and ready for forward flight. The pilots then executed a demanding night instrument take-off or ITO from a hover over the water. The ITO is similar to the “beep-to-hover” in terms of relying on aircraft instruments instead of visual cues, but its purpose is the opposite – to get you away from the water and into a forward flight profile at a safe airspeed and altitude. The maneuver was flawlessly executed and the aircrew soon found themselves above the fog bank in clear skies. The helicopter returned to San Diego to deliver the patient to medical authorities. The STEEL EXECUTIVE crewman subsequently recovered. ²²

LCDR Lewis earned the Distinguished Flying Cross for this mission, while ASM3 Farmer earned the Air Medal. The medals were presented by RADM James Williams, Commander, 11th Coast Guard District, in a ceremony at Air Station San Diego on 23 February 1972.

The Lewis and Farmer citations are below:

LCDR Lewis also earned the American Helicopter Society (now the Vertical Flight Society) Frederick L. Feinberg Award on 19 May 1972 at the Sheraton-Park Hotel, Washington, D. C – presented to the pilot or crew of a vertical flight aircraft who demonstrated outstanding skills or achievement during the preceding 18 months.

The award was presented by RADM William A. Jenkins, Chief, Office of Operations, Coast Guard Headquarters, who outlined the case as follows:

“Commander Lewis was selected for his sea rescue of an ill crewman from the merchant ship, S.S. Steel Executive, at night and under extremely hazardous weather conditions. Despite very dense fog, Lt. Cdr. Lewis took off and proceeded to the estimated position of the vessel some 220 miles south of San Diego, Calif. , and — by applying extremely skillful instrument approach procedures — was able to find the vessel with visibility reduced to an eighth of a mile and less at times, and by hovering 50 feet above the vessel, he rescued its seriously ill crewman and safely delivered the patient to medical authorities. The crewman subsequently recovered. This demonstration of courage, skill and airmanship has deservingly earned him the Frederick L. Feinberg Award.” ²³

LCDR Lewis provided the following acceptance speech:

“It’s indeed a deep personal honor for me to receive this award from the American Helicopter Society and from the Kaman organization. But in a sense I really feel that it’s unfortunate that this award should be given to an individual. Without attempting to feign false modesty, I sincerely feel that this award should be shared with many others; specifically the other 3 members of my crew, my service — the Coast Guard — and really, in a sense, you, the members of the American helicopter industry. I am sure there are people sitting here in the audience this evening that participated in the design, the development, and the production of the very fine Sikorsky HH-3 helicopter that was used in this rescue. In honoring the Coast Guard by my selection, I really feel that you honored a service that from the helicopters very beginning — we employed it to rescue thousands of people and saved millions of dollars of property. My rescue that is honored here this evening is really very typical of many other rescues that the Coast Guard has accomplished. And so — even though it’s my name alone that is on this award — I sincerely believe that the honor belongs to my entire crew for that evening that this rescue was accomplished and I feel also that it should be shared with the many other Coast Guard crews who accomplished many other rescues of equal ability or what may it be, but I feel I should share the honor with them.” ²⁴

Later that summer (1972), LCDR Lewis transferred to Air Station St. Petersburg, FL where he continued flying the HH-3F helicopter. Unfortunately, six months after the Feinberg Award presentation, on 16 December 1972, HH-3F assigned to Air Station St. Petersburg was lost off Sarasota along with the crew LCDR Paul R. Lewis, MAJ Marvin A. Cleveland, USAF (Exchange pilot), AD1 Edward J. Nemetz, AT3 Clinton A. Edwards, and four rescued crewmen from the 54-foot fishing vessel WANDA DENE William Peek, George Dayhoss, Herbert Hardy and Paul Manley. It was late on Saturday when the WANDA DENE, sent out a distress call. The stricken vessel was 35 miles southwest of Key West, taking on water and sinking in rough seas. HH-3F was launched with its crew of four for a long range rescue. The helicopter arrived overhead the WANDA DENE several hours later and successfully hoisted the four crewmen from the sinking vessel in challenging conditions. The then flew to Naval Air Station Key West to refuel. From there , now with eight people aboard, departed at about 7 PM for a return flight to St. Petersburg. Normal flight operations were reported with regular radio position reports until about 8:30 PM. Two days later a small portion of the helicopter was found in the Gulf of Mexico south of Fort Myers. Despite a massive search, very little of the aircraft and only one body, that of one of the fisherman, was ever recovered. The cause of the crash was never determined.

On 04 March 2011, a dedication ceremony was held at Air Station Clearwater, FL to posthumously name an annex building in honor of the Service and Sacrifice displayed by LCDR Paul R. Lewis. Members of the Lewis Family including daughter Kara Lewis, wife, Jackie Lewis, sister Abby Sauer, son Curt Lewis, daughter Megan Lewis, sister Joan Chaffee, and Abby’s husband, Gene Sauer were in attendance. Here is a section of the presentation that was made that day:

“LCDR Lewis was a tall, athletic Coast Guard Academy graduate who was regarded as the type of officer and pilot that others strive to become. He graduated in 1960, and went to serve his time aboard a Coast Guard cutter before attending flight school.

Prior to being stationed at Air Station St. Petersburg, LCDR Lewis served at the following air stations: Miami, Kodiak and San Diego. LCDR Lewis was known for his exceptional crew resource management and inclusion of his crew in all his flying duties. Among the pilots he was heralded as a flight instructor and examiner who knew the aircraft better than anyone.
LCDR Lewis is notably remembered for being the first Coast Guard pilot awarded the Frederick L. Feinberg Award for a rescue he performed offshore in San Diego. For that same rescue, he was awarded the Distinguished Flying Cross.”
While the building was named to honor Lewis, the air station believed Lewis would have wanted to honor the service and sacrifice of his crew as well. Hence, the auditorium within the building was named for Major Cleveland, the conference room for AD1 Nemetz, and the training room for AT3 Edwards.

