Tag Archives: Croix de Guerre

22 August 1922

Second Lieutenant Stanley Cockerell, Royal Flying Corps

22 August 1922: Captain Stanley Cockerell, A.F.C., a test pilot for Vickers Ltd (Aviation Department), made the first flight of the prototype Type 56 Victoria Mk.I, J6869, at Brooklands, Surrey, England.

The Victoria was a twin-engine biplane military transport, developed from the earlier Vickers Vernon and Virginia. It was operated by a crew of two in an open cockpit and could carry up to 22 troops.

A Vickers Victoria (San Diego Air and Space Museum Archives Catalog # Iraq_00831)
A Royal Air Force Vickers Victoria transport. (San Diego Air and Space Museum Archives Catalog # Iraq_00831)

The prototype Vickers Victoria was powered by two water-cooled, normally-aspirated,  1,461.135 cubic-inch-displacement (23.944 liters) D. Napier and Son Ltd. Lion I, a 60° “triple Four” or “broad-arrow” 12-cylinder engine (also known as a W-12), rated at 450 horsepower at 1,925 r.p.m., each. This was a very complex engine, using individually machined steel cylinders surrounded by welded stamped-steel water jackets. The cylinders were closed at the upper end, rather than having a separate cylinder head. Four valve ports were machined into the “crown.” Each cylinder had two intake and two exhaust valves, which were operated by a dual overhead camshaft arrangement. The cylinders were screwed into a aluminum “head block” which provided stiffening to the assembly, and contained intake and exhaust runners and cooling passages. The three individual banks of four cylinders were attached to the crankcase by studs. The engine’s crankshaft used large roller main bearings for support. The engine used a dry sump lubrication system with an oil pick up at each end. The propeller was driven through a 2:1 reduction gear unit. Cast aluminum alloy pistons were fitted to a master rod with two side rods. The Napier Lion was was compact, very light for the power it produced, and also very efficient. The Napier Lion I weighed approximately 860 pounds (390 kilograms).

The Vickers Victoria had a maximum speed of 110 miles per hour (177 kilometers per hour), and a service ceiling of 16,200 feet (4,940 meters). Its range was 770 miles (1,240 kilometers).

97 Victoria transports were built by Vickers. The type remained in service with the Royal Air Force until 1935 and saw extensive use in Iraq and Afghanistan.

Stanley Cockerell, 1933
Stanley Cockerell, 1933. (A Fleeting Peace)

Stanley Cockerell had been an aircraft mechanic before becoming a fighter pilot. On 27 October 1916, Serjt. Cockerell was assigned to the Royal Flying Corps. He was credited with seven aerial victories during World War I, while flying the Airco DH.2, DH.5 and the Sopwith Camel.

Albert I, King of the Belgians, conferred the Chevalier de l’Ordre de la Couronne to Temporary 2nd Lieutenant Cockerell, 21 September 1917. On 25 October 1917, Cockerell was promoted to the temporary rank of Captain. He was awarded the Belgian Croix de Guerre 11 March 1918.

For a flight from England to South Africa in a Vickers Vimy, 24 January–26 February 1920, (“The Times Flight”) Captain Cockerell was awarded the Air Force Cross by George V.

On 4 June 1921, Flight Lieutenant Stanley Cockerell, A.F.C., Royal Air Force, was transferred to the unemployed list.

In 1921, Cockerell married Miss Lorna Lockyer. They would have seven children.

In 1922, Cockerell competed in the King’s Cup, a cross country air race, flying a Vicker’s Type 61 Vulcan, G-EBEM. He finished in 7th place. In the 1923 race, he flew a Type 74 Vulcan, but that airplane did not finish.

Stanley Cockerell and his six-year-old daughter, Kathleen, were killed during the Battle of Britain, when the Luftwaffe bombed Sunbury-on-Thames, 29 November 1940. Mrs. Cockerell was also killed during The Blitz.

A Royal Air Force Vickers Victoria transport, J7924, photographed in flight over Iraq. (RAF)

© 2017, Bryan R. Swopes

Joseph Sadi-Lecointe (11 July 1891–15 July 1944)

Joseph Sadi-Lecointe, 1924

Joseph Sadi-Lecointe was born 11 July 1891 at Saint-Germain-sur-Bresle, Departement de la Somme, Picardie, France.

Sadi-Lecointe was employed as an aircraft welder. On 30 January 1910, without any instruction, he took off from Issy-les-Moulineaux in a monoplane designed by George and Gendre Zénith. The Aero Club de France awarded him its license number 431 on 10 February 1911.

Adjutant Joseph Sadi-Lecointe with a Morane-Saulnier, circa 1915. (Musée de l’air et de l’espace)

He joined the Service Aéronautique (the original form of the French Air Force) as a mechanic in October 1912, and was designated pilote militaire nº375, 20 September 1913.

