THE 456th FIGHTER INTERCEPTOR SQUADRON

THE PROTECTORS OF  S. A. C.

 

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Curtiss P-40 "Tomahawk"

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Like it or not, the USAAF had only the P-40 available when it went to war. It rarely outperformed the fighters that it opposed, but it was one of the sturdiest fighters produced during World War II. Remembered as a "best second choice," innumerable pilots owe their lives to its rugged quality.

The Curtiss P-40 was undoubtedly one of the most controversial fighters to serve in quantity during the Second World War. It was praised and abused, lauded and vilified, but the fact remains that, as the first American single-seat fighter to be manufactured on a mass-production basis, it bore much of the brunt of the air warfare over several battle fronts. Its performance was inferior to the performances of the majority of its antagonists, but this shortcoming was partly compensated for by its tractability and its sturdiness which enabled it to withstand a considerable amount of punishment. It was amenable to adaptation and it was available when most sorely needed.

Not particularly good technically or in performance, though very durable, P-40s continued to be produced until the end of 1944, serving also with air force units of Turkey, South Africa, Canada, Australia and New Zealand. Later versions were known as Kittyhawks to the RAF and its Allies. Not usually realized is that the name Warhawk applied only to the United States Army Air Force P-40s starting with the P-40F version, a much improved plane with a license built version of the British Rolls-Royce Merlin engine installed.

The belief in the "ascendancy of bombardment over pursuit" was rife in 1937 when the Curtiss P-40 was first envisaged, and it is a sobering thought that, with the Bell P-39 Airacobra this product of such a school of thought constituted more than half the strength of all USAAF fighters until July 1943. Prior to September of that year the P-39 and P-40 also comprised more than half the USAAF fighters committed overseas. However, by July 1945 only one P-40 group remained operational.

The prototype P-40 took to the air in the autumn of 1938, and production was initiated in the following year. Performance of the first version of this single-seat fighter had not really come up to expectations, but as several air forces were desperate for new aircraft, the type was welcomed into service. The US had delayed modernizing its Army Air Service until the last minute, so P-40s made up a large part of their equipment during the first years of war. Britain and France also ordered P-40s to contend with the German Luftwaffe, but in the case of France, deliveries came too late and their P-40s were diverted to the Royal Air Force - to be known as Tomahawks. Similarly, the Soviet Union's outdated air force had fared badly at the hands of the Germans, and P-40s were also sent there.

The P-40 was initially designed around the Allison V-1710 liquid-cooled inline engine which offered better streamlining, more power per unit of frontal area, and better specific fuel consumption than did air-cooled radials of comparable power. Unfortunately, the rated altitude of the Allison engine was only some 12,000 feet, rendering combat above 15,000 feet a completely impracticable proposition. The P-40's ancestry dated back as far as 1924; the famed Curtiss Hawk fighters being in the forefront of all US warplanes. But its development was hindered from the start. The overall limitations of its design were such that the addition of multi-speed superchargers was considered inadvisable in view of the pending production of superior fighter designs. The achievements of the P-40 were therefore all the more creditable.

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The Curtiss P-40 served during most of the Second World War with one air force or another, and under several different names including Tomahawk and Kittyhawk in Britain and Warhawk in the United States.

The prototype XP-40, the Curtiss Hawk Model 81, owed its origin to the earlier Model 75 of 1935 vintage. With the standardization of the Allison V-1710 , the P-36 design was reworked to incorporate this engine, becoming the XP-37 which was equipped with a General Electric turbo-supercharger, and featured numerous other modifications, including a rearward positioned cockpit. Thirteen YP-37s were built for service evaluation; but, with increasingly ominous signs of an approaching war, development of this fighter was abandoned in favor of a less complex and more direct conversion of the P-36 for the Allison engine, the XP-40. This was, in fact, the tenth production P-36A with an integrally-supercharged 1,160 h.p. Allison V-1710-19 (C13) engine, and first flew with its new power plant in the autumn of 1938. Successful in a US Army Pursuit Contest staged at Wright Field, in May 1939 it was awarded what was at that time the largest-ever production order for a US fighter, totaling nearly thirteen million dollars.

The P-40 was a relatively clean design, and was unusual for its time in having a fully retractable tail wheel. One hundred and ninety-seven P-40s were built in 1939-40 for the USAAF, and many more were sold abroad to Britain and France. In the RAF, which service purchased 140 outright, it was known as the Tomahawk Mk. I, IA, and IB, and carried two .303 in. Browning machine-guns in place of the 0.30in.-calibre guns fitted in USAAF machines. It retained the standard synchronized armament of two 0.5 in.-calibre machine-guns in the top nose decking.


 

The Flying Tigers

Many US volunteer pilots flew on behalf of Britain, the Soviet Union and China before the United States entered the war. A group of them, equipped with P-40s, went to help the Chinese in their struggle against the Japanese in 1942, where they became known as the 'Flying Tigers' because of their uniquely painted aircraft. This group later became part of the USAAF proper, and P-40s were thereafter used widely in the Pacific.

In the middle of 1941 General Claire Chennault began recruiting for his Volunteer Group--better known as the Flying Tigers--to fight the Japanese from China, for which 100 P40s were ordered for purchase through a loan from the US Government. Ninety aircraft, mostly P-40Bs, were actually delivered, sufficient for three squadrons, plus a few spares. At the time of the USA's entry into the war there were eighty American pilots in the Volunteer Group, and shortly after arriving at Kunming the P-40s drew first blood, six out of ten attacking Japanese bombers being destroyed by two of the AVG squadrons on December 20. There were no American casualties on this occasion, but the third squadron, left behind at Mingaladon, Burma, was less fortunate, and lost two pilots on their first interception, on December 23,1941. The American pilots had underestimated the maneuverability of the lightly built Japanese Zero fighters, and failed to utilize their superior speed and diving ability to advantage. It was soon the cardinal rule that a P-40 should always avoid mixing it individually with a Japanese fighter, owing to the Curtiss machine's inferior climb rate and maneuverability, but the P-40 substantiated a reputation for ruggedness that it was already acquiring with the RAF in the Middle East, and its armor protection saved many AVG pilots in subsequent combat.

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Many US volunteer pilots equipped with P-40s, went to help the Chinese in their struggle against the Japanese in 1942, where they became known as the 'Flying Tigers'.

Both the Flying Tigers in China and the RAF squadrons in the Middle East had their P-40Bs replaced by P-40Es. The AVG after continuous operation, was down to some twenty P-40Bs by March 1942, when some thirty P-40Es were ferried to China by air from Accra, in Africa. The improved performance offered by these more potent P-40s was found to be extremely valuable against the Mitsubishi A6M Zero-Sen fighters which, first introduced in the Chinese theatre in 1940, were becoming increasingly numerous. The ground-attack potential of the P-40E was also much superior. The AVG pilots had resorted to carrying 30-lb. incendiary and fragmentation bombs in the flare chutes of their P-40Bs, but it was questionable whether this was not more hazardous to the attackers than to the attacked. But some indication of the P-40's capabilities in resolute hands is given by the fact that from its inception in December 1941 until July 4, 1942, when it was absorbed by the USAAF, the AVG was officially credited with the destruction of 286 Japanese aircraft for the loss of eight pilots killed in action, two pilots and one crew chief killed during ground attack, and four pilots missing. The top-scoring AVG pilot, Robert H. Neale, was credited with the destruction of sixteen enemy aircraft while flying the P-40, and eight other pilots claimed ten or more victories.