¹ Staff writer, “Ex-Area Flier Lost In Crash”, Democrat and Chronicle, Rochester, NY. December 19, 1972, page 22. NOTE: The crewman, name and ailment unknown, may have been suffering from appendicitis and needed to get to a higher level of medical care within 6-12 hours. Various articles describe the issue as “severely ill crewman”; “ill crewman”; “seriously ill seaman”; “injured merchant seaman”; “seaman in need of an operation” and “injured crewman”, but I was unable to ascertain the exact ailment.

² Vietnam Era Voyages as reported in Lloyds Shipping Index (SS Steel Executive)

³ Larry Farmer (HH-3F Flight Mechanic) in email message to author on January 12, 2022 (and subsequent phone interview).

⁴ John Phillip Sousa, “Fog Thwarted Mission – Hero Recalls Perilous Rescue,” The San Diego Union, San Diego, CA, February 27, 1972, page B-3.

⁵ Ibid.

⁶ Air Station San Diego – “Awards Board Minutes” – Case -71, page 3.

⁷ Sousa newspaper article.

⁸ Ibid.

⁹ LCDR D. K. Shorey, “The PATCH: Precision Approach to Coupled Hover”, Flight Lines, Summer 1972, pages 2-3.

¹⁰ Ibid.

¹¹ Ibid.

¹² Farmer email.

¹³ Air Station San Diego.

¹⁴ Farmer email.

¹⁵ Ibid.

¹⁶ Ibid.

¹⁷ Ibid.

¹⁸ Ibid.

¹⁹ Ibid.

²⁰ Air Station San Diego.

²¹ Ibid.

²² “28th Forum, Trade Exhibit Registers 800 as 533 See Honors Night Awards Distributed” Vertiflite July/August 1972, pages 6-9.

²³ Ibid.
Ibid.
Ormie King, “Ormie King’s Legends of Auburn: Honoring a native son”, The Post Standard, Syracuse, NY. May 05, 2011 – available here: https://www.syracuse.com/neighbors/2011/05/ormie_kings_legends_of_auburn_honoring_a_native_son.html .

²⁴ Ibid.

_____________________________________________________________________________________________

Retired CAPT Sean M. Cross served 25 years in the Coast Guard as a helicopter pilot and aeronautical engineer. Flying both the MH-60T and MH-65D, he accumulated over 4,000 flight hours while assigned to Air Stations Clearwater, FL; Cape Cod, MA; San Diego, CA; Elizabeth City, NC and Traverse City, MI – which he commanded.

“LCDR Paul R. Lewis is first Coast Guard Aviator name etched on the Feinberg Award and the story of HOW it got there should be preserved for posterity.”

© 2022, Sean M. Cross

 

5 February 1962

Lieutenant Robert W. Crafton, U.S. Navy, and Captain Louis K. Keck, U.S. Marine Corps, with the record-setting Sikorsky HSS-2 Sea King. (FAI)
Lieutenant Robert W. Crafton, U.S. Navy, and Captain Louis K. Keck, U.S. Marine Corps, with the record-setting Sikorsky HSS-2 Sea King. (FAI)

5 February 1962: A Sikorsky HSS-2 Sea King (later redesignated SH-3A) became the world’s fastest helicopter by establishing a Fédération Aéronautique Internationale (FAI) world speed record for helicopters of 339 kilometers per hour (210.645 miles per hour) over a 19 kilometer (11.8 mile) course between Milford and New Haven, Connecticut.¹ The pilots were Lieutenant Robert Wiley Crafton, United States Navy and Captain Louis K. Keck, United States Marine Corps. Both pilots were awarded the Distinguished Flying Cross and the American Helicopter Society’s Frederick L. Feinberg Award.

Having served the United States Navy for 45 years, the Sea King is still in service world-wide, most notably as the VH-3D “Marine One” presidential helicopter.

Sikorsky HSS-2 Sea King, Bu. No. 147xxx, modified for the speed record attempt. (FAI)
Sikorsky HSS-2 Sea King, Bu. No. 147xxx, modified for the speed record attempt. (FAI)

The Sikorsky HSS-2 Sea King was the first of the S-61 series of military and civil helicopters. It is a large twin-engine helicopter with a single main rotor/tail rotor configuration. The fuselage is designed to allow landing on water. The XHSS-2 made its first flight 11 March 1959. The helicopter was originally used as an anti-submarine helicopter.

The HSS-2 is 72 feet, 6 inches (22.098 meters) long and 16 feet, 10 inches (5.131 meters) high with all rotors turning. The helicopter’s width, across the sponsons, is 16 feet. The main rotors and tail can be folded for more compact storage aboard aircraft carriers, shortening the aircraft to 46 feet, 6 inches (14.173 meters). The empty weight of the HSS-2 is 10,814 pounds (4,905 kilograms). The overload gross weight is 19,000 pounds (8,618 kilograms).

The main rotor has five blades and a diameter of 62 feet, 0 inches (18.898 meters). Each blade has a chord of 1 foot, 6¼ inches (0.464 meters). The rotor blade airfoil was the NACA 0012, which was common for helicopters of that time. The total blade area is 222.5 square feet (20.671 square meters), and the disc area is 3,019 square feet (280.474 square meters). The tail rotor also has five blades and a diameter of 10 feet, 4 inches (3.150 meters). They each have a chord of 7–11/32 inches (0.187 meters). At 100% NR, the main rotor turns 203 r.p.m. and the tail rotor, 1,244 r.p.m.