Sadi-Lecointe was promoted to sergeant 6 July 1914. He served as a pilot during World War I, flying the Blériot XI-2 with l’escadrille BL 10 from 1 August 1914 to 6 March 1915. After serving five weeks with the RGA, Sergent Sadi-Lecointe was transferred to N 48, flying the Nieuport X. He was promoted to Adjutant, a warrant officer rank, 17 April 1915. On 23 November 1915 became a flight instructor at l’Ecole de Pilotage d’Avord. Sadi-Lacointe was promoted to sous-lieutenant in October 1916. On 17 September 1917 he was assigned as a test pilot at BlériotSociété Pour L’Aviation et ses Dérivés, where he worked on the development of the famous SPAD S.XIII C.1 fighter.

Joseph Sadi-Lecointe was a test pilot for the Société Pour L’Aviation et ses Dérivés SPAD S.VII C.1 and S.XIII C.1 fighters. (Bibliothèque nationale de France)

After the War, he was a test pilot for Nieuport-Delâge, and participated in numerous races and set a series of speed and altitude records with the company’s airplanes. He won the Coupe Deutsche de la Meurthe, 3 August 1920, and the Gordon Bennett Aviation Trophy Race, 28 September 1920, flying a Nieuport-Delâge Ni-D 29V. He also won the Coupe Beaumont, 23 June 1924, flying the Nieuport-Delâge Type 42. Joseph Sadi-Lecointe was appointed Chevalier de la Légion d’honneur in 1924.

Joseph Sadi-Lecointe with the Blériot-SPAD S.26 during trials for the Coupe d’Aviation Maritime Jacques Schneider races, 1919. (Bibliothèque nationale de France)
Joseph Sadi-Lecointe in the cockpit of his Nieuport-Delâge NiD-29 V racer during te eGordon Bennett races. (Bibliothèque nationale de France)
Nieuport-Delâge NiD-42 S. (FAI)
Sadi-Lecointe’s record-setting Nieuport-Delâge NiD-40 R. (FAI)

Sadi-Lecointe returned to military service in 1925 and participated in the Second Moroccan War. Then in 1927, he returned to his position as chief test pilot for Nieuport-Delâge. From 1936 to 1940, he served as Inspecteur général de l’aviation civile (Inspector General of Aviation) for the French Air Ministry. With the outbreak of World War II in 1939, Lieutenant Colonel Sadi-Lecointe was again recalled to military service as Inspector of Flying Schools.

With the Fall of France, Sadi-Lacointe was dismissed by the Vichy government. He joined La Résistance française, and operated with the group, Rafale Andromède. He was arrested 21 March 1944 and held at the Fresnes prison in Paris, where he was interrogated and tortured. He was released to l’hôpital Saint-Louis, Paris, and died there, 15 July 1944.

Centre pénitentiaire de Fresnes

Joseph Sadi-Lecointe, Commandeur Ordre national de la Légion d’honneur, was awarded the Croix de Guerre in three wars. He was posthumously awarded the Médaille de la Résistance. The Aéro-Club de France awarded him its Grande Médaille d’Or. During his flying career, Sadi-Lecointe set six World Records for Speed,¹ and two World Records for Altitude.²

MORT POUR LA FRANCE

The Cross of Lorraine was the symbol of La Résistance française during World War II. (© Ray Rivera)

¹ FAI Record File Numbers: 15489, Speed over 100 km, 279,50 km/h (173.67 m.p.h.), 25 September 1920; 15494, Speed over 200 km, 274,60 km/h (170.63 m.p.h.), 28 September 1920; 15498, Speed over a straight 1 km course, 296,69 km/h (184.36 m.p.h.), 10 October 1920; 15499, Speed over a straight 1 km course, 302,53 km (187.98 m.p.h.), 20 October 1920; 15279, Speed, 375 km/h (233 m.p.h.), 15 October 1923; and Speed over a given distance of 500 km, 306,70 km/h (190.58 m.p.h.), 23 June 1924.

² FAI Record File Numbers: 8246, 10 741 m (35,240 ft.), 5 September 1923; 11750, 8 980 m (29,462 ft.), 11 March 1924.

© 2019, Bryan R. Swopes

6 June 1955

Massif du Mont-Blanc depuis le sommet du Brévent, 2006. Mont Blanc, north face from Brevant. (Yann via Wikipedia)
Massif du Mont-Blanc depuis le sommet du Brévent, 2006. Mont Blanc, north face from Brevant. (Yann via Wikipedia)

6 June 1955: Mont Blanc (the “White Mountain”), at 4.808,73 mètres (15,776.67 feet), is the highest mountain in the Alps, and second highest in Europe. (Because the summit consists of ice and snow, the actual elevation of the summit varies from year to year, and season to season. This is the 2013 measurement.)