Specifications:
Curtiss P-40N-20/35-CU Warhawk
Dimensions:
Wing span: 37 ft. 4 in. (11.37 m)
Length: 33 ft. 4 in. (10.15 m)
Height: 12 ft. 4 in. (3.75 m)
Weights:
Empty: 6,700 lb. (3,039 kg)
Operational: 8,400 lb. (3,810 kg)
Performance:
Maximum Speed: 325 m.p.h. (523 km/h) @ 25,000 ft. (7,620 m)
343 m.p.h. (552 km/h) @ 15,000 ft. (4,572 m)
308 m.p.h. (495 km/h) @ 5,000 ft.(1,524 m)
 
Service Ceiling: 30,000 ft. (9,144 m)
Range: 750 miles (1,207 km) @ 10,000 ft. ft. (3,048 m)
Max. Range: 2,800 miles (4,506 km) @ 10,000 ft. (3,048 m)
Powerplant:
One Allison V-1710-99 , Vee, 12 cylinder, liquid cooled engines.
Engine power developed 1,200 h.p. (894 kw) @ takeoff and
1,125 h.p. (838 kw) @ 17,300 ft. (5,273 m) with a single speed supercharger.
Armament:
Six 0.5-in. Browning machine-guns with 281 rpg with provision for
external bomb load of three 500-lb. bombs.

One of the most significant steps in P-40 development came in 1941, when a British-built Rolls-Royce Merlin 28 engine with a single-stage, two-speed supercharger was installed in a Kittyhawk I airframe to improve its high-altitude performance. The Curtiss H-87-D, or XP-40F, as the Merlin-powered prototype became known, then had 1,300 hp available for takeoff, and 1,120 hp at 18,500 feet, which offered vast improvements over earlier models and endowed a maximum speed of 373 mph. This was reduced slightly in the YP-40F, which, like later variants, had the Packard-built Merlin V-1650-1 and revised cooling, the air intake above the cowling being incorporated in the radiator scoop. Gross weight climbed to 9,870 lb.

Following experiments in cooling-drag reduction in 1943 with a P-40K-10-CU which had its "beard" radiator removed to wing installations, and in rear vision improvements by installing a "bubble" canopy on a standard P-40L, a general " clean-up " program was initiated, resulting in the sole XP-40Q. With a 1,425 hp Allison V-1710-121 engine, the XP-40Q was modified from the first P-40K-I to have a "bubble" canopy and cut-down rear fuselage, wing radiators and, eventually, clipped wing tips. A four-blade propeller was fitted, and water injection installed. With a weight of only 9,000 lb, the XP40Q attained a maximum speed of 422 mph. This was still less than the speed attained by contemporary production Mustangs and Thunderbolts , however, and the XP-40Q did not achieve production.

The Aviation History On-Line Museum.
 
 
 

The World's Only Flyable P-40C

The Flying Tigers

 

 Pilot's Manual For The Curtiss P-40 "Tomahawk"

 

 

Curtiss P-40 "Tomahawk" : One of WW II’s Most Famous Fighters

Robert Guttman

If the Curtiss P-40 Warhawk was not the best fighter in the arsenal of the U.S. Army Air Corps (USAAC) when the United States entered the conflict, it was the most numerous type available. The Lockheed P-38 Lightning could outperform the P-40, especially at high altitude, but the P-40 was less expensive, easier to build and maintain, and — most important — it was in large-scale production at a critical period in the nation’s history when fighter planes were needed in large numbers.

A total of 11,998 P-40s were built before production was finally terminated in 1944. Warhawks constituted the principal armament of the U.S. Army Air Forces (USAAF) fighter squadrons throughout 1942 and 1943. Even after the appearance of newer types of fighter aircraft in the USAAF rendered the P-40 obsolete, it continued to contribute to victory in a variety of Allied air forces.

The P-40 was the product of a long development process that began when the USAAC invited various aircraft companies to submit designs for its 1935 fighter competition. Curtiss and Boeing had dominated the U.S. Army and Navy fighter plane business since the end of World War I. In 1933, however, Boeing had beaten Curtiss in competition for a lucrative Army fighter contract with its innovative P-26 Peashooter. The P-26 was a monoplane of all-aluminum, stressed skin construction. Ralph Damon, the head of Curtiss, was determined that his company’s next fighter should have the benefits of the latest design and construction technology. In 1934, he hired Donovan R. Berlin as Curtiss’ new chief engineer. Berlin had previously worked at Douglas and Northrop, two firms that had been at the cutting edge of aircraft design.

The four rival designs for the 1935 fighter competition, from Curtiss-Wright, Seversky, Vought and Consolidated, were the first really modern fighters to be evaluated by the Army. All four were low-wing monoplanes of all-metal, stressed-skin construction with retractable landing gear and enclosed cockpits.

Curtiss designated its entry the Model 75. Since all Curtiss fighter aircraft had been called ‘Hawks’ since the mid-1920s, the new fighter became known as the ‘Hawk 75.’ Powered by a 900-hp Wright air-cooled radial engine, the Hawk 75 was first flown in May 1935 and demonstrated good maneuverability and flying characteristics. Initially, however, the USAAC rejected the Hawk 75 in favor of the Seversky P-35. It subsequently reversed that decision, however, and in 1937 it ordered 210 of the Curtiss fighters — the Air Corps’ largest order of a single type of fighter aircraft since the end of World War I. Fitted with a more powerful Pratt and Whitney R-1830 Twin-Wasp radial engine, the new fighter was designated the P-36A.

Significant as the USAAC order was, it was small compared to the total number of Hawk 75s sold overseas. Curtiss had been selling large numbers of Hawk biplane fighters to various nations in Europe, Asia and Latin America since the 1920s. With war clouds gathering throughout the world in the late 1930s, Curtiss had little difficulty finding foreign buyers for its new monoplane.

By far the largest customer for the Curtiss fighters was France. At the time of the 1938 Munich crisis, the French aircraft industry was having difficulty meeting its air force’s demands for modern fighters. The French government decided that the most expedient solution to the problem was to order 730 Hawk 75s from Curtiss, in the neutral United States. H-75As, as the French called them, were the most numerous fighters in the Armée de l’Air’s inventory when WWII began, and they shot down more German planes than any other French fighter aircraft. The Hawk 75s that had not yet been delivered to France before the country surrendered to Germany in June 1940 were transferred to Britain’s Royal Air Force (RAF), which called them Mohawks.

Some of the French H-75As were seized by the Germans after France’s collapse and sold to the Finns for use against the Soviet Union. Others, still in French hands, were transferred to North Africa, where they continued to operate under the control of the Vichy French government. On at least one occasion, during the Allied landings in Morocco in November 1942, Vichy French H-75As tangled unsuccessfully with U.S. Navy Grumman F4F Wildcats.

Since the end of World War I, domination of the world’s aviation engines had been alternating between liquid-cooled in-line engines and air-cooled radial engines. The liquid-cooled engines were generally more powerful, but they were also heavier, more complex and vulnerable to damage if the coolant leaked out. The radial engines were lighter and more compact, but their larger frontal area created aerodynamic drag. As it happened, the Hawk 75 was developed at a time when the liquid-cooled V-12 engine was just beginning to come back into vogue, both in Europe and the United States. The principal reason was the introduction of high-temperature cooling utilizing Glycol rather than water, a development that made it possible to reduce weight and drag by decreasing the size of the cooling radiator by as much as 75 percent.