The HSS-2 was powered by two General Electric T58-GE-6 turboshaft engines, which had a Normal Power rating of 900 horsepower, and Military Power rating of 1,050 horsepower; both ratings at 19,555 r.p.m. at Sea Level. The main transmission was rated for 2,000 horsepower, maximum. (Later models were built with more powerful T58-GE-8 engines. Early aircraft were retrofitted.)

The HSS-2 has a cruise speed of 125 knots (144 miles per hour/232 kilometers per hour) at Sea Level, and a maximum speed of 133 knots (153 miles per hour/246 kilometers per hour) at Sea Level. The service ceiling is 12,100 feet (3,688 meters). The hover ceiling at normal gross weight is 5,200 feet (1,585 meters), out of ground effect (HOGE), and 7,250 feet (2,210 meters), in ground effect (HIGE). The HSS-2 had a combat endurance of 4 hours and a maximum range of 500 nautical miles (575 statute miles/926 kilometers).

The Sea King was primarily an anti-submarine aircraft. It could be armed with up to four MK 43 or MK 44 torpedoes and one MK 101 nuclear-armed depth bomb. Other weapons loads included four MK 14 depth charges and four MK 54 air depth bombs.

In 1962, the HSS-2 was redesignated SH-3A Sea King. Many early production aircraft have remained in service and have been upgraded through SH-3D, SH-3G, etc. In addition to the original ASW role, the Sea Kings have been widely used for Combat Search and Rescue operations. Marine One, the call sign for the helicopters assigned to the President of the United States, are VH-3D Sea Kings. Sikorsky produced the last S-61 helicopter in 1980, having built 794. Production has been licensed to manufacturers in England, Italy, Canada and Japan. They have produced an additional 679 Sea Kings.

Captain Louis K. Keck, USMC (left), and Lieutenant Robert W. Crafton, U.S. Navy, in the cockpit of their Sikorsky HSS-2 Sea King. (U.S. Navy NH69960)

¹ FAI Record File Number 13121

© 2019, Bryan R. Swopes

Charles Augustus Lindbergh (4 February 1902–26 August 1974)

Charles Augustus Lindbergh, Aviator.

4 February 1902: Charles Augustus Lindbergh, Brigadier General, United States Air Force, Medal of Honor, was born at Detroit, Michigan. He was the son of Swedish immigrant Charles August Lindbergh (born Karl Månsson), an attorney, and Evangeline Lodge Land Lindbergh, a high school chemistry teacher. Lindbergh attended Redondo Beach High School, Redondo Beach, California, 1917–1918.

Lindbergh, age 11, with his dog, Dingo. (The Denver Post)

In 1920–1922 Lindbergh was enrolled as an engineering student at the University of Wisconsin–Madison. He shared an apartment with his mother who was teaching at the nearby Emerson School. A friend from the university showed Lindbergh a brochure from a flight school. Mrs. Lindbergh is reported to have told the friend, “If Charles goes to flying school, I will hold you responsible.” Soon after, Lindbergh left the university and entered a flying school in Nebraska. In 1927, the University of Wisconsin bestowed the honorary degree of Doctor of Laws (LL.D.) on him.

Certainly one of the world’s best known pilots, Lindbergh began flight training at the age of 20. He was an Aviation Cadet, 19 March 1924–16 March 1925, and trained at the United States Army flight schools at Brooks and Kelly Fields, in Texas. He graduated at the top of his class and was commissioned as a Second Lieutenant in the Officers Reserve Corps, U.S. Air Service, with date of rank of 14 March 1925.

Second Lieutenant Charles A. Lindbergh, Air Service, United States Army, circa 1925. (San Diego Air & Space Museum Archives)

Lindbergh was promoted to First Lieutenant, Air Corps, 7 December 1925, and to Captain, 13 July 1926. He flew as an Air Mail pilot and gained valuable flight experience.

Lindbergh was the chief pilot of Robertson Aircraft Corporation at Lambert Field, St. Louis, Missouri. The company was contracted to fly the mail to Chicago, with intermediate stops at Springfield and Peoria, Illinois, using several modified de Havilland DH-4 biplanes. On two occasions, 16 September and 3 November 1926, Lindbergh had to bail out of his mail plane at night.

Air Mail Pilot Charles A. Lindbergh, circa 1927. (NASM)

He resigned from Robertson Aircraft and formed a group to finance and build the Spirit of St. Louis.

On 20 May 1927, Lindbergh departed New York in his custom-built Ryan NYP monoplane, Spirit of St. Louis, and 33 hours, 30 minutes later, he landed at Paris, France, becoming the first person to fly solo across the Atlantic Ocean. For this accomplishment he won the Orteig Prize of $25,000 (about $400,600 in 2022 dollars).

Charles A. Lindbergh with the Ryan NYP Spirit of St. Louis at Roosevelt Field, New York, 20 May 1927.
Charles A. Lindbergh with the Ryan NYP Spirit of St. Louis at Roosevelt Field, New York, 20 May 1927. (Hulton Archive/Getty Images)

When he returned to the United States, Lindbergh was presented the Distinguished Flying Cross by President Coolidge. On 14 December 1927, by Act of Congress, Lindbergh was awarded the Medal of Honor:

“For displaying heroic courage and skill as a navigator, at the risk of his life, by his nonstop flight in his airplane, the Spirit of St. Louis, from New York City to Paris, France, 20–21 May 1927, by which Capt. Lindbergh not only achieved the greatest individual triumph of any American citizen but demonstrated that travel across the ocean by aircraft was possible.”