Jean Moine, chief pilot of Fenwick Aviation S.A., flew a new Bell Aircraft Corporation Model 47G-2 helicopter from the company’s base at Issy-les-Moulineaux, southwest of Paris, to Chamonix in southeastern France, and then on to the village of Le Fayet. This village is located northwest of the Mont Blanc massif at an elevation of 584 meters (1,916 feet) above Sea Level.

Jean Moine, Capitaine, Com
Jean Moine in the cockpit of a Bell Model 47 helicopter. (Hélico-Fascination)

The helicopter, registered F-BHGJ, with manufacturer’s serial number 1342, was the very first Bell Model 47G-2 to be built.

Some items not necessary for the planned flight to the summit were removed from the helicopter to reduce weight: the left fuel tank, battery, generator and seat cushions. The right fuel tank contained just 40 liters (10.6 gallons) of gasoline.

At 5:15 a.m. the following morning, 6 June, Jean Moine and his passenger, André Contamine, an Alpine guide, lifted off from Le Fayet and began a long climb to the Dôme du Goûter, 2 kilometers (1¼ miles) northwest of the summit of Mont Blanc, at 4,304 meters (14,121 feet). After 32 minutes, Moine landed there at 5:43 a.m.

Jean Moine with Bell 47G-2 F-BHGJ
Jean Moine with the first Bell Model 47G-2, F-BHGJ, probably at Dôme du Goûter, 6 June 1955. The helicopter’s left fuel tank and battery have been removed. (Hélico-Fascination)

After remaining at Dôme du Goûter for five minutes, Moine and Contamine again took off, and seven minutes later, landed atop Mont Blanc at 5:55 a.m. Moine estimated the wind speed at 25 knots (13 meters per second). After four minutes at the summit, Moine again lifted off and this time, returned to Chamonix, where the helicopter landed at 6:15 a.m.

Although the Bell 47G-2 has a hover ceiling in ground effect (HIGE) of 10,000 feet (3,048 meters), with winds of 20–25 knots (10.3–12.9 meters per second), the helicopter, while stationary, was actually in translational lift. Combined with very cold temperatures (probably lower than -14.7 °C./5.5 °F.) which reduced the density altitude from ISA standard conditions, the helicopter was easily able to land and takeoff, requiring only 14 inches (0.47 bar) of manifold pressure.

This was the highest landing and takeoff by a helicopter up to that time.

Later that morning, Moine and the Bell 47G-2 made two more flights to Dôme du Goûter, first with Pierre Voisin (?) and again with Contamine.

 Jean Moine and F-BHGJ at the summit of Mont Blanc, just before 6:00 am, 6 June 1955. (André Contamine via Hélico-Fascination)
Jean Moine and F-BHGJ at the summit of Mont Blanc, just before 6:00 am, 6 June 1955. (André Contamine via Hélico-Fascination)

Two short articles in FLIGHT and Aircraft Engineer mention the Mont Blanc landing:

. . . Lands High . . .

FLYING a Bell 47G, M. Jean Moine, accompanied by the guide Contamine, took off from Le Fayet airfield (1,905ft) on Monday and landed first on the Dôme du Goûter (14,116ft) and, seven minutes later, on the summit of Mont Blanc (15,782ft). On the same day S.N.C.A.S.E. claimed the world’s helicopter height record when the Alouette II, powered by a Turboméca Artouste, reached 27,100ft. The machine took off from Buc, near Paris, climbed for 42 min and landed at Montesson. The pilot was M. Jean Boulet.

FLIGHT and AIRCRAFT ENGINEER, No. 2420 Vol. 67. Friday, 10 June 1955, at Page 784

. . . and:

. . . There followed, on June 6th, a landing by Jean Moine in a Bell 47-G2 on Mont Blanc, altitude 15,781 feet, now the highest landing by a rotating wing aircraft. . .

     The actual machine which landed on the summit of Mont Blanc , the Bell 47G2, powered by a 260 h.p. Lycoming engine de-rated to 200 h.p. was seen at Le Bourget. The use of a de-rated engine, the makers claim, increases considerably the engine overhaul life and also engine maintenance problems.

      According to the pilot, Jean Moine, the mountain landing was made without difficulty, in spite of no little turbulence caused by a 20 knot wind, and there was a sufficient reserve of power, with a passenger aboard, to enable the machine to hover in the ground cushion in the normal way before touching down.

FLIGHT and AIRCRAFT ENGINEER, No. 2424 Vol. 68. Friday, 8 July 1955 at Page 54

Logbook entries of Mount Blanc flight
Entries in Jean Moine’s logbook of the Mount Blanc flight, 6 June 1955.