In February 1937, while the USAAC was still evaluating the P-36 for production, it contracted with Curtiss to re-engineer the fighter to test the potential of a highly promising new liquid-cooled V-12 engine, the turbosupercharged General Motors Allison V-1710. To save money, the factory rebuilt the original Hawk 75 prototype to create the new prototype. First flown in 1937, the XP-37, as the new fighter was called, was not an unqualified success. Although its 1,150-hp Allison engine and aerodynamic lines gave it far better performance than the P-36, it had a number of serious drawbacks as a combat plane. The General Electric turbo-supercharger boosted the engine’s critical operating altitude — i.e., the altitude at which the supercharger would operate at peak efficiency — to 20,000 feet, but it proved unreliable and likely to catch fire. In addition, the cockpit had to be moved aft to balance the heavy engine and its bulky turbo-supercharger, which reduced pilot visibility.

Despite the promising performance of the turbo-supercharged Allison engine, the problems encountered with the XP-37 were rapidly reducing the likelihood that the airplane ever would be placed in production. Therefore, Don Berlin decided to take a different approach to a P-36 derivative equipped with an Allison engine. On March 3, 1938, Curtiss submitted a proposal to the Air Corps to modify a P-36 airframe to accept an Allison engine fitted with a mechanically driven supercharger. The modifications to the airframe were less extreme than those required for the XP-37, as they did not require moving the cockpit aft. The engine also proved to be more reliable than the turbo-supercharged Allison used in the XP-37, although its critical operating altitude was reduced to 10,000 feet, with performance falling off at higher altitudes up to its service ceiling of 32,750 feet. At Curtiss the new fighter design was known as the Model 81, but the Air Corps called it the XP-40.

The prototype XP-40 was first flown on October 14, 1938, only two weeks after the settlement of the Munich crisis bought the world a one-year reprieve from war. It was modified from the 10th production P-36A airframe. The XP-40’s sharply pointed nose was longer than that of the P-36, though not so long as that of the XP-37. Since the cockpit was not displaced aft, the pilot’s view was better than in the XP-37. The radiator, which had been buried in the fuselage between the engine and cockpit of the XP-37, was now installed under the fuselage, aft of the wings.

Although Curtiss had guaranteed that the XP-40 would achieve 360 mph, the prototype was not immediately able to do so. After a series of modifications that took several more months, however, the fighter demonstrated a top speed of 366 mph at 15,000 feet. The most conspicuous change was the relocation of the radiator to a new position under the nose, giving the P-40 its most characteristic feature.

The XP-40 won the Army’s 1939 fighter competition against the Lockheed XP-38 Lightning, Bell XP-39 Airacobra, Republic AP-4, and Curtiss’ own XP-37 and Hawk 75R, the latter a turbo-supercharged version of the radial-engine P-36. The XP-38 outperformed the XP-40, especially at high altitudes, and was more heavily armed, but the XP-40 had the advantage of being based on an existing fighter design that was already on the production line. That meant that Curtiss could put the P-40 into production with a minimum of delay, and at the highly competitive price of $24,566.60 apiece. On April 26, 1939, Curtiss was awarded a contract for 524 P-40s — once again, the largest order for fighter planes placed by the Army since 1918.

The P-40 prototype was armed with one .50- and one .30-caliber machine gun — the standard USAAC fighter armament during the 1930s — but the production model was armed with two .50-caliber machine guns. In keeping with President Franklin D. Roosevelt’s policy of making the latest American military hardware available to the Allies, 140 of the original batch of P-40s were diverted to France. They were armed with one .50-caliber machine gun in the fuselage and four 7.5mm guns in the wings. None of those P-40s were delivered by the time France capitulated, however. Instead, the export P-40s were delivered to the RAF and became known as Tomahawk Mk.Is.

The British were grateful for all the combat aircraft they could get in 1940, but they did not regard the Tomahawk Mk.I as suitable for combat. Many of the Tomahawk Mk.Is still had metric instruments and other French equipment that were not compatible with RAF service, and their French throttle control levers worked in reverse of the way British or American ones did. More important, they lacked self-sealing fuel tanks and had neither armor nor bulletproof windscreens to protect their pilots. Consequently, the Tomahawk Mk.Is were relegated to tactical reconnaissance duties.

As a result of European combat experience, Curtiss installed armor in the P-40 and increased its armament, adding a .30-caliber machine gun in each wing. The improved fighters were called P-40Bs by the Americans and Tomahawk Mk.IIs by the British. The next model, known as the P-40C, also had self-sealing fuel tanks and yet another .30-caliber machine gun in each wing. The USAAC ordered a total of 324 P-40Bs and P-40Cs during 1941. At the same time, the British ordered 930 P-40Cs. Those with British radio equipment were called Tomahawk Mk.IIas, while the ones delivered to the RAF with American radios were designated Tomahawk Mk.IIbs.

First flown in April 1941, the P-40C was considered the first truly combat-ready version of the P-40 line. A price had been paid for the necessary improvements, however. The aircraft’s gross weight had increased from 7,215 to 8,058 pounds, an increase of 843 pounds or approximately 11 percent, with no increase in engine power. The P-40C’s rate of climb suffered, it was less maneuverable, and its maximum speed fell to 340 mph. By comparison, the Messerschmitt Me-109E used by the Luftwaffe in 1941 weighed only 6,100 pounds and had a top speed of 360 mph. Air Chief Marshal Sir Kenneth Cross, who served in the RAF’s Desert Air Force, recalled that ‘the Tomahawk was beautifully built, but…short on performance compared to the (Messerschmitt) 109F and G.’

By the end of 1941 the USAAC had deployed P-40s overseas. Thirty were flown to Iceland from the aircraft carrier Wasp, and 99 of them were stationed in Hawaii. In addition, four squadrons of P-40s were deployed in the Philippines. It was with the British that the Tomahawk Mk.IIs first saw action, however, flying reconnaissance sorties and fighter sweeps across the English Channel with the RAF and Royal Canadian Air Force (RCAF) in 1941. By May 1941 Tomahawks were also operating in the Middle East, eventually serving in that theater with Australian and South African fighter squadrons as well as the RAF. In addition, the British sent 195 Tomahawks to the Soviet Union after the Germans invaded that country on June 22, 1941.

The first serious use of the P-40 as a fighter occurred when Iraqi forces led by Rashid Ali El-Ghailani rose against the British in Iraq on May 2, 1941. When the Germans and Italians sent aircraft to assist the revolt, staging from Vichy French bases in Lebanon and Syria, the British sent three Bristol Blenheims to bomb the air base at Palmyra on May 14, escorted by two Tomahawks of No. 250 Squadron, RAF, flown by Flying Officers G.A. Wolsey and F.J.S. Aldridge. The Iraqi revolt was crushed by May 30, but the British decided that Vichy France’s violation of neutrality justified the invasion and occupation of Lebanon and Syria. Tomahawks of No. 3 Squadron, Royal Australian Air Force (RAAF), took part in the first attack on June 8, helping to destroy a Dewoitine D.520 fighter and damage three others at Rayak airfield. Elsewhere on that same day, two of No. 250 Squadron’s Tomahawks drew first blood for the P-40 in the air when they shot down an Italian Cant Z.1007bis reconnaissance plane five miles northwest of Alexandria, Egypt. The Vichy French put up a spirited fight before finally signing an armistice on July 14, but the Tomahawks of No. 3 Squadron RAAF also acquitted themselves well, holding their own against France’s top-of-the-line D.520s and shooting down two out of eight German Junkers Ju-88As of II Gruppe, Lehrgeschwader 1, operating from Crete, that tried to interfere with British landings on the Levantine coast on June 12.