Charles Augustus Lindbergh’s Medal of Honor at the Missouri History Museum, St. Louis, Missouri. (Robert Lawton)

Captain Lindbergh was promoted to the rank of Colonel, Officers Reserve Corps, U.S. Army Air Corps, 18 July 1927. In the 1930s, he had various assignments, including evaluating new aircraft at Wright Field.

Two years after his transatlantic flight, Lindbergh married Miss Anne Spencer Morrow, daughter of the United States Ambassador to Mexico, 27 May 1929, at Englewood, New Jersey. They would have six children.

Charles and Anne Morrow Lindbergh with their Lockheed Model 8 Sirius, NR211, at Grand Central Airport, Glendale, California, shortly before their departure for New York, 20 April 1930. (HistoryNet)

In 1930–1931, the Lindberghs flew a Lockheed Model 8 Sirius named Tingmissartoq from the United States to China, traveling through Canada, Alaska, Siberia, and Japan.  Anne Morrow Lindbergh wrote about the journey in North to the Orient (Harcourt, Brace and Co., 1935). The Sirius was equipped with floats for a part of the trip. In 1933 they flew the Model 8 to explore air routes in Europe, Africa and South America. NR211 is in the collection of the Smithsonian Institution, National Air and Space Museum.

Charles Lindbergh testifies at “The Trial of the Century.” The defendant, Bruno Richard Hauptmann, is at the lower right with his back toward the camera. (Library of Congress/New York World-Telegram & Sun Collection 3c09416)

Their first son, Charles Augustus Lindbergh, Jr., was kidnapped from the family’s home, 1 March 1932. A ransom of $50,000 was paid (equivalent to $1,015,526 today), however the boy’s body was found 12 March. At “The Trial of the Century,” Bruno Richard Hauptman was convicted of the crime. He was later executed.

Left to Right: Albert Kisk, Harry Guggenheim, Dr. Goddard, Charles A. Lindbergh, Nils Lindquist and Charles Mansur. (U.S. Air Force photograph.)

During the mid-1930s, Lindbergh was an active supporter of the rocketry experiments of Dr. Robert H. Goddard. He had other interests a well. With Nobel Prize winner Dr. Alexis Carrel, he invented the Perfusion Pump to allow oxygenated blood to be supplied to human organs. This eventually led to the “heart-lung machine” that made “open heart” surgery possible.

“Charles Lindbergh and Alexis Carrel with the glass heart,” Samuel Johnsonson Woolf, 1938. (National Portrait Gallery, Smithsonian Institution)
Colonel Lindbergh in the cockpit of a Curtiss Wright P-36A Hawk, 38-102, circa 1938. This airplane was destroyed during the attack on Pearl Harbor, Hawaii, 7 December 1941. (Niagara Aerospace Museum)

During World War II, Lindbergh served as a civilian adviser and flew the Chance Vought F4U-1 Corsair in combat missions with Marine fighter squadrons VMF-216 and VMF-222. He also flew the Lockheed P-38 Lightning with the Army Air Force 433rd Fighter Squadron, 475th Fighter Group.

Charles A. Lindbergh with a Chance Vought F4U-1 Corsair at Emirau Island in the Bismarck Archipelago, May 1944. (U.S. Navy)
Charles A. Lindbergh in the cockpit of a Chance Vought F4U-1 Corsair, Green Islands, Solomon Sea, May 1944. (NASM)
Another photograph showing Charles A. Lindbergh in the cockpit of a Chance Vought F4U-1 Corsair of VF-24, Roi-Namur, Kwajalein Atoll, Marshall Islands, circa 1944.

On 28 July 1944, Lindbergh was flying “Blue 3” with a flight of P-38s from the 433rd along the north coast of New Guinea. Over Elpaputih Bay, Blue Flight encountered enemy aircraft. Lindbergh shot down one of them. Various sources identify the aircraft as a Mitsubishi Ki-51 Type 99 “Sonia” flown by Captain Saburo Shimada.

He is starting down in a wing over—out of control. The nose goes down. The plane turns slightly as it picks up speed—down—down—down toward the sea. A fountain of spray—white foam on the water—waves circling outward as from a stone tossed in a pool—the waves merge into those of the sea—the foam disappears—the surface is at it was before.

The Wartime Journals of Charles A. Lindbergh, by Charles Augustus Lindbergh, Harcourt Brace Jovanovoch, Inc., New York, 1970, at page 889

 

Charles A. Lindbergh with a Lockheed P-38J Lightning, circa July 1944. (U.S. Air Force)

In 1954, President Dwight D. Eisenhower reactivated his Army Air Corps commission and appointed him Brigadier General, United States Air Force.

Charles A. Lindbergh was the author of We (G.P. Putnam’s Sons, New York, 1927), Of Flight and Life, (Charles Scribner’s Sons, New York, 1948), and The Spirit of St. Louis (Charles Scribner’s Sons, New York, 1953). This third book won the Pulitzer Prize for biography in 1954, and is very highly recommended by This Day in Aviation. The book was made into a motion picture in 1957, directed by Billy Wilder and starring Jimmy Stewart as Lindbergh. (This film was a major influence on the author of TDiA.)

In 1972, while accompanying a television crew investigating a “lost tribe” in the Philippine Islands, Lindbergh and the group were stranded when their helicopter broke down. They were rescued by the 31st Aerospace rescue and Recovery Squadron, based at Clark Field.

Charles Lindbergh died on Maui, Hawaii, 26 August 1974. He was buried at the Palapala Ho’omau Church Cemetery, Kipahulu, Maui.