Jean Moine was born at Paris, France at 1915. He studied at Lycée Condorcet, a high school in Paris. In 1935, he learned to fly in a Potez 36 two-place trainer at l’aéro-club at Orly. In 1937 joined the Armée de l’air (the French Air Force). With the fall of France in 1939, Capitaine Moine continued to serve with the Forces Aériennes Françaises Libres (the Free French Air Force.) Assigned to Groupe Bretagne (GB II/20) he flew 46 combat missions with the Glenn L. Martin Co. B-26 Marauder, a twin-engine medium bomber.

Glenn L. Martic Co. B-26 Marauder.
Forces Aériennes Françaises Libres (Free French Air Force) Glenn L. Martin Company B-26G-11-MA Marauder 43-34594, nº 29, Groupe Bretagne. (Collection J. Moulin)

Captain Moine was awarded the Croix de Guerre and the Médaille de la Résistance (Medal of the Resistance). He was appointed Commandeur Ordre national de la Légion d’honneur.

Following World War II, Jean Moine served as chief pilot for a small regional airline, Lignes Aériennes du Sud-Ouest. In 1950, Moine joined Fenwick Aviation S.A., Paris, France, as chief pilot and general manager. The company sold and operated aircraft produced by several American manufacturers, including the Bell Aircraft Corporation. He learned to fly helicopters at the Bell plant at Buffalo, New York. While there, he also studied Bell’s flight school operation. Returning to France, he organized Fenwick Aviation’s flight school at Issy-les-Moulineaux.

Moine rose to vice president and chief executive officer. He served as Fenwick’s president from 1966 to 1976.

Bell Model 47 helicopters at Fenwick Avaition,
Bell Model 47 helicopters at Fenwick Aviation, a major distributor for Bell Aircraft Corporation in Europe. (Hélico-Fascination)

Leaving Fenwinck, he joined Transair Helicopters Group. One of the missions this company performed was transporting marine pilots by helicopter to ships at sea, flying an Aérospatiale Alouette III based at Cherbourg.

In December 1975, HRH Prince Charles awarded the Berguet Trophy of the Royal Aero Club and the Aero Club of France to Moine for his outstanding contributions to rotary wing flight.

Moine served as president of l’Aéro-Club de France from 1982–1986.

When Jean Moine retired, he had accumulated a total of 7,000 flight hours, about equally divided between fixed-wing and rotary-wing aircraft.

Jean Moine, Commandeur Ordre national de la Légion d’honneur, died 7 March 2002 at the age of 86 years.

This advertisement for the Bell 47G-2 shows an early production aircraft painted yellow. This may be c/n 1342. (Bell Helicopter Company)
This advertisement for the Bell Model 47G-2 shows an early production aircraft painted yellow and black, the standard paint scheme. (Bell Helicopter Company)

The Bell Model 47, designed by Arthur M. Young, of the Bell Aircraft Corporation, Buffalo, New York, was the first helicopter to receive civil certification from the Civil Aviation Administration, predecessor of the Federal Aviation Administration. On 8 March 1946, the aircraft received CAA Type Certificate H-1.

The Bell 47G was the first helicopter manufactured by the Bell Aircraft Corporation at the company’s new plant at Fort Worth, Texas. It was also produced under license by Agusta, Kawasaki and Westland.

The Bell Model 47G and 47G-2 Trooper are nearly identical, essentially differing only in the engine used. It is a 3-place, single-engine light helicopter, operated by a single pilot. The helicopter has dual flight controls and can be flown from either the left or right. The airframe is constructed of a welded tubular steel framework with a sheet metal cockpit. The landing gear consists of two lateral, horizontal tubular cross tubes, and two longitudinal “skids,” curved upward at the front. Ground handling wheels are attached to the skids. The most distinctive feature of the Bell 47 is the large plexiglass “bubble” windshield. The main rotor flight controls use a system of bell cranks and push-pull tubes. The cyclic is hydraulically boosted. The tail rotor is controlled by pedals and stainless steel cables.

With rotors turning, the Bell 47G-2 has an overall length of 41 feet, 4.75 inches (12.618 meters). From the forward tip of the skids to the aft end of the tail rotor guard, the fuselage is 31 feet, 5.40 inches long (9.586 meters). The main rotor has a diameter of 35 feet, 1.50 inches (10.706 meters). The tail rotor diameter is 5 feet, 8.125 inches (1.730 meters). Height to top of main rotor mast is 9 feet, 3.613 inches (2.835 meters).

The Bell 47G-2 has an empty weight of approximately 1,564 pounds (709 kilograms), depending on installed equipment. Its maximum gross weight is 2,450 pounds (1,111 kilograms), a 100 pound (45 kilogram) increase over the Franklin-powered Model 47G.