During the summer of 1941, No. 112 Squadron RAF, which had lost all its Gloster Gladiators in Greece the previous spring, was re-equipped with Tomahawks. Its pilots took one look at their sleek new mounts and decided that the P-40’s cowling would make an ideal place to paint the squadron badge, a black cat. The results, however, looked more fishlike than feline, and soon a variety of shark mouths were being applied to the Tomahawks and, later, to the deeper-jowled Kittyhawks. For some reason, British authorities did not discourage No. 112 Squadron’s flamboyant liveries. The P-40 shark mouth would soon be adopted in other units and other air forces.

David B. Brown, who flew Kittyhawks in No. 112 in 1942 and later Supermarine Spitfires, recalled: ‘The Kittyhawk, while offering a more roomy and comfortable cockpit than the Spitfire, with a bonus of improved visibility, was more sluggish on controls and inferior in performance when compared with the Spitfire V. Furthermore, even though we could cope with moderate aerobatics and mock dogfights, there was still a feeling of ‘touchiness’ about the P-40 so that you wanted plenty of altitude before you could relax….’

Me-109F aces such as Hans-Joachim Marseille took a grisly toll of P-40s, but some of the more talented Commonwealth pilots rang up their own fair tallies of Axis planes while flying the Curtiss fighters. Australian ace of aces Clive R. Caldwell, flying Tomahawks in No. 250 Squadron and later Kittyhawks as commander of No. 112 Squadron, was credited with 18 German and Italian aircraft, plus two to four shared, six probable and 15 damaged over the Western Desert, later adding seven Japanese planes to his score while flying Spitfires over the South Pacific.

American P-40s first saw action at Pearl Harbor on December 7, 1941. Of the 99 P-40Bs stationed in Hawaii that day, only seven managed to get airborne during the attack. They shot down five Japanese planes, including four — two Nakajima B5N2 torpedo bombers, a Mitsubishi A6M2 Zero fighter and an Aichi D3A1 dive bomber — by 2nd Lt. George S. Welch of the 47th Squadron, 15th Pursuit Group. By the end of the day, however, only 25 P-40s remained operational. Three had been shot down, and the rest were destroyed on the ground.

In the Philippines, as in Hawaii, attrition was high — 26 P-40s were destroyed on December 8, 1941, mostly because they were caught on the ground. Although initially shocked by the startling performance of the Zero fighters that faced them, the four squadrons of P-40s put up a gallant struggle against the Japanese invaders.

The first USAAC ace of World War II was 1st Lt. Boyd D. Wagner, a P-40E pilot of the 17th Squadron, 24th Pursuit Group, in the Philippines. During a surprise attack on the Japanese army’s 50th Sentai, newly arrived at Aparri airfield on December 12, Wagner was attacked by four Nakajima Ki.27 fighters. He evaded two, then suddenly cut his throttle to make the other two overshoot him and shot down both. After strafing five to seven Japanese planes on the ground, Wagner was attacked by three more Ki.27s but managed to shoot down two of them and then escaped. He was subsequently awarded the Distinguished Service Cross, as was 1st Lt. Russell M. Church, Jr., who was shot down in flames and killed by anti-aircraft fire in the course of the raid. Wagner repeated his performance at Vigan field on December 16, hitting eight enemy planes on the ground and shooting down a Ki.27 that managed to take off, for his fifth victory in as many days. By then, however, there were too few of the Curtiss fighters available to do more than delay the inevitable. Lacking spare parts and replacement aircraft, the Americans were overwhelmed by May 1942.

Thomas L. Hayes, who flew P-40Es with the 35th Pursuit Group, was originally supposed to go to Mindanao, but when his squadron was unable to reach the Philippines it was diverted to Java in mid-January 1942. ‘The water-cooled Allison…moved the center of gravity forward,’ Hayes recalled. ‘The P-40 was much heavier than the P-36, and visibility was somewhat restricted with that extended nose. The P-40 also had more difficult landing characteristics than the P-36 — its greater weight, combined with the narrow landing gear and long nose, gave it a greater tendency to ground loop.’

‘The most serious deficiency in my training was gunnery,’ he added. ‘The only time I had squeezed the trigger was strafing an oil slick dropped in the Pacific. Tactics were a close second. We were indebted to our veterans, who told us, ‘You’re not going to turn and fight with a Zero — you won’t live to tell about it.’ Tactics were hit and run — if one had the altitude on a Zero, one could dive and get him. But engagements usually began with the Japanese above the P-40s — they threw the first punch.’

Hayes was shot down and wounded by a Zero on February 20, 1942, crash-landing his P-40E in a rubber plantation. After escaping from the Dutch East Indies, he went on to fly P-39s over New Guinea, and North American P-51s over Europe with the 357th Fighter Group, Eighth Air Force, finishing the war with credit for destroying 8 1/2 German aircraft.

By far the most renowned of all Curtiss fighters were the 100 dispatched to China for use by the American Volunteer Group (AVG), or ‘Flying Tigers.’ Usually referred to as P-40s, they were technically Tomahawk Mk.IIbs that had originally been built for the British. The Flying Tigers got the idea for their famous shark mouth marking from magazine photographs of No. 112 Squadron’s colorful Tomahawks. The AVG’s exploits made the shark mouth so famous, however, that P-40 units all over the world began copying it from them.

The AVG never had more than three squadrons of 18 P-40s at any time. Flying their first combat mission on December 20, 1941, the Flying Tigers operated under extremely difficult conditions at the end of the world’s longest supply line — and with the war’s lowest supply priority. Nevertheless, by the time the group disbanded six months later, its pilots had shot down 286 Japanese aircraft. During a period in the war when everybody else in the Far East was being soundly defeated by the Japanese, their achievements were truly phenomenal.

The AVG owed its success to the tactical doctrines developed by its leader, Colonel Claire Lee Chennault. A former USAAC fighter pilot who had carefully observed Japanese aircraft over China, Chennault understood the strengths and weaknesses of both the Japanese and American fighters. Using that knowledge, he established an advance warning system, which involved Chinese observers relaying information to AVG air bases, giving his pilots prior intelligence on what Japanese forces were coming and when they would arrive. He also drilled three fundamental rules into his pilots. First, never ever try to turn with a Japanese fighter in a dogfight, since it could maneuver its way onto a P-40’s tail within two turns; instead, use the P-40’s superior diving speed to escape, then climb and re-engage. Second, Chennault advocated head-on passes, because the Curtiss, with its two .50- and four .30-caliber machine guns, could outgun its Japanese army counterparts, which were still armed with only two 7.7mm weapons. The third rule was to harass the Japanese planes after they retired — since they lacked self-sealing fuel tanks, a few holes in their tanks would probably cause them to run out of fuel before they reached their home bases. These rules were the secrets of the Flying Tigers’ success.

Technically, the AVG personnel were U.S. civilians employed by the Nationalist Chinese government. Because of that, their P-40s were painted with Chinese insignia. Their success, highly publicized in the United States, was actually something of an embarrassment to the USAAC and its successor, the USAAF. The AVG was disbanded when an agreement was reached with the Chinese government to induct the Flying Tigers and their P-40s into the USAAF on July 4, 1942.

Curtiss-Wright was well aware of the P-40C’s shortcomings. In 1940 it developed a replacement fighter, mounting 10 machine guns and powered by an improved version of the Allison engine. Known as the XP-46, the new fighter did not enter production because Maj. Gen. H.H. Arnold, the Army Air Corps chief of staff, insisted that P-40 production should not be interrupted. Instead, Curtiss-Wright developed a new version of the P-40 incorporating the same 1,150-hp Allison V-1710-39 engine intended for the XP-46. The new P-40’s nose was considerably altered because the new engine was shorter and had a higher thrust line, and the radiator air intake was enlarged. The armament was changed to four .50-caliber guns in the wings. First flown in May 1941, the improved fighter was called the P-40D Warhawk by the USAAC and Kittyhawk Mk.I by the British. In April 1941, Curtiss built the first of 2,320 P-40Es, or Kittyhawk Mk.Ias, armed with six .50-caliber wing guns.