© 2022, Bryan R. Swopes

29 December 1944

Flight Lieutenant Richard Joseph Audet, Royal Canadian Air Force, with his Supermarine Spitfire LF Mk.IX, MK950, assigned to No. 411 Squadron, Royal Canadian Air Force.

29 December 1944: Flying Officer Richard Joseph Audet, Royal Canadian Air Force, was a section leader of No. 411 Squadron, an RCAF squadron under the control of the Second Tactical Air Force, Royal Air Force. The squadron was based at an advanced airfield in The Netherlands.

In the early afternoon, Audet’s Yellow Section engaged a flight of twelve Luftwaffe fighters, four Messerchmitt Bf 109s and eight Focke-Wulf Fw 190s, near Rheine, in northwestern Germany.

Flying a Supermarine Spitfire LF Mk.IX .5, RR201, Flying Officer Audet led his section into the attack. He later reported:

I was leading Yellow section of 411 Squadron in the Rheine/Osnabruck area when Control reported Huns at Rheine and the squadron turned in that direction. An Me 262 was sighted and just at that time I spotted 12 e/a on our starboard side at 2 o’clock. These turned out to be a mixture of approximately 4 Me 109’s and 8 FW 190’s.

1) I attacked an Me 109 which was the last a/c in the formation of about twelve all flying line astern. At approximately 200 yds and 30° to starboard at 10,000 feet I opened fire and saw strikes all over the fuselage and wing roots. The 109 burst into flames on the starboard side of the fuselage only, and trailed intense black smoke. I then broke off my attack.

2) After the first attack I went around in a defensive circle at about 8500 feet until I spotted an FW 190 which I immediately attacked from 250 yards down to 100 yards and from 30° to line astern. I saw strikes over cockpit and to the rear of the fuselage. It burst into flames from the engine back, and as I passed very close over top of it I saw the pilot slumped over in his cockpit, which was also in flames.

3) My third attack followed immediately on the 2nd. I followed what I believed was an Me 109 in a slight dive. He then climbed sharply and his coupe top flew off at about 3 to 4,000 feet. I then gave a very short burst from about 300 yards and line astern and his aircraft whipped downwards in a dive. The pilot attempted or did bale out. I saw a black object on the edge of the cockpit but his ‘chute ripped to shreds. I then took cine shots of his a/c going to the ground and bits of parachute floating around. I saw this aircraft hit and smash into many flaming pieces on the ground. I do not remember any strikes on this aircraft. The Browning button only may have been pressed.

4) I spotted a FW 190 being pursued at about 5,000′ by a Spitfire which was in turn pursued by an FW 190. I called this Yellow section pilot to break and attacked the 190 up his rear. The fight went downwards in a steep dive. When I was about 250 yards and line astern of this 190 I opened fire. There were many strikes on the length of the fuselage and it immediately burst into flames. I saw this FW 190 go straight into the ground and burn.

5) Several minutes later while attempting to form my section up again I spotted an FW 190 from 4000 feet. He was at about 2000 feet. I dived down on him and he turned in to me from the right. Then he flipped around in a left hand turn and attempted a head-on attack. I slowed down to wait for the 190 to flypast in range. At about 200 yds and 20° I gave a very short burst, but couldn’t see any strikes. This a/c flicked violently, and continued to do so until he crashed into the ground. The remainder of my section saw this encounter and Yellow 4 (F/O McCracken) saw it crash in flames.

—Post Mission Report of Flying Officer R. J. Audet, 29 December 1944

This air battle had been Flying Officer Audet’s first engagement with enemy aircraft. It was over within a matter of minutes. For his actions of 29 December 1944, Richard Audet was awarded the Distinguished Flying Cross.

Air Ministry, 16th February, 1945.

The KING has been graciously pleased to approve the following awards in recognition of gallantry and devotion to duty in the execution of air operations:—

Distinguished Flying Cross.

Flying Officer Richard Joseph Audet (Can/J.20136), R.C.A.F., 411 (R.C.A.F.) Sqn.

This officer has proved himself to be a highly skilled and courageous fighter. In December, 1944, the squadron was involved in an engagement against 12 enemy fighters in the Rheine/Osnabrück area. In a most spirited action, Flying Officer Audet achieved outstanding success by destroying 5 enemy aircraft. This feat is a splendid tribute to his brilliant shooting, great gallantry and tenacity.

Flight Lieutenant Richard Joseph Audet in the cockpit of a Supermarine Spitfire. (RCAF)

Richard Joseph Audet was born 13 March 1922 at Lethbridge, Alberta, Canada. He was the sixth child of Paul Audet, a rancher, and Ediwisca Marcoux Audet. “Dickie” Audet rode a horse to school at the age of ten years, traveling about 18 miles (29 kilometers) every morning.

Audet studied at Garbutt Business College in Lethbridge, and worked as a stenographer and bookkeeper at RCAF Air Station High River.

Dick Audet enlisted in the Royal Canadian Air Force at Calgary, Alberta, 28 August 1941. He was trained as a fighter pilot and was commissioned as a Pilot Officer, 24 October 1942. His pilot’s wings were presented to him by The Right Honourable William Lyon MacKenzie King, tenth Prime Minister of the Dominion of Canada.

R.C.A.F. Form R. 100, enlistment document of Richard Joseph Audet. (Royal Canadian Air Force)

Pilot Officer Audet was sent to England, crossing the North Atlantic aboard ship and arriving 6 December 1942. He was assigned to the No. 6 Elementary Flying School at RAF Little Rissington, Gloucestershire, and then No. 17 Advanced Flying Unit at RAF Calvely, Nantwich, Cheshire. He was promoted to Flying Officer 23 April 1943, and transferred to No. 53 Operational Training Unit at RAF Heston, west of London, where he transitioned to the Supermarine Spitfire fighter.