The main rotor, in common to all American-designed helicopters, rotates counter-clockwise as seen from above. (The advancing blade is on the helicopter’s right.) The anti-torque (tail) rotor is mounted to the right side of an angled tail boom extension, in a tractor configuration, and rotates counter-clockwise as seen from the helicopter’s left. (The advancing blade is above the axis of rotation.)

This photograph of a Bell 47 presents a good view of the stabilizer bar, pitch links and hydraulic dampers.
This photograph of a Lycoming-powered Bell 47G-2 hovering in ground effect presents a good view of the stabilizer bar, pitch links and hydraulic dampers. (Wikipedia)

The main rotor is a two-bladed, under-slung, semi-rigid assembly that would be a characteristic of helicopters built by Bell for decades. The main rotor system incorporates a stabilizer bar, positioned below and at right angles to the main rotor blades. Teardrop-shaped weights are placed at each end of the bar, on 100-inch (2.540 meters) centers. The outside diameter of the stabilizer bar is 8 feet, 6.781 inches (2.611 meters). The pilot’s inputs to the cyclic stick are damped through a series of mechanical linkages and hydraulic dampers before arriving at the pitch horns on the rotor hub. The result is smoother flight, especially while at a hover. The stabilizer bar action is commonly explained as being “gyroscopic,” but this is incorrect. (A similar system is used on the larger Bell 204/205/212 helicopters.)

The working parts of this Agusta-Bell 47G-3B-1 are clearly visible in this photograph. (M. Bazzani/Heli-Archive)

The Bell 47G and 47G-2 used laminated-wood main rotor blades, with a metal spar, covered with fabric. The blades’ trailing edge tapers slightly from root to tip. The airfoil is symmetrical, transitioning from NACA 0015 at the root to NACA 0011 at the tip. The normal operating range of the main rotor is 322–360 r.p.m. (294–360 r.p.m. for autorotation). A longitudinal hole in the blade tip for a recessed tension-adjusting nut produces a distinctive whistling sound.

The 47G-2 used a more powerful AVCO Lycoming VO-435-A1A, -A1B, -A1D, -A1E or -A1F engine in place of the Franklin 6V4-200-C32AB. The VO-435 is an air-cooled, normally-aspirated 433.972-cubic-inch-displacement (7.112 liter) vertically-opposed six-cylinder direct-drive engine. The engine has a compression ratio of 7.30:1 and requires a minimum of 80/87 octane aviation gasoline. The VO-435A series engine has a Maximum Continuous Power rating of 250 horsepower at 3,200 r.p.m., and 260 h.p. @ 3,400 r.p.m. for takeoff. Installed in the Bell 47G-2, the engine’s maximum power limit is 28.8 inches of mercury (0.975 bar) manifold pressure at 3,100 r.p.m. (200 horsepower) to increase time-between-overhaul (TBO) limits. The VO-435 is 34.73 Inches (0.882 meters) high, 33.58 inches (0.878 meters) wide and 24.13 inches (0.613 meters) deep, and weighs 393.00 pounds (178.26 kilograms) to 401.00 pounds (182.89 kilograms), depending of the specific engine variant.

Bell Model 47G, 47G-2 diagram
Bell Model 47G/47G-2 left profile.

Engine torque is sent through a centrifugal clutch to a gear-reduction transmission, which drives the main rotor through a two-stage planetary gear system. The transmission also drives the tail rotor drive shaft, and through a vee-belt/pulley system, a large fan on the forward face of the engine to provide cooling air.

The Bell 47G/G-2 has a maximum speed (VNE) of 100 miles per hour (161 kilometers per hour) from Sea Level to 1,400 feet (427 meters). Above that altitude, VNE is reduced 3.5 miles per hour (5.6 kilometers per hour) for every 1,000 foot (305 meters) increase in altitude. On a Standard Day, the hover ceiling in ground effect (HIGE) of the Bell 47G-2, at maximum gross weight, is 10,000 feet (3,048 meters) above Sea Level, and out of ground effect (HOGE), 3,200 feet (975 meters).

Fuel is carried in two gravity-feed tanks, mounted above and on each side of the engine. The total fuel capacity is 43.0 gallons (162.8 liters), however, usable fuel is 41.0 gallons (155.2 liters). The helicopter has a maximum range of 238 miles (383 kilometers).

In production from 1946 until 1974, more than 7,000 Model 47 helicopters were built, worldwide. It is estimated that about 10% of these aircraft remain in service.

In 2010, the type certificates for all Bell 47 models were transferred to Scott’s Helicopter Service, Le Sueur, Minnesota, which continues to manufacture parts and complete helicopters.