In an attempt to improve the P-40’s performance above 15,000 feet, Curtiss installed a Rolls-Royce Merlin engine in a P-40D to produce the XP-40F. The British were concerned that Rolls-Royce might not be able to supply enough Merlin engines for their own and the Americans’ needs, and at the same time, General Arnold was concerned that Allison could not supply sufficient liquid-cooled engines to fulfill the Army Air Corps’ requirements. As a result, on September 13, 1940, the British contracted Packard to build 6,000 Merlins for the RAF and 3,000 for the USAAC. The production P-40F Warhawk, or Kittyhawk Mk.II, became the first American fighter to use the 1,300-hp Packard Merlin and first flew in October 1941. With a top speed of 364 mph, the P-40F was 10 mph faster than the P-40E. The only external difference between the P-40E and F was the absence of the air scoop on top of the P-40F’s cowling, due to the Merlin’s updraft carburetor. A total of 1,311 P-40Fs were built, as well as 700 similar but lighter-weight P-40Ls. When the supply of P-40F and L airframes outstripped the supply of Packard Merlins early in 1943, 600 of them were completed with Allison engines and designated P-40Rs.

Between 1942 and 1943 the P-40Es were superseded by 1,300 improved aircraft with 1,325-hp Allison V-1710-73 engines, called P-40Ks. The P-40M was a similar, but lighter version of the P-40K with a carburetor air bypass grille on the cowling just forward of the exhausts. The aircraft’s tail was also slightly lengthened to improve directional stability. Both models were designated Kittyhawk M.IIIs by the RAF.

In order to further improve the P-40’s performance, Curtiss introduced additional weight-saving measures, including reducing the amount of fuel and eliminating two of the wing-mounted .50-caliber guns. At the same time, the designers improved rear visibility by increasing the glazing behind the cockpit. Called the Kittyhawk Mk.IV by the British, the lightweight P-40N Warhawk was the most-produced P-40 variant. With a top speed of 378 mph, the P-40N also had the best performance of the production-model P-40s. The 5,219th and last P-40N was completed on November 30, 1944. In addition to the USAAF, P-40Ns were used by the Dutch, Australians and New Zealanders in Europe and the South Pacific, and many were supplied to the Soviet Union.

In 1944, Curtiss-Wright made a final attempt to improve the P-40 by installing an enhanced 1,425-hp Allison V-1710-121 engine equipped with a two-stage supercharger in a P-40K. A new-style radiator was also built into the wing center section. The XP-40K was rebuilt three times. In its final form, with a shallow chin air scoop, clipped wings and a bubble canopy, the Curtiss fighter’s appearance was somewhat reminiscent of a P-51D Mustang. The XP-40Q, as the new version was redesignated, was the fastest of the Warhawks, with a top speed of 422 mph at 20,000 feet. Unfortunately, by the time the XP-40Q was built, the more capable P-51D was already available in large numbers. Only three were built, and only one was evaluated — and rejected — by the USAAF.

One XP-40Q turned up in Cleveland, Ohio, for the Thompson Trophy Race on September 1, 1947. Flown by Joe Ziegler, the Warhawk was excluded from the race because it qualified 13th, and only 12 planes were supposed to be allowed to compete. Ziegler started the race anyway, but on the 13th lap the XP-40Q’s engine stopped. Ziegler was forced to bail out, breaking one of his legs, and a woman spectator was injured by the jettisoned canopy. Thus ended the career of the ultimate P-40.

The P-40’s performance was always regarded as inferior to its German contemporaries, the Me-109 and Focke Wulf Fw-190, especially at altitudes above 15,000 feet. It could also be outmaneuvered and outclimbed by the Japanese Mitsubishi Zero. The availability of better fighters, such as the P-38 Lightning, P-47 Thunderbolt and P-51 Mustang, rendered the Warhawk obsolete by 1944. Nevertheless, many continued to be used in the South Pacific and China-Burma-India theaters right up until the end of World War II. Some P-40Ns were retained after the war by the Dutch East Indies Air Force and the Nationalist Chinese Air Force. The last known instance of P-40Ns’ being used in action was by the Dutch against Indonesian insurgents in 1948.

The P-40N was not only the last production model of the Warhawk family but also the last production fighter from Curtiss-Wright. Curtiss produced several fighter prototypes in an effort to supersede the P-40, but none were accepted for production due to the availability of more suitable existing models, such as the North American P-51. The last Curtiss fighter was the XP-87 Blackhawk, a postwar four-engine jet night fighter that was rejected by the U.S. Air Force in favor of Northrop’s F-89 Scorpion. The company still had several important military aircraft in production after the P-40 program was terminated, including the C-46 Commando transport, the SB2C Helldiver dive bomber and the SC-1 Navy scout seaplane. However, Curtiss-Wright’s dominance of the American fighter business, which had lasted since the early 1920s, ended with the P-40.

Although the P-40 was not the best fighter plane of its era, it was among the most ubiquitous. Few aircraft have seen combat in as many theaters, under as wide a variety of climactic conditions, or with as many different air arms as the Warhawk. P-40s were in action from the Arctic to the tropics, from the desert to the jungle, and from sea level to the Himalayas. In addition to the U.S. Army Air Forces, Warhawks were used by British, Australian, New Zealand, South African, Canadian, Dutch, Free French, Soviet, Chinese, Egyptian and Turkish fighter units. Whether it was known as the P-40, the Tomahawk, the Kittyhawk or the Warhawk, Curtiss-Wright’s fighter was one of the truly classic combat aircraft of World War II.
 


This article was written by Robert Guttman and originally published in the November 2000 issue of Aviation History.

 

 

The "Tomahawk" Files

XP-40, P-40A, P-40B, P-40C

Joe Baugher's Tomahawk files

 

P-40 Warhawk

The P-40 was the best known Curtiss-Wright airplane of World War II. It was also one of the most controversial fighters of the war. It was vilified by many as being too slow, lacking in maneuverability, having too low a climbing rate, and being largely obsolescent by contemporary world standards even before it was placed in production. The inadequacies of the P-40 were even the subject of a Congressional investigation. It gets regularly included on lists of the worst combat aircraft of World War 2.

All of these criticisms certainly had some degree of validity, but it is also true that the P-40 served its country well during the first year of the war in the Pacific when very little else was available. Along with the P-39 Airacobra, the P-40 was the only American fighter available in quantity to confront the Japanese advance during the first year of the Pacific War. It helped stem the speed of the Japanese advance until more modern types could be made available in quantity. The P-40 had no serious vices and was a pleasant aircraft to fly, and, when flown by an experienced pilot who was fully aware of its strengths and weaknesses, was able to give a good account of itself in aerial combat. The P-40 continued in production long after later types were readily available, the numbers manufactured reaching the third highest total of American World War II fighters, after the Republic P-47 and the North American P-51.

The P-40 was obsolete by European standards even before the first prototype flew, and it never did catch up. Its initial inadequacies in the form of low firepower and lack of self-sealing fuel tanks or armor were a reflection of mid-'thirties USAAC requirements which were outmoded. The P-40 had been developed as basically a low-altitude close-support fighter under mid-1930s US tactical concepts which envisaged more need for low-level ground support operations than for high-altitude interceptions. The military doctrine of the "ascendancy of bombardment over pursuit" was dominant in 1937 when the P-40 first appeared. This doctrine assumed that the prospect of high-altitude enemy air attack on the USA was extremely remote, with coastal defense and ground attack in the defense of US territory being seen as the the main tasks for any future fighter aircraft. Low-altitude performance and rugged construction received priority over high-altitude capabilities.