Flying Officer Richard J. Audet married Miss Iris Christina Gibbons of Pinner, a village in the London Borough of Harrow, at Northhampton, Northamptonshire, England, 9 July 1944.

Audet joined No. 411 Squadron, Royal Canadian Air Force, 14 September 1944. He was promoted to the rank of Flight Lieutenant, 23 October 1944.

During January 1945, Flight Lieutenant Audet was credited with destroying another 6.5 enemy aircraft: 4.5 Focke-Wulf FW-190s (one shared) and two Messerschmitt Me 262 jet fighters (one on the ground), and a third Me 262, damaged.

Distinguished Flying Cross and Bar

On 3 March 1945, Flight Lieutenant Audet was strafing railway trains near Coesfeld, Coesfelder Landkreis, Nordrhein-Westfalen, Germany, when his Spitfire LF Mk.IXE, MK950, was shot down. The Spitfire was seen to crash in flames and explode. Audet was listed as missing in action, and was presumed to have been killed. His remains were not recovered.

On 9 March 1945, Flight Lieutenant Richard Joseph Audet was posthumously awarded a Bar to his Distinguished Flying Cross (a second award).

There is no grave for Dick Audet. His name appears with those of 20,287 others on the Runnymede Memorial, Surrey, England, and among the nearly 400 on the Lethbridge Cenotaph at Lethbridge, Alberta. Audet Lake, north of Fort McMurray, Alberta, and Rue Richard Joseph Audet in Saugenay, Quebec, were named in his honor.

A Supermarine Spitfire LF Mk.IX .5 of No. 412 Squadron, RCAF, taxiing at an advanced landing field, Volkel, Holland, 27 October 1944. This is the same type Spitfire as flown by Dick Audet. Note the position of the .50-caliber machine guns, just inboard of the 20 mm cannon. Photograph by Flight Lieutenant T. Lea, RAF. © IWM (CL 1451)

The aircraft flown by Dick Audet on 29 December 1944, was a Supermarine Spitfire LF Mk.IX .5 (redesignated LF Mk.IXe in 1945), Royal Air Force serial number RR201. The identification letters on the fuselage were DB-G. It was built at built at the Castle Bromwich Aircraft Factory, at Warwickshire, West Midlands, in late summer or early fall 1944.

The Supermarine Spitfire was a single-place, single-engine low-wing monoplane of all-metal construction with retractable landing gear. The fighter had been designed by Reginald Joseph Mitchell CBE. The prototype first flew 5 March 1936.

The Spitfire LF Mk.IXe was optimized for low-altitude operations. The Spitfire F Mk.Vb was 29 feet, 11 inches (9.119 meters) long with a wingspan of 36 feet, 10 inches (11.227 meters) and overall height of 11 feet, 5 inches (3.480 meters). The exact dimensions of the LF Mk.IXe are not known but are presumably similar. Some Mk.IXe fighters had “clipped” wings, while others did not.

The LF Mk.IXe had an empty weight of 5,749 pounds (2,608 kilograms) and gross weight of 7,450 pounds (3,379 kilograms).

The Spitfire LF Mk.IXe was powered a liquid-cooled, supercharged, 1,648.959-cubic-inch-displacement (27.022 liters) Rolls-Royce Merlin 66 single overhead camshaft (SOHC) 60° V-12 engine with a compression ratio of 6.00:1. It was equipped with a two-speed, two-stage supercharger. The Merlin 66 was rated at 1,315 horsepower at 3,000 r.p.m. and 12 pounds per square inch boost (0.83 Bar), for Take Off; 1,705 horsepower at 3,000 r.p.m. at 5,750 feet (1,753 meters) and 1,580 horsepower at 3,000 r.p.m. at 16,000 feet (4,877 meters), with 18 pounds boost (1.24 Bar). These power ratings were obtained with 130-octane aviation gasoline. When 150-octane gasoline became available, the Merlin 66 was cleared to use 25 pounds of boost (1.72 Bar). The Merlin 66 had a propeller gear reduction ratio of 0.477:1 and drove a four-bladed Rotol Hydulignum (compressed laminated wood) propeller with a diameter of 10 feet, 9 inches (3.277 meters). The engine weighed 1,645 pounds (746 kilograms).

The Spitfire LF Mk.IXe had  cruise speed of 220 miles per hour (354 kilometers per hour) at 20,000 feet (6,096 meters); a maximum speed of 384 miles per hour (618 kilometers per hour) at 10,500 feet (3,200 meters), and 404 miles per hour (650 kilometers per hour) at 21,000 feet (6,401 meters). Diving speed was restricted to 450 miles per hour (724 kilometers per hour) below 20,000 feet (6,096 meters). The airplane’s service ceiling was 42,500 feet (12,954 meters).

The Spitfire LF Mk.IXe was armed with two 20-milimeter Hispano Mk.II autocannon, with 135 rounds of ammunition per gun, and two Browning AN-M2 .50-caliber machine guns, with 260 rounds per gun. The .50-caliber machine guns were mounted in the wings, just inboard of the 20 mm cannon.

This photograph of a Supermarine Spitfire LF Mk.IXe shows the position of the .50-caliber machine guns, inboard of the 20 mm cannon.