Bell 47G-2 F-BHGJ was delivered to Fenwick Aviation SA, along with the second production G-2, 3 February 1955. It was acquired by France Aviation SA, Aéroport de Toussus le Noble, Chateaufort, south of Versailles, on 13 June 1955. It was next registered to SA Gyrafrique, Algeria, 8 November 1955. On 5 August 1960, the helicopter was once again reregistered, this time to SA Gyrasahara. Gyrafrance SA (Gyrafrance Hélicoptères), Aéroport de Frejorgues, Mauguio, became the registered owner, 23 July 1964. On 9 August 1991, the registered owner was Societe Nouvelle Gyrafrance SA, Aéroport de Montpellier–Méditerranée, Mauguio. F-BHGJ was registered to SA Aero 34, also located at the Aéroport Montpellier–Méditerranée, Mauguio, 23 March 1995, and then Aeromecanic 34 SARL, Marignane, 1 August 2001. From 12 October 2004 until 18 February 2015, the helicopter was owned by Heli System, Frontignan, on the Mediterranean coast. The first Bell 47G-2, F-BHGJ, is currently owned by Conseil Aménagement Foncier, Frontignan.

Recommended: The Bell 47 Helicopter Story, by Robert S. Petite and Jeffrey C. Evans, Graphic Publishers, Santa Ana, California, November 2013.

© 2017, Bryan R. Swopes

18 May 1916

Kiffin Yates Rockwell, Escadrille Américaine, 1916. (Kiffin Ayers)
Kiffin Yates Rockwell, Escadrille de La Fayette, 1916 (Kiffin Ayres)

18 May 1916: Corporel Kiffin Yates Rockwell, Escadrille de La Fayette (Escadrille Nº. 124), shot down an enemy airplane near Hartmannswillerkopf, a 956 meter (3,137 feet) peak in the Vosges Mountains, along the border between France and Germany.

Rockwell is credited as the first American pilot to shoot down an enemy aircraft during World War I. ¹

Rockwell wrote to his brother, Paul Ayres Rockwell:

Thursday, May 18, 1916

Dear Paul:

     Well, at last I have a little something to tell you. This morning I went out over the lines to make a little tour. I was somewhat the other other side of our lines, when my motor began to miss a bit. I turned around to go to a camp near the lines.

     Just as I started to head for there I saw a boche machine about seven hundred meters under me and a little inside our lines. I immediately reduced my motor and dived for him. He saw me at the same time, and began to dive towards home. It was a machine with a pilot and a gunner, carrying two rapid fire guns, one facing front, and one in the rear that turned on a pivot so it could be fired in any direction.

     The gunner immediately opened fire on me, and my machine was hit; but I didn’t pay any attention to that, and kept going straight for him until I got within twenty-five or thirty meters of his machine. Then, just as I was afraid of running into him, I fired four or five shots, and swerved my machine to the right to keep from having a collision.

     As I did that I saw the gunner fall back dead on the pilot, his machine-gun fall from its position and point straight up in the air, and the pilot fall to one side of the machine as if he too were done for. The machine itself fell to one side, then dived vertically towards the ground with a lot of smoke coming out of the rear. I circled around, and three or four minutes later saw smoke coming up from the ground just beyond the German trenches.

     The captain said he would propose me for the Medaille Militaire, but I don’t know whether I will get it or not.

     Yesterday Thaw had a fight that ended by the boche diving towards the ground. He was signaled as leaving the air on being seriously hit, but being able to get in his own lines.

     Am very busy just now, as the order has just come for us to go to Verdun. Jim sent you a telegram about my fight.

     Much Love.

Kiffin

Kiffin Rockwell, in a Nieuport fighter, Verdun, July 1916. (Virginia Military Institute)

The Asheville Times reported:

Kiffin Rockwell Brings Down German Aeroplane

     Paris, May 19.—Corporal Kiffen [sic] Rockwell of Asheville and Atlanta, a member of the American flying squadron, yesterday attacked a German aeroplane operating near Hartmanns Weiler-Kopf. The German machine was brought down in flames.

     Corporal Kiffen Rockwell, of this city who with his brother Paul Rockwell, sailed for England at the very outbreak of the war and joined the Foreign Legion, is now an aviator in the French-American flying corps and on Wednesday took part in the first action of the corps since its organization as a separate unit. Although the flyers were subjected to heavy fire as they recrossed the front, it is stated, Corporal Rockwell escaped unharmed.

     After the two brothers joined the Foreign Legion they served in the trenches in the first Teutonic drive on Paris during which Paul was wounded. He soon recovered, however, and is doing newspaper work in Paris.

The Asheville Times, Volume XXI, No. 83, 19 May 1916, Page 1, Columns 2–3

In May 1916, Escadrille N°. 124 was equipped with both the Nieuport XI C.1 and Nieuport XVI C.1 fighters. It is not known which type Rockwell flew on 18 May. Neither is the type of aircraft which Rockwell shot down. (one unverified source describes it as a Luft-Verkehrs-Gesellschaft G.m.b.H. reconnaissance airplane.)