During the war, the Senate Special Committee to Investigate the National Defense Program (usually known as the "Truman Committee", after its chairman, Senator Harry Truman of Missouri) criticized the P-40 on several accounts, particularly on the original volume purchase of an inadequate design and its continued production long after later designs were readily available. However, they finally concluded that this was not brought about by any undue favoritism to Curtiss.

Some indication of the enormous P-40 production program undertaken by Curtiss can be assessed by its claim on factory floor space and manpower. During 1941, the Curtiss Airplane Division expanded its manufacturing area by 400 percent. The total work force was 45,000. This expansion included two new plants, one at Buffalo, New York and the other at Columbus, Ohio, to supplement the original Curtiss plant in St.Louis, Missouri. At the peak of wartime production, the entire Curtiss Airplane Division complex of factories was producing sixty aircraft A DAY!

The origin of the P-40 can be traced back to the Curtiss P-36 (Model 75) fighter, which was powered by a radial, air-cooled engine. A step in the direction toward what was eventually to emerge as the P-40 was the XP-37, which was described in an earlier post. The P-36 design was reworked to incorporate the Allison V-1710 liquid-cooled V-type engine, resulting in the XP-37. The XP-37 was equipped with a General Electrc turbosupercharger, and featured a cockpit pushed very far to the rear. Thirteen YP-37 service-test aircraft were built, but problems with the turbosupercharger caused the development of the P-37 to be abandoned in favor of a less complex and more straightforward conversion of the P-36 for the Allison V-1710 engine.

Realizing that the radial-engined P-36A was at the limit of its development, Curtiss designer Donovan Berlin got USAAC permission in July 1937 to install a 1150 hp Allison V-1710-19 liquid-cooled engine with integral supercharging in the 10th P-36A (Serial No 38-10). This project was given the company designation of Model 75P, and the USAAC gave the project a new fighter designation, XP-40.

The XP-40 flew for the first time on October 14, 1938, with Edward Elliot at the controls. Armament was two 0.50-inch machine guns located in the upper fuselage deck and synchronized to fire through the propeller arc, standard armament for US pursuit aircraft at the time. Wing racks could be fitted for six 20-pound bombs. A small oil cooler was located beneath the pointed nose. The air intake for the single-stage supercharger was mounted on top of the engine cowling between the two machine guns, but during tests it was replaced by a long cowled intake duct which became characteristic of all the early P-40 production models. Initially, the coolant radiator was placed under the fuselage aft of the wing, but it was gradually moved forward until it finally ended up located underneath the extreme nose. The radiator intake was redesigned to include an oil cooler and two coolers for the ethylene/glycol engine coolant. The initial XP-40 had a single exhaust port on each side of the fuselage, but in its final form it had six separate exhaust ports on each side. The initial XP-40 had inherited from the P-36 a set of mainwheel fairing plates which covered the mainwheels when they retracted into their wing wells, but these were eventually deleted and replaced by two small doors which closed over the wheel struts upon retraction.

The maximum speed of the XP-40 was 342 mph at 12,200 feet at a gross weight of 6260 pounds. This was faster than the Hawker Hurricane, but slower than the Spitfire or the Bf 109E. Empty weight was 5417 pounds, and fully-loaded weight was 6870 pounds. Range was 460 miles at 299 mph with 100 gallons of fuel. With 159 gallons of fuel at 200 mph, a range of 1180 miles was claimed, almost twice that of the contemporary Hurricane, Spitfire, and Bf 109E. Wingspan was 37 feet 4 inches, wing area was 236 square feet, length was 31 feet 1 inch, and height was 12 feet 4 inches. The wingspan and wing area were to remain the same throughout the entire history of the P-40 production run.

In the late 1930s, the USAAC was planning to expand its force, and on January 25, 1939. manufacturers were invited to submit proposals for pursuit aircraft. The Army was still thinking in terms of low-altitude, short-range fighters. Among the contenders were the Lockheed XP-38, the Bell XP-39, the Seversky/Republic XP-41 (AP-2) and XP-43 (AP-4), and no less than three planes from Curtiss, the H75R, XP-37, and XP-42. Although the XP-40 could not match the performance (especially at altitude) of the turbosupercharged types, it was less expensive and could reach quantity production fully a year ahead of the other machines. In addition, the XP-40 was based on a already-proven airframe that had been been in production for some years. Consequently, on April 26, 1939, the Army adopted a conservative approach and ordered 524 production versions under the designation P-40 (Curtiss Model 81). At that time, it was the largest-ever production order for a US fighter, and dwarfed the service test orders placed that same day for YP-38 and YP-39 fighters. A couple of weeks later, 13 YP-43s were also ordered.

The P-40 was similar to the final XP-40 configuration except for 1040 hp V-1710-33 (C15) engines and provisions for the mounting of one 0.30-inch machine gun in each wing. Flush riveting was used to reduce drag. Armor, bulletproof windshields, and leakproof fuel tanks were added in service. The P-40 was a relatively clean design, and was unusual for the time in having a fully retractable tailwheel.

The first flight of a P-40 (Ser No 39-156) was on April 4, 1940. Maximum speed was 357 mph at 15,000 feet, service ceiling was 32,750 feet, and initial climb rate was 3080 feet per minute. An altitude of 15,000 feet could reached in 5.2 minutes. The length of the P-40 was 31 feet 8 3/4 inches, which became standard for all early models. Weights were 5376 pounds empty, 6787 pounds gross, and 7215 pounds maximum.

Deliveries of the P-40 to Army units began in June of 1940. Three of the P-40s were used for service testing, the USAAC contract making no provisions for the standard practice of supplying YP models.

Foreign air forces were beginning to take notice of the P-40, and in May of 1940, the Armee de l'Air of France placed an order for 140 H-81A (export model of the P-40).

Only 200 of the initial P-40 order were actually completed as P-40s. Serials were 39-156/280 and 40-292/357. The remaining 324 aircraft of the order had their delivery deferred to enable Curtiss to expedite the delivery of the 140 H-81As to France. However, none of these actually reached France before the Armistice in June 1940, and the contract was taken over by the Royal Air Force as Tomahawk I.

16 P-40s were sent to the Soviet Union after the German invasion.

The P-40 lacked such things as armor for the pilot, self-sealing fuel tanks, and a bulletproof windshield, so it was not considered as being suitable for combat. On October 22, 1942, the P-40s still in USAAF service were ordered restricted from combat duty and were redesignated RP-40.

The P-40A designation was skipped in the initial designation assignments. However, it was applied retroactively to P-40 Ser No 40-326 when it was converted to a camera-carrying photographic reconnaissance model at Bolling Field in March of 1942.

The P-40B (Model H81B) differed from the P-40 in having an extra 0.30-inch machine gun in each wing. The engine was still the V-1710-33. In September 1940, 131 P-40Bs were procured by the Army to replace the deferred P-40s. Serials were 41-5205/5304 and 41-13297/13327. The first P-40B flew on March 13, 1941. The P-40B retained the same dimensions of the P-40, but weight was increased to 5590 pounds empty, 7326 pounds gross, and 7600 pounds maximum loaded. Because of the additional weight, the P-40B had an inferior performance to the P-40, maximum speed being 352 mph, service ceiling being 32,400 feet, and initial climb rate being 2860 feet per minute. Normal range was 730 miles, but a maximum range of 1230 miles could be attained at the minimum cruise settings.