© 2018, Bryan R. Swopes

15 December 1959

Major Joseph W. Rogers, U.S. Air Force, in the cockpit of Convair F-106A Delta Dart 56-0467, at Edwards AFB, 15 December 1956. (U.S. Air Force)
Major Joseph W. Rogers, U.S. Air Force, in the cockpit of Convair F-106A Delta Dart 56-0467, at Edwards AFB, 15 December 1959. (U.S. Air Force)

15 December 1959: At Edwards Air Force Base, California, Major Joseph William Rogers, United States Air Force, flew a Convair F-106A Delta Dart all-weather interceptor, serial number 56-0467, to a new Fédération Aéronautique Internationale (FAI) World Record for Speed over a 15 Kilometer-to-25 Kilometer Straight Course, breaking the record set two years earlier by Major Adrian E. Drew with a modified McDonnell F-101A Voodoo.¹

At an altitude of 40,000 feet (12,192 meters), Rogers made two passes over the straight 11 mile (17.7 kilometers) course, once in each direction, for an average speed of 2,455.736 kilometers per hour (1,525.924 miles per hour)—Mach 2.31. For his accomplishment, he was awarded the Distinguished Flying Cross, the FAI’s Henry De La Vaulx Medal, and the Thompson Trophy.

Convair F-106A Delta dart 56-0467, FAI World Speed Record holder, parked on Rogers Dry lake at Edwards AFB. (U.S. Air Force)
Convair F-106A Delta Dart 56-0467, FAI World Speed Record holder, parked on Rogers Dry Lake at Edwards AFB. Note the jettisonable external fuel tanks. (U.S. Air Force)
A copy of Joseph W. Rogers Diplôme de Record from the FAI. NOTE: The signature of LE PRESIDENT DE LA F.A.I. at the lower right of the document. (F-106DeltaDart.com)
A copy of Joseph W. Rogers’ Diplôme de Record from the FAI. NOTE: The signature of LE PRÉSIDENT DE LA F.A.I. at the lower right of the document. (f-106deltadart.com)
The Thompson Trophy
The Thompson Trophy

Major Rogers was the Air Force F-106 project officer assigned to Convair. He first attempted the record with another F-106A, 56-0459, but when that Delta Dart developed uncontrollable compressor stalls, 56-0467 was substituted. (This has led to confusion over which aircraft actually set the record, but in an interview, Colonel Rogers confirmed that it was 467.)

Joseph William Rogers was born at Chillicothe, Ohio, 28 May 1924. He grew up on a farm, and attended West High School, graduating in 1942. He enlisted in the U.S. Army Air Corps in 1943 and trained as a pilot. From 1944 he was assigned as a flight instructor in California. Rogers remained in the Air Force after World War II.

During the Korean War, Joe Rogers got the nickname “Whistlin’ Joe” when he put whistles on the wings of his North American Aviation F-51D Mustang in an effort to frighten enemy troops. 1st Lieutenant Rogers was awarded the Silver Star for his actions of 8 October 1950, in close support of a British infantry unit, which was surrounded on a hilltop by the enemy.

Though not officially credited, it is widely accepted that on 8 November 1950, with his Mustang Buckeye Blitz VI, he shot down an enemy Mikoyan-Gurevich MiG-15 jet fighter. An aerial victory of a piston-engine fighter over a jet fighter was a very rare occurrence. Rogers was one of a group of “The American Fighting Man” named Man of the Year by TIME Magazine. He flew 170 combat missions in the F-51 and another 30 in the Lockheed F-80 Shooting Star.

Captain Joseph W. Rogers, U.S. Air Force, in teh cocpt of BUCKEY BLITZ VI, Korea, 1950. (U.S. Air Force)
Captain Joseph W. Rogers in the cockpit of his North American F-51D Mustang, Buckeye Blitz VI, assigned to the 36th Fighter Bomber Squadron, 8th Fighter Bomber Group, Korea, 1950. Note the red dive bombing stripes on the upper surface of the Mustang’s left wing. (Photograph by Lieutenant Colonel William J. O’Donnell, commanding officer, 36th FBS, via ww2color.com)

Rogers was a 1954 graduate of the Air Force Test Pilot School and worked as a test pilot on the North American Aviation F-86D Sabre radar-equipped interceptor, and then the Convair F-102 Delta Dagger and F-106 Delta Dart.

From 1960 to 1964 Rogers commanded the 317th Fighter Interceptor Squadron at Elmendorf Air Force Base, Alaska, which was, at that time, the largest squadron in the United States Air Force. In 1963, he flew a F-102 in the annual William Tell competition at Tyndall Air Force Base, Florida, which he won, and was named the Air Force’s “Top Gun.”

Colonel Joseph W. Rogers with a Lockheed SR-71A. (U.S. Air Force)

Next, Rogers he commanded the Lockheed SR-71A and F-12A Test Force at Edwards Air Force Base. He is one of the few pilots to have ejected from an SR-71A, when 61-7953 went out of control, 18 December 1969. Both he and Radar Intercept Officer Lieutenant Colonel Gary Heidelbaugh safely escaped the doomed Blackbird.

Colonel Rogers was Vice Commander of the 3d Fighter Wing, flying the McDonnell F-4 Phantom II during the Vietnam War. After serving as Assistant Deputy Commander of the 7th and 13th Air Forces, he was appointed Chief of Staff for Operations at the Aerospace Defense Command Headquarters, Peterson Air Force Base, Colorado. Rogers retired from the Air Force in 1975 after 32 years of service.

Joe Rogers worked for Northrop Aerospace for the next 13 years, marketing the company’s F-5 and F-20 fighters.

During his service in World War II, the Korean War and the Vietnam War, Colonel Rogers was awarded the Silver Star, the Legion of Merit with two Oak Leaf Clusters, Distinguished Flying Cross with two Oak Leaf Clusters, and Air Medal with thirteen Oak Leaf Clusters.