Photograph shows members of the Lafayette Escadrille composed of American aviators who flew with the French air force during World War I. Shown are Kiffin Yates Rockwell (1892-1916), Lieutenant Colonel Georges Thenault (commander), Norman Price (1887-1916), Lieutenant Alfred de Laage de Meux, Sgt. Elliot Cowdin, Sgt. Weston Birch “Bert” Hall, James Rogers McConnell (1887-1917) and Victor Chapman. (George Grantham Bain Collection, Library of Congress, LC-B2-3884-11)

Kiffin Yates Rockwell was born 20 September 1892 at Newport, Tennessee, United States of America. He was the third child of James Chester Rockwell, a Baptist minister, and Loula Ayres Rockwell. His father died of typhoid fever a week before Kiffin’s first birthday. Mrs. Rockwell would become a school teacher to support her family. She was soon placed in charge of the public schools in Newport. In 1902, she enrolled at the American College of Osteopathy, Kirksville, Missouri, and became a doctor of osteopathic medicine. After she graduated, the Rockwell family relocated to Asheville, North Carolina.

Rockwell family home at 142 Hillside Street, Asheville, North Carolina. (Buncombe County Special Collections)

Kiffin Rockwell attended Orange Street School and Asheville High School, both in Asheville, North Carolina. On 1 February 1909, he entered the Virginia Military Institute, Lexington, Virginia. Rockwell was appointed to the United States Naval Academy, Annapolis, Maryland, but enrolled at Washington and Lee University, also located in Lexington, where his older brother, Paul, was studying. Kiffin was a member of the Class of 1913, and of the Sigma Phi Epsilon (ΣΦΕ) Fraternity, Epsilon Chapter. He was also a member of the university’s North Carolina Club. Rockwell left Washington and Lee in 1911 to pursue a career in journalism.

Rockwell worked for an advertising agency in San Francisco, California, then joined his brother at a newspaper in Atlanta, Georgia.

Kiffin Yates Rockwell’s U.S. passport application.

On 7 August 1914, Kiffin Rockwell and his brother sailed to France aboard the American Line steamship, S.S. St. Paul. On 21 August, they enlisted in the Légion étrangère (the French Foreign Legion) and served with Battalion C, Second Marching Regiment, Second Foreign Battalion.

American Line steamship S.S. St. Paul. (John S. Johnston, Detroit Publishing Company/Library of Congress)

In March 1915, Rockwell transferred to 1re Division Marocaine (1st Regiment, Moroccan Division). He was wounded by machine gun fire 9 May 1915 at La Targette, north of Arras. After recuperating, he requested a transfer to the Service Aeronautique, which was accepted. He began flight training in September 1915. Rockwell was a founding member of the Escadrille Americaine (Lafayette Escadrille) of the Aéronautique Militaire (the French Air Service).

Kiffin Rockwell, French Foreign Legion, December 1914. (Virginia Military Institute)

Sergeant Kiffin Yates Rockwell, while flying a Nieuport XVII C.1 over Thann, a town at the foot of the Vosges Mountains, was killed in action 23 September 1916. He was hit in the chest by the gunner of a two-place Aviatik.

In a letter to his mother, Rockwell had written,

If I die you will know that I died as every man should—in fighting for the right. I do not consider that I am fighting for France alone, but for the cause of humanity, the greatest of all causes.

Rockwell was officially credited with four aerial victories. He was awarded the Médaille Militaire and the Croix de Guerre. He was appointed a Chevalier de la légion d’honneur.

His remains were buried at the Luxeuil-les-Bains Communal Cemetery, Luxeuil-les-Bains, Departement de la Haute-Saône, Franche-Comté, France. His commanding officer, Captain Georges Thenault, said of him, “His courage was sublime. . . The best and bravest of us is no longer here.”

Rockwell is commemorated at the Mémorial Escadrille La Fayette, Marnes-la-Coquette, Departement des Hauts-de-Seine, Île-de-France, France.

(Find A Grave)

¹ American ace Sergent Gervais Raoul Victor Lufbery, also a member of the Lafayette Escadrille, shot down his first enemy aircraft 30 July 1916.

© 2023, Bryan R. Swopes

23 April 1918

1st Lieutenant Paul Frank Baer, Air Service, United States Army. (Campbell Studios, New York)

23 April 1918: at 09:55 a.m., near Saint-Gobain, France, 1st Lieutenant Paul Frank Baer, 103rd Aero Squadron (Pursuit), shot down an enemy Albatross C two-place biplane. This was Baer’s fifth victory in aerial combat, making him the first American “ace.” ¹ [Official credit for this shoot-down is shared with Lt. C. H. Wilcox.]