The export equivalent of the P-40B was the Tomahawk IIA (Model H81-A2). They differed from the American version by having the wing guns replaced by 0.303-inch Brownings. 110 were produced for the RAF. RAF serials were AH881/990. 23 of these planes were transferred to the USSR, and one (AH938) went to Canada as an instructional airframe.

The initial P-40 order was finally completed with 193 P-40Cs (company designation H81-B). Serials were 41-13328/13520. The first flight of a P-40C was made on April 10, 1941. The P-40C retained the 1150 hp Allison V-1710-33 engine, but was fitted with a new fuel system with 134 gallons in new tanks with improved self sealing. In addition, provisions were made for a 52-gallon drop tank below the fuselage. The P-40C had a SCR-247N radio instead of the SCR-283. These additions produced yet another upward crawl in the weight --- the weights for the P-40C were 5812 pounds empty, 7459 pounds gross, and 8058 pounds maximum loaded. Consequently, the performance continued to degrade. Maximum speed was 345 mph at 15,000 feet. Normal and maximum ranges were 730 and 945 miles respectively. Service ceiling was 29,500 feet, and initial climb rate was 2650 feet per minute. Dimensions were wingspan 27 feet 3 1/2 inches, length 31 feet 8 1/2 inches, height 10 feet 7 inches, wing area 236 square feet.

The export equivalent of the P-40C was the Tomahawk IIB (Model H81-A2). A total of 930 were built. RAF serials were AH991/999 (all to USSR), AK100/570 (36 to China), AM370/519 (64 to China), and AN218/517. 100 of these planes, unofficially designated H81-A3, were transferred to China where they were used by the American Volunteer Group --- the famous "Flying Tigers". 23 went to the USSR, and unspecified numbers went to Turkey and Egypt. The rest were used extensively by the RAF and South African Air Force in the North African theatre.

AVG Tomahawk IIB
Much-rebuilt Tomahawk IIB, recovered from Russia and painted in the colors of Bob Neale of the AVG. The plane is on display at the Naval Aviation Museum, Pensacola.

At a very early stage, the Curtiss P-40 attracted the attention of foreign air forces. On May 10, 1939, the French ordered 140 export versions of the P-40 for the Armee de l'Air. These aircraft were designated Hawk 81-A1 by the manufacturer. The Hawk 81-A1s were identical to the US P-40 except that they had French instruments and equipment and were equipped with reverse-movement "French-fashion" throttles. The first of the French-ordered H81-A1s flew on June 6, 1940, and a few were actually completed with French markings. However, before any of their H81-A1s could be delivered, France surrendered. Britain agreed to take over the entirety of the French order, and gave the H81-A the name Tomahawk I in RAF service. RAF serials were AH741/840 and AH841/880.

The USAAC had agreed to defer deliveries of their P-40s so that the Tomahawk Is could be supplied to Britain as soon as possible. The first Tomahawk Is reached England in September of 1940. The two 0.5-inch machine guns in the nose were retained, but they were supplemented by four wing-mounted 0.303-inch Browning machine guns in place of the 7.5-mm FN-Brownings specified by the French. Such was the urgency of their delivery to Britain that many of the 140 machines still had French instruments and bore cockpit lettering in French when they arrived.

However, Britain quickly concluded that these planes were not suitable for combat, since they lacked armor protection for the pilot, armor-glass windshields, or self-sealing fuel tanks. Nevertheless, since a German invasion was feared to be imminent, they were actually issued to several operational squadrons.

However, the Hun never invaded England, and so the Tomahawk Is were used only for training roles within Britain. Overseas, the first Desert Air Force squadron to be equipped with Tomahawks was No. 112 which exchanged its Gloster Gladiators for the Curtiss fighter. No 112 Squadron became famous for its "shark's tooth" insignia on the engine cowling, and this scheme was later adopted by the American Volunteer Group in China. AH774,793, and 840 were sold to Canada for use as instructional airframes, but they retained their RAF serials.

The Tomahawk IIA (Model H81-A2) was equivalent to the US P-40B. It had protective armor and externally-covered self-sealing tanks. 110 were built for the RAF under a direct-purchase contract. It carried two 0.30-inch machine guns in the wings in addition to the two 0.50-in guns in the fuselage. A British radio was fitted. RAF serials were AH881/990. AH938 was transferred to Canada as an instructional airframe. 23 of these planes were transferred to the USSR.

The Tomahawk IIB (Model H81-A2) was generally equivalent to the US P-40C. It had four 0.303-inch Browning machine guns in the wings in addition to the two nose-mounted 0.50-in guns. [But see my and Erik Shilling's comments on this subject in the facsimile Pilot's Notes on this website. -- DF] Whereas the Tomahawk IIA had a British radio, the Tomahawk IIB had US equipment. A total of 930 of these planes were produced in four lots. RAF serials were AH991/999, AK100/570 (36 of this batch were shipped to China and were selected at random with no particular sequence), AM370/519 (64 were shipped to China, selected at random), and AN218/517. They were used extensively by the RAF and the South African Air Force in North Africa starting on June 16, 1941.

After the German invasion of the USSR in June 1941, one hundred and ninety-five Tomahawk IIBs were shipped to the USSR, some from the USA, others selected from the reserve forced based in the United Kingdom in anticipation of the German invasion which never came. These Russian Tomahawks went into action on the Moscow and Leningrad fronts in October 1941, and were the first US-built planes to be used by the Russians in the new battle area.

An unspecified number of Tomahawk IIBs were sent to bolster Turkish neutrality in November 1941. Turkey was supplied with planes from both the Allies and the Axis during World War II.

The Tomahawk IIs were active in the Middle East from October of 1941 onward. They shared in the strafing of the retreating Axis troops. The ability of the Tomahawk to absorb an incredible amount of punishment became almost legendary. They served with Nos 2, 26, 73, 112, 136, 168, 239, 241, 250, 403, 414, 430 and 616 Squadrons of the RAF. They also served with Nos 2 and 4 Squadrons of the South African Air Force and No 3 Squadron of the Royal Australian Air Force. At low altitudes, the Tomahawk II was actually superior to the Bf 109, but this advantage rapidly disappeared when combat took place at altitudes above 15,000 feet. The weight which handicapped the performance of the Tomahawk did have one tangible benefit --- the rugged structure could absorb a terrific amount of battle damage and still allow the airplane to return to base. Although generally outclassed by the Bf 109, the Tomahawk was a capable fighter in the hands of experienced pilots such as Neville Duke. Wing Commander Clive Caldwell of the RAAF scored more than twenty victories while flying a Tomahawk in the Middle East. However, much of the opposition to the Tomahawk was provided by obsolescent fighter biplanes (e.g. Fiat CR-42) and underpowered, lightly armed fighter monoplanes such as the Fiat G-50 of the Regia Aeronautica. It had difficulty with the more advanced Macchi C-202 Folgore.

100 of the RAF Tomahawk IIBs were released to China and served with the American Volunteer Group (AVG) --- the famous "Flying Tigers". Company records list them as Model H81-A3. The Tomahawk IIB was more-or-less equivalent to the P-40C, but some sources list the Flying Tiger Tomahawks as being equivalent to the P-40B. There is confusion on this point.

It is with the Flying Tigers that the P-40 achieved immortality. Newly-promoted to Brigadier General in the Chinese Army, Claire Chennault went to the USA in November 1940 to recruit pilots for the AVG. The AVG came into existence in August 1941. General Chennault ordered 100 P-40s through a loan from the US government. By the time of Pearl Harbor, some 80 American pilots were serving with the AVG based at Kunming and Mingaladon. Contrary to popular understanding, the AVG did not actually enter combat until AFTER Pearl Harbor. The famous "shark's teeth" marking did not originate with the Flying Tigers, but was copied from the markings used by the Tomahawks of the RAF's No. 112 Squadron in North Africa.