Joe Rogers was married to the former Charis Tate. They had three children. Mrs. Rogers passed away in 2003.

Colonel Joseph W. Rogers died at Healdsburg, California, 6 August 2005, at the age of 81 years. He is buried at Arlington National Cemetery, alongside his wife.

Convair F-106A Delta Dart 56-0467 after setting World Speed Record. (U.S. Air Force)
Convair F-106A Delta Dart 56-0467 after setting World Speed Record. Note the missing paint on vertical fin as a result of the high speed flight. (U.S. Air Force)

The Convair F-106A Delta Dart was the primary all-weather interceptor of the United States Air Force from 1959 to 1988, when it was withdrawn from service with the Air National Guard. It was a single-seat, single engine delta-winged aircraft capable of speeds above Mach 2. The airplane was a development of the earlier F-102A Delta Dagger, and was initially designated F-102B. However, so many changes were made that it is considered to be a new aircraft.

The F-106A is 70 feet, 8¾ inches (21.558 meters) long with a wingspan of 38 feet, 4 inches (11.684 meters). The total area of the delta wing is 697.83 square feet (64.83 square meters). The angle of incidence was 0° and there was no dihedral. The leading edges were swept aft 60°. The top of the vertical fin was 20 feet, 3¼ inches (6.179 meters) high. The Delta Dart weighs 23,646 pounds (10,726 kilograms) empty, and has a maximum takeoff weight (MTOW) of 38,729 pounds (17,567 kilograms).

The F-106 was powered by a Pratt & Whitney J75-P-17 afterburning turbojet engine. The J75-P-17 was a two-spool axial-flow turbojet engine with afterburner. It used a 15-stage compressor section (8 high- and 7 low-pressure stages) and a 3-stage turbine section (1 high- and 2-low pressure stages. The J75-P-17 had a maximum continuous power rating of 14,100 pounds of thrust (62.72 kilonewtons), and military power rating of 16,100 pounds (71.62 kilonewtons) (30-minute limit). It produced a maximum of 24,500 pounds (108.98 kilonewtons) with afterburner (5-minute limit). The engine was 3 feet, 8.25 inches (1.124 meters) in diameter, 19 feet, 9.6 inches long (6.035 meters), and weighed 5,875 pounds (2,665 kilograms)

The interceptor has a cruise speed of 530 knots (610 miles per hour/982 kilometers per hour). and a maximum speed of 1,153 knots 1,327 miles per hour/2,135 kilometers per hour) at 35,000 feet (10,668 meters). The F-106A had a service ceiling is 53,800 feet (16,398 meters) and a rate of climb of 48,900 feet per minute (248 meters per second). Its combat radius was 530 nautical miles (610 statute miles/982 kilometers) and the maximum ferry range was 1,843 nautical miles (2,121 statute miles/3,413 kilometers).

The Delta Dart was armed with four GAR-3A radar-homing, or -4A (AIM-4F, -4G) infrared-homing Falcon air-to-air guided missiles, and one MB-1 (AIM-2A) Genie unguided rocket with a 1.5 kiloton W-25 nuclear warhead. The missiles were carried in an internal weapons bay. In 1972, the General Electric M61A1 Vulcan 20mm cannon was added to the rear weapons bay with 650 round of ammunition. (The number of gun-equipped Delta Darts is uncertain.)

Convair built 342 F-106 interceptors. 277 were F-106As and the remainder were F-106B two-seat trainers.

Convair F-106A Delta Dart 56-0467 in flight. (U.S. Air Force)
Convair F-106A Delta Dart 56-0467 in flight. Because of the filter used by the photographer, areas that are actually painted bright “day-glow” orange appear to be  white. (U.S. Air Force)
Convair F-106A Delta Dart 56-0467 in flight, seen from left rear quarter. (U.S. Air Force)
Convair F-106A Delta Dart 56-0467 in flight, seen from left rear quarter. (U.S. Air Force)

F-106A 56-0467 was built in April 1958 and was the eighteenth production aircraft. After being used for flight testing at Edwards Air Force Base it was converted back to an operational interceptor and assigned to the 329th Tactical Fighter Squadron at nearby George Air Force Base.

Convair F-106A Delta Dart 56-0467 on display at at Edwards AFB, May 1961.
Convair F-106A Delta Dart 56-0467 on display at Edwards AFB, May 1961. (Gary Abel from Marty Isham Collection via f-106deltadart.com)

On 14 August 1961, while taking off from George Air Force Base, Victorville, California, on a routine training mission, 56-0467’s right tire blew out. The pilot, James Wilkinson, flew until most of the airplane’s fuel had been exhausted, and then landed at Edwards Air Force Base because of its longer runway and available emergency equipment. After touching down, the right wheel and brake assembly caught fire. The flames quickly spread to the wing and fuselage. The aircraft slid to a stop and the pilot safely escaped. 467 was totally destroyed.

56-0459, which had been scheduled to make the speed record flights, is on display at the McChord Air Force Base Museum.

Major Joe Rogers with Convair F-106A Delta Dart 56-0459 at Edwards Air Force Base before a speed record attempt. (U.S. Air Force)
Major Joe Rogers with Convair F-106A Delta Dart 56-0459 at Edwards Air Force Base before a speed record attempt. This airplane was originally scheduled for the speed record attempt. (U.S. Air Force)
U.S. Air Force public relations photograph.
U.S. Air Force public relations photograph.

¹ FAI Record File Number 9064

© 2018, Bryan R. Swopes