Albatros C.VII C.2197/16 (Wikipedia)

Paul Frank Baer was born 29 January 1894 at Fort Wayne, Indiana, the fourth of four children of Alvin E. Baer, a railroad engineer, and Emma B. Parent Baer.

In 1916, Baer served under Brigadier John J. General Pershing during the Mexican Expedition to capture the outlaw and revolutionary Francisco (“Pancho”) Villa. He then went to France and enlisted the Aéronautique Militaire, in 20 February 1917. He was sent for flight training at the Avord Groupemant des Divisions d’Entrainment (G.D.E.). He graduated as a pilot, 15 June 1917, with the rank of corporal.

After flight training, Corporal Baer was assigned to Escadrille SPA 80, under the command of Capitaine Paul Ferrand, 14 August 1917 to 20 January 1918, flying the SPAD S.VII C.1 and SPAD S.XIII C.1. Baer was next transferred to Escadrille N. 124, the Escadrille Américaine, under Georges Thénault. This unit was equipped with the Nieuport-Delâge Ni-D 29 C1.

Nieuport-Delâge Ni-D 29C.1, s/n 12002, right front quarter view.

After the United States entered the War, Baer was transferred to the 103rd Aero Squadron, American Expeditionary Forces, and commissioned as a 1st Lieutenant with a date of rank retroactive to 5 November 1917. At that time, the 103rd was under the command of Major William Thaw II, and was operating near La Cheppe, France, flying the SPAD S.VII C.1 chasseur.

SPAD S.XIII C.1 S7714 of the 103rd Aero Squadron, France, 1918. The pilot is Captain Robert Soubiran, the squadron’s commanding officer. (U.S. Air Force)

Lieutenant Baer is officially credited by the United States Air Force with 7.75 enemy airplanes shot down between 11 March and 22 May 1918, ² and he claimed an additional 7. (Credit for two airplanes was shared with four other pilots.) After shooting down his eighth enemy airplane on 22 May 1918, Baer and his SPAD S.XIII C.1 were also shot down. He was seriously injured and was captured by the enemy near Armentières and held as a Prisoner of War. At one point, Baer was able to escape for several days before being recaptured.

For his service in World War I, 1st Lieutenant Paul Frank Baer was awarded the United States’ Distinguished Service Cross with one oak leaf cluster (a second award). He was appointed Chevalier de la Légion d’honneur by Raymond Poincaré, the President of France. He was also awarded the Croix de Guerre with seven palms.

SPAD S.XIII C.1 at Air Service Production Center No. 2, Romorantin Aerodrome, France, 1918. (U.S. Air Force)

After World War I, Baer, as a “soldier of fortune,” organized a group of pilots to fight against “the Bolsheviks” in Poland. He returned to the United States, departing Boulogne-sur-mer aboard T.S.S. Nieuw Amsterdam, and arriving at New York City, 4 November 1919. He then flew as a test pilot, an air mail pilot in South America, and worked as an aeronautical inspector for the U.S. Department of Commerce, based at Brownsville Airport, Texas. In 1930, he was employed as a pilot for the China National Aviation Corporation.

Baer was flying from Nanking to Shanghai for with an amphibious Loening Air Yacht biplane, named Shanghai. The airplane crashed after striking the mast of a boat on the Huanpu River. He died at the Red Cross Hospital at Shanghai, China, at 9:00 a.m., 9 December 1930. A Chinese pilot, K. F. Pan, and an unidentified female passenger were also killed. General Hsiung Shih-hui and four other passengers on board were seriously injured.

Paul Baer’s remains were returned to the United States aboard S.S. President McKinley and were buried at the Lindenwood Cemetery in Fort Wayne, Indiana.

In 1925 a new airport was opened in Fort Wayne and named Paul Baer Municipal Airport. During World War II, the airport was taken over by the military and designated Baer Army Airfield. It is now Fort Wayne International Airport (FWA).

A CNAC Loening Air Yacht amphipian at Lungwha, China, circa 1930. (SFO Aviation Museum & Library R2014.1811.001)
Lufbery

¹ TDiA would like to thank CMSgt Bob Laymon USAF (Ret.) (AKA, “Scatback Scribe”) for pointing out that while Lt. Baer was the first American to become an ace flying in the American service, that,

“The first American Ace was actually Gervais Raoul V. Lufbery, an American immigrant that was serving with the French Air Service when he shot down his 5th German plane in 1916: http://www.veterantributes.org/TributeDetail.php?recordID=903

² U.S. AIR SERVICE VICTORY CREDITS, WORLD WAR I, USAF Historical Study No. 133, Historical Research Division, Air University, Maxwell Air Force Base, Alabama, June 1969, at Page 7

© 2019, Bryan R. Swopes