The AVG drew first blood on December 20, destroying six out of ten attacking Japanese bombers. When the AVG encountered the Japanese Zero for the first time, they initially underestimated the maneuverability of their opponent, and they lost two pilots on December 23. [Actually, the Dec. 20 encounter ended with three Kawasaki Ki-48 "Lily" bombers shot down and one force-landed in Vietnam. The retractable-gear aircraft that fought the AVG were Nakajima Ki-43 Hayabusa fighters, later called "Oscar" in the west. -- DF] It was soon learned that it was wise not to mix it up with the Zero on a one-to-one basis because of the inferior maneuverability and climb rate of the Curtiss, but instead to use the P-40's superior speed and diving ability to advantage. The most effective tactic against the Zero was a diving pass followed by a rapid departure from the scene. The P-40 gained a reputation for ruggedness which enabled many an AVG pilot to return safely home after his plane was damaged in combat.

by Joe Baugher

 

 

Last Updated

05/03/2010

 

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HOME > FLYING TIGERS > RECRUITERS

Recruiting the AVG:
Bruce Leighton's memo

[A tip of the virtual hat to Alan Armstrong, who located this memo at the Museum of Naval Aviation History, Pensacola. Undated, it was probably written in May 1941. Bruce Leighton was a retired navy officer and a vice-president of Intercontinent Corporation, owned by Bill Pawley and his brothers. I have reproduced it as nearly as possible in the original format. Items in brackets were added by me, and the same is true of boldfaced phrases. Note that paragraph (2)(b) promises that the AVGs will retain seniority and rank, but not time toward retirement. Indeed, crediting AVG time toward retirement is specifically ruled out in other documents on file at Pensacola. — Dan Ford]

 

STATEMENT OF MR. BRUCE LEIGHTON CONCERN-
ING THE CENTRAL AIRCRAFT MANUFACTURING COMPANY

    Following a long history of growing interest in U.S. Government aid to China, the Chinee Government sent a special mission to Washington early this year [1941] to arrange for loans and other assistance to build up their depleted air force.

    Arrangements were made for $100,000,000 loan and for the immediate release to China by the British of 100 Curtiss P-40 pursuit planes from then current British allocations, and numerous representations took place between U.S. Government and Chinese representatives as to the facilities available in China to assure that aircraft supplied would be effectively operated.

    The history of Chinese air activities had made it plain that the Chinese air force is not at present adequately trained or organized or equipped to maintain and effectively operate modern high-performance aircraft. Means must be provided for the Chinese to obtain the services of American pilots and key ground personnel with experience in military operations to act as a nucleus tactical organization upon which to progressively build a modern air force in China by (a) later additions to American personnel and (b) accelerated training of native Chinese personnel.

    Because practically all experienced men of necessary qualifications in this country have been called into active military or naval service, the only immediate source of supply is from the active military services, but for obvious reasons individuals engaged in operations of this nature contemplated in China must have no connection with the U.S. Government services while so engaged. They must act as individuals and on their own responsibility. Experience in previous attempts to form operating and maintenance groups of American personnel in China in various activities has clearly shown that direct employment of such groups of individuals by Chinese government agencies does not bring effective results. Successful results have been obtained only where the personnel are employed and paid by some responsible American concern having long experience in China.

    The Intercontinent Corporation is such a concern. It had for years been engaged in aircraft activities in China, and through a subsidiary, the Central Aircraft Manufacturing Company, had maintained aircraft manufacturing activities for more than five years in China, and had been particularly active in the training of Chinese mechanics and establishment of repair and maintenance facilities in many parts of China since the beginning of hostilities in Shaighai in 1937. It maintains offices in New York, Chungking, Rangoon, and HongKong, and now operates a factory and assembly and repair base in China adjacent to the Burma route [at Loiwing], which is the only facility at present available for the assembly of aircraft shipped into China via that route.

    CAM Co's president, Mr. W. D. Pawley, and its vice-presidnet, Mr. B. G. Leighton, (a former naval officer with 12 years of active service in the U.S. Naval Air Forces, and now a Lieutenant Commander in the Naval Reserve, on inactive duty), are well known in military and naval circles in this country and intimately familiar with conditions in China, and personally acquainted with many responsible Chinese government officials.

    Called into consultation by the Secretary [of the Navy] and the Chinese Embassy, they volunteered the services of their organization for the recruiting and employement of the pilots and ground personnel, and organization of repair facilities in China, the understanding being that men so recruited would be employed under contract, ostensibly as civilian employees in the same status as technical personnel whome they [CAMCO] had been regularly employing for their normal manufacturing activities for years past. These services are being rendered without compensation, other than reimbursement to CAM Co by the Chinese government for direct out-of-pocket expenses. The financial conditions are set forth in the attached copy of formal agreement between Chinese Embassy and CAM Co.

    To put the project into effect many complicated details have had to be arranged with U.S. Government offices. All arrangements have been handled orally with no file record of any nature. The procedure is as follows:

    (1). CAM Co's representatives have been given letters of introduction by SecNav's office and by Office of Chief of Air Corps to Commanding Officers of naval and military units, to whom CAM Co representatives orally explained the nature of their visit and the interest of the U.S. Government departments, suggesting that the Commanding Officers obtain any required oral confirmation from Washington.

    (2). After clearing with the Commanding Officer of the station, CAM Co representative contacts individual Reserve officers and enlisted men attached to the station, and receives written employment applications from those interested. Pursuant to oral advices given CAM Co by the Army and Navy Washington offices concern, (U.S. Air Corps Personnel Division and BuNav), applicants are orally informed that:

    (a) Resignations or discharges will be approved to accept employement with CAM Co. (Standard forms for resignation and discharge requests have been supplied by Washington offices concerned.).

    (b) Although they completely sever their official connections with the United States military service, it is the intent of the War and Navy Departments that upon completion of their employment with CAM Co, and to the extent permitted by the broad discretionary powers of the Secretaries of War and Navy in relation to Reserve personnel, that they will be accepted for re-commission or re-enlistment in the active Reserve in such rank or grade and under such conditions as will give them the same seniority and other benefits, including disability benefits, as they would have enjoyed had they remained on active duty in the Army or Navy Reserve.

    (3). Successful applicants are processed as follows: CAM Co representative visits station and:

    (a) Executes employment contract (Standard form attached)

    (b) Receives applicant's signed resignation or request for discharge.

    (c) Assists applicant to fill out passport application.

    (d) Proceeds to Washington with (b) and (c), clears (b) with Army or Navy personnel office concerned, clears (a) with Passport Division of State Department and obtains passport, obtains required visas from British and Chinese Embassies.

    (e) Arranges transportation to China, including necessary arrangements for forwarding by CAM Co. offices in the Orient to final destination.

    (f) Notifies applicant when all is cleared, and instructs him where and when to report.

    (4). Weekely summary reports of progress are submitted to SecNav. and to Special Chinese Affairs desk in State Department.

    (5). If interested, offices and desks in Washington are consulted and kept constantly informed of progress through frequent personal visits of CAM Co personnel in Washington.

    The original program called for the shipment to China of 100 Curtiss P-40's. Subsequently arrangements have been made under Lend-Lease Act for the supply to China of substantial additional numbers of aircraft and extension of the original project, and further plans are at present under consideration for the supply of bomber type planes, as soon as personnel and facilities are available to handle.

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